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Космические корабли и станции, автоматические КА и методы их проектирования, бортовые комплексы управления, системы и средства жизнеобеспечения, особенности технологии производства ракетно-космических систем

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Применить Всего найдено 11303. Отображено 199.
20-03-2015 дата публикации

ЦЕНТРОБЕЖНЫЙ ПОТОЛОЧНЫЙ ВЕНТИЛЯТОР

Номер: RU2544396C2

Настоящее изобретение относится к центробежному потолочному вентилятору. Предлагаемый вентилятор содержит кожух, двигатель и крыльчатку. Указанный кожух имеет верхнюю поверхность с воздухоприемником и нижнюю поверхность с воздухоотводом. Согласно предпочтительному варианту изобретения указанная нижняя поверхность имеет округлую, чашеобразную форму, причем в ней выполнена совокупность отверстий, задающих воздухоотвод. Указанная крыльчатка содержит вращающийся вал и совокупность лопаток, расположенных вокруг указанного вала. Указанные лопатки предпочтительно выполнены изогнутой формы для обеспечения движения воздуха во всех направлениях между первым направлением, по существу, перпендикулярным вращающемуся валу, и вторым направлением, по существу, параллельным вращающемуся валу, благодаря чему обеспечивается равномерная вентиляция помещения. В предлагаемом вентиляторе также может быть предусмотрен нагревательный элемент для нагревания воздуха, выходящего из вентилятора. Изобретение направлено ...

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10-04-2016 дата публикации

ВЕНТИЛЯТОР В СБОРЕ

Номер: RU2580781C2

Настоящее изобретение относится к вентилятору в сборе. Он включает сопло и основную часть, на которой установлено сопло. Сопло содержит заднюю секцию, имеющую первое впускное отверстие для воздуха и первое выпускное отверстие для воздуха, и первый внутренний проход для перемещения воздуха из первого впускного отверстия для воздуха к первому выпускному отверстию для воздуха; и переднюю секцию, имеющую второе впускное отверстие для воздуха и одно второе выпускное отверстие для воздуха, и второй внутренний проход, который изолирован от первого внутреннего прохода, для перемещения воздуха из по меньшей мере одного второго впускного отверстия для воздуха к второму выпускному отверстию для воздуха. Секции сопла определяют внутреннее отверстие, через которое воздух снаружи вентилятора в сборе вытягивается воздухом, испускаемым из сопла. Основная часть включает в себя средства создания потока для создания первого воздушного потока через первый внутренний проход и второго воздушного потока через ...

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30-06-2017 дата публикации

ВЕНТИЛЛЯЦИОННЫЙ БЛОК

Номер: RU2624158C2

Изобретение относится к вентиляционному блоку. Вентиляционный блок, содержащий центробежный ротор (2), диффузор (4), связанный с центробежным ротором (2) и содержащий первый и второй выходы (6, 7), выходы расположены на противоположных сторонах центробежного ротора (2) и определяют продувной канал (5), центробежный ротор (2) вставлен в продувной канал (5), центробежный ротор (2), первый выход (6) и второй выход (7) выровнены по отношению друг к другу в соответствии с главной осью (X), перпендикулярной оси (R) вращения. Диффузор (4) содержит направляющие средства (12, 14) для направления воздушного потока (F) в продувном канале (5), каждое первое и второе средства (12, 14) отклонения потока имеет первую поверхность (12а, 14а), которая изогнута так, что ее вогнутый участок обращен по направлению к ротору (2). Первая поверхность (12а, 14а) первого и второго средств (12, 14) отклонения потока образована частью цилиндрической поверхности, имеющей главную ось, которая совпадает с осью (R) вращения ...

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20-06-2014 дата публикации

ВЕНТИЛЯТОР

Номер: RU2519886C2

Настоящее изобретение относится к вентилятору, предназначенному для создания воздушной струи в комнате, в офисе или других бытовых условиях. Напольный вентилятор для создания воздушного потока, содержащий основание, в котором расположена крыльчатка, двигатель, предназначенный для вращения крыльчатки для создания воздушного потока, и диффузор, расположенный ниже по потоку относительно крыльчатки; устройство для выпуска воздуха; телескопическую трубку, расположенную между основанием и устройством для выпуска воздуха и предназначенную для перемещения воздушного потока к устройству для выпуска воздуха; и средство, предназначенное для направления воздушного потока, выброшенного из диффузора, в трубку, при этом направляющее воздушный поток средство содержит множество лопастей, каждая из которых предназначена для направления соответствующей части воздушного потока, выброшенного из диффузора, по направлению к трубке. Что позволяет создать устойчивый и безопасный напольный вентилятор. 14 з.п. ф-лы ...

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24-07-2017 дата публикации

ВЕНТИЛЯТОР В СБОРЕ

Номер: RU2626213C1

Настоящее изобретение относится к вентилятору, который обеспечивает создание потока увлажненного воздуха. Увлажняющее устройство содержит: сопло, имеющее первое впускное отверстие для воздуха и первое выпускное отверстие для воздуха, первый внутренний проход для перемещения воздуха из первого впускного отверстия для воздуха к первому выпускному отверстию для воздуха, второе впускное отверстие для воздуха, второе выпускное отверстие для воздуха и второй внутренний проход для перемещения воздуха из второго впускного отверстия для воздуха к второму выпускному отверстию для воздуха, при этом сопло определяет внутреннее отверстие, через которое воздух из наружного пространства увлажняющего устройства вытягивается воздухом, испускаемым из выпускных отверстий для воздуха; и основную часть, на которой установлено сопло и которая содержит основание и водяной бачок, установленный на основании, причем основание содержит средства создания потока для создания первого воздушного потока через первый внутренний ...

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24-03-2017 дата публикации

ВЕНТИЛЯТОР В СБОРЕ

Номер: RU2614378C1

Вентилятор в сборе, включающий в себя сопло и основную часть, на которой установлено сопло. Сопло содержит заднюю секцию, имеющую по меньшей мере одно первое впускное отверстие для воздуха, по меньшей мере одно первое выпускное отверстие для воздуха и первый внутренний проход для перемещения воздуха из первого впускного отверстия для воздуха к первому выпускному отверстию для воздуха; и переднюю секцию, имеющую по меньшей мере одно второе впускное отверстие для воздуха, по меньшей мере одно второе выпускное отверстие для воздуха и второй внутренний проход, который изолирован от первого внутреннего прохода, для перемещения воздуха из второго впускного отверстия для воздуха ко второму выпускному отверстию для воздуха. Секции сопла определяют внутреннее отверстие, через которое воздух снаружи вентилятора в сборе вытягивается воздухом, испускаемым из сопла. Основная часть включает в себя средства создания потока для создания первого воздушного потока через первый внутренний проход и второго ...

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18-09-2018 дата публикации

Безлопаточный диффузор малорасходной центробежной компрессорной ступени

Номер: RU183324U1

Полезная модель относится к области машиностроения и предназначена для использования в центробежных компрессорах. Задачей заявляемой полезной модели является снижение коэффициента потерь безлопаточного диффузора за счет снижения потерь трения при безотрывном течении, что в свою очередь ведет к повышению коэффициента полезного действия малорасходной центробежной компрессорной ступени. Безлопаточный диффузор малорасходной центробежной компрессорной ступени, представляющий собой кольцевой элемент проточной части, образованный расходящимися коническими поверхностями, в котором начальная часть выполнена суженной, угол наклона наружной стенки диффузора равен углу наклона конической образующей покрывающего диска на выходе из рабочего колеса, а образующая внутренней поверхности диффузора составляет угол с наружной стенкой диффузора в пределах 040’ - 120’.

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17-09-2021 дата публикации

Направляющий аппарат погружного многоступенчатого лопастного насоса

Номер: RU206623U1

Полезная модель относится к насосам и может быть применена в погружных многоступенчатых центробежных насосах для добычи флюида из скважин. Направляющий аппарат 1 погружного многоступенчатого лопастного насоса состоит из цилиндрического корпуса 2, с верхним диском 3 на выходе из направляющего аппарата и центральной втулкой 4. На выходе из направляющего аппарата 1, в верхнем диске 3 между цилиндрическим корпусом 2 и центральной втулкой 4 выполнено кольцевое отверстие 5, образующее выходную кольцевую камеру 6. На диске 3 в его нижней части, внутри цилиндрического корпуса 2 размещены открытые лопатки 7, формирующие проточные каналы 8 направляющего аппарата 1, при этом в верхнем диске 3 между лопатками 7 и цилиндрическим корпусом 2 выполнена кольцевая канавка 9, глубина которой соответствует высоте лопаток 5. Кольцевая канавка 9 образует входную кольцевую камеру 10 направляющего аппарата 1. Лопатки 7, формирующие проточные каналы 8 направляющего аппарата 1, входная 10 и выходная 6 кольцевые камеры обеспечивают гидравлическую связь проточных частей рабочего колеса 11 и направляющего аппарата 1. Технический результат заключается в повышении надежности работы направляющего аппарата в условиях высокого содержания механических примесей в пластовой продукции. 3 ил. РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 206 623 U1 (51) МПК F04D 13/10 (2006.01) F04D 29/44 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ПОЛЕЗНОЙ МОДЕЛИ К ПАТЕНТУ (52) СПК F04D 13/10 (2021.08); F04D 29/44 (2021.08) (21)(22) Заявка: 2021114697, 25.05.2021 (24) Дата начала отсчета срока действия патента: Дата регистрации: 17.09.2021 (45) Опубликовано: 17.09.2021 Бюл. № 26 2 0 6 6 2 3 R U (56) Список документов, цитированных в отчете о поиске: RU 180414 U1, 13.06.2018. RU 191187 U1, 29.07.2019. RU 2677299 C1, 16.01.2019. RU 2364755 C1, 20.08.2009. RU 72733 U1, 27.04.2008. US 3070027 A1, 25.12.1962. (54) Направляющий аппарат погружного многоступенчатого лопастного насоса (57) Реферат: ...

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10-09-2012 дата публикации

ВЕНТИЛЯТОР В СБОРЕ

Номер: RU2460904C1

Вентилятор 10 в сборе предназначен для создания воздушной струи. Вентилятор содержит выпуск 14, установленный на основании. Основание содержит внешний корпус 16 и корпус 64 крыльчатки 52, расположенный во внешнем корпусе 16. В корпусе 64 имеются отверстие 70 для впуска воздуха и отверстие для выпуска воздуха и расположены крыльчатка 52 и двигатель 56, предназначенный для приведения в действие крыльчатки 52 с целью создания воздушного потока через корпус 64. Выпуск содержит внутреннюю полость 86, предназначенную для направления воздушного потока из отверстия для выпуска воздуха корпуса 64 крыльчатки 52, и сужение 26, через которое воздушный поток выбрасывают из вентилятора 10. Между внешним корпусом 16 и корпусом 64 крыльчатки 52 расположен гибкий уплотняющий элемент. Изобретение направлено на снижение потерь и увеличение создаваемого воздушного потока, а также уменьшение шума. 18 з.п. ф-лы, 17 ил.

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28-09-2018 дата публикации

Способ сборки набора рабочих колес с помощью стяжных стержней, рабочее колесо и турбомашина

Номер: RU2668297C1
Принадлежит: НУОВО ПИНЬОНЕ СРЛ (IT)

Изобретение относится к сборке набора рабочих колес, расположенных смежно друг с другом в осевом направлении и имеющих соответствующие сквозные осевые. Используют по меньшей мере два осевых стяжных стержня, как минимум с одним соединительным элементом, который в осевом направлении расположен смежно с двумя рабочими колесами соответственно на двух его сторонах и имеет сквозное осевое отверстие. Соединительный элемент используют для закрепления конца первого осевого стяжного стержня с одной стороны сквозного осевого отверстия указанного элемента и закрепления конца второго осевого стяжного стержня с другой стороны сквозного осевого отверстия указанного элемента. Обычно и предпочтительно соединительный элемент представляет собой одно из рабочих колес указанного набора. Изобретение направлено на повышение надежности установки. 3 н. и 8 з.п. ф-лы, 5 ил.

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27-11-2012 дата публикации

ДИФФУЗОР, СОДЕРЖАЩИЙ ЛОПАТКИ С ОТВЕРСТИЯМИ

Номер: RU2011119619A
Принадлежит:

... 1. Диффузор (18) для компрессора смешенного потока или центробежного компрессора газовой турбины, содержащий по меньшей мере одну лопатку (20, 120), имеющую сторону (I) нагнетания, сторону (E) всасывания и первую боковую поверхность (22, 122), причем лопатка имеет множество отверстий (26, 126, 34, 134, 32, 132), открывающихся на сторону (E) всасывания и/или сторону (I) нагнетания и сообщающихся с по меньшей мере одной полостью, образованной в лопатке, при этом полость (30, 36, 200, 210) проходит в поперечном направлении относительно лопатки и открывается на первую боковую поверхность, отличающийся тем, что поперечное сечение полости (30, 36, 200, 210) изменяется в поперечном направлении лопатки, причем это поперечное сечение увеличивается по направлению к первой боковой поверхности.2. Диффузор по п.1, отличающийся тем, что он содержит первый ряд отверстий (26, 126), открывающихся на сторону (E) всасывания и сообщающихся с по меньшей мере одной полостью (30, 200), выполненной в лопатке и ...

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10-09-2015 дата публикации

ВЕНТИЛЯТОР В СБОРЕ

Номер: RU2014107461A
Принадлежит:

... 1. Вентилятор в сборе, содержащий:- сопло, содержащее заднюю секцию, которая имеет по меньшей мере одно первое впускное отверстие для воздуха, по меньшей мере одно первое выпускное отверстие для воздуха и первый внутренний проход для перемещения воздуха из по меньшей мере одного первого впускного отверстия для воздуха к по меньшей мере одному первому выпускному отверстию для воздуха; и переднюю секцию, которая имеет по меньшей мере одно второе впускное отверстие для воздуха, по меньшей мере одно второе выпускное отверстие для воздуха и второй внутренний проход для перемещения воздуха из по меньшей мере одного второго впускного отверстия для воздуха к по меньшей мере одному второму выпускному отверстию для воздуха; при этом секции сопла определяют внутреннее отверстие, через которое воздух снаружи вентилятора в сборе затягивается воздухом, испускаемым из сопла; и- основную часть, на которой установлено сопло и которая содержит средства создания первого воздушного потока через первый внутренний ...

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27-02-2013 дата публикации

ВЕНТИЛЯТОР

Номер: RU2011134679A
Принадлежит:

... 1. Вентилятор, предназначенный для создания воздушной струи и содержащий основание с отверстием для впуска воздуха и отверстием для выпуска воздуха, причем в основании расположена крыльчатка и двигатель, предназначенный для вращения крыльчатки с целью создания воздушного потока из отверстия для впуска воздуха до отверстия для выпуска воздуха; и вертикальное удлиненное кольцеобразное сопло, содержащее внутренний канал, предназначенный для приема воздушного потока из основания, и выпускной участок, предназначенный для выпуска воздушного потока, при этом сопло определяет отверстие, через которое воздушный поток, выходящий из выпускного участка, имеет возможность всасывания воздуха снаружи вентилятора.2. Вентилятор по п.1, в котором форма внутреннего канала обеспечивает разделение воздушного потока на два воздушных потока и направление каждого воздушного потока вдоль соответствующей стороны отверстия.3. Вентилятор по п.1, в котором сопло содержит кольцеобразную внутреннюю часть корпуса и кольцеобразную ...

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27-06-2015 дата публикации

КРЫЛЬЧАТКА ЦЕНТРОБЕЖНОГО КОМПРЕССОРА

Номер: RU2013156810A
Принадлежит:

... 1. Крыльчатка (201) центробежного компрессора (3), причем крыльчатка содержит диск (202) и лопатки (205), которые прикреплены к диску (202) на передней поверхности (203) диска (202) и каждая из которых имеет хвост (215) лопатки, кромку (216) лопатки, передний край (206) и задний край (207), отличающаяся тем, что точка пересечения между задним краем (207) и хвостом (215) лопатки дополнительно смещена вперед на по меньшей мере половину толщины диска (202), по сравнению с хвостом (215) лопатки на промежуточном диаметре (D) крыльчатки (201), а точка пересечения между задним краем (207) и кромкой (216) лопатки также дополнительно смещена вперед, по сравнению с кромкой (216) лопатки на промежуточном диаметре крыльчатки (201).2. Крыльчатка (201) по п.1, отличающаяся тем, что хвост (215) лопатки на периферии (209) крыльчатки (201) ориентирован в направлении, которое является по существу радиальным.3. Крыльчатка (201) по п.1, отличающаяся тем, что дополнительно содержит венец (211), соединенный ...

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26-02-2019 дата публикации

ДИФФУЗОР ЦЕНТРОБЕЖНОГО КОМПРЕССОРА

Номер: RU186988U9

Диффузор центробежного компрессора содержит радиальную и осевую части с диффузорними лопатками и лопатками спрямляющего аппарата. В зонах входных кромок диффузорних лопаток и лопаток спрямляющего аппарата стенка задняя диффузора выполнена с утолщением. На входных кромках диффузорних лопаток выполнена удлиненная несимметричная фаска; осевая часть стенки задней диффузора выполнена единой деталью, стенки диффузора скреплены болтовым соединением. Диффузор имеет экран, который отражает тепло от камеры сгорания. Решается задача повышения запаса газодинамической стойкости компрессора.

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27-12-2011 дата публикации

СВЕРХЗВУКОВОЙ РОТОР КОМПРЕССОРА, СВЕРХЗВУКОВОЙ КОМПРЕССОР (ВАРИАНТЫ) И СПОСОБ СЖАТИЯ ТЕКУЧЕЙ СРЕДЫ

Номер: RU2010125956A
Принадлежит:

... 1. Сверхзвуковой ротор компрессора, имеющий внутреннюю цилиндрическую полость, наружный обод и по меньшей мере один радиальный проточный канал, который обеспечивает возможность проточного сообщения между указанными полостью и ободом и содержит наклонную направляющую сверхзвукового сжатия. ! 2. Сверхзвуковой ротор по п.1, имеющий несколько радиальных проточных каналов. ! 3. Сверхзвуковой ротор по п.1, содержащий лопатки, которые расположены между парой опорных пластин ротора, и по меньшей мере одна из которых содержит наклонную направляющую сверхзвукового сжатия. !4. Сверхзвуковой компрессор, содержащий: ! (a) впускное отверстие для текучей среды, ! (b) выпускное отверстие для текучей среды и ! (c) по меньшей мере один сверхзвуковой ротор, имеющий внутреннюю цилиндрическую полость, наружный обод и по меньшей мере один радиальный проточный канал, который обеспечивает проточное сообщение между указанными полостью и ободом и содержит наклонную направляющую сверхзвукового сжатия. ! 5. Сверхзвуковой ...

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30-04-2008 дата публикации

Compressor controlling method for industrial axial gas turbine of power station, involves extracting highly compressed air in proximity or downstream of selected axial section by housing of compressor in asymmetrical sample

Номер: DE102007051633A1
Принадлежит:

The method involves extracting highly compressed air in proximity or downstream of a selected axial section (20) by a housing (18) of a compressor in an asymmetrical sample along the peripheral of the housing to counteract against flow disruptions. The highly compressed air is extracted through a set of holes or slots (16), which are asymmetrically arranged around the periphery of the housing of the compressor.

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04-06-1987 дата публикации

STUFENGEHAEUSE

Номер: DE0003542378A1
Принадлежит:

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21-03-2012 дата публикации

A fan assembly

Номер: GB0201202000D0
Автор:
Принадлежит:

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01-12-2010 дата публикации

A fan assembly

Номер: GB0201017706D0
Автор:
Принадлежит:

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06-01-2016 дата публикации

A humidifying apparatus

Номер: GB0002505754B

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23-10-2013 дата публикации

Gas turbine engine with secondary air flow circuit

Номер: GB0002501409A
Принадлежит:

One embodiment of the present invention is a unique gas turbine engine. Another embodiment of the present invention is a gas turbine engine having a unique secondary air flow circuit. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for gas turbine engines and secondary air flow circuits. Further embodiments, forms, features, aspects, benefits, and advantages of the present application will become apparent from the description and figures provided herewith.

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08-04-2009 дата публикации

Shroud-Diffuser assembly

Номер: GB0000903050D0
Автор:
Принадлежит:

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04-07-2018 дата публикации

An electric supercharger having a radial flow compressor Assembly

Номер: GB0002557909A
Принадлежит:

A reconfigurable radial flow compressor assembly 3 for an electric supercharger 1 has a vaned insert 22 releasable attached in the diffuser 13 between the compressors wheel 5 and a volute 10 leading to the outlet. The configuration allows the diffuser to be interchangeable between a vaned and non-vaned configuration. Cartridges with and without guide vanes are also disclosed. The walls of either the vaned or non-vanned insert may form part of the diffuser passage 14 together with an opposite surface wall of the diffuser. Vanes are provided in the diffuser to improve the flow characteristics, for example choke and surge, of the compressor. The reconfigurable compressor increases the scope of application over conventional compressors and optimises the manufacturing process. A kit of parts, electrical supercharger, engine system, method of operation and method of manufacture relating to the compressor are also disclosed.

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29-10-2008 дата публикации

A fan

Номер: GB0000817362D0
Автор:
Принадлежит:

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15-04-2009 дата публикации

A fan

Номер: GB0000903680D0
Автор:
Принадлежит:

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09-12-2009 дата публикации

Improved tunnel ventilation system

Номер: GB0000918692D0
Автор:
Принадлежит:

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07-07-2010 дата публикации

Centrifugal pump.

Номер: AP0000002131A
Принадлежит:

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30-04-2006 дата публикации

Centrifugal pump.

Номер: AP2006003574A0
Автор: LINDSKOG MARTIN
Принадлежит:

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31-05-2016 дата публикации

AN ADJUSTABLE SIDE LINER FOR A PUMP

Номер: AP0000003711A
Принадлежит:

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30-06-2016 дата публикации

LINER COUPLING PIN

Номер: AP0000003742A
Принадлежит:

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31-12-2014 дата публикации

A pump housing support

Номер: AP2014008116A0
Принадлежит:

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31-12-2010 дата публикации

A pump housing support.

Номер: AP2010005495A0
Принадлежит:

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31-12-2010 дата публикации

An adjustable side liner for a pump.

Номер: AP2010005494A0
Принадлежит:

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31-12-2010 дата публикации

Liner coupling pin.

Номер: AP2010005496A0
Принадлежит:

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31-01-2015 дата публикации

Liner coupling pin

Номер: AP2015008225A0
Принадлежит:

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31-10-2012 дата публикации

Pump intake device

Номер: AP2012006475A0
Автор: WALKER CRAIG IAN
Принадлежит:

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31-10-2012 дата публикации

Pump intake device

Номер: AP0201206475A0
Автор: WALKER CRAIG IAN
Принадлежит:

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31-10-2012 дата публикации

Pump intake device

Номер: AP0201206475D0
Автор: WALKER CRAIG IAN
Принадлежит:

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15-05-2007 дата публикации

CENTRIFUGAL PUMP

Номер: AT0000361429T
Принадлежит:

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15-11-2004 дата публикации

CAMP LOTS BLOOD PUMP

Номер: AT0000281191T
Принадлежит:

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15-06-2011 дата публикации

BLOWER

Номер: AT0000512306T
Принадлежит:

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15-06-2011 дата публикации

BLOWER ARRANGEMENT

Номер: AT0000512339T
Принадлежит:

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15-07-2019 дата публикации

COOLANT PUMP FOR INTERNAL COMBUSTION ENGINE

Номер: AT0000517125B1
Принадлежит:

Die Erfindung betrifft eine Kühlmittelpumpe (4) für eine Brennkraftmaschine (1), mit einem einen Gehäusedeckel (6) aufweisenden Gehäuse (5), in welchem ein um eine Drehachse (7) drehbares Laufrad (8) angeordnet ist, welches koaxial zur Drehachse (7) einen Saugmund (19) aufweist, wobei das Gehäuse (5) zumindest einen im Wesentlichen normal zur Drehachse (7) ausgebildeten Zulaufkanal (19) ausbildet, um Kühlmittel von einem von der Drehachse (7) beabstandeten seitlichen Pumpeneintritt (15) zum Saugmund (19) zu führen, und wobei der Zulaufkanal (18) zumindest ein strömungsbeeinflussendes Element (20, 21) aufweist. Um wenig Bauraum zu beanspruchen und eine homogene Anströmung des Laufrades zu ermöglichen, ist vorgesehen, dass – in Richtung der Drehachse (7) betrachtet - zumindest ein strömungsbeeinflussendes Element (20, 21) im Bereich einer vorzugsweise normal auf die Drehachse (7) und/oder durch die Drehachse (7) verlaufend ausgebildeten Längsmittelachse (18´) des Zulaufkanales (18) angeordnet ...

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15-11-2016 дата публикации

KÜHLMITTELPUMPE FÜR EINE BRENNKRAFTMASCHINE

Номер: AT517125A1
Автор: Pöschl Robert Dr.
Принадлежит:

The invention relates to a coolant pump (4) for an internal combustion engine (1), having a housing (5) which has a housing cover (6) and in which an impeller (8) is arranged which is rotatable about an axis of rotation (7) and has a suction nozzle (19). The housing (5) forms at least one intake channel (18) substantially normal with respect to the axis of rotation (7), in order to guide coolant from a lateral pump inlet (15) spaced apart from the rotary shaft (7) to the suction nozzle (19), wherein the intake channel (18) has at least one element (20, 21) which influences the flow. In order to take up very little installation space and to enable a homogeneous flow onto the impeller, according to the invention the at least one element (20, 21) which influences the flow - viewed in the direction of the axis of rotation (7) - is arranged in the region of a longitudinal central axis (18') of the intake channel (18) preferably normal with respect to the axis of rotation (7) and/or extending ...

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15-12-1992 дата публикации

ROTARY FLUID-FLOW MACHINE, APPLICABLE AS PUMP, COMPRESSORS, PROPELLERS, GENERATOR OR POWER TURBINE.

Номер: AT0000083298T
Принадлежит:

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29-09-2011 дата публикации

A fan

Номер: AU2010219491B2
Принадлежит:

A bladeless fan assembly comprises a nozzle (14) mounted on a base (12) housing means for creating an air flow. The nozzle (14) comprises an interior passage (94) for receiving the air flow, a mouth (26) for emitting the air flow, and a plurality of stationary guide vanes (120) located within the interior passage (94) and each for directing a portion of the air flow towards the mouth(26). The nozzle (14) defines an 10 opening (24) through which air from outside the fan assembly is drawn by the air flow emitted from the mouth(26).

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03-11-2011 дата публикации

A fan assembly

Номер: AU2010219490B2
Принадлежит:

A fan assembly for creating an air current comprises an air inlet (20), an air outlet (14), an impeller (64) and a motor (68) for rotating the impeller to create an air flow passing from the air inlet to the air outlet. The air outlet (14) comprises an interior passage (94) for receiving the air flow and a mouth (26) for emitting the air flow. The air outlet defines an opening (24) through which air from outside the fan assembly is drawn by the air flow emitted from the mouth. The motor (68) has a rotor which, in use, is capable of rotating at a speed of at least 5,000 rpm.

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10-09-2010 дата публикации

A fan

Номер: AU2010219489A1
Принадлежит:

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26-11-2015 дата публикации

A fan assembly

Номер: AU2013217475B2
Принадлежит:

A nozzle for a fan assembly includes an air inlet, a plurality of air outlets, and an annular casing having an annular inner wall defining a bore through which air from outside the nozzle is drawn by air emitted from the air outlets and an outer wall extending about the inner wall. The annular casing includes an air passage for conveying air to the air outlets. The air passage has an inlet section located between the inner wall and the outer wall and extending about the bore of the nozzle, and a plurality of outlet sections each extending across the bore for conveying air to a respective air outlet. To achieve an even air pressure at each end of each of the outlet sections, the inlet section of the air passage is arranged to convey air to each end of each of the outlet sections.

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24-07-2014 дата публикации

A fan assembly

Номер: AU2013217475A1
Принадлежит:

A nozzle for a fan assembly includes an air inlet, a plurality of air outlets, and an annular casing having an annular inner wall defining a bore through which air from outside the nozzle is drawn by air emitted from the air outlets and an outer wall extending about the inner wall. The annular casing includes an air passage for conveying air to the air outlets. The air passage has an inlet section located between the inner wall and the outer wall and extending about the bore of the nozzle, and a plurality of outlet sections each extending across the bore for conveying air to a respective air outlet. To achieve an even air pressure at each end of each of the outlet sections, the inlet section of the air passage is arranged to convey air to each end of each of the outlet sections.

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17-06-2010 дата публикации

A fan

Номер: AU2009326183A1
Принадлежит:

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23-12-2010 дата публикации

FLOW OUTPUT NOZZLE FOR CENTRIFUGAL PUMP

Номер: CA0002765508A1
Принадлежит:

A flow outlet for a pump includes a pocket section which defines a pocket section diameter. A throat section downstream of the pocket section, the throat section defines a throat section diameter less than the pocket section diameter.

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17-12-2009 дата публикации

ADJUSTABLE SIDE LINER FOR PUMP

Номер: CA0003076345A1
Принадлежит: MOFFAT & CO.

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17-12-2009 дата публикации

LINER COUPLING PIN

Номер: CA0002899851A1
Принадлежит:

... ²A coupling pin for use in a pump housing, the pump housing including an outer ²casing and ²an inner pump liner, the coupling pin being suitable for locating the liner ²and casing relative ²to one another, the coupling pin including a shank and a head at one end of ²the shank. The ²head includes a cammed surface thereon which is adapted to co-operate with a ²follower on ²the liner, and a locating section on a remote or terminal end of the head ²which is adapted to ²be positioned against a seat in the outer casing when fitted. The arrangement ²is such that ²rotation of the coupling pin causes the follower to track along the cammed ²surface so as to ²cause relative movement between the outer casing and the inner pump liner.² ...

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22-01-2015 дата публикации

COMPLIANT ABRASION RESISTANT BEARINGS FOR A SUBMERSIBLE WELL PUMP

Номер: CA0002918462A1
Принадлежит:

An electrical submersible pump assembly includes a centrifugal pump having impellers and diffusers. A thrust runner is coupled to a motor shaft for rotation along with the impellers. The runner receives thrust from at least one of the impellers and transfers the thrust to a bushing non rotatably mounted in one of the diffusers. The bushing has a thrust transferring end adjacent a thrust receiving shoulder in the diffuser. The bushing is axially movable in the receptacle. An annular spring located between the thrust receiving shoulder in the receptacle and the thrust transferring end of the bushing urges the bushing away from the thrust receiving shoulder.

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10-09-2010 дата публикации

A FAN ASSEMBLY

Номер: CA0002746548A1
Принадлежит:

A pedestal (12) for a fan assembly (10) comprises a telescopic duct (18) for conveying an air flow to an outlet of the fan assembly(10). The duct (18) comprises an outer tubular member (34) comprising a first stop member(130), an inner tubular member (36) located at least partially within and slidable relative to the outer tubular member (34), the inner tubular member (36) comprising a second stop member (140) for engaging the first stop member (130) to inhibit withdrawal of the inner tubular member (36) from the outer tubular member(34), and a mainspring (150) rotatably mounted on the second stop member(140), the mainspring (150) having a free end (156) retained by the first stop member(130).

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04-12-2012 дата публикации

A FAN ASSEMBLY

Номер: CA0002746497C

A bladeless fan assembly (10) for creating an air current comprises a nozzle (14) mounted on a base(12). The nozzle comprises an interior passage (86)and a mouth for receiving the air flow from the interior passage and through which the air flow is emitted from the fan assembly. The nozzle (14) defines an opening (24) through which 10 air from outside the fan assembly is drawn by the air flow emitted from the mouth. The nozzle is detachable from the base(12), which is preferably sized to be accommodated within the opening (24) of the nozzle (14) for transportation.

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10-09-2010 дата публикации

A FAN

Номер: CA0002746547A1
Принадлежит:

A bladeless fan assembly comprises a nozzle (14) mounted on a base (12) housing means for creating an air flow. The nozzle (14) comprises an interior passage (94) for receiving the air flow, a mouth (26) for emitting the air flow, and a plurality of stationary guide vanes (120) located within the interior passage (94) and each for directing a portion of the air flow towards the mouth(26). The nozzle (14) defines an 10 opening (24) through which air from outside the fan assembly is drawn by the air flow emitted from the mouth(26).

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20-12-2016 дата публикации

A FAN

Номер: CA0002746547C

A bladeless fan assembly comprises a nozzle (14) mounted on a base (12) housing means for creating an air flow. The nozzle (14) comprises an interior passage (94) for receiving the air flow, a mouth (26) for emitting the air flow, and a plurality of stationary guide vanes (120) located within the interior passage (94) and each for directing a portion of the air flow towards the mouth(26). The nozzle (14) defines an 10 opening (24) through which air from outside the fan assembly is drawn by the air flow emitted from the mouth(26).

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09-09-2011 дата публикации

PUMP INTAKE DEVICE

Номер: CA0002791079A1
Принадлежит:

A pump intake device comprising a main body which includes a side wall section having an inner side and an outer side, an intake section extending from the outer side of the side wall section and an intake passage extending through the intake section, the intake passage having an inner surface and an entry end and an exit end with a central axis extending between the entry and exit ends, a first portion of the inner surface having one or more first guides thereon for directing fluid passing through the intake passage so that in use said fluid leaves the exit end at the first portion with an exit angle which is inclined relative to the central axis.

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08-09-1990 дата публикации

CENTRIFUGAL COMPRESSOR HAVING HYBRID DIFFUSER AND EXCESS AREA DIFFUSING VOLUTE

Номер: CA0002011675A1
Принадлежит:

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31-10-1947 дата публикации

Zentrifugal-Fördermaschine.

Номер: CH0000251494A
Принадлежит: BUECHI ALFRED, BUECHI,ALFRED

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31-08-1943 дата публикации

Leitvorrichtung an Zentrifugalpumpen oder -gebläsen.

Номер: CH0000228507A
Принадлежит: BUECHI ALFRED, BUECHI,ALFRED

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30-11-1967 дата публикации

Pompe ou compresseur

Номер: CH0000447460A

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28-09-2012 дата публикации

Inductor to rotating hub and converge to suction stage of a pump.

Номер: CH0000704632B1
Принадлежит: SNECMA

Linvention concerne un étage daspiration (12) pour une pompe (10) à roue centrifuge, létage daspiration (12) comprenant un inducteur rotatif (18) muni dun moyeu (20) et disposé en amont de la roue centrifuge (14), létage daspiration (12) comprenant en outre un redresseur (34) disposé entre linducteur (18) et la roue centrifuge (14), le redresseur (34) comprenant une pluralité daubes (36). Linvention se caractérise par le fait que le moyeu (20) présente une surface aval (20b) sétendant axialement en convergeant vers la roue centrifuge, et en ce que les aubes (36) du redresseur (34) ont des extrémités libres, lesdites aubes faisant radialement saillie vers ladite surface aval de telle sorte que les extrémités libres des aubes viennent affleurer ladite surface aval (20b).

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30-06-2009 дата публикации

Fluid-flow machine with radially flowed through compressor wheel.

Номер: CH0000698256B1

Die Erfindung betrifft eine Strömungsmaschine mit radial durchströmten Verdichterrad (3), das auf einer in einem Lagergehäuse (1) gelagerten Welle (2) aufgenommen und in einem Verdichtergehäuse (8) mit einem schneckenförmigen Strömungskanal (9) angeordnet ist, wobei eine Aussenkontur (6) einer Nabe (4) des Verdichterrads (3) und eine Innenkontur (7) des Verdichtergehäuses (8) den von einer axialen Richtung in eine radiale Richtung umgelenkten Strömungskanal (9) ausbilden, wobei das Verdichtergehäuse (8) aus einem äusseren Spiralgehäuse (10) und einem inneren Gehäuseeinsatzstück (12) gebildet ist, wobei das äussere Spiralgehäuse (10) einen in die radiale Richtung nach aussen umgelenkten Kanalabschnitt (11) des Strömungskanals (9) umfasst und mittels einer ersten Fixierung (18) am Lagergehäuse (1) festgelegt ist, und wobei das innere Gehäuseeinsatzstück (12), nämlich dessen Innenkontur (13), mit der Aussenkontur (6) der Nabe (4) des Verdichterrads (3) einen im Wesentlichen in axialer Richtung ...

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31-08-2009 дата публикации

Fluid-flow machine with radially flowed through compressor wheel and with retaining mechanism.

Номер: CH0000698497B1

Die Erfindung betrifft eine Strömungsmaschine mit radial durchströmtem Verdichterrad. Das Verdichtergehäuse ist aus einem äusseren Spiralgehäuse (10) und einem inneren Gehäuseeinsatzstück (12) gebildet. Durch Alterung kann es zum Bruch des Verdichterrades kommen. Die Bruchstücke sollen im Idealfall von dem Gehäuseeinsatzstück (12) aufgefangen werden, um die Containmentsicherheit der Strömungsmaschine zu gewährleisten. Wegen der durch die auftreffenden Bruchstücke des Verdichterrades schlagartig freiwerdenden Kräfte, schlägt die vorliegende Erfindung einen speziellen Konstruktionsaufbau insbesondere des als Ersatzteil vorgesehenen inneren Gehäuseeinsatzstücks (12) vor, so dass die Bruchstücke sicher und kostengünstig in der Strömungsmaschine gehalten werden können, d.h. die Containmentsicherheit der Strömungsmaschine gewahrt ist.

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30-04-2009 дата публикации

Fluid-flow machine, in particular supercharger.

Номер: CH0000698022B1
Автор: KNEIP SVEN, SCHORER PAUL

Die Erfindung betrifft eine Strömungsmaschine, insbesondere Abgasturbolader, mit radial durchströmtem Verdichterrad (2), das auf einer in einem Lagergehäuse gelagerten Welle (1) aufgenommen und in einem Verdichtergehäuse mit einem schneckenförmigen Strömungskanal angeordnet ist, wobei eine Aussenkontur einer Nabe des Verdichterrads (2) und eine Innenkontur des Verdichtergehäuses den von einer axialen Richtung in eine radiale Richtung umgelenkten Strömungskanal ausbilden, wobei das Verdichtergehäuse aus einem äusseren Spiralgehäuse (5) und einem inneren Gehäuseeinsatzstück (6) gebildet ist, wobei das äussere Spiralgehäuse (5) mittels einer starren Fixierung am Lagergehäuse festgelegt ist, und wobei das innere Gehäuseeinsatzstück (6) zwischen dem Spiralgehäuse (5) und dem Verdichterrad (2) angeordnet und mittels einer flexiblen Fixierung (8) am Spiralgehäuse (5) festgelegt ist. Erfindungsgemäss umfasst die zweite Fixierung (8), die der Befestigung des Gehäuseeinsatzstücks (6) am Spiralgehäuse ...

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28-09-2018 дата публикации

Compressor for a turbocharger.

Номер: CH0000713634A2
Принадлежит:

Die Erfindung betrifft einen Verdichter für einen Turbolader, beinhaltend wenigstens Folgendes: Ein Verdichtergehäuse (10) mit einem Lufteinlass zum Aufnehmen von in dem Verdichter zu verdichtender Luft und mit einem Luftauslass zum Auslassen von in dem Verdichter verdichteter Luft, eine sich in axialer Richtung erstreckende Triebwelle, welche drehbar in dem Verdichtergehäuse (10) gelagert und über einen daran angreifenden Antrieb drehantreibbar ist, ein Verdichterlaufrad (40), das in dem Verdichtergehäuse (10) in Bezug auf einen Luftströmungspfad zwischen dem Lufteinlass und dem Luftauslass und auf der Triebwelle (30) angeordnet ist, eine sich radial erstreckende Diffusorpassage (14) in dem Verdichtergehäuse (10), welche eine erste radiale Wandung (22) und eine zweite radiale Wandung (24) aufweist, eine Verdichterspirale (15), welche sich als Luftpassage im Luftströmungspfad über die Diffusorpassage (14) an das Verdichterlaufrad (40) anschliesst und in den Luftauslass mündet, einen separaten ...

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30-07-2021 дата публикации

Verdichter für einen Turbolader.

Номер: CH713634B1

Die Erfindung betrifft einen Verdichter für einen Turbolader, beinhaltend wenigstens Folgendes: Ein Verdichtergehäuse (10) mit einem Lufteinlass zum Aufnehmen von in dem Verdichter zu verdichtender Luft und mit einem Luftauslass zum Auslassen von in dem Verdichter verdichteter Luft, eine sich in axialer Richtung erstreckende Triebwelle welche drehbar in dem Verdichtergehäuse (10) gelagert und über einen daran angreifenden Antrieb drehantreibbar ist, ein Verdichterlaufrad (40), das in dem Verdichtergehäuse (10) in Bezug auf einen Luftströmungspfad zwischen dem Lufteinlass und dem Luftauslass und auf der Triebwelle angeordnet ist, eine sich radial erstreckende Diffusorpassage (14) in dem Verdichtergehäuse (10), welche eine erste radiale Wandung (22) und eine zweite radiale Wandung (24) aufweist, eine Verdichterspirale (15), welche sich als Luftpassage im Luftströmungspfad über die Diffusorpassage (14) an das Verdichterlaufrad (40) anschließt und in den Luftauslass mündet, einen separaten ...

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31-03-2016 дата публикации

INTAKE DEVICE PUMP

Номер: EA0201500877A1
Автор:
Принадлежит:

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25-07-2019 дата публикации

PUMP INTAKE DEVICE

Номер: UA0000119640C2
Автор: WALKER CRAIG IAN
Принадлежит:

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30-09-2016 дата публикации

PUMP INTAKE DEVICE

Номер: EA0000024499B1
Принадлежит:

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05-11-2019 дата публикации

The suction piping for compressor, compression unit and refrigerator

Номер: CN0110418899A
Автор:
Принадлежит:

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21-04-2020 дата публикации

Air supply device and dust collector

Номер: CN0108026937B
Автор:
Принадлежит:

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15-03-2019 дата публикации

Compression device and supercharger

Номер: CN0107850090B
Автор:
Принадлежит:

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15-02-1949 дата публикации

Directing device for centrifugal machines

Номер: FR0000942669A
Принадлежит:

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27-07-1979 дата публикации

Centrifugal pump or compressor - has nozzles to direct fluid stream tangentially to volute outer casing to prevent eddy formation

Номер: FR0002413571A1
Автор:
Принадлежит:

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29-06-1962 дата публикации

Circuit with transistors for the transmission of a current of given intensity and reversible direction

Номер: FR0001297566A
Автор:
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17-08-1950 дата публикации

Номер: FR0000964401A
Автор:
Принадлежит:

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10-11-1989 дата публикации

CENTRIFUGAL PUMP

Номер: FR0002631084A1
Автор: POULAIN JEAN, JEAN POULAIN
Принадлежит:

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10-09-2010 дата публикации

A FAN

Номер: WO2010100460A1
Принадлежит:

A pedestal fan (10) comprises a base(16) housing an impeller (64) and a motor (68) for rotating the impeller to create an air flow, an air outlet (14), and a telescopic duct (18) for conveying the air flow to the air outlet.

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15-10-2009 дата публикации

Centrifugal Fan and Air Conditioner Using the Same

Номер: US2009255654A1
Принадлежит:

The present invention provides a centrifugal fan by which air velocity distribution in the height direction of impellers at a fan blow-out port is made uniform and running noise is reduced, and an air conditioner whose running noise is reduced by applying the centrifugal fan thereto. The centrifugal fan is provided with a hub for fixing the rotary shaft of a motor, a main plate formed on the outer circumference of the hub, a shroud disposed to be opposed to the main plate, which forms an air passage, a plurality of impellers disposed between the main plate and the shroud, and a bellmouth disposed at the suction side of the shroud. Projections or recesses are formed on the surface of the shroud facing the bellmouth, which projections or recesses form air streams flowing from the center of the shroud toward the outer circumference thereof along the surface when running a fan. The air conditioner has a thus constructed centrifugal fan mounted therein.

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03-11-2016 дата публикации

METHOD OF ASSEMBLING A SET OF IMPELLERS THROUGH TIE RODS IMPELLER AND TURBOMACHINE

Номер: US20160319820A1
Принадлежит:

A set of impellers that are axially adjacent to each other and that have respective axial through holes are assembled. At least a first and a second axial tie rods are used. At least one connection element being axially adjacent to two impellers respectively at its two sides and having an axial through hole is provided. The connection element is used for securing, at one side of its axial through hole, an end of the first axial tie rod and, at the other side of its axial through hole, an end of the second axial tie rod. Typically, the connection element is one of the impellers of the set.

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07-03-2017 дата публикации

Centrifugal compressor diffuser vanelet

Номер: US0009587646B2

A system, in certain embodiments, includes a centrifugal compressor diffuser including a flow path having a first surface and a second surface defining opposite axial sides of the flow path. The centrifugal compressor diffuser also includes multiple vanes extending from the first surface to the second surface of the flow path. A first profile of each vane varies along an axial direction. The centrifugal compressor diffuser further includes multiple vanelets extending from the first surface toward the second surface in the axial direction. A first axial extent of each vanelet is less than a second axial extent of the flow path. In addition, a second profile of each vanelet varies along the axial direction and/or the vanelets form a non-periodic pattern around a circumference of the flow path.

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10-07-2014 дата публикации

Вентиляторный блок воздухонагнетателя

Номер: RU0000142830U1

1. Блок воздухонагнетателя для системы обогрева, вентиляции и кондиционирования воздуха, который содержит кожух с установленным в нем мотором, первый вентилятор и второй вентилятор, функционально соединенные с мотором и выровненные по одной оси относительно друг друга таким образом, чтобы втягивать воздух из первого впускного отверстия и второго впускного отверстия соответственно, а также выпускное отверстие, в которое поступает воздух от первого вентилятора и второго вентилятора и которое направляет воздух в пассажирский салон.2. Блок воздухонагнетателя по п.1, который содержит вал, приводимый в действие мотором и проходящий от первого и второго противоположных концов мотора, где первый вентилятор соединен с первым концом вала, а второй вентилятор соединен со вторым концом вала.3. Блок воздухонагнетателя по п.2, в котором кожух также имеет первое впускное отверстие, через которое первый вентилятор втягивает воздух в кожух, и второе впускное отверстие, через которое второй вентилятор втягивает воздух в кожух.4. Блок воздухонагнетателя по п.3, в котором первый вентилятор выполнен с возможностью втягивать рециркуляционный воздух из пассажирского салона и воздух снаружи от пассажирского салона.5. Блок воздухонагнетателя по п.1, в котором первый вентилятор выполнен с возможностью втягивать рециркуляционный воздух из пассажирского салона и воздух снаружи от пассажирского салона.6. Блок воздухонагнетателя по п.1, в котором второй вентилятор выполнен с возможностью втягивать рециркуляционный воздух из пассажирского салона и воздух снаружи пассажирского салона.7. Блок воздухонагнетателя по п.1, в котором первый в РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 142 830 U1 (51) МПК B60H 1/28 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ТИТУЛЬНЫЙ (21)(22) Заявка: ЛИСТ ОПИСАНИЯ ПОЛЕЗНОЙ МОДЕЛИ К ПАТЕНТУ 2014106120/11, 19.02.2014 (24) Дата начала отсчета срока действия патента: 19.02.2014 Приоритет(ы): (30) Конвенционный приоритет: (72) Автор(ы): МЭРАНВИЛЛ Клэй ...

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10-06-2016 дата публикации

Ступень высокоскоростного многоступенчатого погружного центробежного насоса

Номер: RU0000162421U1

1. Ступень высокоскоростного многоступенчатого погружного центробежного насоса, содержащая рабочее колесо со ступицей и направляющий аппарат, состоящий из стакана, верхнего диска с радиально-осевой опорой, нижнего диска с радиальной опорой и лопаток, нижний диск направляющего аппарата с радиальной опорой, которые выполнены монолитно со стаканом, причем стакан выполнен из перфорированного металлического цилиндра со слоем полимерного материала на его внутренней поверхности и перфорациями, заполненными полимерным материалом, причем верхний диск, нижний диск, лопатки направляющего аппарата и рабочее колесо изготовлены из полимерного материала.2. Ступень по п. 1, отличающаяся тем, что в качестве полимерного материала используются композиции на основе полифениленсульфида.3. Ступень по п. 1, отличающаяся тем, что перфорации металлического цилиндра выполнены в поперечном сечении в виде кругов диаметром от 1 мм до 6 мм, общей площадью от 10 до 70% от внутренней площади металлического цилиндра, причем круги расположены по поверхности равномерно.4. Ступень по п. 2, отличающаяся тем, что перфорации металлического цилиндра выполнены в поперечном сечении в виде кругов диаметром от 1 мм до 6 мм, общей площадью от 10 до 70% от внутренней площади металлического цилиндра, причем круги расположены по поверхности равномерно, а в качестве полифениленсульфида используется фортрон.5. Ступень по п. 1, отличающаяся тем, что перфорации металлического цилиндра выполнены в поперечном сечении в виде овалов, общей площадью от 10 до 70% от внутренней площади металлического цилиндра, причем овалы расположены по поверхности равномерно.6. Ступень по п. 2, отличающаяся тем, что перфорации м РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 162 421 U1 (51) МПК F04D 13/10 (2006.01) F04D 29/02 (2006.01) F04D 29/44 (2006.01) F04D 29/22 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ТИТУЛЬНЫЙ (21)(22) Заявка: ЛИСТ ОПИСАНИЯ ПОЛЕЗНОЙ МОДЕЛИ К ПАТЕНТУ 2015118507/06, 18.05.2015 (24) Дата начала ...

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27-12-2016 дата публикации

Центробежный компрессор

Номер: RU0000167153U1

Центробежный компрессор, содержащий корпус, крышку, входной направляющий аппарат, включающий переднюю и заднюю стенки с расположенными между ними лопатками, установленный между крышкой и корпусом и образующий с ними проточную часть, и соединенный задней стенкой с корпусом, отличающийся тем, что передняя стенка снабжена кольцевым выступом, а крышка - ответным уступом, и они контактируют между собой. РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 167 153 U1 (51) МПК F04D 29/28 (2006.01) F04D 29/44 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ТИТУЛЬНЫЙ (21)(22) Заявка: ЛИСТ ОПИСАНИЯ ПОЛЕЗНОЙ МОДЕЛИ К ПАТЕНТУ 2016117746/06, 04.05.2016 (24) Дата начала отсчета срока действия патента: 04.05.2016 (72) Автор(ы): Ремизов Алексей Владимирович (RU) (73) Патентообладатель(и): Акционерное общество "ОДК-Газовые Турбины" (RU) R U Приоритет(ы): (22) Дата подачи заявки: 04.05.2016 (45) Опубликовано: 27.12.2016 Бюл. № 36 R U 1 6 7 1 5 3 (57) Формула полезной модели Центробежный компрессор, содержащий корпус, крышку, входной направляющий аппарат, включающий переднюю и заднюю стенки с расположенными между ними лопатками, установленный между крышкой и корпусом и образующий с ними проточную часть, и соединенный задней стенкой с корпусом, отличающийся тем, что передняя стенка снабжена кольцевым выступом, а крышка - ответным уступом, и они контактируют между собой. Стр.: 1 U 1 U 1 (54) ЦЕНТРОБЕЖНЫЙ КОМПРЕССОР 1 6 7 1 5 3 Адрес для переписки: 152914, Ярославская обл., г. Рыбинск, ул. Толбухина, 16, главному конструктору АО "ОДК-ГТ" Гузаеву Е.В. U 1 U 1 1 6 7 1 5 3 1 6 7 1 5 3 R U R U Стр.: 2

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05-12-2018 дата публикации

Насос нефтяной магистральный с однозавитковым отводом и направляющим аппаратом

Номер: RU0000185455U1

Полезная модель относится к насосостроению. Насос центробежный, горизонтальный, одноступенчатый, межопорный, включает корпус с полуспиральным подводом, спиральным отводом и направляющим аппаратом, ротор с рабочим колесом двустороннего входа закрытого типа, радиальный и осерадиальный подшипники, торцовые уплотнения. Направляющий аппарат выполнен сменным, при этом количество лопаток направляющего аппарата меньше количества лопаток рабочего колеса. Отвод насоса спиральный однозавитковый. Полезная модель направлена на улучшение КПД насоса, снижение действующих на ротор радиальных сил и уменьшение вибрационных нагрузок. РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 185 455 U1 (51) МПК F04D 29/44 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ПОЛЕЗНОЙ МОДЕЛИ К ПАТЕНТУ (52) СПК F04D 29/448 (2018.08) (21)(22) Заявка: 2018122150, 14.06.2018 (24) Дата начала отсчета срока действия патента: Дата регистрации: 05.12.2018 (45) Опубликовано: 05.12.2018 Бюл. № 34 Адрес для переписки: 665734, Иркутская обл., г. Братск, ул. Олимпийская, 14, ООО "Транснефть-Восток" (73) Патентообладатель(и): Публичное акционерное общество "Транснефть" (ПАО "Транснефть") (RU), Общество с ограниченной ответственностью "Транснефть-Восток" (ООО "Транснефть-Восток") (RU) (54) НАСОС НЕФТЯНОЙ МАГИСТРАЛЬНЫЙ С ОДНОЗАВИТКОВЫМ ОТВОДОМ И НАПРАВЛЯЮЩИМ АППАРАТОМ (57) Реферат: Полезная модель относится к насосостроению. выполнен сменным, при этом количество лопаток Насос центробежный, горизонтальный, направляющего аппарата меньше количества одноступенчатый, межопорный, включает корпус лопаток рабочего колеса. Отвод насоса с полуспиральным подводом, спиральным спиральный однозавитковый. Полезная модель отводом и направляющим аппаратом, ротор с направлена на улучшение КПД насоса, снижение рабочим колесом двустороннего входа закрытого действующих на ротор радиальных сил и типа, радиальный и осерадиальный подшипники, уменьшение вибрационных нагрузок. торцовые уплотнения. Направляющий аппарат R U 1 ...

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17-05-2019 дата публикации

Диффузор центробежного компрессора

Номер: RU0000189277U1

Полезная модель относится к области компрессоростроения и предназначена для улучшения массогабаритных и газодинамических характеристик компрессора за счет преобразования скоростного напора в напор давления. Технический результат - повышение адиабатического КПД центробежного компрессора, уменьшение потерь полного давления воздуха на участке воздушного тракта между рабочим колесом компрессора и камерой сгорания. Диффузор центробежного компрессора, представляющий собой единую конструкцию, содержащую диск с центральным отверстием, на котором радиально расположены спрямляющие лопатки, на торцевой части диска расположены лопатки диффузора, при этом входной угол лопатки диффузора в среднем ее сечении определяется по формуле, где С– абсолютная скорость потока воздуха на выходе из рабочего колеса, а С– радиальная составляющая абсолютной скорости потока воздуха на выходе из рабочего колеса, периферийное сечение лопаток диффузора повернуто вокруг их входной кромки на α= 4° относительно среднего сечения лопаток диффузора в направлении вращения ротора, а корневое сечение лопаток диффузора повернуто на α= 5° в направлении против вращения ротора, хорда сечений радиальных спрямляющих лопаток определяется по формуле, где l– это относительная высота лопатки спрямляющего аппарата, изменяющаяся в пределах от 0 до 1, b= 2.15h– хорда корневого сечения спрямляющей лопатки, где h– абсолютная высота спрямляющей лопатки, причем стенки спрямляющих лопаток оканчивается непосредственно за корневым сечением спрямляющих лопаток в направлении ниже по потоку от лопаток, а на верхних гранях лопаток диффузора установлены шпильки с резьбой. РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 189 277 U1 (51) МПК F04D 29/44 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ПОЛЕЗНОЙ МОДЕЛИ К ПАТЕНТУ (52) СПК F04D 29/44 (2019.02) (21)(22) Заявка: 2018147247, 28.12.2018 (24) Дата начала отсчета срока действия патента: Дата регистрации: 17.05.2019 (45) Опубликовано: 17.05.2019 Бюл. № 14 1 8 9 ...

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24-02-2021 дата публикации

Входной патрубок центробежного вентилятора

Номер: RU0000202531U1

Полезная модель относится к области вентиляторостроения, а именно к входным устройствам центробежных вентиляторов.Технический результат заявляемой полезной модели направлен на повышение КПД вентилятора за счет уменьшения потерь энергии воздушного потока во входном патрубке за счет снижения степени турбулизации.Технический результат достигается тем, что входной патрубок центробежного вентилятора содержит направляющий аппарат, причем направляющий аппарат установлен в начальной части патрубка и выполнен в виде решетки из пластин, а на конечном участке патрубка установлена направляющая решетка, выполненная в виде радиально ориентированных пластин, наклоненных относительно оси патрубка на острый угол, при этом входной патрубок содержит также штуцер для подачи вязкой среды, размещенный непосредственно перед угловым участком. 7 ил. РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 202 531 U1 (51) МПК F04D 29/44 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ПОЛЕЗНОЙ МОДЕЛИ К ПАТЕНТУ (52) СПК F04D 29/44 (2020.08) (21)(22) Заявка: 2020116855, 20.05.2020 (24) Дата начала отсчета срока действия патента: Дата регистрации: 24.02.2021 (45) Опубликовано: 24.02.2021 Бюл. № 6 2 0 2 5 3 1 R U (54) Входной патрубок центробежного вентилятора (57) Реферат: Полезная модель относится к области вентиляторостроения, а именно к входным устройствам центробежных вентиляторов. Технический результат заявляемой полезной модели направлен на повышение КПД вентилятора за счет уменьшения потерь энергии воздушного потока во входном патрубке за счет снижения степени турбулизации. Технический результат достигается тем, что входной патрубок центробежного вентилятора содержит направляющий аппарат, причем Стр.: 1 (56) Список документов, цитированных в отчете о поиске: SU 1108252 A1, 15.08.1984. RU 2536572 C2, 27.12.2014. US 20070059170 A1, 15.03.2007. RU 2124651 C1, 10.01.1999. направляющий аппарат установлен в начальной части патрубка и выполнен в виде решетки из пластин, а на конечном ...

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15-03-2012 дата публикации

Internally-cooled centrifugal compressor with cooling jacket formed in the diaphragm

Номер: US20120063882A1
Принадлежит: Southwest Research Institute SwRI

An internally-cooled centrifugal compressor ( 10 ) having a shaped casing ( 26 ) a diaphragm ( 32 ) disposed within said shaped casing ( 26 ) having a gas side and a coolant side so that heat from a gas flowing though the gas side is extracted via the coolant side. An impeller ( 28 ) disposed within the diaphragm ( 32 ) has a stage inlet ( 22 ) on one side and an stage outlet ( 24 ) for delivering a pressurized gas to a downstream connection through the stage outlet coupling ( 14 ). The coolant side of said diaphragm ( 32 ) includes at least one passageway for directing a coolant in a substantially counter-flow direction from the flow of gas through the gas side.

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05-07-2012 дата публикации

Discharge scroll and turbomachine

Номер: US20120171030A1
Принадлежит: Mitsubishi Heavy Industries Ltd

Provided is an exhaust scroll capable of reducing mixing loss caused by fluid swirling inside the exhaust scroll and fluid flowing thereinto, while collecting and discharging the fluid which has flowed. The exhaust scroll is provided with a scroll body ( 11 ) in which a space having a substantially annular cross section is formed and a connecting portion ( 12 ) which connects an exhaust passage ( 8 ) with the scroll body ( 11 ) to forcibly decelerate fluid (A) discharged from the exhaust passage ( 8 ), thereby allowing the fluid (A) to flow into the scroll body ( 11 ).

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06-09-2012 дата публикации

Pump

Номер: US20120224961A1
Принадлежит: EGO Elektro Geratebau GmbH

A pump for a dishwasher has an impeller for conveying fluid, wherein it is formed as a centrifugal pump with the fluid to be conveyed being sucked-in in a central axial manner and flowing out in a radial manner. The impeller extends on a bottom surface above a pump base, wherein several fixed flow directing blades are arranged radially outside the impeller, said flow directing blades extending in a helicoidal manner with the pitch extending in the rotational direction of the impeller away from the pump base. At least one flow directing blade extends as far as up to the bottom surface of the impeller for picking up a circulating funnel or tube produced of fluid with air bubbles therein.

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13-09-2012 дата публикации

Intermediate floor for a radial turbine engine

Номер: US20120230812A1
Автор: Peter Robens, Werner Jonen
Принадлежит: SIEMENS AG

A radial turbomachine includes a radial diffuser channel with a diaphragm, a deflecting channel connecting to the radial diffuser channel downstream thereof, and a return flow channel connecting to the deflecting channel downstream thereof. The main flow direction of the radial diffuser channel runs radially from inside to outside. The main flow direction of the deflecting channel is deflected from radially outward to radially inward. The main flow direction of the return channel runs radially from outside to inside. The diaphragm comprises first, second and third outer surface sections. The first outer surface section has a convex shape for delimiting the deflecting channel. At least one consumption-gas removal channel is provided in the diaphragm so that, if the main flow in the deflecting channel comprises solid or liquid particles, a consumption gas can be discharged therefrom through the consumption-gas removal channel as low-particulate gas of a main flow.

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31-01-2013 дата публикации

Acoustic Array of Polymer Material

Номер: US20130025967A1
Автор: David C. Seib
Принадлежит: Dresser Rand Co

The invention is an acoustic liner for attenuating noise in rotating machinery. The acoustic liner may include a plurality of cells coupled together to form an annular cell matrix, the plurality of cells being made of a non-metallic material, for example, plastics, polymers, thermoplastics, or thermosets. Each cell of the acoustic liner may be hexagonally-shaped such that the annular cell matrix forms a honeycomb structure.

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14-03-2013 дата публикации

Variable-speed oil-free refrigerant centrifugal compressor with variable geometry diffuser

Номер: US20130064682A1
Автор: Joost Brasz, Lin Sun
Принадлежит: Danfoss Turbocor Compressors BV

A refrigerant compressor includes a housing providing a refrigerant outlet having a throat. An electric motor is provided in the housing to directly drive an impeller via a shaft about an axis in response to a variable speed command. The impeller includes an outlet end aligned with variable geometry diffuser. A magnetic bearing assembly rotationally supports the shaft relative to the housing in response to a magnetic bearing command. A member is arranged to adjust the throat area, and which can move in a direction generally parallel to the axis in response to an actuator receiving a compressor regulation command. A controller is configured to respectively provide the variable speed command, the magnetic bearing command and the compressor regulation command to the electric motor to vary throat area, the magnetic bearing assembly and the actuator to obtain a desired compressor operation without the need of variable inlet geometry.

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21-03-2013 дата публикации

Ventilating fan

Номер: US20130072105A1

A ventilating fan includes a sirocco fan disposed in a box-shaped body and an adapter connected to an air outlet of the sirocco fan. The sirocco fan is composed of two opposite scroll plates with scroll shapes and a casing plate sandwiched between the two scroll plates. An overall air inlet of the sirocco fan is disposed on the first scroll plate and a central line of the air outlet of the adapter is offset towards the second scroll plate. The present invention is advantageous in that no turbulence is generated at the adapter and the wind amount of the ventilating fan is thus ensured and noise is reduced. Therefore, the present invention can provide a small air blowing device with high efficiency and improve stability of performance of the product.

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09-05-2013 дата публикации

Pump with Hydraulic Isolator

Номер: US20130115071A1
Принадлежит: Individual

Embodiments of the invention provide a hydraulic isolator to split a volute of a pump into two compartments. The hydraulic isolator is positioned within the volute and includes an inlet positioned around a volute inlet channel of the pump, and an outlet positioned adjacent to an outlet channel of the pump. The hydraulic isolator also includes a toroidal portion to at least partially surround an impeller of the pump.

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23-05-2013 дата публикации

Electric blower and vacuum cleaner comprising same

Номер: US20130125339A1
Принадлежит: Panasonic Corp

Disclosed is an electric blower having a stator, a rotor, a bracket, a rotary fan, an air guide and a fan case. The air guide comprises a partition plate, a diffuser disposed around outer periphery of the rotary fan in the air guide, a partition-plate sloped portion and a guide vane. The fan case has a fan-facing portion, a fan case shoulder bent at the outermost part of the fan-facing portion, and a cylindrical portion extending cylindrically in an axial direction from the fan case shoulder. The fan case shoulder is so bent that it forms substantially a right angle.

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23-05-2013 дата публикации

Fan assembly

Номер: US20130129490A1
Принадлежит: Dyson Technology Ltd

A nozzle for a fan assembly has an air inlet, an annular air outlet, and an interior passage for conveying air from the air inlet to the air outlet. The interior passage is located between an annular inner wall, and an outer wall extending about the inner wall. The inner wall at least partially defines a bore through which air from outside the nozzle is drawn by air emitted from the air outlet. The inner wall is eccentric with respect to the outer wall so that the cross-sectional area of the interior passage varies about the bore. The variation in the cross-sectional area of the interior passage can control the direction in which air is emitted from around the air outlet to reduce turbulence in the air flow generated by the fan assembly.

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08-08-2013 дата публикации

Blade cascade and turbomachine

Номер: US20130202444A1
Автор: Roland Wunderer
Принадлежит: MTU AERO ENGINES GMBH

A blade cascade for a turbomachine having a plurality of blades arranged next to one another in the peripheral direction, at least two blades having a variation for generating an asymmetric outflow in the rear area, as well as a turbomachine having an asymmetric blade cascade, which is connected upstream from another blade cascade, are disclosed.

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12-09-2013 дата публикации

Humidifying apparatus

Номер: US20130234347A1
Принадлежит: Dyson Technology Ltd

Humidifying apparatus includes a base housing a motor and impeller unit for generating a first air flow. A removable nozzle includes an interior passage for receiving the first air flow and an air outlet for emitting the first air flow. The nozzle defines an opening through which air from outside the apparatus is drawn by air emitted from the air outlet. The apparatus is configured to humidify a second air flow, which is emitted from a plurality of second air outlets. The second air flow is humidified with water supplied from a water tank mounted on the base. The water tank has a handle which is moveable between a stowed position and a deployed position, and which is biased towards the deployed position. The nozzle is configured to urge the handle towards the stowed position.

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19-09-2013 дата публикации

Centrifugal fan and fan with sound-muffling box having the centrifugal fan built-in

Номер: US20130243585A1
Принадлежит: Panasonic Corp

A centrifugal fan includes a casing side plate with a casing inlet, a spiral scroll, a tongue, a casing outlet, a main plate, a retaining ring, multiple blades arranged between the main plate and the retaining ring, and an air-intake space surrounded by the blades. The centrifugal fan further includes an airflow accelerator in the air-intake space for increasing an airflow speed of a gas toward the blades.

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24-10-2013 дата публикации

DIFFUSER CASE REMOVAL APPARATUS AND METHOD

Номер: US20130276285A1
Принадлежит:

A method and apparatus is provided for removing a centrifugal compressor diffuser case from a turbofan gas turbine engine case which may be used while the engine is installed on an aircraft or when the engine has been removed from the aircraft. The tool includes movable gripping members at least one force member for exerting a pushing action on the engine structure on which the diffuser case is mounted the method includes gripping a peripheral portion of the diffuser case and applying an axial pushing force on the case relative to the engine case to thereby overcome an interference fit between the diffuser case and the engine case. 16.-. (canceled)7. A method of removing a centrifugal compressor diffuser case from a circumferential flange of a turbofan gas turbine engine case in which the diffuser case is mounted with an interference fit , the method comprising:removing at least one fastener connecting the diffuser case to the flange so that substantially only the interference fit joins the diffuser case to the flange;installing a plurality of tools around a periphery of the diffuser case;gripping a portion of the diffuser case with each of the tools; and thenpushing axially against the flange in a concerted fashion with each of the tools with sufficient force to overcome the interference fit between the diffuser case and the flange and thereby axially move the diffuser case away from the flange.8. The method as defined in claim 7 , wherein installing the plurality of tools includes engaging positioning members of each of the tools with corresponding engaging elements of at least one of the diffuser case and the gas turbine engine.9. The method as defined in claim 7 , wherein gripping the portion of the diffuser case with each of the tools includes rotating gripping members of each of the tools to a position in engagement with the portion.10. The method as defined in claim 7 , wherein gripping the portion of the diffuser case with each of the tools includes gripping ...

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07-11-2013 дата публикации

FAN

Номер: US20130294905A1
Принадлежит:

A floor standing pedestal fan for creating an air current includes a base housing an impeller and a motor for rotating the impeller to create an air flow, an air outlet, and a telescopic duct for conveying the air flow to the air outlet.

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28-11-2013 дата публикации

DIFFUSER HAVING DETACHABLE VANES WITH POSITIVE LOCK

Номер: US20130315741A1
Принадлежит: Cameron International Corporation

A system, in certain embodiments, includes a centrifugal compressor diffuser that includes an elliptical plate including multiple vane receptacles disposed about an axis of the plate and multiple detachable vanes attached to the plate. Each vane receptacle includes a first two dimensional (2D) projection along a plane of the elliptical plate and each detachable vane includes a second two dimensional (2D) projection along a base portion of the vane, where each detachable vane is disposed in a respective vane receptacle with the first and second 2D projections blocking movement of the detachable vane in at least a first axial direction relative to the elliptical plate. In certain embodiments, the first and second 2D projections may include a first tab to fit in a recess between a pair of second tabs, respectively, or vice versa. However, in other embodiments, the first and second 2D projections may include alternative mating surfaces. 1. A system , comprising: a base portion; and', 'a plurality of detachable vanes attached to the base portion, wherein each detachable vane comprises a cross-sectional profile that varies along a span of the detachable vane., 'a centrifugal compressor diffuser, comprising2. The system of claim 1 , wherein the base portion comprises an elliptical plate.3. The system of claim 1 , wherein the base portion comprises a plurality of first two-dimensional (2D) mounts that interlock with a plurality of second two-dimensional (2D) mounts of the respective plurality of detachable vanes.4. The system of claim 3 , wherein the each first 2D mount of the plurality of first 2D mounts couples to a mating second 2D mount of the plurality of second 2D mounts corresponding to a respective vane of the plurality of detachable vanes to create an interlocked connection.5. The system of claim 4 , wherein each interlocked connection blocks axial separation of the respective vane relative to the base portion.6. The system of claim 4 , wherein each first 2D mount ...

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26-12-2013 дата публикации

PUMP

Номер: US20130343882A1
Автор: Albert Tobias, Koegel Uwe
Принадлежит:

An impeller radial pump includes a pump chamber with a central suction and with a pump chamber outlet, wherein an impeller is provided in the pump chamber. Radially outside of the impeller, a circular ring shaped and circumferential pump chamber ring section is provided as a part of the pump chamber, wherein the pump chamber ring section essentially has an extension along the axial direction of the pump from the impeller against the suction direction. The pump chamber ring section has a varying width and is configured to be narrower in a compression region in the circulation direction. 1. A pump , in particular for home appliances such as dish washers or washing machines , said pump being configured as a radial pump , having a pump chamber with a central suction and with a pump chamber outlet , wherein in said pump chamber an impeller rotates for transporting fluid and for discharging said fluid from said suction in a radial direction out of said impeller into said pump chamber , wherein said discharged fluid is moved for circulation in said pump chamber towards said pump chamber outlet , wherein radially outside said impeller , a circular ring shaped and circumferential pump chamber ring section is provided as a part of said pump chamber , wherein said pump chamber ring section essentially has a length along an axial direction of said pump from said impeller against a suction direction up to said pump chamber outlet , wherein said axial length of said pump chamber ring section is four times to ten times its width , wherein said pump chamber ring section has a varying width and is configured to be narrower in a compression region in a circulation direction , wherein said pump chamber is configured without a guide ring for said fluid and does not have guide elements of a type of said guide ring.2. The pump according to claim 1 , wherein said pump chamber ring section is configured to be gradually or continuously increasingly narrower in said circulation direction ...

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26-12-2013 дата публикации

SCROLL STRUCTURE OF CENTRIFUGAL COMPRESSOR

Номер: US20130343885A1
Принадлежит: MITSUBISHI HEAVY INDUSTRIES, LTD.

An axial cross-sectional shape of a scroll flow path is a roughly circular shape, a diffuser outlet connected to the roughly circular shape is shifted to a position which is closer to a circle center than to a position of a tangent line to the circular shape and which does not reach the circle center, the circular shape is formed from a scroll chamber which juts out in the axial direction relative to the position of the diffuser outlet and a shift chamber that forms a remainder of the roughly circular shape in a direction opposite to the scroll chamber and the shift chamber is at least formed on the scroll flow path of a winding end portion in a circumferential direction of a spiral. 1. A scroll structure of a centrifugal compressor comprising a diffuser which is provided on an outer circumferential side of an impeller and a scroll flow path which is formed in a spiral shape that connects to an outer circumference of the diffuser , wherein an axial cross-sectional shape of the scroll flow path is a roughly circular shape , a diffuser outlet connected to the roughly circular shape is shifted to a position which is closer to a circle center than to a position of a tangent line to the circular shape and which does not reach the circle center , the roughly circular shape is formed from a scroll chamber which juts out in the axial direction relative to the position of the diffuser outlet and a shift chamber that forms a remainder of the roughly circular shape in a direction opposite to the scroll chamber , and the shift chamber is at least formed on the scroll flow path of a winding end portion in a circumferential direction of a spiral.2. The scroll structure of a centrifugal compressor according to claim 1 , wherein the shift chamber starts shifting from a position approximately 180 degrees preceding the winding end portion in a circumferential direction and increases so as to reach maximum at a position of approximately 360 degrees claim 1 , and a shift amount ...

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02-01-2014 дата публикации

Centrifugal compressor

Номер: US20140003930A1
Принадлежит: Toyota Motor Corp

A compressor has a hub-side wall of a hub-side wall plate, a shroud-side wall that faces the hub-side wall and forms a diffuser path between the shroud-side wall and the hub-side wall, vanes that protrude from the hub-side wall plate into the diffuser path, and an actuator capable of changing the distance between the vanes and the shroud-side wall in accordance with a flow rate of air in the diffuser path. Adjacent ones of the adjacent vanes do not overlap with each other when viewed from a center axis of the compressor. When the actuator maximizes the distance between the vanes and the shroud-side wall, the distance between the vanes and the shroud-side wall is smaller than the distance between the hub-side wall and areas of the shroud-side wall that face the vanes.

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06-02-2014 дата публикации

Multi-degree of freedom resonator array

Номер: US20140034416A1
Автор: Zheji Liu
Принадлежит: Dresser Rand Co

Apparatus and methods for attenuating noise, vibration, and/or acoustic energy in a turbomachine. The apparatus includes a first base plate having first base plate perforations defined therethrough. The apparatus also includes first and second spacers each extending from the first base plate, being spaced apart from each other, and defining a first channel therebetween. The apparatus further includes a first insert disposed in the first channel and having insert perforations defined therethrough, the first base plate, the first and second spacers, and the first insert at least partially defining a first acoustic chamber therebetween, wherein the base plate perforations and the insert perforations are in communication with the first acoustic chamber.

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06-03-2014 дата публикации

CENTRIFUGAL COMPRESSOR DIFFUSER VANELET

Номер: US20140064953A1
Принадлежит: Cameron International Corporation

A system, in certain embodiments, includes a centrifugal compressor diffuser including a flow path having a first surface and a second surface defining opposite axial sides of the flow path. The centrifugal compressor diffuser also includes multiple vanes extending from the first surface to the second surface of the flow path. A first profile of each vane varies along an axial direction. The centrifugal compressor diffuser further includes multiple vanelets extending from the first surface toward the second surface in the axial direction. A first axial extent of each vanelet is less than a second axial extent of the flow path. In addition, a second profile of each vanelet varies along the axial direction and/or the vanelets form a non-periodic pattern around a circumference of the flow path. 1. A system comprising: a flow path having a first surface and a second surface defining opposite axial sides of the flow path;', 'a plurality of vanes extending from the first surface to the second surface of the flow path, wherein a first profile of each vane varies along an axial direction; and', 'a plurality of vanelets extending from the first surface toward the second surface in the axial direction, wherein a first axial extent of each vanelet is less than a second axial extent of the flow path, and wherein a second profile of each vanelet varies along the axial direction, the plurality of vanelets form a non-periodic pattern around a circumference of the flow path, or a combination thereof., 'a centrifugal compressor diffuser comprising2. The system of claim 1 , wherein the first surface comprises a shroud-side mounting surface.3. The system of claim 1 , wherein the first axial extent of each vanelet is less than approximately 25 percent of the second axial extent of the flow path.4. The system of claim 1 , wherein the second profile of each vanelet varies along the axial direction claim 1 , and the plurality of vanelets form the non-periodic pattern around the ...

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13-03-2014 дата публикации

INTEGRATED ENDSHIELD AND PUMP VOLUTE FOR AN ELECTRIC PUMP AND METHOD OF FORMING AN ELECTRIC PUMP

Номер: US20140072464A1
Принадлежит: NIDEC MOTOR CORPORATION

An electric pump comprises a stator, a rotor, and an endshield. The interface plate is fixed to the stator and is configured to couple the electric motor to a pump. The pump volute is formed as an integral portion of the endshield, thereby minimizing the axial length of the electric pump. A drainage passageway is provided on the endshield to harmlessly drain away any fluid that seeps past the pump's seals. In one embodiment of the invention, the drainage passageway is a groove that faces the stator and is configured to facilitate the evaporation of and leak fluid by channeling the fluid near the stator, which warms the fluid and thereby increases the fluid's evaporation rate. 1. An electric pump for use in an appliance , said electric pump comprising:a stator;a rotor including a shaft rotatable about an axis;a pump volute;an impeller at least in part positioned inside the pump volute;an endshield fixed to the stator and defining a shaft opening,said shaft extending through the shaft opening along the axis; anda seal positioned between the endshield and the shaft, an impeller section at least substantially adjacent the impeller, and', 'a motor section at least substantially adjacent the stator,', 'said seal positioned between the impeller section and the motor section,', 'said seal and said endshield configured to cooperatively at least substantially prevent ingress of fluid from the impeller section to the motor section,, 'said shaft including'}said endshield and said volute being monolithically formed,said endshield at least in part defining a drainage passageway in fluid communication with the motor section such that any fluid that leaks to the motor section from the impeller section is received by the drainage passageway.2. The electric pump of claim 1 ,said pump further comprising a bearing that supports the shaft,said endshield supporting the bearing.3. The electric pump of claim 2 ,said bearing directly engaging the motor section of the shaft.4. The electric ...

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20-03-2014 дата публикации

Humidifying apparatus

Номер: US20140077398A1
Принадлежит: Dyson Technology Ltd

Humidifying apparatus includes a base housing an impeller and a motor for driving the impeller to generate a first air flow. A nozzle includes an interior passage for receiving the first air flow and an air outlet for emitting the first air flow. The nozzle defines an opening through which air from outside the apparatus is drawn by air emitted from the air outlet. The apparatus is configured to humidify a second air flow, which is emitted from a plurality of second air outlets. The second air flow is humidified with water supplied from a water tank mounted on the base. The water tank has an upwardly curved upper surface. The nozzle is mounted on the apparatus so that the upper surface of the water tank at least partially covers a lower section of an external surface of the nozzle.

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20-03-2014 дата публикации

REGENERATIVE-TYPE FLUID MACHINERY HAVING A GUIDE VANE ON A CHANNEL WALL

Номер: US20140079543A1

Disclosed is a regenerative fluid machine having guide vanes on a flow channel wall. The regenerative fluid machine includes a circular plate-shaped impeller having a plurality of vanes radially formed on an outer circumference thereof at regular intervals, casings in which the impeller is housed, and flow channels, each of which has a suction hole and a discharge hole in opposite ends thereof, and which are circumferentially disposed within the casings so as to face the vanes. The plurality of guide vanes having an inclined angle (θ) with respect to a radial direction protrude from the flow channel wall in a rotational direction of the impeller so that a relative inflow angle (β) of the fluid introduced into the impeller grooves is increased and thus an absolute inflow angle (α) is decreased. 1. A regenerative fluid machine having guide vanes on a flow channel wall comprising:{'b': 10', '12, 'a circular plate-shaped impeller () that has a plurality of vanes () radially formed on an outer circumference thereof at regular intervals;'}{'b': 20', '10, 'casings () in which the impeller () is housed; and'}{'b': 30', '32', '34', '10, 'flow channels (), each of which has a suction hole () and a discharge hole () in opposite ends thereof, and which are circumferentially formed in the casings so as to face the vanes (),'}{'b': 40', '10', '30', '30', '30', '30', '14', '40', '30, 'i': a,', 'b,', 'c, 'wherein the plurality of guide vanes () having an inclined angle (θ) with respect to a radial direction protrude in a rotational direction of the impeller () throughout an entire wall () of each flow channel () so that a relative inflow angle (β) of a fluid introduced into impeller grooves () is increased, and an absolute inflow angle (α) of the fluid is decreased, and the guide vanes () are formed at a height of 5 to 30% of a depth of the flow channel ().'}240303234. The regenerative fluid machine of claim 1 , wherein the guide vanes () are formed on at least ⅓ of an area of the ...

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07-01-2016 дата публикации

Parallel Twin-Impeller Compressor Having Swirl-Imparting Device For One Impeller

Номер: US20160003046A1
Принадлежит: Honeywell International Inc

An turbocharger includes a parallel twin-impeller compressor and separate inlets into the two impellers. A first or outboard impeller receives one stream of inlet air and a second or inboard impeller receives its own separate stream of inlet air by way of a generally annular inlet volute surrounding the inlet to the second impeller. Air is fed from the inlet volute radially inwardly through a feed passage to the inlet to the second impeller. A plurality of inlet guide vanes are located in the feed passage for the second impeller, the inlet guide vanes creating a swirling air stream into the second impeller. Introduction of swirl to the second impeller alters the flow distribution between the impellers and affects the stability of the overall stage.

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05-01-2017 дата публикации

MULTISTAGE CENTRIFUGAL PUMP WITH INTEGRAL ABRASION-RESISTANT AXIAL THRUST BEARINGS

Номер: US20170002823A1
Принадлежит:

A multistage centrifugal pump includes a housing, a rotatable shaft and first and second turbomachinery stages. The first turbomachinery stage includes a first diffuser connected to the housing, a first impeller connected to the rotatable shaft. The second turbomachinery stage includes a second diffuser connected to the housing and a second impeller connected to the rotatable shaft. The multistage centrifugal pump further includes an integral axial load and bearing system that includes at least one diffuser bushing and at least one impeller bearing. The integral axial load and bearing system permits the independent axial movement of the first and second impellers. The integral axial load and bearing system also provides an opposite force to up-thrust and down-thrust produced by the first and second turbomachinery stages. 1. A multistage centrifugal pump comprising:a rotatable shaft;an upstream impeller connected to the rotatable shaft;a stationary diffuser;a downstream impeller connected to the rotatable shaft; and a diffuser bushing contained within the stationary diffuser;', 'an upstream impeller bearing connected to the rotatable shaft; and', 'a downstream impeller bearing connected to the rotatable shaft., 'an integral axial load and bearing system, wherein the integral axial load and bearing system comprises2. The multistage centrifugal pump of claim 1 , wherein the diffuser bushing comprises a central interior passage and the upstream impeller bearing comprises a central cylinder that extends inside the central interior passage of the diffuser bushing.3. The multistage centrifugal pump of claim 2 , wherein the downstream impeller bearing comprises a central cylinder that extends inside the central interior passage of the diffuser bushing.4. The multistage centrifugal pump of claim 3 , wherein the integral axial load and bearing system further comprises a gap within the interior of the diffuser bushing between the central cylinder of the upstream impeller ...

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05-01-2017 дата публикации

Turbocharger

Номер: US20170002826A1
Автор: Jinhee BYON
Принадлежит: IHI Corp

A turbocharger includes: an annular diffuser flow passage formed by two opposed surfaces of a compressor housing and a bearing housing; and a seal plate located inside of the diffuser flow passage in a radial direction, and disposed to be opposed to a back surface of a compressor wheel. A gap in the radial direction is formed between a radially inside end of the opposed surface of the bearing housing that forms the diffuser flow passage and an outer peripheral edge of the compressor wheel. The seal plate has a larger diameter than that of the compressor wheel. A protrusion, which extends more to the compressor housing side than does a region opposed to a back surface of the compressor wheel, is provided in a region of the seal plate facing the gap.

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05-01-2017 дата публикации

Blower for breathing apparatus

Номер: US20170002830A1
Принадлежит: Fisher and Paykel Healthcare Ltd

A blower for a breathing apparatus has a diffuser for increasing static pressure and/or reducing noise and/or mitigating pressure instabilities and/or managing reverse flow.

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04-01-2018 дата публикации

COMPRESSOR STAGE EGR INJECTION

Номер: US20180003133A1
Принадлежит:

A product may include a bearing housing in which a shaft may be supported by a bearing so that it may rotate. A compressor wheel may be disposed on the shaft. A compressor cover may be connected with the bearing housing, which may form a compressor body and may define a chamber within which the compressor wheel may rotate. A diffuser may extend radially outward from the chamber and may receive gas from the compressor wheel. An inlet may be provided to the compressor body, which may receive a supply of exhaust gas. An EGR distribution cavity may be defined within the compressor body and may extend around the shaft. An EGR inlet channel may extend into the bearing housing from the inlet to the EGR distribution cavity. An EGR passage may extend from the EGR distribution cavity to the diffuser. 1. A product comprising a bearing housing in which a shaft is supported by a bearing to rotate , a compressor wheel disposed on the shaft , a compressor cover connected with the bearing housing creating a compressor body defining a chamber within which the compressor wheel rotates , a diffuser extending radially outward from the chamber and receiving gas from the compressor wheel , an inlet on the compressor body receiving a supply of exhaust gas , an EGR distribution cavity defined completely within the compressor body and extending around the shaft , an EGR inlet channel extending into the bearing housing from the inlet to the EGR distribution cavity , and an EGR passage extending from the EGR distribution cavity to the diffuser.2. The product according to wherein the shaft rotates on an axis and the EGR inlet channel extends in a direction toward the axis.3. The product according to wherein the EGR distribution cavity extends in a circle around the shaft and at any point along the circle has a consistent cross section.4. The product according to wherein the compressor wheel includes a compressor wheel tip at its radially outermost perimeter claim 1 , and wherein the bearing ...

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04-01-2018 дата публикации

COMPRESSOR

Номер: US20180003191A1
Автор: French Pierre Bernard
Принадлежит:

A compressor comprises a compressor housing, a compressor wheel mounted within the housing and having compressor blades, and a bearing housing. The compressor housing comprises a cover member and a diffuser member that is connected to both the cover member and the bearing housing. The diffuser member has a radially outer portion connected to the cover member and a radially inner portion connected to the bearing housing. The diffuser member has a first weakened region defined at a first position intermediate the radially outer portion and the radially inner portion, and a first strengthened region defined at a second position intermediate the radially outer portion and the radially inner portion, said second position being radially inwards or outwards of the first weakened region. 1. A compressor comprising a compressor housing , a compressor wheel mounted within the housing and having compressor blades , and a bearing housing , the compressor housing comprising a cover member and a diffuser member that is connected to both the cover member and the bearing housing , the diffuser member having a radially outer portion connected to the cover member and a radially inner portion connected to the bearing housing , wherein the diffuser member has a first weakened region defined at a first position intermediate the radially outer portion and the radially inner portion and a first strengthened region defined at a second position intermediate the radially outer portion and the radially inner portion , said second position being radially inwards or outwards of the first weakened region.2. A compressor according to claim 1 , wherein the first strengthened region is defined by a section of the diffuser member that has an axial thickness that is greater than an axial thickness of the first weakened region.3. A compressor according to claim 1 , wherein the first strengthened region is defined by a first protrusion that extends generally axially from the diffuser member.4. A ...

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04-01-2018 дата публикации

FURNACE SUBASSEMBLY, FURNACE BLOWER AND ASSOCIATED METHOD

Номер: US20180003382A1
Принадлежит:

A furnace blower assembly includes a blower housing a blower and a motor. The blower is positioned within the housing and is adapted to rotate relative to the housing. The motor is coupled to the blower. The housing defines an outlet having an external periphery and an internal periphery. The external periphery or the internal periphery of the outlet is adapted to be fitted to a portion of the external periphery or the internal periphery of the duct. The outlet defines a longitudinal axis. The outlet has a peripheral edge and a protrusion extending outwardly from the external periphery or the internal periphery of the outlet. The protrusion is spaced from the peripheral edge of the outlet and is adapted to abut the peripheral edge of the duct. 1. A furnace blower assembly for cooperation with a duct having an interior periphery and an exterior periphery thereof and defining a peripheral edge thereof , said furnace blower assembly comprising:a blower housing;a blower positioned at least partially within said housing, said blower being adapted to rotate relative to said housing about a blower axis; anda motor operatively coupled to said blower, said housing defining an outlet thereof, the outlet having an external periphery thereof and an internal periphery thereof, a portion of one of the external periphery and the internal periphery of the outlet adapted to be at least fitted to a portion of one of the external periphery and the internal periphery of the duct, the outlet defining a longitudinal axis thereof, the outlet defining a peripheral edge thereof, the outlet defining a protrusion extending outwardly from one of the external periphery and the internal periphery of the outlet, said protrusion spaced from the peripheral edge of the outlet, said protrusion adapted to abut the peripheral edge of the duct.2. The furnace blower assembly as set forth in :wherein a portion of the internal periphery of the outlet is adapted to be fitted to a portion of the external ...

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02-01-2020 дата публикации

CENTRIFUGAL ROTARY MACHINE

Номер: US20200003226A1
Автор: YAMASHITA Shuichi

A flow path includes a return bend portion which guides a working fluid to an inside in the radial direction by reversing the working fluid discharged to an outside in a radial direction from an upstream-side impeller, and a guiding flow path which is connected to a downstream side of the return bend portion and leads the working fluid to the inside in the radial direction so as to guide the working fluid to the downstream-side impeller. In a return vane which is provided in the guiding flow path, a trailing edge is formed such that a second end portion on a second side in an axial direction is positioned closer to an inside in a radial direction than a first end portion on a first side in the axial direction. 1. A centrifugal rotary machine comprising:impellers which are provided in a plurality of stages along an axial direction and discharge a working fluid sucked from a first side in the axial direction to an outside in a radial direction of an axis; anda casing which is provided to surround the impellers and forms a flow path which leads the working fluid discharged from an upstream-side impeller positioned on the first side in the axial direction to a downstream-side impeller positioned on a second side in the axial direction, a return bend portion which guides the working fluid to an inside in the radial direction by reversing the working fluid discharged to an outside in the radial direction from the upstream-side impeller, and', 'a guiding flow path which is connected to a downstream side of the return bend portion and leads the working fluid to the inside in the radial direction so as to guide the working fluid to the downstream-side impeller,, 'wherein the flow path includes'}wherein the centrifugal rotary machine further comprises a plurality of return vanes which are provided in the guiding flow path guiding the working fluid in at least one impeller from among the impellers provided in the plurality of stages and which are provided at intervals in a ...

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02-01-2020 дата публикации

DOUBLE-SUCTION CENTRIFUGAL FAN

Номер: US20200003227A1
Принадлежит: DAIKIN INDUSTRIES, LTD.

A double-suction centrifugal fan includes: a first impeller coupled to a shaft; a second impeller provided with a second inlet port opened opposite to an electric motor and coupled to the shaft at a position farther from the electric motor than the first impeller; a first bell mouth connected to a first inlet port of the first impeller, and a second bell mouth connected to the second inlet port of the second impeller. An axial length L of the second bell mouth is greater than an axial length L of the first bell mouth. 1. A double-suction centrifugal fan , comprising:an electric motor having a shaft;a first impeller provided with a first inlet port opened toward the electric motor, and coupled to the shaft;a second impeller provided with a second inlet port opened opposite to the electric motor, and coupled to the shaft at a position farther from the electric motor than the first impeller;a first bell mouth provided at the first inlet port of the first impeller; anda second bell mouth provided at the second inlet port of the second impeller, wherein{'b': 2', '1, 'an axial length L of the second bell mouth is greater than an axial length L of the first bell mouth.'}2. The double-suction centrifugal fan of claim 1 , whereineach of the first bell mouth and the second bell mouth has a tubular straight portion extending along an axis thereof, and{'b': 2', '1, 'a length Ls of the straight portion of the second bell mouth is greater than a length Ls of the straight portion of the first bell mouth.'}3. The double-suction centrifugal fan of claim 1 , wherein{'b': 2', '1, 'an inner diameter d of an air inflow port of the second bell mouth is greater than an inner diameter d of an air inflow port of the first bell mouth.'}4. The double-suction centrifugal fan of claim 2 , wherein{'b': 2', '1, 'an inner diameter d of an air inflow port of the second bell mouth is greater than an inner diameter d of an air inflow port of the first bell mouth.'} The present invention relates to a ...

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02-01-2020 дата публикации

VARIABLE STAGE COMPRESSORS

Номер: US20200003455A1
Автор: Li Tianlei, SUN Lin, Sun Zili
Принадлежит:

A centrifugal compressor includes a first stage and a second stage. At least one of the first stage and the second stage includes an impeller and a shroud spaced from the impeller and configured to guide a fluid flow through the impeller. The shroud is selectively moveable between an engaged position and a disengaged position. 1. A centrifugal compressor , comprising:a first stage; anda second stage, wherein at least one of the first stage and the second stage includes an impeller and a shroud spaced from the impeller and configured to guide a fluid flow through the impeller, wherein the shroud is selectively moveable between an engaged position and a disengaged position.2. The centrifugal compressor as recited in claim 1 , wherein the impeller is rotatbable about an axis claim 1 , and the shroud is selectively moveable in the axial direction relative to the axis between the engaged position and the disengaged position.3. The centrifugal compressor as recited in claim 1 , wherein the impeller is rotatbable about an axis claim 1 , and the shroud is selectively moveable in the radial direction relative to the axis between the engaged position and the disengaged position.4. The centrifugal compressor as recited in claim 1 , comprising:a control system configured to move the shroud between the engaged position and the disengaged position.5. The centrifugal compressor as recited in claim 1 , wherein the outer surface of the shroud forms a convex surface.6. A method of compressing a refrigerant in a centrifugal compressor claim 1 , the method comprising:determining an efficiency of a first stage of a compressor and an efficiency of a second stage of a compressor; anddisengaging one of the first stage and the second stage based on the determining by moving a shroud away from an impeller.7. The method as recited in claim 6 , wherein the centrifugal compressor is a multi-stage centrifugal compressor.8. The method as recited in claim 6 , wherein the impeller is rotatable ...

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07-01-2021 дата публикации

MULTI-STAGE CENTRIFUGAL COMPRESSOR

Номер: US20210003145A1
Принадлежит:

A multi-stage centrifugal compressor according to at least one embodiment includes: multiple stages of impellers arranged in an axial direction; a casing surrounding the impellers; and a diffuser channel for guiding a working fluid discharged from the impellers outward in a radial direction. In a cross-section along the axial direction, a first diffuser wall surface on a hub side of a pair of diffuser wall surfaces that are opposed in the axial direction across the diffuser channel has a retreating surface retreating toward the hub side from a connection position with a downstream end of a first upstream wall surface to a radially outer side with respect to a tangential direction of the first upstream wall surface at the downstream end of the first upstream wall surface, the first upstream wall surface being positioned upstream of the first diffuser wall surface and connected to the first diffuser wall surface. 1. A multi-stage centrifugal compressor comprising:multiple stages of impellers arranged in an axial direction;a casing surrounding the impellers; anda diffuser channel for guiding a working fluid discharged from the impellers outward in a radial direction,wherein, in a cross-section along the axial direction, a first diffuser wall surface on a hub side of a pair of diffuser wall surfaces that are opposed in the axial direction across the diffuser channel has a retreating surface retreating toward the hub side from a connection position with a downstream end of a first upstream wall surface to a radially outer side with respect to a tangential direction of the first upstream wall surface at the downstream end of the first upstream wall surface, the first upstream wall surface being positioned upstream of the first diffuser wall surface and connected to the first diffuser wall surface.2. The multi-stage centrifugal compressor according to claim 1 ,wherein the first diffuser wall surface has a first outer wall surface positioned on the radially outer side of ...

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07-01-2021 дата публикации

Load-bearing Members for Aircraft Lift and Thrust

Номер: US20210003146A1
Автор: Stephens Thomas G.
Принадлежит: AvionOne Innovations, LLC

An aircraft includes an airframe, ducted fans, and ducts for carrying pressurized air for lift and thrust supplied by the fans. The ducts form part of the airframe and carry static and dynamic loads applied to the airframe. Ducting members supply lift and thrust and transmit them to other airframe components. The ducts also carry the ducted air to exits set distant from the fans to permit flight control of the aircraft. Ducting members also form airfoils creating lift for the aircraft. 1. An aircraft , in an environment in which lift and thrust are supplied thereby and the aircraft experiences static and dynamic loading in flight , comprising:at least one source of pressurized gas;an airframe supporting static and dynamic loading experienced by the aircraft; said ducting connected to the at least one source and forming a flowpath for the pressurized gas;', 'said ducting supporting airframe loading;, 'the airframe comprising ducting;'}said airframe comprising one or more airfoils capable of providing lift to the aircraft; andsaid ducting forming substantially all of said one or more airfoils.2. The aircraft of claim 1 , further comprising:said ducting having a cross section forming an airfoil shape.3. The aircraft of claim 1 , further comprising:said ducting supporting substantially all of the airframe loading in flight.4. The aircraft of claim 1 , further comprising:said airframe comprising a fuselage; andsaid fuselage having an exterior surface; andsaid ducting extending outwardly from said exterior surface.5. The aircraft of claim 1 , further comprising:said at least one source of pressurized gas comprising at least two electric ducted fans; and 'each of said ducts connected to one each of said fans.', 'said ducting comprising at least two ducts;'}said ducting comprising at least one exit each therefrom.6. The aircraft of claim 1 , further comprising: 'said tips being on opposing sides of said divergence;', 'said ducting comprising at least two tips and at least ...

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20-01-2022 дата публикации

CENTRIFUGAL COMPRESSOR AND TURBOCHARGER

Номер: US20220018360A1
Принадлежит: IHI CORPORATION

A centrifugal compressor includes: an impeller including a main body portion and a plurality of blades provided on an outer peripheral surface of the main body portion; an intake flow path facing the impeller in a rotational axis direction; and a throttling mechanism including a throttling member provided in the intake flow path, a ratio obtained by dividing a distance between an outer peripheral end of a leading edge of the blade and the throttling member by a maximum protruding height of the throttling member protruding from an inner wall surface of the intake flow path is equal to or less than 4. 1. A centrifugal compressor comprising:an impeller including a main body portion and a plurality of blades provided on an outer peripheral surface of the main body portion;an intake flow path facing the impeller in a rotational axis direction; anda throttling mechanism including a throttling member provided in the intake flow path, a ratio obtained by dividing a distance between an outer peripheral end of a leading edge of the blade and the throttling member by a maximum protruding height of the throttling member protruding from an inner wall surface of the intake flow path is equal to or less than 4.2. The centrifugal compressor according to claim 1 ,wherein the throttling member includes an opposing surface facing the outer peripheral end in an axial direction of the impeller, andthe opposing surface is located between a position of the outer peripheral end and a position of an inner peripheral end of the leading edge in the axial direction.3. A turbocharger comprising the centrifugal compressor according to .4. A turbocharger comprising the centrifugal compressor according to . This application is a continuation application of International Application No. PCT/JP2020/013848, filed on Mar. 26, 2020, which claims priority to Japanese Patent Application No. 2019-086357 filed on Apr. 26, 2019, the entire contents of which are incorporated by reference herein.The present ...

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20-01-2022 дата публикации

DIFFUSION SYSTEM CONFIGURED FOR USE WITH CENTRIFUGAL COMPRESSOR

Номер: US20220018361A1
Автор: Mazur Steven
Принадлежит:

A compressor includes an impeller and a diffuser. The impeller is mounted for rotation about an axis of the gas turbine engine. The diffuser is coupled to the impeller to receive the high velocity air from the impeller. The diffuser includes a first plate, a second plate spaced apart from the first plate axially, and a plurality of vanes located between the first and second plates. 1. A diffuser adapted for use with a centrifugal compressor , the diffuser comprisinga first plate that extends circumferentially about an axis,a second plate that extends circumferentially about the axis, the second plate spaced apart axially from the first plate relative to the axis to define a flow path between the first plate and the second plate, anda plurality of vanes that extend axially between and interconnect the first plate and the second plate, the plurality of vanes including a first vane and a second vane spaced apart circumferentially from the first vane to define a throat inlet of the diffuser located at a radial throat distance from the axis, the first vane and the second vane each including a leading edge and a trailing edge spaced apart radially from the leading edge to define a camber line that extends within the respective first and second vane and interconnects the leading edge and the trailing edge of the respective first and second vane,wherein the plurality of vanes are backswept such that the camber line of each of the first vane and the second vane is curved and at least one of the first plate and the second plate diverges axially relative to the other of the first plate and the second plate beginning at a location equal to the radial throat distance or radially outward of the radial throat distance.2. The diffuser of claim 1 , wherein both the first plate and the second plate diverge axially away from the other of the first plate and the second plate as the first plate and the second plate extend radially outward relative to the axis.3. The diffuser of claim 2 ...

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14-01-2021 дата публикации

Continuous positive airway pressure (cpap) device

Номер: US20210008310A1
Принадлежит: Murata Manufacturing Co Ltd

A CPAP device includes a housing. A suction port is provided in a top plate portion of a casing of the air blower. The air blower chamber has a facing wall portion facing the top plate portion with a distance therebetween. A wall portion defining the air blower chamber is provided with an introduction port for introducing external air. In a space between the facing wall portion and the top plate portion, a flow adjustment portion that partitions the space into flow paths arranged side by side around a rotation axis is provided. An outer end portion and an inner end portion of each of the flow paths in a direction orthogonal to the rotation axis are respectively constituted of a first open end and a second open end, the first open end and the second open end being open along the direction orthogonal to the rotation axis.

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12-01-2017 дата публикации

FLUID PUMP

Номер: US20170009777A1
Автор: Krug Karl Alexander
Принадлежит: MP Pumps

The present invention relates to a fluid pump having an improved performance. The pump comprises an impeller, volute housing, inner housing geometry, and an adapter. The impeller is configured to generate fluid flow velocity. The volute housing is configured to improve fluid pump performance while reducing power consumption, the volute housing comprises the inner housing geometry. The inner housing geometry is configured to convert the fluid flow velocity that has been generated into pressure. The adapter is designed to protect the unconnected end of the drive shaft and reduce the negative effects of shaft deflection. The adapter also has a structural rib geometry which is configured to provide superior structural integrity at a minimal mass. 1. A fluid pump having an improved performance , said pump comprising: i. a hub profile;', 'ii. an outer diameter;', 'iii. an impeller eye centrally located on said impeller and configured to connect to one end of a drive shaft;', 'iv. a plurality of impeller blades connected to said hub profile and forming a plurality of flow channel areas interposed between two said impeller blades of said plurality of impeller blades; and', 'v. wherein each said flow channel area of said plurality of flow channel areas gradually diverges from said impeller eye to said outer diameter;, 'a. an impeller configured to generate fluid flow velocity, said impeller comprisingb. a volute housing configured to improve fluid pump performance while reducing power consumption, said volute housing having a fluid intake, a fluid discharge, and an inner housing geometry; i. a volute area having a secondary passage and circulation zone;', 'ii. said secondary passage interposed between said volute area and a collection zone, said secondary passage configured to allow volute area fluid reentry during priming and non-reentry after full prime is established;', 'iii. a diffuser located at the periphery of said volute area and configured to alleviate wasted energy ...

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12-01-2017 дата публикации

Humidifying apparatus

Номер: US20170010010A1
Принадлежит: Dyson Technology Ltd

A humidifying apparatus comprising a base comprising a chamber, a water tank removably mounted on the base for supplying water to the chamber, an impeller and a motor for driving the impeller to generate an air flow, an inlet duct for conveying the air flow to the chamber, humidifying means for humidifying the air flow with water from the chamber, and an outlet duct for conveying the humidified air flow from the chamber, wherein a lower surface of the water tank, which in use supports the water tank on the base, comprises a recessed portion for receiving water overflow from the chamber.

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14-01-2016 дата публикации

SHAFTLESS FAN STRUCTURE

Номер: US20160010653A1
Принадлежит:

A shaftless fan includes a fan stator, a vane rotor and a rolling bearing. The rolling bearing is installed between the fan stator and the vane rotor and includes an inner ring, an outer ring, and a plurality of rolling elements rollably installed between the inner and outer rings, and the inner and outer rings of the rolling bearing are rotated in opposite direction with respect to each other, so that the vane rotor can be rotated on the fan stator to connect the fan stator with the vane rotor through the rolling bearing, so as to achieve the shaftless effect. 1. A shaftless fan structure , comprising:a fan stator;a vane rotor; anda rolling bearing, installed between the fan stator and the vane rotor, and including an inner ring, an outer ring, and a plurality of rolling elements rollably installed between the inner and outer rings; wherein the inner and outer rings are rotated in opposite directions with respect to each other, so that the vane rotor can be rotated on the fan stator.2. The shaftless fan structure of claim 1 , wherein the vane rotor includes an impeller claim 1 , a plurality of blades disposed outside the impeller claim 1 , and a magnetic element installed in the impeller claim 1 , and the impeller has a circular wall claim 1 , and each blade is arranged around the periphery of the impeller and mounted onto the circular wall.3. The shaftless fan structure of claim 2 , further comprising a hood for mounting the fan stator thereon claim 2 , and a bearing collar mounted onto the hood and fixed onto the inner ring of the rolling bearing claim 2 , and the outer ring of the rolling bearing being fixed into the circular wall of the vane rotor.4. The shaftless fan structure of claim 3 , wherein the impeller is covered onto the exterior of the fan stator and provided for the fan stator to be accommodated in a space enclosed by the impeller and the circular wall of the impeller.5. The shaftless fan structure of claim 3 , wherein the rolling bearing is a ball ...

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14-01-2016 дата публикации

VACUUM GENERATOR FLOW DIVERTER

Номер: US20160010659A1
Принадлежит:

Embodiments provide systems and methods for providing improved air flow for vacuum generator systems. The systems may include a housing with an impeller and a diverter having an airflow flange comprising an arrow-like projection configured to extend into an airflow space of the housing. The diverter may have curved surfaces that help guide airflow movement within the housing. 1. A diverter for being positioned in a housing of a vacuum generator system , comprising:a securement flange;first and second upper walls; andan airflow flange configured to extend into an airflow space of the housing.2. The system of claim 1 , wherein the securement flange comprises one or more openings.3. The system of claim 1 , wherein the housing comprises an inside housing portion and an outside housing portion claim 1 , wherein the securement flange is sandwiched between the inside housing portion and the outside housing portion.4. The system of claim 1 , wherein the airflow flange comprises an arrow-like projection.5. The system of claim 1 , further comprising a first curved wall extending between the first upper wall and the airflow flange and a second curved wall extending between the second upper wall and the airflow flange.6. A vacuum generator system claim 1 , comprising:a housing comprising first and second portions, the first and second portions each comprising inner curved surfaces;an impeller;a diverter comprising a flange configured to be received between the first and second portions, first and second upper walls configured to abut the housing, an airflow flange comprising an arrow-like projection configured to extend into an airflow space of the housing, a first curved surface extending between the first upper wall and the airflow flange, and a second curved surface extending between the second upper wall and the airflow flange, wherein in use, airflow created up by impeller movement is diverted along the first and second curved walls of the diverter and the inner curved ...

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11-01-2018 дата публикации

CONTROL METHOD FOR INLET SWIRL DEVICE

Номер: US20180010514A1
Автор: HANIG Urs, SHUTTY John
Принадлежит: BORGWARNER INC.

A number of variations may include a method comprising selectively actuating an inlet swirl device to cause a compressor to windmill at a higher speed during an operation mode where fuel consumption of an engine in the vehicle is at a minimal or before an acceleration event. 1. A method comprising:selectively actuating an inlet swirl device to cause a compressor to windmill at a higher speed during an operation mode where fuel consumption of an engine in the vehicle is at a minimal or before an acceleration event.2. The method of wherein the operation mode is at least one of a braking mode claim 1 , a deceleration mode claim 1 , or a coasting mode.3. The method of wherein the operation mode is a gear shift.4. A control method for an inlet swirl device in an engine in a vehicle comprising:determining whether the vehicle is operating in at least one of a first mode, a second mode, or a third mode;actuating a plurality of vanes in the inlet swirl device to move to at least one first angle based on at least one engine control operation in the first mode;actuating the plurality of vanes in the inlet swirl device to move to at least one second angle to induce a high level of swirl of a fluid flow exiting the inlet swirl device in the second mode; andactuating the plurality of vanes in the inlet swirl device to move to at least one third angle to induce the high level of swirl of the fluid flow exiting the inlet swirl device in the third mode.5. The control method of wherein in the first mode claim 4 , fuel consumption by the engine is high claim 4 , and wherein in the second mode fuel consumption by the engine is at a minimum.6. The control method of wherein in the third mode claim 4 , an acceleration event of the vehicle is anticipated.7. The control method of wherein the at least one first angle achieves maximum efficiency of the engine and the at least one second angle and the at least one third angle cause a compressor in the engine to windmill at a high speed.8. The ...

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11-01-2018 дата публикации

CENTRIFUGAL COMPRESSOR BUNDLE AND CENTRIFUGAL COMPRESSOR

Номер: US20180010615A1
Автор: Yamada Hideki

A centrifugal compressor bundle that is provided with a bundle main body in which is formed an annular intake flow channel (FC) that is centered on an axis line (O) and that leads a process gas (G) into a flow channel (FC) of an impeller, and in which is also formed an annular discharge flow channel (FC) that is centered on the axis line (O) and that discharges the process gas (G) from the flow channel (FC) of the impeller. The bundle main body has a plurality of diaphragms that are aligned in the direction of the axis line (O) and that are bonded to each other. From among the plurality of diaphragms, an intake diaphragm in which the intake flow channel (FC) is formed is partitioned so as to have an upper-half part and a lower-half part that sandwich, from above and below, a horizontal plane that includes the axis line (O). The upper-half part and the lower-half part have the same rigidity in the direction of the axis line (O). 1. A centrifugal compressor bundle , comprising:a bundle main body which includes a rotary shaft, an intake flow channel which rotatably supports an impeller which is fixed to the rotary shaft and rotates along with the rotary shaft about an axis line of the rotary shaft, introduces a fluid in a flow channel of the impeller, and is annularly formed about the axis line, and a discharge flow channel which discharges the fluid from a flow channel of the impeller and is annularly formed about the axis line,wherein the bundle main body includes a plurality of diaphragms which are aligned in the direction of the axis line and are connected to each other,wherein among the plurality of diaphragms, an intake diaphragm in which the intake flow channel is formed includes an upper-half portion positioned on an upper side and a lower-half portion positioned on a lower side configured by dividing the intake diaphragm into two portions such as the upper side and the lower side in a state where a horizontal plane including the axis line is interposed ...

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14-01-2021 дата публикации

FAN MOTOR AND MANUFACTURING METHOD THEREOF

Номер: US20210010486A1
Принадлежит:

Disclosed is a fan motor. The present disclosure provides a fan motor including a motor housing receiving a motor therein, a motor bracket disposed on the motor housing, an impeller coupled to a shaft of the motor, and a diffuser disposed between the motor and the impeller and having a vane body, an axial flow vane provided to an inner circumference of the vane body, and a diagonal flow vane provided above the axial flow vane. 1. A fan motor , comprising:a motor housing;a motor disposed within the motor housing;a motor bracket disposed on the motor housing;an impeller coupled to a shaft of the motor; and a vane body,', 'an axial flow vane disposed at an inner circumference of the vane body, and', 'a diagonal flow vane disposed vertically above the axial flow vane., 'a diffuser disposed between the motor and the impeller, the diffuser comprising2. The fan motor of claim 1 , wherein the vane body comprises a hollow ring claim 1 , and the axial flow vane is disposed at an inner surface of the hollow ring.3. The fan motor of claim 2 , wherein the vane body claim 2 , the axial flow vane claim 2 , and the diagonal flow vane are integrally provided.4. The fan motor of claim 3 , wherein the vane body claim 3 , the axial flow vane claim 3 , and the diagonal flow vane are made by injection molding.5. The fan motor of claim 4 , wherein the diffuser further comprises a hub that is disposed within the vane body claim 4 , andwherein an outer circumference of the hub corresponds to a shape of the diagonal flow vane.6. The fan motor of claim 5 , wherein the vane body defines an indentation claim 5 , and the motor bracket comprises a fitted part inserted into the indentation.7. The fan motor of claim 6 , wherein the indentation comprises at least one of a first indentation that extends along a circumferential direction of the vane body or a second indentation that extends along an axial direction of the vane body claim 6 , andwherein the fitted part comprises at least one of a first ...

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10-01-2019 дата публикации

CENTRIFUGAL COMPRESSOR

Номер: US20190010958A1
Принадлежит: IHI CORPORATION

A centrifugal compressor is equipped with a housing including a suction passage which accommodates an impeller. The suction passage is provided with a first opening portion formed at a position facing the impeller, a second opening portion formed on an upstream side of the first opening portion, a circulation flow path which allows the first opening portion and the second opening portion to communicate with each other and extends in an annular shape around a rotational axis of the impeller, and a plurality of guide vanes disposed in the circulation flow path. The circulation flow path includes a first region in which a plurality of guide vanes is disposed at intervals in a circumferential direction, and a second region in which no guide vane is disposed. The second region extends over a wider range in the circumferential direction than the interval between the guide vanes in the first region. 18-. (canceled)9. A centrifugal compressor comprising a housing including an suction passage which accommodates an impeller ,wherein the suction passage is provided with a first opening portion formed at a position facing the impeller, a second opening portion formed on an upstream side of the first opening portion, a circulation flow path which allows the first opening portion and the second opening portion to communicate with each other and extends in an annular shape around a rotational axis of the impeller, and a plurality of guide vanes disposed in the circulation flow path,the circulation flow path includes a first region in which a plurality of guide vanes is disposed at intervals in a circumferential direction, and a second region in which no guide vane is disposed, and the second region extends over a wider range in the circumferential direction than the interval between the guide vanes in the first region.10. The centrifugal compressor according to claim 9 , wherein the housing comprises an annular scroll flow path formed on an outer circumference of the impeller ...

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10-01-2019 дата публикации

Blower Noise Suppressor

Номер: US20190010959A1
Принадлежит:

A blower assembly including a housing, a blower within the housing, and a cut-off that is within the housing downstream of the blower with respect to direction of airflow generated by the blower. Openings are defined by the cut-off. The openings are configured to permit airflow generated by the blower to pass through the openings and to a discharge outlet of the blower assembly. The openings are further configured to reduce blower frequency tone generated as airflow passes across the cut-off. 1. A blower assembly comprising:a housing;a blower within the housing;a cut-off within the housing downstream of the blower with respect to direction of airflow generated by the blower; andopenings defined by the cut-off, the openings configured to permit airflow generated by the blower to pass through the openings and to a discharge outlet of the blower assembly, the openings further configured to reduce blower frequency tone generated as airflow passes across the cut-off.2. The blower assembly of claim 1 , wherein the openings include a plurality of perforations defined by an upstream surface and a downstream surface of the cut-off.3. The blower assembly of claim 1 , wherein the openings include a first slot defined by an upstream surface of the cut-off claim 1 , and a second slot defined by a downstream surface of the cut-off.4. The blower assembly of claim 1 , wherein:the cut-off includes a first chamber having a first upper edge and a second chamber having a second upper edge, the second chamber is smaller than the first chamber and the second upper edge is lower than the first upper edge; andthe openings include a first upstream slot defined by a first upstream surface of the first chamber, a first downstream slot defined by a first downstream surface of the first chamber, a second upstream slot defined by a second upstream surface of the second chamber, and a second downstream slot defined by a second downstream surface of the second chamber.5. The blower assembly of ...

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09-01-2020 дата публикации

RETURN STAGE OF A MULTI-STAGED COMPRESSOR OR EXPANDER WITH TWISTED GUIDE VANES

Номер: US20200011345A1
Автор: Hermes Viktor
Принадлежит: SIEMENS AKTIENGESELLSCHAFT

A return stage through which a process fluid is designed to flow along a throughflow direction of a radial turbomachine, wherein the return stage extends in annular fashion about an axis and is defined radially inwardly by an inner delimiting contour and radially outwardly by an outer delimiting contour. At least one guide vane stage including guide vanes extends at least along a part of the third section and segments the return stage in the circumferential direction into flow channels, wherein in each case a profile midline of a profile cross section defines an inner track on the side of the inner delimiting contour and an outer track on the side of the outer delimiting contour. A radial turbomachine includes at least one such return stage. 1. A return stage (RTC) for throughflow by means of a process fluid along a throughflow direction of a radial turbomachine (RTM) ,wherein the return stage (RTC) extends about an axis (X) in a ring-shaped manner,wherein the return stage (RTC) is defined radially inwardly by an inner delimiting contour (IDC) and radially outwardly by an outer delimiting contour (ODC),{'b': 1', '1, 'wherein the return stage (RTC) extends radially outwardly in a first section (SG) along a first throughflow direction (FD),'}{'b': 1', '2, 'wherein the return stage (RTC) extends, in a manner describing an arcuate deflection, radially inwardly from radially outside along the first throughflow direction (FD) in a second section (SG),'}{'b': 1', '3, 'wherein the return stage (RTC) extends radially inwardly from radially outside along the first throughflow direction (FD) in a third section (SG),'}{'b': 1', '4, 'wherein the return stage (RTC) extends, in a manner describing an arcuate deflection, axially from radially inside along the first throughflow direction (FD) in a fourth section (SG),'}{'b': '3', 'wherein at least one guide vane stage (VST) comprising guide vanes (VNS) extends at least along a part of the third section (SG) and, in the ...

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03-02-2022 дата публикации

RADIAL VENTILATOR

Номер: US20220034328A1
Принадлежит:

A radial ventilator () has a base part (), a housing part (), with a discharge , placed on the base part (), a motor electronics unit (), and an internal rotor electric motor. The motor drives a ventilator wheel () via a shaft (). The motor electronics unit () and a stator () of the electric motor are encapsulated by an extrusion coating () in the base part () and together form an integral one-piece structural unit. The radial ventilator () has a pressure chamber (D) enlarging in a spiral shape around the ventilator wheel (). The pressure chamber (D) is formed and defined by the housing part () and the extrusion coating (). 116.-. (canceled)17. A radial ventilator comprising: a base part , a housing part placed on the base part , a motor electronics unit , and an internal rotor electric motor;a ventilator wheel drive via a shaft of the electric motor;the motor electronics unit and a stator of the electric motor are encapsulated by an extrusion coating in the base part and together form an integral one-piece structural unit; the radial ventilator has a pressure chamber expanding in a spiral shape around the ventilator wheel, the pressure chamber is formed and defined by the housing part and the extrusion coating.18. The radial ventilator as claimed in claim 17 , wherein the extrusion coating comprises a protruding ring section extending in the axial direction claim 17 , the axial end face of the ring section defines the pressure chamber and the ring section defines a receptacle chamber for the motor electronics unit.19. The radial ventilator as claimed in claim 17 , wherein the spiral-shaped pressure chamber is formed by an axial and radial expansion.20. The radial ventilator as claimed in claim 17 , wherein the housing part has a constant diameter delimiting the pressure chamber and a spiral shape of the pressure chamber is exclusively defined by the extrusion coating.21. The radial ventilator as claimed in claim 17 , wherein the electric motor is arranged on a ...

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03-02-2022 дата публикации

Piping assembly and refrigeration system

Номер: US20220034338A1
Принадлежит: Carrier Corp

A piping assembly and a refrigeration system. The piping assembly includes: an inlet portion extending along an inlet axis; an outlet portion extending along an outlet axis, wherein a predetermined angle is formed between the inlet axis and the outlet axis; a transition portion being attached between the inlet portion and the outlet portion and defining a transition axis; a cavity extending from the inlet portion to the outlet portion through the transition portion; and a first straightening portion including a plurality of deflector plates attached to an inner wall of the cavity, wherein the first straightening portion includes at least a first deflector plate and a second deflector plate connected at an angle, and the first deflector plate and the second deflector plate are configured to extend in parallel with a part of the outlet axis and a part of the transition axis.

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19-01-2017 дата публикации

Flow Control Structures For Turbomachines and Methods of Designing The Same

Номер: US20170016457A1
Автор: Japikse David
Принадлежит:

Flow control devices and structures designed and configured to improve the performance of a turbomachine. Exemplary flow control devices may include various flow guiding channels, ribs, diffuser passage-width reductions, and other treatments and may be located on one or both of a shroud and hub side of a machine to redirect, guide, or otherwise influence portions of a turbomachine flow field to thereby improve the performance of the machine. 1. A radial turbomachine , comprising:an impeller including a hub and a plurality of blades and having an exit, each of the plurality of blades having a trailing edge proximate the exit and extending in a spanwise direction between the hub and a shroud side of the blade; anda diffuser having an inlet, a shroud side aligned with the shroud side of the blades, and a hub side aligned with the hub, the shroud side and the hub side of the diffuser defining a diffuser passageway having a width;wherein the impeller is designed and configured to generate a flow field at the diffuser inlet having a greater meridional velocity along one of the hub side and the shroud side of the diffuser than along the other one of the hub and shroud sides, the one of the hub and shroud sides of the diffuser having the greater meridional velocity being the strong side and the other one being the weak side;wherein the diffuser includes at least one strong-side pinch region providing a decrease in the diffuser passageway width that includes a convex surface on the strong side of the diffuser passageway, the convex surface providing a passage width reduction that is greater than any passage width reduction on the weak side of the diffuser.2. A radial turbomachine according to claim 1 , wherein the hub includes a hub surface and an exit portion claim 1 , the hub surface including an inward curvature in the spanwise direction in the exit portion.3. A radial turbomachine according to claim 1 , wherein the convex surface begins adjacent the impeller exit.4. A ...

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19-01-2017 дата публикации

HYDRODYNAMIC MACHINE AND DYNAMIC PRESSURE PUMP THEREFOR

Номер: US20170016493A1
Принадлежит: VOITH PATENT GMBH

A hydrodynamic machine contains a bladed primary wheel driven by a rotary shaft and a bladed secondary wheel, which together form a work chamber filled with a working medium. The machine has a pressure pump for delivering a working medium from the work chamber. The pressure pump has a first inlet, which projects into the work chamber, and has a first inlet opening which is aligned with the rotary shaft in the circumferential direction. The pressure pump has a second inlet which projects into the work chamber and has a second inlet opening which is aligned to the rotary shaft in the circumferential direction opposite to the first inlet opening. The first and second inlets are joined to a common working medium channel behind the two inlet openings. The first and second inlets extend adjacent to each other in the same flow direction separated by a separation wall. 116-. (canceled)17. A hydrodynamic machine , comprising:a bladed primary wheel driven around an axis of rotation;a bladed secondary wheel which together with said bladed primary wheel form a work chamber to be filled with a working medium;a secondary chamber fluidically connected to said work chamber;a dynamic pressure pump for at least indirectly discharging the working medium from said work chamber or from the hydrodynamic machine, said dynamic pressure pump having a dividing wall, a first working medium inlet projecting into said work chamber or said secondary chamber, and a first inlet opening aligned in a circumferential direction with respect to the axis of rotation, said dynamic pressure pump further having a second working medium inlet projecting into said work chamber or into said secondary chamber connected to said work chamber in a manner which allows transmission of the working medium, and a second inlet opening aligned oppositely to said first inlet opening in the circumferential direction with respect to the axis of rotation;said first working medium inlet and said second working medium inlet ...

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21-01-2016 дата публикации

CENTRIFUGAL COMPRESSOR

Номер: US20160017791A1
Автор: NAKAO Hidefumi
Принадлежит:

A centrifugal compressor having a casing that houses an impeller allowing rotation about a rotational axis C, a gas channel, a treatment hollow part provided inside the casing, a first channel open to the gas channel on the downstream side of the blade leading edge of the impeller, a second channel open to the gas channel at the upstream side of the blade leading edge, a guide vane that imparts a swirl component in an opposite rotational direction of the impeller to gas discharged from the second channel, a constricting part that constricts the gas channel, and a rectifying part that rectifies gas in a direction that minimizes the swirl component about the rotational axis C and also increases the component in the direction of the rotational axis C.

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21-01-2016 дата публикации

CENTRIFUGAL FLUID MACHINE

Номер: US20160017888A1
Принадлежит:

A centrifugal fluid machine includes a rotor, a low pressure compression unit provided on one side in the axial direction of the rotor, a high pressure compression unit provided on the other side in the axial direction of the rotor, a partition wall that separates the low and high pressure compression units, and a high pressure-side discharge passage formed on the side of the high pressure compression unit of the partition wall extending in the radial direction of the rotor, and provided along the partition wall wherein the partition wall has a wall body a passage deformation suppression member that is provided between the wall body and the high pressure-side discharge passage and can deform the high pressure-side discharge passage and an biasing mechanism that is provided between the wall body and the passage deformation suppression member

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18-01-2018 дата публикации

SIDE-CHANNEL BLOWER FOR AN INTERNAL COMBUSTION ENGINE

Номер: US20180017069A1
Принадлежит: PIERBURG GMBH

A side-channel blower for an internal combustion engine includes a flow housing, an impeller which rotates in the flow housing, a housing wall which surrounds the impeller, a drive unit which drives the impeller, impeller blades arranged in a radially outer region of the impeller, a radial gap arranged between the impeller and the housing wall, an inlet, an outlet, two flow channels which connect the inlet to the outlet, and an interruption zone arranged between the outlet and the inlet which interrupts the two flow channels in a peripheral direction. The impeller blades open in a radially outward direction. A respective one of the two flow channels is respectively formed axially opposite to the impeller blades in the flow housing. The impeller blades each comprise a V-shaped cross-section. 17-. (canceled)8. A side-channel blower for an internal combustion engine , the side-channel blower comprising:a flow housing;an impeller comprising a rotary axis and being configured to rotate in the flow housing;a housing wall configured to radially surround the impeller;a drive unit configured to drive the impeller;impeller blades arranged in a radially outer region of the impeller, the impeller blades being configured to open in a radially outward direction;a radial gap arranged between the impeller and the housing wall;an inlet;an outlet;two flow channels configured to connect the inlet to the outlet and to be fluidically connected to one another via intermediate spaces between the impeller blades, a respective one of the two flow channels being respectively formed axially opposite to the impeller blades in the flow housing; andan interruption zone arranged between the outlet and the inlet, the interruption zone being configured to interrupt the two flow channels in a peripheral direction,wherein,the impeller blades, as seen from a cross section of a plane on which the rotary axis lies, each comprise a V-shaped cross-section so that, in a direction of rotation of the ...

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18-01-2018 дата публикации

Centrifugal compressor casing and centrifugal compressor

Номер: US20180017073A1
Автор: Hideki Yamada

A centrifugal compressor casing, comprising a bundle which rotatably supports a rotating shaft, and an impeller fixed to the rotating shaft and that rotates with the rotating shaft about an axis of the rotating shaft, and in which an annular suction flow channel centered on the axis introduces fluid into the flow channel of the impeller, and an annular discharge flow channel centered on the axis that discharges the fluid from the flow channel of the impeller, are formed; a casing main body which covers the bundle from the outer circumferential side; and a volute piece which is provided on an inner surface of the casing main body in the discharge flow channel.

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18-01-2018 дата публикации

STATIC HUB TRANSITION DUCT

Номер: US20180017078A1
Принадлежит:

An engine includes a compressor having a first compressor, a second compressor, and a static hub transition duct. The first compressor includes a rotatable portion and a static portion. The second compressor is disposed downstream of the first compressor and includes an inlet and a rotatable portion. The static hub transition duct includes an inner wall and an outer wall. The inner wall is secured to the static portion of the first compressor, and the inner wall and outer wall define a space that fluidically couples the first compressor and the inlet of the second compressor. 1. A compressor of an engine , wherein the engine includes a shaft , comprising:a first compressor, wherein the first compressor includes a first rotatable portion and a static portion, wherein the first rotatable portion is mechanically secured to the shaft;a second compressor downstream of the first compressor, wherein the second compressor includes a second rotatable portion, wherein the second rotatable portion is mechanically secured to the shaft; anda transition duct having an inner wall and an outer wall, wherein the inner wall is secured to the static portion of the first compressor, and the inner wall and outer wall define a space that fluidically couples an exit of the first compressor and an inlet of the second compressor.2. The compressor of claim 1 , wherein the first compressor is an axial compressor and the second compressor is a centrifugal compressor.3. The compressor of claim 1 , wherein the inner wall of the transition duct is secured to a final stator of the axial compressor.4. The compressor of claim 3 , wherein the outer wall of the transition duct is secured to the final stator of the axial compressor.5. The compressor of claim 4 , wherein a casing surrounds the axial compressor.6. The compressor of claim 5 , wherein an extension portion of the casing forms at least a portion of the outer wall of the static transition duct.7. The compressor of claim 3 , further including ...

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18-01-2018 дата публикации

Side-channel blower for an internal combustion engine, comprising a wide interrupting gap

Номер: US20180017084A1
Принадлежит: PIERBURG GMBH

A side-channel blower for an internal combustion engine includes a flow housing, an impeller which rotates in the flow housing, a drive unit which drives the impeller, a housing wall with a radially delimiting housing wall, impeller blades arranged in a radially outer region of the impeller, a radial gap arranged between the impeller and the housing wall, an inlet, an outlet, and two flow channels. The housing wall radially surrounds the impeller. The impeller blades open in a radially outward direction. The two flow channels connect the inlet to the outlet and are fluidically connected to one another via intermediate spaces between the impeller blades. An interruption zone is arranged between the outlet and the inlet which interrupts the two flow channels in a peripheral direction. A radial interrupting gap is arranged between the impeller and the radially delimiting housing wall in the entire interruption zone.

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17-01-2019 дата публикации

FLUID PUMP ASSEMBLY

Номер: US20190017509A1
Принадлежит:

A fluid pump assembly is provided. The pump has a pair of units magnetically coupled to each other. The first unit contains a drive motor and a magnetic assembly. The second unit contains a magnetic assembly and a blade of a propeller/impeller for imparting movement to a fluid. As the first unit is activated by the drive motor, a magnetic flux is created which in turn rotates the magnetic assembly in the second unit, driving the blade. 1. A magnetically driven unit of a fluid pump assembly , comprising:a housing comprising a base and a nozzle;a rotator at least partially contained in the housing, the rotator comprising a magnet constructed and arranged to be magnetically coupled to and rotationally driven by a magnet of a drive unit;a shaft operatively connected to the rotator;a blade operatively coupled with the shaft; anda magnet cover cooperating with the base to enclose the rotator.2. The magnetically driven unit of claim 1 , further comprising an axle concentrically surrounded by the shaft.3. The magnetically driven unit of claim 2 , wherein the axle comprises a flanged base.4. The magnetically driven unit of claim 3 , wherein the flanged base contacts a surface of the base.5. The magnetically driven unit of claim 4 , further comprising a ceramic sleeve concentric with the axle and positioned between the axle and the shaft.6. The magnetically driven unit of claim 5 , wherein at least a portion of the ceramic sleeve is concentric with and surrounded by a bearing.7. The magnetically driven unit of claim 3 , wherein the axle comprises a metallic material.8. The magnetically driven unit of claim 1 , wherein the nozzle comprises a plurality of ribs spaced apart from one another to create openings for allowing fluid to flow therethrough.9. The magnetically driven unit of claim 1 , further comprising a casing surrounding the magnet.10. The magnetically driven unit of claim 1 , further comprising a lower bearing connected to the rotator.11. A fluid pump assembly claim ...

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17-01-2019 дата публикации

BLOWER

Номер: US20190017515A1
Принадлежит: Denso Corporation

A blower configured to suction and discharge first fluid and second fluid includes a fan and a division wall. The fan is configured to rotate relative to the division wall. The division wall is spaced from the fan and positioned in a suction space, the division wall partitioning the suction space into a space through which the first fluid passes and a space through which the second fluid passes. The division wall includes a base and a widened portion. The base guides flows of the first fluid and the second fluid toward the fan. In the suction space, the widened portion is closer to a rotation area of the fan than the base is. A width of the widened portion in a direction along a thickness of an end of the base connected to the widened portion is larger than the thickness of the end of the base.

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16-01-2020 дата публикации

COLLECTOR FOR A COMPRESSOR

Номер: US20200018325A1
Автор: Snell Paul W.
Принадлежит:

Embodiments of the present disclosure are directed toward a compressor includes an impeller configured to compress a working fluid, a diffuser positioned downstream of the impeller with respect to a flow path of the working fluid, where the diffuser is configured to direct the working fluid through a radial passage, and where the diffuser comprises a vaned diffuser portion disposed within the radial passage, and a collector positioned downstream of the diffuser with respect to the flow path of the working fluid, where a chamber of the collector is axially offset from the radial passage of the diffuser. 1. A compressor , comprising:an impeller configured to compress a working fluid;a diffuser positioned downstream of the impeller with respect to a flow path of the working fluid, wherein the diffuser is configured to direct the working fluid through a radial passage, and wherein the diffuser comprises a vaned diffuser portion disposed within the radial passage; anda collector positioned downstream of the diffuser with respect to the flow path of the working fluid, wherein a chamber of the collector is axially offset from the radial passage of the diffuser.2. The compressor of claim 1 , wherein the diffuser comprises a variable geometry diffuser ring portion disposed within the radial passage.3. The compressor of claim 2 , wherein the variable geometry diffuser ring portion comprises a ring configured to extend axially into the radial passage to adjust a flow of the working fluid through the radial passage.4. The compressor of claim 3 , wherein the vaned diffuser portion is positioned downstream of the variable geometry diffuser ring portion with respect to the flow path of the working fluid claim 3 , and wherein a position of the ring of the variable geometry diffuser ring portion is configured to adjust a flow angle of the working fluid directed toward the vaned diffuser portion.5. The compressor of claim 1 , comprising an interface positioned between an outlet of ...

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16-01-2020 дата публикации

Variable geometry diffuser ring

Номер: US20200018326A1
Автор: Paul W. Snell
Принадлежит: Johnson Controls Technology Co

A compressor includes an impeller, a diffuser passage having a diffuser vane therein, and a variable geometry diffuser ring positioned between the impeller and the diffuser vane with respect to a flow of a refrigerant through the compressor. The compressor also includes an actuator configured to move the variable geometry diffuser ring in a direction transverse to the flow of the refrigerant, and between a plurality of ring positions including a fully retracted ring position in which the variable geometry diffuser ring does not block the flow of the refrigerant, and at least one protruded ring position in which the variable geometry diffuser ring adjusts an angle of the flow of the refrigerant upstream of the diffuser vane.

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17-04-2014 дата публикации

Gas turbine diffuser blowing method and corresponding diffuser

Номер: US20140105723A1
Принадлежит: Turbomeca SA

A diffuser of a compressor of centrifugal or mixed type includes two end plates which enclose a plurality of regularly distributed circumferential blades, and at least one transverse upstream passage produced in lower or upper surfaces of the blades. An injection/withdrawal coupling is achieved by a recirculation of a stream in an air passage of the diffuser on the basis of injection of air from at least one point in a leading edge zone of an upstream side of the diffuser. Blowing of air is then effected in at least one groove formed along a lateral flank of each blade by withdrawal of the air stream in a region of a trailing edge. Thereby, effectively separation of the air in a boundary layer in a gas turbine compressor diffuser is realized by re-energizing the boundary layer with air at a higher pressure by a suction/re-injection coupling.

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25-01-2018 дата публикации

BLOWER UNIT

Номер: US20180020838A1
Принадлежит:

An air passage forming member includes an air passage inner wall surface that forms a wall surface of a connecting air passage connected to a cushion air passage. A blower device case has an air intake opening that is connected to the connecting air passage. A centrifugal fan is received in the inside of the blower device case. The air passage forming member is arranged such that at a downstream end of the connecting air passage, the air, which flows along the air passage inner wall surface in the connecting air passage, forms an air flow, which is directed in an axial direction of a fan central axis, or an air flow, which is directed toward an outer side in a radial direction of the fan central axis in comparison to the air flow that is directed in the axial direction. 19.-. (canceled)10. A blower unit comprising:an air passage forming member, in which a connecting air passage is formed, wherein the connecting air passage is connected to a cushion air passage that is formed in a cushion member of a vehicle seat, and the air passage forming member has an air passage inner wall surface that forms a wall surface of the connecting air passage; and a blower device case, in which an air intake opening is formed, wherein the air intake opening is connected to an opposite side of the connecting air passage, which is opposite from the cushion air passage; and', 'a centrifugal fan that is received in the blower device case and draws air, which is present in the cushion air passage, through the connecting air passage and the air intake opening in this order when the centrifugal fan is rotated about a fan central axis, wherein:, 'a blower device that includesthe air passage forming member is arranged such that at a downstream end of the connecting air passage along the air flow, the air, which flows along the air passage inner wall surface in the connecting air passage, forms an air flow, which is directed in an axial direction of the fan central axis, or an air flow, which is ...

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22-01-2015 дата публикации

AIR CYCLE MACHINE COMPRESSOR DIFFUSER

Номер: US20150023787A1
Принадлежит:

A diffuser for an air cycle machine defines airflow both to a compressor rotor from the inlet and from the compressor rotor through a plurality of vanes that define radially extending airflow passages. The size and shape of both the inlet and the vanes of the diffuser define and tailor the character of airflow presented to and leaving the compressor rotor to provide a desired change in air flow. 1. A compressor diffuser comprising:a hub defining an inlet for airflow disposed about an axis;a diffuser portion extending radially outward from the hub portion, the diffuser portion including a plurality of vanes defining radial passages for communicating airflow radially outward, each of the plurality of vanes including a first height at a radially innermost portion of each of the plurality of vanes and a second height at a radially outermost portion of each of the plurality of vanes, with a ratio of the second height to the first height between 1.37 and 1.48, wherein each of the plurality of vanes includes a width transverse to the axis, the width of each of the plurality of vanes continually increasing in a direction radially outward.2. The compressor diffuser as recited in claim 1 , wherein the radial passages comprise a common width beginning at the radially innermost portion to the radially outermost portion.3. The compressor diffuser as recited in claim 1 , wherein the innermost portion of each of the plurality of vanes is spaced a radial distance away from the axis.4. The compressor diffuser as recited in claim 1 , wherein the diffuser portion defines a back side opposite the plurality of vanes claim 1 , the back side including a plurality of boss pads spaced circumferentially about a periphery of the diffuser portion.5. The compressor diffuser as recited in claim 5 , including a seal land extending axially from the back side for sealing against a portion of a compressor housing.6. The compressor diffuser as recited in claim 1 , wherein the inlet comprises a ...

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26-01-2017 дата публикации

PUMP FOR THE CONVEYANCE OF A FLUID WITH VARYING VISCOSITY

Номер: US20170022997A1
Принадлежит:

A pump includes a housing having an inlet and an outlet configured to convey fluid, an impeller configured to convey the fluid from the inlet to the outlet, the impeller being arranged on a rotatable shaft, and a balance drum configured to relieve axial thrust. The balance drum includes a rotor rotationally fixedly connected to the shaft, the rotor having a high and low pressure sides, a stator stationary with respect to the housing, a relief passage extending between the rotor and the stator from the high pressure side up to the low pressure side of the rotor, a return passage connecting the low pressure side of the rotor to the inlet. An intermediate passage opens into the relief passage between the high pressure side and the low pressure side of the rotor. A blocking member is configured to influence the flow through the intermediate passage. 1. A pump for conveying a fluid with varying viscosity , comprising:a housing having an inlet and an outlet configured to convey the fluid;at least one impeller configured to convey the fluid from the inlet to the outlet, the impeller being arranged on a rotatable shaft; anda balance drum configured to relieve axial thrust, the balance drum comprising a rotor rotationally fixedly connected to the shaft, the rotor having a high pressure side and a low pressure side, a stator configured to be stationary with respect to the housing, and a relief passage extending between the rotor and the stator from the high pressure side up to the low pressure side of the rotor;a return passage connecting the low pressure side of the rotor to the inlet;at least one intermediate passage opening into the relief passage between the high pressure side and the low pressure side of the rotor; anda blocking member configured to influence the flow through the intermediate passage.2. A pump in accordance with claim 1 , wherein the relief passage comprises a ring space surrounding the shaft and into which the intermediate passage opens.3. A pump in ...

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26-01-2017 дата публикации

TURBOMACHINE ASSEMBLY

Номер: US20170023011A1
Принадлежит: Nuovo Pignone Srl

The present disclosure relates to a turbomachine assembly, which includes a shaft, a radial gas expander supported on the shaft between a first bearing and a second bearing, and a compressor supported on the shaft in overhung position adjacent to one or the other of the first and second bearings. The compressor includes a plurality of movable inlet nozzles and the radial gas expander includes a plurality of movable guide vanes. 1. A turbomachine assembly comprising:a shaft,a radial gas expander supported on the shaft between at least one first bearing and at least one second bearing, anda compressor supported on the shaft in an overhung position adjacent to at least one of said first or second bearings,said wherein the radial gas expander comprises a plurality of movable guide vanes.2. The turbomachine assembly according to claim 1 , wherein said compressor includes a plurality of movable inlet nozzles.3. The turbomachine assembly according to claim 1 , wherein the radial gas expander comprises at least two radial stages.4. The turbomachine assembly according to claim 3 , wherein at least one of the radial stages comprises a movable set of inlet guide vanes.5. The turbomachine assembly according to claim 4 , wherein each radial stage comprises a respective movable set of inlet guide vanes claim 4 , each set being actuated independently from the other set.6. The turbomachine assembly according to claim 1 , wherein at least a seal is provided on said shaft between the compressor and the radial gas expander.7. The turbomachine assembly according to claim 1 , wherein a first process gas is compressed in said compressor and a second operative gas is expanded in said radial gas expander.8. The turbomachine assembly according to claim 1 , wherein said radial gas expander is part of an organic Rankine cycle.9. The turbomachine assembly according to claim 1 , wherein said shaft operates at a variable speed.10. The turbomachine assembly according to claim 1 , wherein said ...

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25-01-2018 дата публикации

Centrifugal compressor

Номер: US20180023589A1

A centrifugal compressor includes an impeller that rotates about an axis; an inlet guide vane including a plurality of vanes disposed on an upstream side of the impeller and provided at intervals in a circumferential direction of the axis, the inlet guide vane being directed inward in the radial direction between adjacent vanes, and forming a guide flow path having an exit angle in the radial direction and guiding the fluid; and a suction flow path that introduces the fluid from a part in a circumferential direction into the inlet guide vane. The exit angle of the vane of the first region on the one side when viewed from the suction flow path in the inlet guide vane is displaced to the suction flow path side as compared to the exit angle of the vane of a second region on the opposite side of the one side.

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24-01-2019 дата публикации

STATIONARY-BLADE-TYPE ROTATING MACHINE AND METHOD FOR ASSEMBLING STATIONARY-BLADE-TYPE ROTATING MACHINE

Номер: US20190024517A1

A stationary-blade-type rotating machine is provided with a rotational shaft, an impeller, an impeller housing having a scroll passage formed on an outer peripheral side of the impeller, a bearing housing connected to the impeller housing in an axial direction of the rotational shaft, a stationary blade disposed in a radial passage formed between the scroll passage and the impeller and defined by an impeller-housing-side member and a bearing-housing-side member which face each other in the axial direction of the rotational shaft. The fixation unit includes an annular circumferential groove formed in an inner peripheral surface of the impeller housing and a ring-shaped fitting member subjected to a force for expanding in a radial direction while being fitted into the circumferential groove. The fitting member is configured to press the stationary blade to the impeller housing via at least one of the impeller-housing-side member or the bearing-housing-side member. 118-. (canceled)19. A stationary-blade-type rotating machine comprising:a rotational shaft;an impeller mounted to the rotational shaft;an impeller housing accommodating the impeller and having therein a scroll passage formed on an outer peripheral side of the impeller;a bearing housing accommodating a bearing which rotatably supports the rotational shaft and connected to the impeller housing in an axial direction of the rotational shaft;a stationary blade disposed in a radial passage formed between the scroll passage and the impeller, the radial passage being defined by an impeller-housing-side member and a bearing-housing-side member which face each other in the axial direction of the rotational shaft; anda fixation unit pressing and thereby fixing the stationary blade to the impeller housing, an annular circumferential groove disposed in an inner peripheral surface of the impeller housing; and', 'a ring-shaped fitting member subjected to a force to expand in a radial direction while being fitted into the ...

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24-01-2019 дата публикации

BOOST FAN STRUCTURE

Номер: US20190024676A1
Автор: YANG Chao-Fu
Принадлежит:

A boost fan structure includes a base, a motor driver set, a rotary blade set, and an outer shroud. The base has a frame and an inner guider having a body and plural static blades. The body is disposed in the frame and has an annular curved surface and a receiving space. The static blades are formed on the annular curved surface and exposed out of the frame. The motor driver set is disposed in the receiving space. The rotary blade set is disposed on a side of the inner guider and is driven by the motor driver set to rotate. The outer shroud has a shell having a curved inner wall. The shell covers the rotary blade set and the inner guider to be combined with the frame. 1. A boost fan structure , comprising:a base having a frame and an inner guider, wherein the inner guider has a body and a plurality of static blades, wherein the body is disposed in the frame and has an annular curved surface and a receiving space formed in the annular curved surface, wherein the static blades are formed on the annular curved surface and exposed to a side of the frame;a motor driver set disposed in the receiving space;a rotary blade set disposed on a side of the inner guider, wherein the rotary blade set is driven by the motor driver set to rotate; andan outer shroud having a shell with a curved inner wall, wherein the shell covers the rotary blade set and the inner guider to be combined with the frame.2. The boost fan structure according to claim 1 , wherein the frame has a throughhole through which a side of the body is disposed claim 1 , wherein ends of the static blades are individually extended through the throughhole and formed out of the frame.3. The boost fan structure according to claim 1 , wherein a plurality of air channels is formed between the outer shroud claim 1 , the annular curved surface claim 1 , and the static blades.4. The boost fan structure according to claim 1 , wherein the body forms a supporting base at the bottom of the receiving space claim 1 , wherein a ...

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23-01-2020 дата публикации

BACKFEED STAGE AND RADIAL TURBO FLUID ENERGY MACHINE

Номер: US20200025205A1
Автор: Petry Nico
Принадлежит: SIEMENS AKTIENGESELLSCHAFT

A backfeed stage of a radial turbo fluid energy machine having a backfeed channel extending annularly about an axis and four sections adjacent in the flow direction through which process fluid flows. A first section conducts the process fluid radially outward; a second section deflects the process fluid from radially outward to radially inward; a third section conducts the process fluid radially inward; a fourth section redirects the process fluid in the axial direction; the third section has first guide vanes defining flow channels of the backfeed channel in relation to each other in the circumferential direction; the backfeed stage has second guide vanes downstream of the first guide vanes defining the flow channels of the backfeed channel in relation to each other in the circumferential direction. The first guide vanes are arranged only in the third section, the second guide vanes are arranged only in the fourth section. 112.-. (canceled)13. A backfeed stage of a radial turbo fluid energy machine or a radial turbo compressor , for deflecting a flow direction of a process fluid flowing out of an impeller rotating about an axis from radially outward to radially inward , comprising:a backfeed channel which extends annularly about the axis and which has four portions adjacent in the flow direction, through which the process fluid can flow,wherein a first portion is designed to conduct the process fluid radially outward,wherein a second portion is designed to deflect the process fluid from radially outward to radially inward,wherein a third portion is designed to conduct the process fluid radially inward,wherein a fourth portion is designed to divert the process fluid in an axial direction,wherein the third portion has first guide vanes which define flow channels of the backfeed channel relative to each other in a circumferential direction,wherein the backfeed stage has second guide vanes which are arranged downstream of the first guide vanes and define the flow ...

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23-01-2020 дата публикации

CENTRIFUGAL COMPRESSOR WITH INCLINED DIFFUSER

Номер: US20200025214A1
Автор: Wang Chijou
Принадлежит: GM GLOBAL TECHNOLOGY OPERATIONS LLC

A compressor includes a compressor impeller configured to rotate about an axis of rotation as intake gases flow along the compressor impeller. The compressor impeller includes an inducer and an exducer. The compressor impeller defines a first impeller end at the inducer and a second impeller end at the exducer. The second impeller end extends along a radial axis. The compressor further includes a compressor housing encasing the compressor impeller. The compressor housing defines a compressor volute. The compressor housing partially defines a diffuser in fluid communication with the compressor volute. The diffuser is elongated along a diffuser axis. The diffuser axis is obliquely angled relative to the axis of rotation. The diffuser axis is obliquely angled relative to the radial axis to minimize a turbulence of the intake gases flowing from the diffuser to the compressor volute. 1. A centrifugal compressor , comprising:a compressor impeller configured to rotate about an axis of rotation as intake gases flow along the compressor impeller, wherein the compressor impeller includes an inducer and an exducer, the compressor impeller defines a first impeller end at the inducer and a second impeller end at the exducer, the second impeller end extends along a radial axis, and the radial axis is perpendicular to the axis of rotation; anda compressor housing encasing the compressor impeller, wherein the compressor housing defines a compressor volute, the compressor housing partially defines a diffuser in fluid communication with the compressor volute, the diffuser is configured to convert a kinetic energy of the intake gases into static pressure, the diffuser is elongated along a diffuser axis, the diffuser axis is obliquely angled relative to the axis of rotation, the diffuser axis is obliquely angled relative to the radial axis to minimize a turbulence of the intake gases flowing from the diffuser to the compressor volute.2. The centrifugal compressor of claim 1 , further ...

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02-02-2017 дата публикации

FLUID-TRANSFER DEVICE AND METHOD FOR MANUFACTURING SAME

Номер: US20170030372A1
Принадлежит: AIRBUS SAFRAN LAUNCHERS SAS

A fluid transfer device including a rotor having two centrifugal wheels, and a stator incorporating a set of continuous axi symmetric return channels conveying the fluid from the first wheel to the second wheel. Each of the return channels includes in succession a diffusing portion that guides the fluid in a centrifugal direction, a bend portion that redirects the fluid stream in a centripetal direction, a return portion that guides the fluid along a centripetal path, and then an outlet portion formed in a first non-tubular part that guides the fluid towards the second wheel. In these channels, the diffusing portion and the bend portion are distinct parts, and the diffusing portion is formed in a second non-tubular part secured to the first non-tubular part. A method of fabricating the device. 112-. (canceled)13. A fluid transfer device comprising a rotor having at least a first centrifugal wheel and a second centrifugal wheel , and a stator incorporating a plurality of return channels;in which device the return channels are axisymmetric, and each return channel includes in succession along the fluid flow path from the first wheel:a diffusing portion suitable for guiding the fluid stream in a centrifugal flow direction; thena bend portion suitable for redirecting the fluid stream in a centripetal flow direction; thena return portion suitable for guiding the fluid along a centripetal path; and thenan outlet portion formed in a first non-tubular part, and suitable for guiding the fluid towards the inlet of the second centrifugal wheel;wherein each of said return channels is suitable for collecting a portion of a fluid stream leaving the first wheel and for directing this stream portion to an inlet of the second wheel without exchanging the fluid with any other one of said return channels; and in that for each of said channels:the diffusing portion and the bend portion are formed in distinct parts; andthe diffusing portion is formed in a second non-tubular part secured ...

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02-02-2017 дата публикации

A SCROLL FOR A TURBOMACHINE, TURBOMACHINE COMPRISING THE SCROLL, AND METHOD OF OPERATION

Номер: US20170030373A1
Принадлежит:

A scroll for use in conjunction with a fluid compressor is described. The scroll comprises a fluid inlet adapted to receive a fluid flow and a fluid outlet adapted to discharge the fluid flow. The scroll further comprises a scroll-shaped wall defining an inner flow volume. At least one blade is provided in the inner flow volume of the scroll. The blade is configured and arranged for correcting a direction of the flow of fluid in the flow volume when the scroll is operating in off-design conditions. 1. A scroll for use in conjunction with a fluid compressor , the scroll comprising:a fluid inlet adapted to receive a flow of fluid;a fluid outlet adapted to discharge the flow of fluid;a scroll-shaped wall defining an inner flow volume; andat least one blade in the inner flow volume protruding from the scroll-shaped wall for correcting a direction of the flow of fluid in the inner flow volume, when the scroll is operating in off-design conditions.2. The scroll of claim 1 , wherein a plurality of blades are arranged in the inner flow volume of the scroll claim 1 , along at least a portion of a circular development thereof.3. The scroll of claim 2 , wherein the blades are arranged according to a constant pitch around the scroll.4. The scroll of claim 1 , wherein each blade is oriented and configured so as to at least reduce a variation of a ratio between axial component and tangential component of a fluid velocity at variable operating conditions.5. The scroll of claim 1 , wherein each blade extends along the wall from a leading edge claim 1 , located proximate the fluid inlet claim 1 , to a trailing edge.6. The scroll of claim 1 , wherein each blade has an inclination with respect to an axial direction.7. The scroll of claim 1 , wherein each blade forms an angle with respect to an axial direction claim 1 , the angle being variable from the leading edge to the trailing edge of the blade.8. The scroll of claim 7 , wherein the angle between the blade and the axial direction ...

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02-02-2017 дата публикации

METHOD OF INSTALLING A DIFFUSER IN AN AIR CYCLE MACHINE

Номер: US20170030376A1
Принадлежит:

A method of installing a diffuser in an air cycle machine includes placing a first housing on a shaft, placing a seal plate on the shaft, and placing a diffuser on the shaft. Next, the diffuser and the seal plate are aligned with an alignment tool. The alignment tool has a first annular surface to align with a radially outer surface of the seal plate and a second annular surface to align with an annular flange on the diffuser. Finally, the diffuser is fastened to the seal plate and the alignment tool is removed from the diffuser and the seal plate. 1. An alignment tool that can be used to install a diffuser in an air cycle machine , the alignment tool comprising:a body with a cylindrical portion and an end portion;a first surface on a radially inner face of the cylindrical portion positioned axially away from the end portion;a second surface on the radially inner face of the cylindrical portion positioned adjacent to the end portion; anda third surface on a radially inner edge of the end portion.2. The alignment tool of claim 1 , wherein the first surface has a larger diameter than the second surface.3. The alignment tool of claim 1 , wherein the first surface is configured to have a diameter that is substantially equal to a diameter of a radially outer surface of a seal plate in the air cycle machine.4. The alignment tool of claim 1 , wherein the third surface is configured to have a diameter that is substantially equal to a diameter of a radially outer surface of a flange on the diffuser in the air cycle machine.5. The alignment tool of claim 1 , wherein the first surface and the third surface are precision manufactured.6. The alignment tool of claim 1 , and further comprising:a plurality of openings in the cylindrical portion of the alignment tool.7. The alignment tool of claim 1 , and further comprising:an aperture in the end portion of the alignment tool that is configured to receive a timing pin.8. An alignment tool that can be used to install a diffuser in an ...

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02-02-2017 дата публикации

Arrangement of components in a fluid energy machine and assembly method

Номер: US20170030377A1
Принадлежит: SIEMENS AG

An assembly method and an arrangement of components in a fluid energy machine, in particular a turbocompressor, with a longitudinal axis. The arrangement includes: an inner bundle to be arranged in an outer casing of the fluid energy machine, a low-pressure unit of the fluid energy machine, at least one cover of the fluid energy machine for the axial end-side closure of the outer casing on at least one end side, wherein these components are arranged axially adjacent to one another in the sequence cover, low-pressure unit, inner bundle and the cover is releasably attached to the low-pressure unit and the inner bundle is releasably attached to the low-pressure unit such that there results a transportable unit.

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04-02-2016 дата публикации

SYSTEM AND METHOD FOR DETECTING STALL OR SURGE IN RADIAL COMPRESSORS4

Номер: US20160032932A1
Автор: Sorokes James M.
Принадлежит: DRESSER-RAND COMPANY

A system and method are provided for detecting an impending stall or surge in a radial compressor. The system and method may include a plurality of detection devices configured to detect a transition of a low momentum zone of a gas flow through the diffuser from a first position adjacent a shroud wall of the diffuser to a second position adjacent a hub wall of the diffuser. The system and method may also include a control system electrically coupled to the plurality of detection devices and configured to receive a plurality of information signals. Each information signal may be transmitted by a respective one of the plurality of detection devices and may correlate to a location of the low momentum zone. The control system may be configured to process the plurality of information signals and detect the impending stall or surge based on the location of the low momentum zone. 1. A detection system for detecting an impending stall or surge in a radial compressor , comprising:a plurality of detection devices coupled to the radial compressor, at least a portion of each detection device disposed in a diffuser channel of a diffuser of the radial compressor, the plurality of detection devices configured to detect a transition of a low momentum zone of a gas flow through the diffuser from a first position adjacent a shroud wall of the diffuser to a second position adjacent a hub wall of the diffuser; anda control system electrically coupled to the plurality of detection devices and configured to receive a plurality of information signals, each information signal being transmitted by a respective one of the plurality of detection devices and correlating to a location of the low momentum zone, the control system further being configured to process the plurality of information signals and detect the impending stall or surge based on the location of the low momentum zone.2. The system of claim 1 , wherein at least one detection device of the plurality of detection devices ...

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04-02-2016 дата публикации

CENTRIFUGAL BLOWER AND METHOD OF ASSEMBLING THE SAME

Номер: US20160032944A1
Принадлежит:

In one aspect, a centrifugal blower assembly is provided. The centrifugal blower assembly includes a housing defining an interior space and an impeller configured to channel an airflow within the interior space. A motor is coupled to the impeller and configured to rotate the impeller about an axis. The centrifugal blower also includes a plurality of mounting arms. Each mounting arm of the plurality of mounting arms includes a first end coupled to the housing and a second end coupled to the motor. Each mounting arm of the plurality of mounting arms has a cross-sectional profile that comprises a portion of an airfoil shape. 1. A centrifugal blower assembly comprising:a housing defining an interior space;an impeller configured to channel an airflow within the interior space;a motor coupled to said impeller and configured to rotate said impeller about an axis; anda plurality of mounting arms, wherein at least one mounting arm of the plurality of mounting arms includes a first end coupled to said housing and a second end coupled to said motor, said at least one mounting arm having a cross-sectional profile that comprises a portion of an airfoil shape.2. The centrifugal blower assembly in accordance with claim 1 , wherein said housing includes at least one sidewall and an inlet ring that define an inlet opening claim 1 , said first end of said at least one mounting arm coupled to said at least one sidewall.3. The centrifugal blower assembly in accordance with claim 1 , wherein said housing includes at least one sidewall and an inlet ring that define an inlet opening claim 1 , said first end of said at least one mounting arm coupled to said inlet ring.4. The centrifugal blower assembly in accordance with claim 3 , wherein said first end of said at least one mounting arm is integrally formed with said inlet ring.5. The centrifugal blower assembly in accordance with claim 1 , wherein the cross-sectional profile includes an arcuate portion claim 1 , a first leg extending from ...

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04-02-2016 дата публикации

Humidifying apparatus

Номер: US20160033148A1
Автор: William John Darvill
Принадлежит: Dyson Technology Ltd

A humidifying apparatus includes a body and a nozzle detachably mounted on the body. The body includes a chamber, a water tank for supplying water to the chamber, and a motor-driven impeller for generating an air flow over water stored in the chamber. An ultraviolet radiation emitting lamp irradiates water stored in the chamber. The air flow is humidified with water from the chamber, and conveyed to the nozzle for emission from the apparatus. A sensor detects the position of the nozzle relative to the body, and a drive circuit controls the actuation of the lamp depending on an output from the sensor.

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04-02-2016 дата публикации

Humidifying apparatus

Номер: US20160033150A1
Принадлежит: Dyson Technology Ltd

A humidifying apparatus includes a base, a water tank removably mounted on the base for supplying water to a chamber of the base, and a motor-driven impeller for generating an air flow over water stored in the chamber. An ultraviolet radiation emitting lamp irradiates water stored in the chamber. The air flow is humidified with water from the chamber, and conveyed by an outlet duct towards an air outlet for emission from the apparatus. A detachable section of the water tank is opaque to ultraviolet radiation and is positioned over the chamber when the water tank is mounted on the base. The detachable section of the water tank includes an air inlet of the outlet duct and a flange for occluding a peripheral portion of the chamber.

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01-02-2018 дата публикации

DIFFUSER, CENTRIFUGAL COMPRESSION POWER SYSTEM AND BLADELESS FAN

Номер: US20180030998A1
Автор: DOU Hai, MA Lie, SHAO Chen
Принадлежит:

A diffuser includes a lower element and an upper element. The upper element is fixed on the lower element, and the upper element and the lower element are formed separately. The lower element includes a lower inner wall and a lower outer wall, and the upper element includes an upper inner wall and an upper outer wall. The upper inner wall is connected to the lower inner wall to form an internal air-guiding surface, the upper outer wall is connected to the lower outer wall to form an external air-guiding surface, and the internal air-guiding surface is disposed opposite to the external air-guiding surface to define an air-guiding channel for air flow diffusion. The upper element further includes an upper air-guiding wing for connecting the upper inner wall and the upper outer wall, and the lower element further includes a lower air-guiding wing for connecting the lower inner wall and the lower outer wall. 1. A diffuser , comprising:a lower element; andan upper element fixed on the lower element,wherein the upper element and the lower element are formed separately; the lower element comprises a lower inner wall and a lower outer wall, and the upper element comprises an upper inner wall and an upper outer wall; the upper inner wall is connected to the lower inner wall to form an internal air-guiding surface; the upper outer wall is connected to the lower outer wall to form an external air-guiding surface; the internal air-guiding surface is disposed opposite to the external air-guiding surface, and an air-guiding channel configured to diffuse an airflow is defined between the internal air-guiding surface and the external air-guiding surface; the upper element further comprises an upper air-guiding wing for connecting the upper inner wall and the upper outer wall, and the lower element further comprising a lower air-guiding wing for connecting the lower inner wall and the lower outer wall; the upper air-guiding wing is connected to the lower air-guiding wing to form an ...

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02-02-2017 дата публикации

A HEAT-DISSIPATING DEVICE INCLUDING A VAPOR CHAMBER AND A RADIAL FIN ASSEMBLY

Номер: US20170031394A1
Принадлежит:

A vapor chamber to thermally contact a heat-producing component includes an opening. An airflow generator is at least partially mounted in the opening of the vapor chamber. A radial fin assembly extends at least partially around the airflow generator. 1. A heat-dissipating device comprising:a vapor chamber to thermally contact a heat producing component, the vapor chamber including an opening;an airflow generator at least partially mounted in the opening of the vapor chamber; anda radial fin assembly extending at least partially around the airflow generator, the radial fin assembly including fins and flow channels between the fins for passing airflow generated by the airflow generator.2. The heat-dissipating device of claim 1 , wherein the radial fin assembly includes an opening to receive the airflow generator.3. The heat-dissipating device of claim 2 , wherein the vapor chamber includes a housing. the radial fin assembly in thermal contact with the housing.4. The heat-dissipating device of claim 3 , wherein the housing is to thermally contact the heat-producing component.5. The heat-dissipating device of claim 1 , wherein the fins and the flow channels between the fins are arranged radially to allow the airflow to flow in radial directions.6. The heat-dissipating device of claim 5 , wherein the airflow generator is arranged to draw cooling air from above and below the airflow generator claim 5 , and to direct the drawn cooling air through the flow channels in the radial directions.7. The heat-dissipating device of claim 1 , wherein the vapor chamber contains a fluid to carry heat from a first location for thermally contacting the heat-producing component claim 1 , to a second location of the vapor chamber in thermal contact with the radial fin assembly.8. The heat-dissipating device of claim 1 , wherein a profile of the radial fin assembly is one of a circular shape a semi-circular shape claim 1 , an elliptical shape claim 1 , polygonal shape.9. The heat- ...

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31-01-2019 дата публикации

OUTBOARD MOTOR

Номер: US20190031310A1
Принадлежит:

An outboard motor includes an engine including a crankshaft, a generator including a rotor that rotates together with the rotation of the crankshaft and a stator in which a coil is wound so as to face the rotor, and a fan including a blade disposed coaxially with the rotor, provided separately from the rotor, and that rotates together with the rotation of the rotor. 1. An outboard motor comprising:an engine including a crankshaft;a generator including a rotor that rotates together with a rotation of the crankshaft and a stator in which a coil is wound so as to face the rotor; anda fan including a blade disposed coaxially with the rotor, provided separately from the rotor, and that rotates together with the rotation of the rotor.2. The outboard motor according to claim 1 , wherein the blade includes an annular first plate member and a plurality of fins that extend downward from the first plate member and are integral and unitary with the first plate member.3. The outboard motor according to claim 2 , wherein the plurality of fins extend in a radial direction and are arcuately curved in a planar view.4. The outboard motor according to claim 1 , whereinthe fan further includes a first air guide including a floor and a wall that extends upward from the floor and that surrounds fins provided on the blade from a lateral side; andan upper surface of the floor is disposed at a same or substantially a same height as a lower end of the blade.5. The outboard motor according to claim 4 , further comprising a cowling including an engine compartment in which the engine is housed; whereinthe fan further includes a lid-shaped second air guide that covers the first air guide from above between the cowling and the blade; andan upper surface of the blade that faces the lid-shaped second air guide is flat or substantially flat.6. The outboard motor according to claim 5 , further comprising an air guide passage through which air flows laterally from the blade and that extends along an ...

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17-02-2022 дата публикации

VANELESS SUPERSONIC DIFFUSER FOR COMPRESSOR

Номер: US20220049716A1
Принадлежит:

A mixed-flow compressor includes an impeller attached to a shaft and rotatable about a shaft axis. A vaneless diffuser is located axially downstream of the impeller and has a converging portion and a diverging portion. A vaned diffuser is located axially downstream of the vaneless diffuser. 1. A mixed-flow compressor comprising:an impeller attached to a shaft and rotatable about a shaft axis;a vaneless diffuser located axially downstream of the impeller having a converging portion and a diverging portion; anda vaned diffuser located axially downstream of the vaneless diffuser.2. The mixed-flow compressor of claim 1 , wherein the converging portion is located axially upstream of the diverging portion.3. The mixed-flow compressor of claim 2 , wherein the converging portion is connected to the diverging portion with an axially extending mid-portion having a constant cross-sectional area.4. The mixed-flow compressor of claim 1 , wherein the vaneless diffuser includes an inner wall and an outer wall defining a fluid flow path there between.5. The mixed-flow compressor of claim 4 , wherein at least one of the inner wall and the outer wall are rotatable relative to the shaft axis.6. The mixed-flow compressor of claim 4 , wherein both the inner wall and the outer wall are rotatable about the shaft axis.7. The mixed-flow compressor of claim 6 , wherein the inner wall is supported on at least one inner wall bearings and the outer wall is supported on at least one outer wall bearings.8. The mixed-flow compressor of claim 1 , wherein the vaned diffuser includes a plurality of vanes circumferentially spaced from each other around the shaft axis.9. The mixed-flow compressor of claim 1 , wherein the converging portion extends up to 75% of an axial length of the vaneless diffuser.10. The mixed-flow compressor of claim 9 , wherein the converging portion includes up to a 50% reduction in cross-sectional area between an inlet to the converging portion and an outlet of the converging ...

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17-02-2022 дата публикации

MIXED-FLOW COMPRESSOR WITH COUNTER-ROTATING DIFFUSER

Номер: US20220049717A1
Принадлежит:

A compressor includes a housing. An impeller is located within the housing and rotatable about an impeller axis in a first rotational direction. A rotor section is rotatable about the impeller axis in a second rotational direction opposite the first rotational direction. 1. A compressor comprising:a housing;an impeller located within the housing and rotatable about an impeller axis in a first rotational direction; anda rotor section rotatable about the impeller axis in a second rotational direction opposite the first rotational direction.2. The compressor of claim 1 , wherein the rotor section includes a rotor having at least one row of rotor blades.3. The compressor of claim 1 , wherein the impeller includes a hub and a plurality of impeller blades extending outward from the hub toward a portion of the housing.4. The compressor of claim 3 , wherein the rotor section includes a cylindrical rotor with a plurality of rotor blades extending from a surface of the cylindrical rotor.5. The compressor of claim 4 , wherein the plurality of impeller blades each include an upstream end and downstream end with the upstream end being circumferentially spaced in the first rotational direction from the downstream end and the plurality of rotor blades each include an upstream end and a downstream end with the upstream end being circumferentially spaced in the second rotational direction from the downstream end.6. The compressor of claim 5 , wherein each of the plurality of rotor blades and each of the plurality of impeller blades include a curvature in the first circumferential direction.7. The compressor of claim 1 , wherein the impeller is driven by an impeller motor and the rotor is driven by a separate rotor motor.8. The compressor of claim 1 , wherein the impeller is driven by an impeller motor and the rotor section is driven by the impeller motor through a transmission to reverse a rotational output of the impeller motor.9. The compressor of claim 8 , wherein the ...

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17-02-2022 дата публикации

Ceiling fan

Номер: US20220049718A1
Принадлежит: Hunter Fan Co

A ceiling fan or ceiling fan includes a body defining an interior passage having an inlet and an outlet provided on the body. The inlet, outlet, and interior passage can be annular. An impeller is mounted within the interior passage and driven by a motor mounted within the body to draw a volume of air through the interior passage from the inlet to the outlet. A deflector is provided within the body and extending through the outlet including an upper angled surface and a lower angled surface to direct the air in a generally upward or generally downward direction, respectively.

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31-01-2019 дата публикации

IMPELLER WHEEL FOR A CENTRIFUGAL TURBOCOMPRESSOR

Номер: US20190032671A1
Автор: WOICZINSKI Christian
Принадлежит: SIEMENS AKTIENGESELLSCHAFT

An impeller wheel of a turbocompressor, for rotation about an axis, has an inflow cross-section for inflow of a process fluid into the impeller wheel, an outflow cross-section for outflow of the process fluid from the impeller wheel, a wheel disk that defines a hub-side deflection contour from the axial flow direction into the radial flow direction. Blades are applied to the wheel disk, which define flow channels through the impeller wheel, each blade defining a linear inner track and a linear outer track. A meridional angle is defined for each position of a track as the upstream included angle between a meridional plane through the position and a tangent on the track. So that the flow passes through the impeller wheel with improved efficiency, as far as possible without separation, a local extremum of the meridional angle of the inner track is defined. 1. An impeller wheel of a turbocompressor , for rotation around an axis , comprising:an inlet cross section for the basically axial inflow of a process fluid into the impeller wheel,an exit cross section for the basically radial exit of the process fluid from the impeller wheel,a wheel disk which defines a hub-side deflection contour from the axial flow direction to the radial flow direction,blades, attached on the wheel disk, which define flow passages from a leading edge to a trailing edge in the circumferential direction, at least over a part of the flow path of the process fluid through the impeller wheel,wherein each blade, on an extent end edge which is proximal to the wheel disk, defines a linear inner track extending in the flow direction in such a way that orthogonally equal distances to a blade surface on a pressure side and a suction side of the blade exist on both sides of the inner track,wherein the blade, on an extent end edge which is distal to the wheel disk, defines a linear outer track extending in the flow direction in such a way that orthogonally equal distances to a blade surface on the pressure ...

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31-01-2019 дата публикации

COMBINED SECONDARY INLET BELL AND FLOW GRID FOR A CENTRIFUGAL FAN OR CENTRIFUGAL COMPRESSOR

Номер: US20190032676A1
Принадлежит:

A centrifugal fan assembly including fan wheel, a primary inlet bell, a secondary inlet bell, and a flow grid. The primary inlet bell and secondary inlet bell direct air into an inlet of the fan wheel of the centrifugal fan. Also disclosed is a sound reduction assembly for reducing the sound produced by a centrifugal fan or centrifugal compressor. A method of directing air flowing into a centrifugal fan or a centrifugal compressor is also disclosed. 1. A centrifugal fan assembly , comprising:a fan wheel including an axial inlet, the fan wheel radially discharging air;a primary inlet bell that directs the air into the axial inlet of the fan wheel;a secondary inlet bell that directs the air towards the primary inlet bell;a flow grid that guides the air flowing into the secondary inlet bell.2. The centrifugal fan assembly of claim 1 , further comprising:a cabinet including an air inlet and an air outlet, whereinthe fan wheel, the primary inlet bell, and the secondary inlet bell are located within the cabinet, andthe secondary inlet bell is affixed to the cabinet.3. The centrifugal fan assembly of claim 2 , wherein the flow grid is affixed to one of the secondary inlet bell and the cabinet.4. The centrifugal fan assembly of claim 1 , further comprising:a frame for supporting the fan wheel and the primary inlet bell, the fan wheel being rotatably affixed to the frame, and the primary inlet bell being affixed to the frame.5. The centrifugal fan assembly of claim 4 , further comprising:one or more vibration isolators that support the frame, the one or more vibration isolators being affixed to a cabinet of the centrifugal fan assembly, and the one or more vibration isolators supporting the frame such that the frame is configured to be moveable relative to a cabinet.6. The centrifugal fan assembly of claim 5 , wherein each of the one or more vibration isolators includes a spring that is located between the frame and the cabinet claim 5 , the spring biasing the frame away ...

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31-01-2019 дата публикации

PIPING FOR DRIVEN-TYPE FLUID MACHINE

Номер: US20190032833A1

A pipe for a driven-type fluid machine includes: an inlet pipe that is to be connected to a suction port provided in a casing of the driven-type fluid machine, a supply pipe that supplies a fluid, and a bend that connects the supply pipe and the inlet pipe to each other. The bend is shaped such that a pipe width in a plane including a pipe axis of the inlet pipe and a pipe axis of the supply pipe gradually decreases from an upstream portion to a bent portion, and L1≥3×d is satisfied where d is the pipe width at the bent portion and L1 is an axial length of the inlet pipe. 1. A pipe for a driven-type fluid machine , the pipe including an inlet pipe that is to be connected to a suction port provided in a casing of the driven-type fluid machine , a supply pipe that supplies a fluid , and a bend that connects the supply pipe and the inlet pipe to each other , characterized in thatthe bend is shaped such that a pipe width in a plane including a pipe axis of the inlet pipe and a pipe axis of the supply pipe gradually decreases from an upstream portion to a bent portion, andL1≥3×d is satisfied, where d is the pipe width at the bent portion and L1 is an axial length of the inlet pipe.2. The pipe for a driven-type fluid machine according to claim 1 , characterized in that the bend is shaped such that the pipe width in the plane including the pipe axis of the inlet pipe and the pipe axis of the supply pipe gradually decreases from the upstream portion to the bent portion and a pipe width in a plane being perpendicular to the plane including the pipe axis of the inlet pipe and the pipe axis of the supply pipe and including the pipe axis of the inlet pipe gradually increases from the upstream portion to the bent portion.3. The pipe for a driven-type fluid machine according to claim 1 , characterized in that a pipe cross-sectional area of the bend remains constant from the upstream portion to the bent portion.4. The pipe for a driven-type fluid machine according to claim 1 , ...

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30-01-2020 дата публикации

CENTRIFUGAL COMPRESSOR AND TURBO REFRIGERATOR

Номер: US20200032811A1

A suction-and-discharge flow path includes a circumferential flow path that extends in an arc shape about an axis and an external communication path that is connected to both ends of the circumferential flow path. The circumferential flow path has a uniform flow path cross-sectional area in a circumferential direction, and a convex curved surface having a convex curved surface shape is provided between an outer peripheral wall surface of the circumferential flow path and a second inner wall surface of the external communication path. In a case where, when viewed in the axis direction, a curvature radius of the convex curved surface is defined as R and a radial dimension of the circumferential flow path is defined as W, a relationship of W≤R≤3W is established. 1. A centrifugal compressor comprising:a rotary shaft which is configured to rotate around an axis;impellers which arranged to form a plurality of stages with respect to the rotary shaft in an axis direction and are configured to pressure-feed a fluid flowing in from an inlet on one side in the axis direction to an outside in a radial direction; anda casing which surrounds the rotary shaft and the impellers and has an intermediate flow path through which the fluid discharged from a preceding stage impeller of the impellers adjacent to each other is introduced into a subsequent stage impeller and a suction-and-discharge flow path which connects the intermediate flow path and an outside to each other, a circumferential flow path which extends in an arc shape about the axis in a circumferential direction of the axis and communicates with the intermediate flow path in the circumferential direction, and', 'an external communication path which is connected to both circumferential ends of the circumferential flow path and communicates with the outside,, 'wherein the suction-and-discharge flow path includes'}wherein the circumferential flow path has a uniform flow path cross-sectional area in the circumferential ...

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30-01-2020 дата публикации

Regenerative blowers-compressors with shaft bypass fluid re-vents

Номер: US20200032812A1
Автор: Joel Jack Oakman
Принадлежит: VICTORI LLC

A regenerative blower-compressor includes an impeller mounted to a drive shaft within a housing including a channel extending from an inlet adjacent to a low fluid-pressure region of the channel to an outlet adjacent to a high fluid-pressure region of the channel, the impeller extends radially outward through an annular volume within the housing from the drive shaft to blades in the channel and is configured to rotate for rotating the blades through the channel for forcing fluid through the channel from the inlet to the outlet in response to rotation of the drive shaft, the drive shaft extends from the impeller within the annular volume to into a shaft chamber within the housing configured to receive fluid from the high fluid-pressure region of the channel, and a port configured to vent fluid directly from the shaft chamber to into the low fluid-pressure region of the channel.

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30-01-2020 дата публикации

Water pump having direction adjusting mechanism

Номер: US20200032814A1
Принадлежит: Taiwan Microloops Corp

A water pump having direction adjusting mechanism includes: a first housing, formed with an accommodation space and including a first pipe member and a plurality of first fasten parts arranged at a periphery of the first housing; a stator set, including a base plate covered on the first housing, and a coil structure; a partition cover enclosing the coil structure; an impeller set disposed on the partition cover; a rotor set disposed corresponding to the coil structure; and a second housing, engaged at another side of the first housing corresponding to the base plate, and including a second pipe member and a plurality of second fasten parts disposed corresponding to the first fasten parts and arranged at a periphery of the second housing, thereby allowing relative locations of the first pipe member and the second pipe member to be adjusted.

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