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Небесная энциклопедия

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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Мониторинг СМИ

Мониторинг СМИ и социальных сетей. Сканирование интернета, новостных сайтов, специализированных контентных площадок на базе мессенджеров. Гибкие настройки фильтров и первоначальных источников.

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Форма поиска

Поддерживает ввод нескольких поисковых фраз (по одной на строку). При поиске обеспечивает поддержку морфологии русского и английского языка
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Применить Всего найдено 24370. Отображено 100.
05-01-2012 дата публикации

Centrifugal pump apparatus

Номер: US20120003108A1
Принадлежит: NTN Corp, Terumo Corp

A centrifugal blood pump apparatus includes an impeller provided in a blood chamber, first and second permanent magnets provided in one surface and the other surface of the impeller respectively, a third permanent magnet provided in an inner wall of the blood chamber, and a magnetic element and a coil for driving the impeller to rotate with a diaphragm being interposed. First and second grooves for hydrodynamic bearing different in shape and depth from each other are formed in the inner wall of the blood chamber facing the impeller, and third and fourth grooves for hydrodynamic bearing different in shape and depth from each other are formed in the diaphragm facing the impeller. The second and fourth grooves for hydrodynamic bearing generate high hydrodynamic pressure when the impeller is activated to rotate, while the first and third grooves for hydrodynamic bearing generate high hydrodynamic pressure when the impeller steadily rotates.

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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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25-04-2017 дата публикации

Рабочее колесо шламового насоса

Номер: RU0000170449U1

Полезная модель относится к гидромашиностроению и может быть использована для определения параметров рабочего колеса и переднего бронедиска центробежного шламового насоса для увеличения срока их наработки и КПД. Технический результат предлагаемой полезной модели заключается в увеличении срока службы шламового насоса за счет уменьшения гидравлических потерь и износа проточной части насоса при перекачке пульпы. Рабочее колесо шламового насоса включает задний и передний диски и размещенные между дисками лопасти, тыльные поверхности которых имеют наклон 60°÷80° к поверхности заднего диска с образованием проточного канала переменного сечения с выходным отверстием со стороны заднего диска и входным отверстием со стороны переднего диска, при этом отношение толщины каждой лопасти к ширине выпуска проточного канала составляет 0,2÷0,7, а отношение ширины проточного канала выпуска к ширине канала на входе составляет 0,3÷0,45, отношение диаметра рабочего колеса к его ширине составляет 0,3÷0,8, профили внутренних поверхностей переднего и заднего дисков выполнены изогнутыми, при этом отношение радиуса изгиба внутренней поверхности переднего диска к радиусу изгиба внутренней поверхности заднего диска составляет 0,2÷0,5. РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 170 449 U1 (51) МПК F04D 29/22 (2006.01) F04D 7/04 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ФОРМУЛА ПОЛЕЗНОЙ МОДЕЛИ К ПАТЕНТУ РОССИЙСКОЙ ФЕДЕРАЦИИ (21)(22) Заявка: 2016139670, 11.10.2016 (24) Дата начала отсчета срока действия патента: 11.10.2016 (72) Автор(ы): Шапорев Михаил Юрьевич (RU) Дата регистрации: 25.04.2017 (56) Список документов, цитированных в отчете о поиске: CN 204851763 U, 09.12.2015. RU Приоритет(ы): (22) Дата подачи заявки: 11.10.2016 Адрес для переписки: 109456, Москва, Рязанский пр-кт, 75, корп. 4, 1-я башня, 7 этаж, КГ "Вайзэдвайс", ООО "ФПБ "Гардиум", пат. пов. Купцова Е.В., рег. N 1264 1 7 0 4 4 9 R U (57) Формула полезной модели Рабочее колесо шламового насоса, ...

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06-12-2018 дата публикации

Двухступенчатое рабочее колесо центробежного насоса

Номер: RU0000185493U1

Появление новых технологических процессов и производств требует создания высокопроизводительного насосного оборудования, отвечающего требованиям современной науки и техники [3]. Центробежные насосы хорошо работают на всасывание, но имеют низкие показатели на выходе [1]. В исследовании ВГУЭС [4] в области «Влияние формы лопастей на режим работы колеса» приведены выводы: - в уравнение теоретического напора (уравнение Эйлера) не входит вес жидкости. Следовательно, развиваемый насосом напор не зависит от рода перекачиваемой жидкости; - при скорости движения газа, значительно меньшей скорости распространения звука в нем, газ ведет себя как капельная жидкость. В связи с этим уравнение Эйлера справедливо и для газов. Можно с уверенностью заявлять, что предлагаемая модель также надежно будет работать в насосах для перекачки газоконденсатов и газов. Для эффективности этих насосов вторая ступень напора должна проектироваться с учетом сжимаемости перекачивамого в нем газоконденсата или газа. При движении частицы жидкости вдоль стенки лопасти аналога векторы скоростей меняют свое направление, на что затрачивается передаваемая энергия от лопасти. В модели на участке, где лопасти имеют радиальное направление, они сохраняют свое направление, увеличивая лишь абсолютную величину. Основное уравнение турбомашин (Эйлера) связывает геометрические и кинематические характеристики рабочего колеса с развиваемым им напором [4]. H тр =U 2 2 /g, учитывая, что U 2 =π⋅D 2 ⋅n/60, где n - частота вращения, об/мин. Изменения частоты вращения с 1500 об/мин на 3000 об/мин в модели увеличит напор на выходе в 3÷4 раза по сравнению с аналогом. РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 185 493 U1 (51) МПК F04D 29/22 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ПОЛЕЗНОЙ МОДЕЛИ К ПАТЕНТУ (52) СПК F04D 29/2222 (2018.05) (21)(22) Заявка: 2017118230, 25.05.2017 (24) Дата начала отсчета срока действия патента: (73) Патентообладатель(и): Шипеленко Сергей Петрович (RU) Дата ...

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31-01-2020 дата публикации

Радиальное рабочее колесо вентилятора

Номер: RU0000195574U1

Полезная модель относится к вентиляторной технике, а именно, к радиальным рабочим колесам вентиляторов. Технический результат: повышение напорной характеристики при увеличении прочности лопаток и радиального рабочего колеса. Радиальное рабочее колесо содержит передний 1 и основной 2 диски, расположенные между ними лопатки 3. Поверхность переднего диска 1 имеет вид усеченного конуса с криволинейной образующей, лопатки 3 выполнены листовыми с передней кромкой 5 с вихреобразователем 6, выполненным, например, в виде стержня 12, и с вырезом 7 у основного диска 2. Вихреобразователь 6 соединен с основным диском 2 с образованием зазора 8 между ним, передней кромкой 5 и основным диском 2. Лопатка 3 на выходе 10 из рабочего колеса имеет наплыв 11, примыкающий к переднему диску 1. В зазоре 8 вихреобразователем 6 формируется вихревое обтекание лопатки 3, что затягивает отрыв пограничного слоя с поверхности лопатки 3 и основного диска 2, с одновременным увеличением прочности лопатки 3 и рабочего колеса. 2 з.п. ф-лы, 6 ил. РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 195 574 U1 (51) МПК F04D 29/28 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ПОЛЕЗНОЙ МОДЕЛИ К ПАТЕНТУ (52) СПК F04D 29/28 (2019.08) (21)(22) Заявка: 2019137102, 19.11.2019 (24) Дата начала отсчета срока действия патента: (73) Патентообладатель(и): Общество с ограниченной ответственностью "АЭРДИН" (RU) Дата регистрации: 31.01.2020 (45) Опубликовано: 31.01.2020 Бюл. № 4 1 9 5 5 7 4 R U (54) РАДИАЛЬНОЕ РАБОЧЕЕ КОЛЕСО ВЕНТИЛЯТОРА (57) Реферат: Полезная модель относится к вентиляторной например, в виде стержня 12, и с вырезом 7 у технике, а именно, к радиальным рабочим основного диска 2. Вихреобразователь 6 соединен колесам вентиляторов. Технический результат: с основным диском 2 с образованием зазора 8 повышение напорной характеристики при между ним, передней кромкой 5 и основным увеличении прочности лопаток и радиального диском 2. Лопатка 3 на выходе 10 из рабочего рабочего колеса. Радиальное ...

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19-01-2012 дата публикации

High-Flow-Capacity Centrifugal Hydrogen Gas Compression Systems, Methods and Components Therefor

Номер: US20120011857A1
Принадлежит: Concepts ETI Inc

Hydrogen gas compression systems that each include a multistage centrifugal compressor in which each stage has an inlet-to-outlet pressure rise ratio of about 1.20 or greater. In one embodiment, the multistage compressor includes six high-speed centrifugal compressors driven at a speed of about 60,000 rpm. The compressor has an output of more than 200,000 kg/day at a pressure of more than 1,000 psig. The compressors for the compression stages are distributed on both sides of a common gear-box, which has gearing that allows axial thrusts from the compressors to be handled effectively. Each stage's compressor has a unique impeller, which is secured to a support shaft using a tension-rod-based attachment system. In another embodiment, the multistage compressor is driven by a combustion turbine and one or more intercoolers are provided between compression stages. Each intercooler is cooled by coolant from an absorption chiller utilizing exhaust gas from the combustion turbine.

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26-01-2012 дата публикации

Diagonal fan

Номер: US20120020778A1
Автор: Gerhard Ruck
Принадлежит: ruck Ventilatoren GmbH

A diagonal fan for gaseous media has a diagonal impeller with a plurality of vanes, which are fastened on a carrier plate, and a guide device, adjoining the diagonal impeller in the axial direction on the outflow side, for increasing the pressure of the medium, with a plurality of guide vanes. The vanes of the diagonal impeller and/or the guide vanes of the guide device are three-dimensionally twisted. By means of an intake unit, the gaseous medium can be directed into the diagonal impeller. The intake unit and/or an exhaust unit, by means of which the gaseous medium can be directed out of the guide device, is, or are, provided as an exchangeable module and can be fastened on the diagonal fan by means of a fastening element.

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02-02-2012 дата публикации

Impeller and rotary machine

Номер: US20120027599A1
Автор: Jo Masutani
Принадлежит: Mitsubishi Heavy Industries Ltd

An impeller of a rotary machine, in which the direction of flow changes from an axial direction to a radial direction as it goes from the inside in the radial direction of a fluid flow passage to the outside in the radial direction thereof, includes: a hub surface constituting at least a portion of the fluid flow passage; a blade surface constituting at least a portion of the fluid flow passage; and a bulge that bulges toward the inside of the fluid flow passage at a corner where a pressure surface, which configures the blade surface, comes in contact with the hub surface in the vicinity of an inlet of the fluid flow passage.

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16-02-2012 дата публикации

Article Comprising an Impeller II

Номер: US20120039713A1
Автор: J. Michael Shifflette
Принадлежит: NuCardia Inc

An impeller for use in conjunction with a percutaneously-insertable blood pump or other rotatable equipment includes a blade that is segmented into a plurality of overlapping or abutting bladelets. In some embodiments, the bladelets are foldable and one side of each bladelet is concave.

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01-03-2012 дата публикации

Compact scroll fan assembly

Номер: US20120051904A1
Принадлежит: 3M Innovative Properties Co

A radial fan assembly for use in a powered air purifying respirator includes at least an impeller, a printed circuit board and a scroll casing. The scroll casing has a first and a second scroll casing element. The second scroll casing element includes at least a portion of the printed circuit board. When the radial fan assembly is used in a powered air purifying respirators, the respirator may also include components such as a filter assembly.

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15-03-2012 дата публикации

Shrouded thrust bearings

Номер: US20120063942A1
Принадлежит: Heartware Inc

A rotary blood pump includes a casing defining a pumping chamber. The pumping chamber has a blood inlet and a tangential blood outlet. One or more motor stators are provided outside of the pumping chamber. A rotatable impeller is within the pumping chamber and is adapted to cause blood entering the pumping chamber to move to the blood outlet. The impeller has one or more magnetic regions. The impeller is radially constrained in rotation by magnetic coupling to one or more motor stators and is axially constrained in rotation by one or more hydrodynamic thrust bearing surfaces on the impeller.

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12-04-2012 дата публикации

Grinder pump basin system

Номер: US20120085688A1
Принадлежит: Zoeller Pump Co LLC

A grinder pump basin system is provided which includes a basin; a cover plate; a bracket secured to the cover plate; and a grinder pump with cutter plate with openings and a cutter blade secured to the bracket above a bottom surface of the basin. The bracket includes a front portion, which prevents waste water from interacting adversely with the grinder pump when it enters the basin. A discharge system for the grinder pump is secured to an outlet of the grinder pump and includes a discharge pipe and a flexible discharge coupling. Flow directional jets are also provided in an elbow of the pump discharge system to direct waste water and solids away from the grinder pump.

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10-05-2012 дата публикации

Screw-Type Centrifugal Pump with Cutting Inserts

Номер: US20120114462A1
Принадлежит: Vaughan Co Inc

A screw-type centrifugal pump with scissoring back cutters and having a housing with an intake opening and an outlet opening, both in fluid communication with an internal chamber, and an impeller assembly positioned within the chamber, is disclosed. Generally speaking, the impeller assembly has a hub having a back shroud and being attached to a rotatable pump shaft, with an impeller attached to the hub. An insert cutter positioned on a surface of the hub shroud opposite the impeller includes a cutting edge configured for shearing operation, while a stationary back plate having a surface adjacent to and facing the hub shroud includes a cutting rib having a cutting edge configured for shearing operation. The insert cutter and cutting rib work jointly to create a cutting action as the hub rotates in the chamber.

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28-06-2012 дата публикации

Axial gas thrust bearing for rotors in rotating machinery

Номер: US20120163742A1
Принадлежит: STATOIL ASA

An axial gas thrust bearing for rotors in rotating machinery includes at least one radial disk, integral with or fastened to the rotor and one fixed seal facing each disk or two fixed seals positioned to surround each disk, lower portions of the seals being situated at a distance from the rotor to allow the inflow of compressed fluid passing in the gap between the respective disk and seals, thereby combining the properties of a balance piston and thrust bearing disk.

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09-08-2012 дата публикации

Rotor for a turbomachine

Номер: US20120201682A1
Принадлежит: Dyson Technology Ltd

A rotor that includes an impeller secured to a shaft. The impeller has a bore and a counterbore. The shaft forms an interference fit with the bore and is adhered to the counterbore. A method of manufacturing the rotor is also described.

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04-10-2012 дата публикации

Impeller and centrifugal fan

Номер: US20120251321A1
Автор: Manabu FUCHIBE
Принадлежит: Minebea Motor Manufacturing Corp

Herein disclosed are an impeller and a centrifugal fan having the same. The impeller includes a cup-shaped metallic hub having a cylindrical portion. The hub includes a flange extending outwardly from an edge of the cup, a plurality of resin vanes disposed above an outer portion of the flange and coaxially with the cylindrical portion, and an annular part made of resin supporting the plurality of resin vanes thereon and holding the outer portion of the flange embedded therein.

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18-10-2012 дата публикации

Cross flow fan, air blower and air conditioner

Номер: US20120263573A1
Принадлежит: Mitsubishi Electric Corp

There is provided a cross flow fan that makes uniform a distribution of wind velocity along an axial direction of the fan at an exit of an air trunk and that lessens chance of separation of an air flow on an inlet side of the fan, and there are thereby provided a cross flow fan that accomplishes a lower input and smaller noise and an air blower and an air conditioner that use the cross flow fan. A cross flow fan being rotatably placed in a horizontally-long air trunk, and including a plurality of annular rings that are substantially parallel to each other and a plurality of blades that are radially interposed between adjacent rings, each having a circular arc cross sectional shape, and a camber angle of the blade is smaller at the ring side than at a center area of the blade between the rings in a longitudinal direction.

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18-10-2012 дата публикации

Impeller and turbomachinery including the impeller

Номер: US20120263599A1
Принадлежит: Hitachi Plant Technologies Ltd

An impeller includes a hub plate and a plurality of blades circumferentially disposed at intervals on one surface side of the hub plate. Each blade has a shape formed by piling up a plurality of blade sections in a blade height-wise direction of each blade in a reference impeller in which the hub plate intersects with the blades and which includes a linear element blade in the blade height-wise direction so as to form a curvilinear element blade. In piling up the blade sections, amounts of tangential lean and sweep to be applied to the blade sections are increased as it goes from an end face of at least one of a hub plate side end and a counter hub plate side end toward a span intermediate part of the blade.

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08-11-2012 дата публикации

Pump Impeller

Номер: US20120282085A1
Принадлежит: Sulzer Pump Solutions Ireland Ltd

The present invention provides a pump impeller which has improved anti clogging characteristics, in particular through the use of an impeller vane having a specially profiled leading edge which, during operation of the impeller, forces rags or the like down along the leading edge, which increases in thickness along the length thereof, until the rags become re-entrained in the fluid and thus exit the impeller avoiding the clogging thereof.

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15-11-2012 дата публикации

Rotor with asymmetric blade spacing

Номер: US20120288373A1
Принадлежит: Hamilton Sundstrand Corp

A turbine apparatus comprises a rotor with a hub section defined about a rotational axis and a plurality of blades attached to the hub section. The plurality of blades comprises a first group having a first angular spacing in a first circumferential sector of the rotor, and a second group having a second angular spacing in a second circumferential sector of the rotor. The first angular spacing is different from the second angular spacing, and the rotor blades are asymmetric about the rotational axis.

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20-12-2012 дата публикации

Wheel and replaceable nose piece

Номер: US20120321458A1
Принадлежит: Honeywell International Inc

An assembly includes a nose piece and a boreless compressor wheel having a nose end configured for receipt of the nose piece and a receptacle at a base end configured for receipt of a rotatable shaft. A method includes fitting a nose piece to a boreless compressor wheel, measuring unbalance and, based in part on the measuring, removing material from the nose piece. Various other examples of devices, assemblies, systems, methods, etc., are also disclosed.

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27-12-2012 дата публикации

Impeller of centrifugal compressor

Номер: US20120328444A1
Принадлежит: Mitsubishi Heavy Industries Ltd

Interference of a leakage vortex flow generated at the tip end side of the full blade with the leading edge of the splitter blade is avoided and high pressure ratio and enhanced efficiency can be achieved. A throat of am impeller is formed so that a distance from a leading edge of a rear side full blade on the rear side of the rotation direction of the compressor to a front side full blade adjacent to the rear side full blade is minimized, and the leading edge of the splitter blade is placed in a fluid flow streaming along the flow passage between the mutually adjacent full blades, on the downstream side of a leakage vortex line formed to connect the middle location of the throat to the leading edge of the front side full blade.

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21-02-2013 дата публикации

Segmented fan assembly

Номер: US20130045120A1
Принадлежит: General Electric Co

Systems and devices for thermodynamically regulating portions of a dynamoelectric machine are disclosed. In one embodiment, a fan assembly element includes: an axially inner shroud segment configured to form a portion of an annular assembly about a rotor of a dynamoelectric machine, wherein the axially inner shroud segment includes a rotor hub interface configured to physically connect to a complementary portion of a rotor hub; a set of fan blades physically connected to and extending axially from a face of the axially inner shroud segment; and an axially outer shroud segment physically connected to the set of fan blades.

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28-03-2013 дата публикации

ELECTRICAL MACHINE HAVING A FAN WHEEL

Номер: US20130078102A1
Автор: Dikmenli Erdogan
Принадлежит: ROBERT BOSCH GMBH

The invention relates to an electrical machine having a fan wheel which comprises an injection-moulded blade carrier ring with fan blades as well as an annular insertion part which is integrated into the blade carrier ring and which comprises passage openings via which the blade carrier ring is connected to the fan blades. 14528524. An electrical machine having a fan impeller , having at least one injection-molded blade support ring having fan blades () and an annular insert part () which is integrated in the blade support ring () , characterized in that passage openings () are made in the insert part () , the blade support ring () being connected to the fan blades () via said passage openings.252. The electrical machine as claimed in claim 1 , characterized in that a smallest inside radius (r) of the insert part () is smaller than a smallest inside radius (r) of the blade support ring ().345. The electrical machine as claimed in claim 1 , characterized in that the fan blades () each have a radial extent and rest on an end face of the insert part () over the entire radial extent.4542. The electrical machine as claimed in claim 1 , characterized in that a surface of an end face of the insert part () which is situated opposite the fan blades () is covered by material of the blade support ring ().525. The electrical machine as claimed in claim 1 , characterized in that the blade support ring () surrounds a radially outer circumferential face of the insert part ().6592. The electrical machine as claimed in claim 1 , characterized in that a radially outer circumferential face of the insert part () is provided with an interlocking geometry in the form of radial indentations () or projections claim 1 , and the interlocking geometry is covered by the blade support ring ().79. The electrical machine as claimed in claim 6 , characterized in that the indentations () are in the form of triangular notches.848. The electrical machine as claimed in claim 1 , characterized in that ...

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11-04-2013 дата публикации

Blade structure for centrifugal fan

Номер: US20130089425A1
Автор: Chun-Ming Wu
Принадлежит: Individual

A blade structure for centrifugal fan includes a hub, a first blade unit, and a second blade unit. The hub includes at least one connection section, to a radially outer end of which an annular body is connected. The annular body has a first side and an opposite second side; and the first and the second blade unit are arranged on and spaced along the first and the second side of the annular body, respectively. By providing the first and the second blade unit around the hub of a centrifugal fan, the air flows and pressure produced by the centrifugal fan can be largely increased at effectively reduced noise.

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18-04-2013 дата публикации

COMPRESSOR UNIT

Номер: US20130094950A1
Автор: Bode Ralf, Lang Sebastian
Принадлежит:

A compressor unit includes a motor and a compressor in a casing of a gastight form. The casing houses the motor and the compressor. The motor includes a rotor surrounded by a stator which has an encapsulation formed on the inner diameter as a separating can, so that a medium being handled does not damage the stator. The separating can includes a polymer matrix which is reinforced using a plurality of fibers. The polymer matrix is at least partly a ceramic fiber reinforced polymer matrix. The plurality of fibers are formed as continuous filaments. The continuous filaments include the length of at least 30 mm. 1. A compressor unit , comprising:a motor and a compressor in a casing of a gastight form,wherein the casing houses the motor and the compressor, a stator,', 'a rotor surrounded by the stator, and', a polymer matrix which is reinforced using a plurality of fibers,', 'wherein the polymer matrix is at least partly a ceramic fiber reinforced polymer matrix,', 'wherein the plurality of fibers are formed as continuous filaments, and', 'wherein the continuous filaments include the length of at least 30 mm., 'a separating can which forms an encapsulation on an inner diameter of the stator so that a medium being handled by the compressor unit does not damage the stator, the separating can comprising], 'wherein the motor comprises2. The compressor unit as claimed in claim 1 , wherein the plurality of fibers comprise silicon carbide.3. The compressor unit as claimed in claim 1 , wherein the plurality of fibers comprise aluminum oxide.4. The compressor unit as claimed in claim 1 , wherein the plurality of fibers comprise zirconium dioxide.5. The compressor unit as claimed in claim 1 , wherein a surface of the separating can is interspersed with a plurality of ceramic particles.6. The compressor unit as claimed in claim 3 , wherein the surface of the separating can is interspersed with a plurality of ceramic particles. This application is a continuation of the US patent ...

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18-04-2013 дата публикации

PUMP AND METHOD FOR MIXED FLOW BLOOD PUMPING

Номер: US20130096364A1
Принадлежит:

A blood pump includes a hub having an axis of rotation and a generally cylindrical shape. The hub has an upstream end region, a central region, and a downstream end region, and the hub includes a magnetic material. Blades that are disposed on the downstream end region of the hub extend downstream of the hub. 1. A blood pump comprising:a hub having an axis of rotation and a generally cylindrical shape, the hub having an upstream end region, a central region, and a downstream end region, the hub including a magnetic material; and an upstream portion that is located proximate the hub and is configured to add energy to fluid having forward flow along the axis of the hub, and', 'a downstream portion that is configured to add energy to the fluid having forward flow in a direction radially outward from the hub., 'blades located at the downstream end region of the hub, the blades extending downstream of the hub, each blade including'}2. The blood pump of claim 1 , wherein the downstream portions of the blades extend radially outward from the hub.3. The blood pump of claim 1 , wherein the blood pump includes a housing claim 1 , and the hub is suspended within the housing by fore and aft bearings.4. The blood pump of claim 1 , wherein the central region and the upstream end region are devoid of blades.5. The blood pump of claim 1 , further comprising:a housing defining an inlet, an outlet, and a flow path from the inlet to the outlet; anda motor stator disposed within the housing.6. The blood pump of claim 5 , further comprising stator blades disposed within the flow path proximate the upstream end region of the hub claim 5 , the stator blades being coupled to an upstream bearing component for supporting the upstream end region of the hub.7. The blood pump of claim 5 , further comprising a downstream bearing component for supporting the downstream end region of the hub claim 5 , the downstream bearing component being located proximate the downstream end region of the hub and ...

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02-05-2013 дата публикации

PROPELLER FAN AND MANUFACTURING METHOD THEREOF

Номер: US20130108461A1
Автор: Yoshida Shunzen
Принадлежит: FUJITSU GENERAL LIMITED

A propeller fan molded by injection molding using a resin material containing a continuous fiber, includes a hub having an end surface wall and a peripheral wall; and a plurality of blades on an outer periphery of the hub, the propeller fan being molded by providing a plurality of injection positions for injecting the resin material containing the continuous fiber in a part of the end surface wall corresponding to a root portion of one of the blades of the hub. 1. A propeller fan molded by injection molding using a resin material containing a continuous fiber , comprising:a hub having an end surface wall and a peripheral wall; anda plurality of blades on an outer periphery of the hub,wherein the propeller fan is molded by providing a plurality of injection positions for injecting the resin material containing the continuous fiber in a part of the end surface wall corresponding to a root portion of one of the blades of the hub.2. The propeller fan according to claim 1 , wherein the plurality of injection positions is provided so that a flow direction of the resin material containing the continuous fiber in the root portion of the one blade of the hub is regulated by the flow of the resin material from the injection positions adjacent to each other claim 1 , and is in a direction perpendicular to a width direction of the root portion of the blade.3. The propeller fan according to claim 1 , wherein the plurality of injection positions is dispersed and placed in a circumferential direction around a rotation center of the propeller fan.4. The propeller fan according to claim 1 , wherein the plurality of injection positions is dispersed and placed on the same circumference around the rotation center of the propeller fan.5. A method of manufacturing a propeller fan comprising:molding the propeller fan including a hub having an end surface wall and a peripheral wall, and a plurality of blades on an outer periphery of the hub, using a metal mold including a cavity and a ...

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09-05-2013 дата публикации

Impeller vane with leading edge enhancement

Номер: US20130115047A1
Принадлежит: Baker Hughes Inc

A centrifugal pumping system having a stack of impellers and diffusers for pressurizing fluid. The impellers are rotated by a motor for pressurizing and lifting fluid from within a wellbore. Undulating profiles are provided on leading edges of the impellers for inducing turbulence in the fluid being pumped. Increasing turbulence better homogenizes the fluid, so that choked flow is avoided when different density components are present in the fluid. Reducing the possibility of choked flow increases pump efficiency and lift capacity.

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09-05-2013 дата публикации

Compressor wheel shaft with recessed portion

Номер: US20130115088A1
Принадлежит: Honeywell International Inc

A turbocharger assembly includes a compressor wheel with a base surface, a nose surface, a z-plane disposed between the base surface and the nose surface and a bore extending from the base surface to the nose surface and a shaft that includes a first pilot surface disposed in the bore of the compressor wheel at a position between the z-plane and the nose surface, a second pilot surface disposed in the bore of the compressor wheel at a position between the z-plane and the base surface, and a recessed surface disposed between the first pilot surface and the second pilot surface. A nut adjustably disposed on the shaft adjacent to the nose surface can tension the shaft to apply a compressive load between the base surface and the nose surface of the compressor wheel. Various other examples of devices, assemblies, systems, methods, etc., are also disclosed.

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16-05-2013 дата публикации

Fluid Movement System and Method for Determining Impeller Blade Angles for Use Therewith

Номер: US20130121804A1
Автор: Kerry N. Oliphant
Принадлежит: Concepts ETI Inc

A fluid movement system that includes an impeller having a blade with a leading edge blade tip angle determined as a function of an increase in mass flow rate due to reinjection of flow from a flow stability device located proximate to the leading edge tip of the blade. In an exemplary method, the leading edge blade tip angle can be determined based on selecting a blade incidence level based on a mass flow gain versus flow coefficient curve. Blade leading edge tip angles determined in accordance with a method of the present invention are typically greater than blade leading edge tip angles determined using traditional methods. The greater blade leading edge tip angles can lead to more robust blades designs.

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16-05-2013 дата публикации

CENTRIFUGAL CHOPPER PUMP

Номер: US20130121811A1
Принадлежит:

A chopper pump is provided with a motor having a drive shaft and a casing connected to the motor and defining a bowl with an inlet for receiving waste material. A cover plate assembly is secured about the inlet. The cover plate assembly having a base with a central opening and a plurality of serrations formed into the base and spaced about the central opening, each serration being formed into a curved pocket and longitudinally tapered to form an edge on an inner surface of the base. The chopper pump also includes a cutter having a hub that is connected to the drive shaft. The cutter extends through the central opening of the base and includes at least two blades extending radially outward to guide waste material toward the plurality of serrations. 1. A chopper pump comprising:a motor having a drive shaft;a casing connected to the motor and defining a bowl with an inlet for receiving waste material;a cover plate assembly secured about the inlet, the cover plate assembly having a base with a central opening, and a plurality of serrations formed into the base and spaced about the central opening, each serration being formed into a curved pocket and longitudinally tapered to form an edge on an inner surface of the base; anda cutter connected to the drive shaft and extending through the central opening of the base, the cutter having at least two blades extending radially outward to guide waste material toward the plurality of serrations.2. The chopper pump of wherein each curved pocket is angled forward relative to a direction of rotation of the drive shaft to form a point on a leading edge of each serration.3. The chopper pump of further comprising:an impeller disposed within the bowl and connected to the drive shaft, the impeller having at least two vanes extending radially outward for converting motor torque into a centrifugal force;a wall extending transversely from an outer edge of the base;at least two mounting blocks extending radially inward from the wall; anda ...

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23-05-2013 дата публикации

Expandable impeller pump

Номер: US20130129503A1
Принадлежит: PENN STATE RESEARCH FOUNDATION, Thoratec LLC

An impeller includes a hub, and a plurality of blades supported by the hub, the blades being arranged in at least two blade rows. The impeller has a deployed configuration in which the blades extend away from the hub, and a stored configuration in which at least one of the blades is radially compressed, for example by folding the blade towards the hub. The impeller may also have an operational configuration in which at least some of the blades are deformed from the deployed configuration upon rotation of the impeller when in the deployed configuration. The outer edge of one or more blades may have a winglet, and the base of the blades may have an associated indentation to facilitate folding of the blades.

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23-05-2013 дата публикации

Blower

Номер: US20130129545A1
Принадлежит: Panasonic Corp

A blower includes a motor, a fan, a casing, a control circuit, a roll pin, and a boss portion, and an end face of the boss portion at one side inserted to the shaft is provided with a groove having an opening and an bottom part to engaged with the roll pin, side walls of the groove are slanted to widen from a bottom part to the opening, the side walls have straight portions formed to confront each other in parallel to a longitudinal direction of the shaft and extending toward the opening from a start point corresponding to a central axis of the roll pin, and a distance between the confronting straight portions is equal to a diameter of the roll pin.

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27-06-2013 дата публикации

IMPELLER

Номер: US20130164136A1
Автор: VESTERGAARD BOLL Jens
Принадлежит: Grundfos Holding A/S

An impeller () for a centrifugal pump includes a first shroud having a plurality of blades (). A second shroud is joined onto the first shroud by way of welding. Each blade () has an apex region (), at which the blade contacts the second shroud. At least one of the blades () in a first section () of the apex region () has a weld connection to the second shroud, and in at least one second section () of the apex region () is free of a weld connection. 12. An impeller () for a centrifugal pump , the impeller comprising:{'b': '8', 'a first shroud having a plurality of blades (); and'}a second shroud joined onto the first shroud by way of welding,{'b': 8', '12, 'wherein each blade () has an apex region () where the blade contacts the second shroud, and'}{'b': 8', '20', '12', '14', '12, 'wherein at least one of the blades () in a first section () of the apex region () has a weld connection to the second shroud, and in at least one second section () of the apex region () is free of a weld connection.'}221216. The impeller () according to claim 1 , wherein the apex region () comprises a third section () which is free of a weld connection.322012141612. The impeller () according to claim 2 , wherein the first section () of the apex region () extends over a length (d) which is larger than a total length of the second section () and the third section () of the apex region ().42201214121612. The impeller () according to claim 2 , wherein the first section () is arranged in a middle of the apex region () claim 2 , the second section () on an outer edge region of the apex region () and the third section () on an inner edge region of the apex region ().52141212. The impeller () according to claim 1 , wherein the second section () extends over a length (d) of the apex region () which makes up 5% to 10% of a total length of the apex region ().62161212. The impeller () according to claim 2 , wherein the third section () extends over a length (d) of the apex region () which makes up 10 ...

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11-07-2013 дата публикации

CROSS FLOW FAN AND AIR-CONDITIONING APPARATUS INCLUDING SAME

Номер: US20130177395A1
Принадлежит: Mitsubishi Electric Corporation

A cross flow fan including an impeller having at least two rings arranged with intervals in a fan rotation axis O direction and a plurality of blades that are arranged, between correlated rings, with intervals in a circumferential direction of the rings, in which the blade is divided into plural areas in the fan rotation axis O direction, and both ends adjacent to the rings are denoted as the blade-ring proximate sections and the center portion of the blade is denoted as the inter-blade-ring center section. The blade is formed such that the thickness of the inner peripheral blade end of the blade that is the inner peripheral end of the impeller is smaller in the inter-blade-ring center section than in the blade-ring proximate section. 111-. (canceled)12. A cross flow fan , comprising: at least two support plates arranged with intervals in a rotation axis direction, and', 'a plurality of blades arranged between correlated support plates, the blades being arranged with intervals in a circumferential direction of the support plates, wherein, 'an impeller including,'}each blade between the support plates is divided into a plurality of areas in the rotation axis direction such that both ends adjacent to the support plates are a first area and a center portion of the blade is a second area,a thickness of the blade in the second area is formed so as to become gradually thinner to an inner peripheral blade end that is an end of the blade on an inner-circumferential side of the impeller, andthe thickness of the inner peripheral blade end is formed such that the second area is smaller in thickness than the first area.13. The cross flow fan of claim 12 , wherein the thickness of the blade in the first area is formed so as to become gradually thicker from an outer peripheral blade end that is an end of the blade on an outer-circumferential side of the impeller to the inner peripheral blade end.14. The cross flow fan of claim 12 , wherein claim 12 ,after the thickness of the ...

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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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22-08-2013 дата публикации

RADIAL IMPELLER WITH A RADIALLY FREE BASIC RIM

Номер: US20130216393A1
Принадлежит: Thermodyn

The invention provides an impeller designed to be mounted on a rotary shaft. The impeller comprises a basic rim provided with blades protruding on one surface of the basic rim, and a hub capable of being coupled to the basic rim and to the rotary shaft. In certain embodiments, the impeller comprises an annular plate and the hub, the plate and the basic rim are configured to interact together so as to hold the basic rim axially and to maintain a freedom of radial deformation of the basic rim relative to the hub and to the plate. 1. An impeller designed to be mounted on a rotary shaft comprising a basic rim provided with blades protruding on one face of the basic rim , and an annular hub capable of being coupled to the basic rim and to the rotary shaft , characterized in that it comprises an annular plate and in that the hub , the plate and the basic rim are configured to interact together so as to hold the basic rim axially and to maintain a freedom of radial deformation of the basic rim relative to the hub and to the plate.2. The impeller according to claim 1 , in which the basic rim comprises a circular key on its inner perimeter capable of interacting with a first notch (made in the hub and a second notch made in the plate claim 1 , the first and the second notch being placed opposite one another so that the circular key of the basic rim is held in the notches when the hub claim 1 , the plate and the basic rim are assembled.3. The impeller according to claim 2 , in which the circular key comprises two outer O-rings respectively placed on either side of the basic rim on the outer radial surface of the circular key claim 2 , and two inner O-rings respectively placed on either side of the basic rim on the inner radial surface of the circular key.4. The impeller according to claim 2 , comprising radial guiding means capable of limiting the friction between the basic rim and the hub claim 2 , and between the basic rim and the plate during the radial deformation of the ...

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12-09-2013 дата публикации

Centrifugal fan

Номер: US20130236303A1
Принадлежит: Nidec Corp

A centrifugal fan may include an impeller arranged to rotate about a rotation axis, an impeller case arranged to accommodate the impeller, a motor arranged to rotate the impeller, and a motor case arranged to accommodate the motor. The impeller may include a boss portion joined to a shaft arranged to rotate about the rotation axis, a hub arranged to extend radially outward from the boss portion, and a plurality of blades. Each blade may be arranged to extend radially outward. An inner wall of the impeller case may include an inside surface extending radially outward along an upper end portion of each blade. A side end portion of an air inlet defined in a central portion of the impeller case may include a curved surface projecting radially inward.

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12-09-2013 дата публикации

Catheter device

Номер: US20130237744A1
Принадлежит: AIS GMBH AACHEN INNOVATIVE SOLUTIONS

The catheter device comprises a drive shaft connected to a motor, and a rotor mounted on the drive shaft at the distal end section. The rotor has a frame structure which is formed by a screw-like boundary frame and rotor struts extending radially inwards from the boundary frame. The rotor struts are fastened to the drive shaft by their ends opposite the boundary frame. Between the boundary frame and the drive shaft extends an elastic covering. The frame structure is made of an elastic material such that, after forced compression, the rotor unfolds automatically.

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19-09-2013 дата публикации

COUPLING, ROTOR, AND ASSEMBLY FOR A PUMP

Номер: US20130243516A1
Автор: Walder Marcel
Принадлежит: Ixetic Hueckeswagen GmbH

A coupling for pump, in particular a vacuum pump. The coupling has at least one feed for lubricant. 110-. (canceled)11. A coupling for a pump comprising:a feed for lubricant.12. The coupling as recited in wherein the lubricant feed is disposed in a rotor-coupling region for a coupling element of a rotor of the pump.13. The coupling as recited in wherein the lubricant feed includes a lubricating groove in a rotor-side end face of the coupling.14. The coupling as recited in wherein the lubricating groove opens into a depression of the rotor-coupling region.15. The coupling as recited in wherein the lubricating groove opens into an indentation formed on an inner side of a pot wall of a pot-like receiving body.16. The coupling as recited in wherein two lubricating grooves are disposed diametrically in the rotor-side end face of the coupling.17. The coupling as recited in wherein the coupling is a sintered part. The present invention relates to a coupling, a rotor, and an assembly for pump, in particular a vacuum pump.A coupling for a pump, in particular a vacuum pump, having a rotor-coupling region for a coupling element of the rotor and a drive-coupling region for a coupling element of the drive is known from International Publication WO 2010/043191 A1.It is an object of the present invention to prolong the lifetime of a pump, in particular a vacuum pump having a coupling and/or a rotor.In a coupling for a pump, in particular a vacuum pump, the above object is achieved by providing the coupling with at least one feed means for lubricant. Oil or oil mist, for example, can be fed through the lubricant feed means to the coupling for lubrication purposes. This makes it possible to minimize wear during the operation of the coupling, and to meet endurance requirements.In a preferred exemplary embodiment of the coupling, the lubricant feed means is disposed in a rotor-coupling region for a coupling element of the rotor. Alternatively or additionally, the or a further ...

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03-10-2013 дата публикации

Cross flow fan and indoor unit of air-conditioning apparatus

Номер: US20130259669A1
Принадлежит: Mitsubishi Electric Corp

An impeller element includes a plurality of blades disposed along an outer circumference of a circular support plate. Each blade is divided into a plurality of blade sections in a rotational axis direction. At least one of the divided blade sections as a long-chord blade section is configured such that a chord as a line segment connecting a blade outer-circumferential edge and a blade inner-circumferential edge of the blade in a cross section perpendicular to a rotational axis of the blade has a greater length than a chord of another one of the blade sections as a short-chord blade section. The blade inner-circumferential edge of the at least one long-chord blade section having the longer chord protrudes toward the inner circumferential side, relative to the blade inner-circumferential edge of the at least other one of the blade sections as the short-chord blade section having the shorter chord.

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03-10-2013 дата публикации

FAN WITH METALLIC HUB AND PLASTIC IMPELLER AND METHOD FOR MANUFACTURING SUCH FAN

Номер: US20130259692A1
Автор: CHEN WEN-CHENG
Принадлежит: Foxconn Technology Co., Ltd.

An exemplary fan includes a hub and an impeller. The hub is made of metal, and includes a flange. The impeller is made of plastic. The impeller is formed around the hub and has the flange embedded therein. A method for manufacturing the fan is also provided. 1. A fan , comprising:a hub made of metal, the hub comprising a flange; andan impeller made of plastic, the impeller being an injection molded body formed around the hub and having the flange embedded therein.2. The fan of claim 1 , wherein the hub further comprises a top wall and a cylindrical wall extending axially and downwardly from a periphery of the top wall.3. The fan of claim 2 , wherein the flange extends radially and outwards from a bottom edge of the cylindrical wall.4. The fan of claim 1 , wherein the impeller comprises a blade ring and a plurality of blades extending outwards from an outer circumferential surface of the blade ring claim 1 , and the plurality of blades are spaced from each other.5. The fan of claim 4 , wherein the impeller further comprises an outer ring interconnecting outer free ends of the blades.6. The fan of claim 1 , wherein a plurality of slots are defined in the flange of the hub claim 1 , and the slots are filled with plastic material comprised in the impeller.7. The fan of claim 6 , wherein the plurality of slots is five slots evenly arranged along a circumferential direction of the flange.8. The fan of claim 6 , wherein the blade ring comprises an upper portion and a lower portion claim 6 , with the flange embedded in the blade ring between the upper portion and lower portion.9. The fan of claim 8 , wherein the blade ring further comprises a plurality of connecting portions in the slots claim 8 , respectively claim 8 , the connecting portions comprise the plastic material filled in the slots claim 8 , and the connecting portions interconnect the upper portion and the lower portion claim 8 , with the upper portion claim 8 , the connecting portions and the lower portion ...

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03-10-2013 дата публикации

Rotary pump with a vane provided in each pump outlet

Номер: US20130259730A1
Автор: Albert W. Patterson
Принадлежит: Individual

A pump housing has a cylindrical interior surface having outlets and a pair of side surfaces defining, in combination with the interior surface, a substantially cylindrical chamber. The surfaces have inlets. A rotor has a void, lobes and, for each lobe, a throughpassage. The rotor is positioned in the chamber such that the void communicates with the inlet to receive fluid and the throughpassage for each lobe provides communication between the void and chamber. The rotor is rotatably mounted in the chamber such that the lobes traverse the cylindrical surface. Provided for each outlet is a vane. As the rotor turns, the rotor outer surface is traversed by the vane to create, as the vane traverses a throughpassage, a chamber ahead of the vane which increases in volume and communicates with the throughpassage, and a chamber behind the vane which decreases in volume and communicates with the outlet port.

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10-10-2013 дата публикации

CENTRIFUGAL COMPRESSOR

Номер: US20130266450A1
Автор: Hoshi Toru, Tomita Isao
Принадлежит: MITSUBISHI HEAVY INDUSTRIES, LTD.

Provided is a centrifugal compressor including a first splitter blade arranged nearer to a suction side Sb of a full blade F located upstream in a rotating direction of the compressor, and a second splitter blade provided farther from the suction side Sb of the full blade F and being shorter than the first splitter blade . Leading edges and on the shroud side of the first splitter blade and the second splitter blade are offset from positions dividing the space between the full blades at equal intervals by the number of splitter blades therebetween toward the suction side Sb of the full blade. 16-. (canceled)7. A centrifugal compressor impeller , comprising:a plurality of full blades that stand equally spaced in a circumferential direction and extend from a fluid inlet part to a fluid outlet part on a surface of a hub; andtwo or more splitter blades each provided to extend from a point in a flow passage formed between the full blades arranged adjacent to each other, to the outlet part,the compressor further comprising:a first splitter blade provided on a side nearer to a suction side of a full blade located upstream in a rotating direction of the compressor and having a length in a flow passage direction shorter than that of the upstream side full blade; anda second splitter blade provided on a suction side of the first splitter blade and having a length in the flow passage direction shorter than that of the first splitter blade, whereinleading edge portions on a shroud side of the first splitter blade and the second splitter blade are offset from positions dividing a space between the full blades at equal intervals by the number of splitter blades therebetween toward the suction side of the full blade.8. The centrifugal compressor according to claim 7 , wherein an offset amount of the second splitter blade toward the suction side of the full blade is larger than an offset amount of the first splitter blade toward the suction side of the full blade.9. The centrifugal ...

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17-10-2013 дата публикации

IMPELLER AND METHOD OF MANUFACTURING THE SAME

Номер: US20130272883A1
Автор: Kim Jin-Hyoung, PAENG Ki
Принадлежит: SAMSUNG TECHWIN CO., LTD.

Provided is a method of manufacturing an impeller, the method including: providing a disc comprising a plurality of blades; casting a shroud to a first state in a mold; providing a mounting space in the mold; mounting the disc in the mounting space and casting the shroud to a second state with the mounted disc. 1. A method of manufacturing an impeller , the method comprising:providing a disc comprising a plurality of blades;casting a shroud to a first state in a mold;providing a mounting space in the mold;mounting the disc in the mounting space; andcasting the shroud to a second state with the mounted disc.2. The method of claim 1 , wherein the first state is a semi-solid state and the second state is a completely solidified state.3. The method of claim 2 , wherein the plurality of blades and the shroud are coupled to each other after casting of the shroud to the second state.4. The method of claim 3 , wherein the casting of the shroud to the second state comprises cooling the shroud to the completely solidified state.5. The method of claim 1 , wherein the mold comprises an outer cast and a center cast that form a space corresponding to a shape of the shroud claim 1 ,wherein the casting of the shroud to the first state comprises:injecting a melted metal into the space; andcooling the melted metal to a semi-solid state.6. The method of claim 5 , wherein the providing of the mounting space comprises preparing the mounting space of the disc by removing the center cast.7. The method of claim 6 , further comprising removing the outer cast.8. The method of claim 1 , further comprising polishing a surface of the shroud.9. The method of claim 1 , wherein the providing of the disc comprises filling a filling material between the plurality of blades.10. The method of claim 9 , wherein the filling material comprises molding sand.11. The method of claim 10 , further comprising removing the molding sand by beating and breaking the molding sand.12. The method of claim 9 , wherein ...

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17-10-2013 дата публикации

IMPELLER, ROTOR COMPRISING SAME, AND IMPELLER MANUFACTURING METHOD

Номер: US20130272895A1
Принадлежит:

An impeller is formed of two parts, i.e., an inner peripheral side part and an outer peripheral side part. The inner peripheral side part is molded in a cylindrical shape. The outer peripheral side part is formed by integrally molding an annular disc externally fitted to an outer peripheral surface of the inner peripheral side part, a plurality of blades provided at an interval in a circumferential direction on a surface that faces the other side in the axis line direction of the annular disc and forming al flow path extending in a radial direction, and a cover covering the plurality of blades from the other side in the axis line direction and having an insertion hole to which the inner peripheral side part is inserted in the axis line direction at an interval in a radial direction. 1. An impeller comprisingan inner peripheral side part, andan outer peripheral side part, whereinthe inner peripheral side part is in a cylindrical shape around an axis line, and an annular disc externally fitted to a portion at one side in the axis line direction in an outer peripheral surface of the inner peripheral side part;', 'a plurality of blades that are provided at intervals in a circumferential direction on a surface that faces the other side in the axis line direction of the annular disc and form a flow path extending in a radial direction; and', 'a cover that covers the plurality of blades from the other side in the axis line direction and has an insertion hole into which the inner peripheral side part is inserted in the axis line direction at an interval in a radial direction, and, 'the outer peripheral side part includesthe outer peripheral side part is configured by which the annular disc, the blades and the cover are integrally molded.2. The impeller according to claim 1 , whereinthe annular disc is externally fitted to the inner peripheral side part through shrink fitting.3. The impeller according to claim 2 , wherein:an edge portion rising in a cylindrical shape from an ...

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24-10-2013 дата публикации

Axially-split radial turbine

Номер: US20130280036A1
Принадлежит: Honeywell International Inc

An axially-split radial turbine includes a forward rotor section and an aft rotor section being mechanically and abuttingly coupled to one another along an annular interface that resides within a plane generally orthogonal to a rotational axis of the axially-split radial turbine. The axially-split radial turbine can be provided as part of a gas turbine engine.

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24-10-2013 дата публикации

Fan impeller structure and manufacturing method thereof

Номер: US20130280086A1
Автор: Chu-hsien Chou
Принадлежит: Individual

A fan impeller structure and a manufacturing method thereof. The fan impeller structure includes a base seat, multiple blades and a ring member. Each blade has a main body made of plastic material and at least one fixing member made of metal material. The base seat and the ring member are made of metal material. The base seat and the ring member are respectively disposed on two sides of the blades. By means of the manufacturing method, the blades can be diversified and the universality of the blades is greatly increased to lower the manufacturing cost.

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24-10-2013 дата публикации

FAN DEVICE

Номер: US20130280090A1
Автор: KAWAI Yoichi, SATO Sumio
Принадлежит: MINEBEA CO., LTD.

A structure that rigidly connects a shaft and a hub in a fan device with a motor, ensuring the squareness of the shaft in relation to the hub, and not worsening the flowability of the resin that constitutes the hub during injection molding, is provided. The fan device includes an approximately cylindrical hub with a bottom and made of resin, vanes positioned at an outer circumference of the hub a shaft attached to the bottom of the hub and a reinforcing plate for reinforcing the bottom of the hub The shaft is connected to the reinforcing plate and a through hole filled with the resin for making the hub is provided on the reinforcing plate. 1. A fan device comprising:an approximately cylindrical hub with a bottom and made of a resin;vanes positioned at an outer circumference of the hub;a shaft attached to the bottom of the hub; anda reinforcing plate for reinforcing the bottom of the hub;wherein the shaft is connected to the reinforcing plate, and a through hole filled with the resin forming the hub is provided on the reinforcing plate.2. The fan device according to claim 1 , wherein a boss part is provided at the center part of the bottom of the hub in which the boss part has a thickness in an axial direction greater than the thickness of the bottom of the hub at a position located in an outside radial direction claim 1 , and the reinforcing plate is extended in a radial direction to the outside of the boss part.3. The fan device according to claim 1 , wherein one of the surfaces of the reinforcing plate is exposed to the outside or the inside of the hub.4. The fan device according to claim 1 , wherein a position of the through hole is used as an injection gate for forming the hub claim 1 , when viewed from an axial direction.5. The fan device according to claim 1 , wherein multiple through holes are further provided claim 1 , and the multiple through holes are arranged at positions that are in point symmetry with respect to the rotation center of the shaft claim 1 ...

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31-10-2013 дата публикации

Low flow-high pressure centrifugal pump

Номер: US20130287558A1
Автор: Frederic W. Buse
Принадлежит: Individual

Low flow centrifugal pump that develops more than 25 percent greater pressure than equivalent standard type spiral impellers with circular casings.

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21-11-2013 дата публикации

Fan

Номер: US20130309065A1
Принадлежит: Dyson Technology Ltd

A fan for generating an air current includes a body having an air inlet, and a nozzle connected to the body. The nozzle includes an interior passage for receiving an air flow from the body and an air outlet from which the air flow is emitted from the fan. The interior passage extends about an opening or bore through which air from outside the nozzle is drawn by air emitted from the air outlet. The body includes a duct having an air inlet and an air outlet, an impeller located within the duct for drawing the air flow through the duct, and a motor for driving the impeller. A noise suppression cavity is located beneath the air inlet of the duct. The cavity has an inlet which is located beneath, and is preferably concentric with, the air inlet of the duct.

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28-11-2013 дата публикации

IMPELLER FOR ELECTRIC BLOWER

Номер: US20130315743A1
Автор: CHO Yong Wan
Принадлежит: SAMSUNG ELECTRO-MECHANICS CO., LTD.

Disclosed herein is an impeller for an electric blower including: an upper plate; a lower plate; and a blade positioned between the upper plate and the lower plate, wherein the lower plate includes a burring part formed at an inner diameter portion thereof to which a shaft is insertedly coupled. In addition, disclosed herein is an impeller for an electric blower including: an upper plate; a lower plate; and a blade positioned between the upper plate and the lower plate, wherein the lower plate includes a burring part formed at an inner diameter portion thereof to which a shaft is insertedly coupled and a washer part extended in a direction perpendicular to the burring part. 1. An impeller for an electric blower comprising:an upper plate;a lower plate; anda blade positioned between the upper plate and the lower plate,wherein the lower plate includes a burring part formed at an inner diameter portion thereof to which a shaft is insertedly coupled.2. The impeller as set forth in claim 1 , wherein the burring part is protruded so that the inner diameter portion of the lower plate into which the shaft is inserted stands up vertically toward the upper plate.3. The impeller as set forth in claim 1 , wherein the shaft is insertedly coupled to the burring part of the lower plate claim 1 , and the nut is screw-coupled to an upper end portion of the shaft so as to be positioned at an upper end portion of the burring part.4. The impeller as set forth in claim 1 , further comprising auxiliary members positioned at an inner diameter portion of the impeller to which the shaft is coupled.5. The impeller as set forth in claim 4 , wherein the auxiliary members are coupled to both surfaces of the lower plate claim 4 , having the lower plate therebetween claim 4 , and an upper surface of the auxiliary member positioned on an upper surface of the lower plate is fixed by the nut.6. An impeller for an electric blower comprising:an upper plate;a lower plate; anda blade positioned between ...

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05-12-2013 дата публикации

CENTRIFUGAL BLOWER WITH COOLING FUNCTION

Номер: US20130319642A1
Автор: Higashiyama Naohisa
Принадлежит: KEIHIN THERMAL TECHNOLOGY CORPORATION

A centrifugal blower with a cooling function includes an impeller, a scroll casing, and an evaporator. The impeller includes a plurality of blades provided around a rotary shaft and blows out in a radially outward direction air taken in along the axial direction of the rotary shaft. The scroll casing accommodates the impeller, and has an intake port, a spiral air passage, and a discharge port. The evaporator is disposed in the air passage of the scroll casing. The evaporator includes a plurality of refrigerant passage members which are stacked in the longitudinal direction of the rotary shaft of the impeller and each of which has a refrigerant flow channel. An air-passing clearance is provided between adjacent refrigerant passage members. The centrifugal blower with a cooling function is used for a vehicle air conditioner. 1. A centrifugal blower with a cooling function comprising:an impeller which includes a plurality of blades provided around a rotary shaft and which blows out in a radially outward direction air taken in along an axial direction of the rotary shaft;a scroll casing which accommodates the impeller and which has an intake port for taking in air along the axial direction of the rotary shaft of the impeller, a spiral air passage through which the air blown out from the impeller flows, and a discharge port for blowing out the air having flowed through the air passage; andan evaporator which is disposed in the air passage of the scroll casing and which has a refrigerant flow channel and an air-passing clearance through which the air flowing through the air passage passes.2. A centrifugal blower with a cooling function according to claim 1 , wherein the evaporator includes a plurality of refrigerant passage members stacked in the longitudinal direction of the rotary shaft of the impeller claim 1 , the refrigerant flow channel is provided in each of the refrigerant passage members claim 1 , and the air-passing clearance is provided between adjacent ...

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05-12-2013 дата публикации

Impeller manufacturing method

Номер: US20130320073A1
Принадлежит: Mitsubishi Heavy Industries Ltd

The present invention relates to an impeller manufacturing method in which a thermal cycle is performed on an assembly body with a brazing material formed of a Ni-containing Au alloy being placed at a bond portion of at least two impeller constituent members. The thermal cycle includes a temperature increasing process with a temperature increasing rate of 20° C./hr. to 100° C./hr., the process including a first intermediate retention and a second intermediate retention each keeping the temperature, the first intermediate retention performed in a temperature range of 500° C. to 850° C. and the second intermediate retention performed in a temperature range of 850° C. to 950° C. (but not including 850° C.). In the thermal cycle, the temperature is increased in a temperature range exceeding 950° C. after the second intermediate retention at a rate lower than that before the second intermediate retention.

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05-12-2013 дата публикации

Propeller For Ventilator, With A Variable Blade Angle

Номер: US20130323062A1
Принадлежит: VALEO SYSTEMES THERMIQUES

A blower wheel comprises a hub, a guide and blades extending radially between the hub and the guide, each blade comprising a root at its junction with the hub and a head at the junction with the guide, each blade having a leading edge and a trailing edge between which, at each flattened cross section, a chord is defined. For each blade, in the radial direction from the root to the head, the pitch angle between the chord and the rotation axis of the wheel varies and the variation in the pitch angle between the root and the head has a point of inflexion between a first level and a second level. 1. A blower wheel for cooling an engine for driving a motor vehicle , said blower wheel comprising a hub , a guide and blades extending radially between the hub and the guide , each blade comprising a root at its junction with the hub and a head at the junction with the guide , each blade having a leading edge and a trailing edge between which , at each flattened cross section , a chord is defined , wherein for each blade , in the radial direction from the root to the head , a pitch angle between the chord and the rotation axis of the wheel varies and wherein the variation in the pitch angle between the root and the head has a point of inflexion between a first level and a second level.2. The wheel as claimed in claim 1 , wherein in the radial direction claim 1 , the pitch angle increases sharply with the radius up to the first level and the pitch angle increases again with the radius between the first level and the second level.3. The wheel as claimed in claim 1 , wherein at the head claim 1 , the pitch angle reduces sharply between the second level and the head.4. The wheel as claimed in claim 3 , wherein in the radial direction claim 3 , the pitch angle reduces sharply with the radius up to the first level and the pitch angle reduces again with the radius between the first level and the second level.5. The wheel as claimed in claim 1 , wherein the pitch angle increases ...

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12-12-2013 дата публикации

PUMP AND METHOD FOR PRODUCING AN IMPELLER FOR A PUMP

Номер: US20130330170A1
Автор: Albert Tobias
Принадлежит:

In a centrifugal pump for pumping a fluid with central axial suctioning and radial discharging of the fluid to be pumped out of the impeller, the impeller includes an upper cover plate and a lower cover plate and multiple interposed blades therebetween. In the radial inner region, the blades extend essentially parallel to the rotation axis of the impeller in the axial direction of the pump and thus are upright, wherein said blades in the course radially outwards thereof are increasingly inclined or extend oblique. 1. A pump , in particular for home appliances such as dish washers or washing machines , having an impeller for pumping a fluid , wherein said pump is configured together with said impeller for operation as a centrifugal pump , with a central axial suctioning and a radial discharging of said fluid to be pumped out of said impeller , wherein said impeller comprises an upper cover plate and a lower cover plate and multiple interposed blades therebetween , wherein said blades are less steep inclined relative to a central longitudinal axis of said pump in a radial inner region of said impeller than in a radial outer region of said impeller.2. The pump according to claim 1 , wherein said blades in the course thereof are increasingly inclined or extend increasingly oblique from said radial inner region to said radial outer region.3. The pump according to claim 2 , wherein in said radial inner region said blades extend essentially parallel to a rotation axis of said impeller in said axial direction of said pump claim 2 , said blades thus being extending upright.4. The pump according to claim 1 , wherein an inclination of said blades is configured such that said blades are inclined or extend oblique relative to said upper cover plate in a rotation direction of said impeller.5. The pump according to claim 1 , wherein a change of an inclination of said blades is monotonously increasing from said radial inner region of said impeller to said radial outer region of ...

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19-12-2013 дата публикации

CENTRIFUGAL PUMP AND A DOUBLE BENT ROTOR BLADE FOR USE IN SUCH A CENTRIFUGAL PUMP

Номер: US20130336774A1
Принадлежит: IHC Holland IE B.V.

The invention relates to a centrifugal pump () comprising a pump housing () which is provided with an axial inlet (), an outlet () and a rotor () which is attached in the pump housing () such that it can rotate about an axial rotation axis A. The rotor () is provided with a central boss (), a shaft shield () fastened to the boss (), a suction shield () attached so as to be axially set apart from the shaft shield (), which suction shield () has an axial supply () aligned with the axial inlet () of the pump housing (), and a plurality of rotor blades () which are fastened between the shields (). The radial inner ends () of the rotor blades () are connected to the suction shield () by a substantial perpendicular connection. 11. Centrifugal pump () , in particular for the pumping of a mixture of substances possibly including soil , comprising:{'b': 2', '6', '5', '3', '2, 'a pump housing () which is provided with an axial inlet () and an outlet () attached tangentially to a circumferential wall () of the pump housing (),'}{'b': 7', '2', '7', '9', '11', '9', '12', '11', '12', '14', '6', '2', '15', '11', '12', '17', '18, 'a rotor () which is attached in the pump housing () such that it can rotate about an axial rotation axis A, which rotor () is provided with a central boss (), a shaft shield () fastened to the boss (), a suction shield () attached so as to be axially set apart from the shaft shield (), which suction shield () has an axial supply () aligned with the axial inlet () of the pump housing (), and a plurality of double bent rotor blades () which are fastened between the shields (, ) and each extend substantially transversely to the rotation axis A between a radial outer end () and a radial inner end (), characterized in that'}{'b': 18', '12', '18', '15', '11', '12', '181', '12', '14', '182', '11', '14, 'the radial inner ends () forming a substantially right angle with respect to the suction shield () and wherein the radial inner ends () of the rotor blades () ...

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19-12-2013 дата публикации

CROSS-FLOW FAN, MOLDING DIE, AND FLUID FEEDER

Номер: US20130336793A1
Принадлежит: SHARP KABUSHIKI KAISHA

A cross-flow fan includes a plurality of fan blades provided to be circumferentially spaced apart from each other. The fan blade has an inner edge portion arranged on the radially inner side to/from which air flows in/out, and an outer edge portion arranged on the radially outer side to/from which air flows in/out. Fan blade has a blade surface extending between the inner edge portion and the outer edge portion. The blade surface includes a pressure surface arranged on the rotation direction side of the cross-flow fan and a suction surface arranged on the back side of the pressure surface. When cut along a plane orthogonal to the rotation axis of the cross-flow fan, the fan blade has a blade cross-sectional shape in which a concave portion concave from the pressure surface is formed. 1. A cross-flow fan comprising a plurality of vane portions provided to be circumferentially spaced apart from each other , each having an inner edge portion arranged on a radially inner side to/from which air flows in/out , and an outer edge portion arranged on a radially outer side to/from which air flows in/out , whereinsaid vane portion has a blade surface extending between said inner edge portion and said outer edge portion and including a pressure surface arranged on a rotation direction side of the cross-flow fan and a suction surface arranged on a back side of said pressure surface, andwhen cut along a plane orthogonal to a rotation axis of the cross-flow fan, said vane portion has a blade cross-sectional shape in which a concave portion concave from said pressure surface is formed.2. The cross-flow fan according to claim 1 , wherein when cut along the plane orthogonal to the rotation axis of the cross-flow fan claim 1 , said vane portion has a blade cross-sectional shape in which said concave portion is formed only at said pressure surface claim 1 , of said pressure surface and said suction surface.3. The cross-flow fan according to claim 1 , whereinsaid concave portion has a ...

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02-01-2014 дата публикации

BLOWER ASSEMBLY

Номер: US20140003927A1
Автор: Iyer Jayanthi
Принадлежит: VISTEON GLOBAL TECHNOLOGIES, INC.

A blower assembly includes a housing having a blower wheel disposed therein and a pre-swirler disposed in a fluid inlet of the housing. The pre-swirler includes an array of spaced apart vanes extending radially outwardly from a central hub. The vanes extend from the hub to an outer ring that is attached to the housing of the blower assembly. The vanes are configured to cooperate with the blower wheel to minimize a noise, a vibration, and a harshness (NVH) of the blower assembly, while maximizing an efficiency thereof. 1. A blower assembly comprising:a housing including a fluid inlet and a spaced apart fluid outlet;a blower wheel disposed in the housing, the blower wheel including an inlet ring and plurality of spaced apart blades; anda pre-swirler disposed in the fluid inlet of the housing, the pre-swirler including at least one vane having a leading edge, a trailing edge, and an outer edge extending between the leading edge and the trailing edge, wherein at least one of a blade exposure distance is less than about 10 mm and a blower wheel overlap distance is greater than about 5.5 mm.2. The blower assembly of claim 1 , wherein the blade exposure distance is a distance between a junction point of the trailing edge with the outer edge of the at least one vane of the pre-swirler and an end of a trailing edge of at least one of the blades of the blower wheel.3. The blower assembly of claim 1 , wherein the blower wheel overlap distance is a distance between a junction point of the trailing edge with the outer edge of the at least one vane of the pre-swirler and a peripheral surface of the inlet ring of the blower wheel.4. The blower assembly of claim 1 , wherein the leading edge of the at least one vane of the pre-swirler is substantially linear and spaced apart from the trailing edge.5. The blower assembly of claim 1 , wherein the outer edge of the at least one vane of the pre-swirler is curved.6. The blower assembly of claim 1 , wherein the at least one vane of the ...

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09-01-2014 дата публикации

Blower wheel with improved wheel hub to blade interface

Номер: US20140010657A1
Автор: Jayanthi Iyer
Принадлежит: Visteon Global Technologies Inc

A blower wheel for use in a blower assembly includes a hub, a concentrically arranged outer ring, an array of spaced apart blades extending between the hub and the outer ring. The hub includes an outer first surface and an inner second surface. An interface between an outer edge of a first end of each of the blades and an outer peripheral edge of the outer first surface of the hub is minimized, increasing an effective blade exit height of the blower wheel. As such, an effective open area for airflow between the blades of the blower wheel is increased over that of the prior art blower wheels. Further, a substantially planar lower face of the hub provides additional structural integrity to the hub, and thereby the blades.

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16-01-2014 дата публикации

Turbocharger system with reduced thrust load

Номер: US20140017099A1
Принадлежит: General Electric Co

An exemplary compressor is provided. The compressor includes a plurality of blades, a hub defining a front surface and a back surface, and a first flow restriction structure provided at the back surface of the hub. The plurality of blades are arranged in a predefined manner on the front surface for receiving input air flow at a first pressure and compressing the input air flow to provide an output air flow at a second pressure higher than the first pressure. The first flow restriction member is configured for preventing at least a portion of the output air flow at the second pressure from entering into the back surface of the hub to reduce an air pressure at the back surface of the hub.

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13-02-2014 дата публикации

SLURRY PUMP IMPELLER

Номер: US20140044545A1
Принадлежит: Weir Minerals Australia, Ltd.

A slurry pump impeller which includes a front shroud and a back shroud each having an inner main face with an outer peripheral edge and a central axis, a plurality of pumping vanes extending between the inner main faces of the shrouds, the pumping vanes being disposed in spaced apart relation. Each pumping vane includes a leading edge in the region of the central axis and a trailing edge in the region of the outer peripheral edges of the shrouds with a passageway between adjacent pumping vanes. Each passageway has associated therewith a discharge guide vane, each discharge guide vane being disposed within a respective passageway and located closer to one or the other of the pumping vanes and projecting from the inner main face of at least one of the or each shrouds. 1. A slurry pump impeller which includes a front shroud and a back shroud each having an inner main face with an outer peripheral edge and a central axis , a plurality of pumping vanes extending between the inner main faces of the shrouds , the pumping vanes being disposed in spaced apart relation , each pumping vane including opposed main side faces one of which is a pumping or pressure side face , a leading edge in the region of the central axis and a trailing edge in the region of the outer peripheral edges of the shrouds with a passageway between adjacent pumping vanes , each passageway having associated therewith a discharge guide vane , each discharge guide vane being disposed within a respective passageway and located closer to one or the other of the pumping vanes and projecting from the inner main face of at least one of the or each shrouds.2. A slurry pump impeller according to claim 1 , wherein each discharge guide vane is located closer to the pumping or pressure side face of the closest adjacent pumping vane.3. A slurry pump impeller according to claim 2 , wherein each discharge guide vane has an outer end adjacent the peripheral edge of one of the shrouds claim 2 , the discharge guide vane ...

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20-02-2014 дата публикации

Impeller, rotary machine including the same, and method for manufacturing impeller

Номер: US20140050585A1
Принадлежит: Mitsubishi Heavy Industries Ltd

An impeller including: blades disposed in a circumferential direction of the impeller; a disk located close to a second end side of an axis of the impeller with respect to the blades, to which the blades are attached, and configured to be attached to a rotating shaft; and a shroud located close to a first end side of an axis of the impeller with respect to the blades, and to which the blades are attached. Flow passages are formed by the blades, the disk and the shroud. The blades, the shroud and a first portion of the disk close to the second end side of the axis of the impeller are integrated so as to form a first member. A second portion of the disk close to the first end side of the axis of the impeller forms a second member.

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27-02-2014 дата публикации

IMPELLER FOR CENTRIFUGAL PUMP AND CENTRIFUGAL PUMP OF VEHICLE WASHER DEVICE

Номер: US20140056734A1
Автор: YAMAUCHI Yuusuke
Принадлежит: ASMO CO., LTD.

An impeller for a centrifugal pump comprising a boss supported by a rotation shaft of a motor so as to be rotatable as a unit with the rotation shaft; and a plurality of blades that extend from the boss towards a radial direction outside of the boss, and that discharge liquid towards a leading end side thereof by rotating; wherein each blade comprises one side face that is a face on a first side in a rotation direction of the impeller and includes a projecting face that projects from a base end portion at a boss side of the one side face towards the first side in the rotation direction with respect to a line that connects the base end portion and a center of rotation of the blades. 1. An impeller for a centrifugal pump comprising:a boss that is supported by a rotation shaft of a motor so as to be rotatable as a unit with the rotation shaft; anda plurality of blades that extend from the boss towards a radial direction outside of the boss, and that discharge liquid towards a leading end side thereof by rotating;wherein each of the blades comprises one side face that is a face on a first side in a rotation direction of the impeller and includes a projecting face that projects from a base end portion at a boss side of the one side face towards the first side in the rotation direction with respect to a line that connects the base end portion and a center of rotation of the blades.2. The impeller of claim 1 , wherein the one side face is configured as a curved face that forms a projection towards the first side in the rotation direction claim 1 , as viewed along a blade rotation axis direction.3. The impeller of claim 1 , wherein a leading end side of the one side face is disposed further towards a second side in the rotation direction of the impeller than the projecting face with respect to the line that connects the base end portion and the center of rotation of the blades.4. The impeller of claim 1 , wherein:a plurality of pairs of the blades are formed opposing each ...

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06-03-2014 дата публикации

Impeller and rotary machine provided with the same

Номер: US20140064975A1

The present invention is related to an impeller and a rotary machine including an inner diameter portion, a disk portion, a blade portion, and a cover portion. The disk portion includes a main body portion provided the blade portion, and a fixing portion disposed at an inner side in a radial direction of the rotor than the main body portion and fitted at the outside of an outer peripheral surface of the inner diameter portion. The fixing portion is formed so as to protrude toward the other side in the axial direction from the main body portion.

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20-03-2014 дата публикации

GRINDER

Номер: US20140077011A1
Автор: Watts Kyle T.
Принадлежит:

A grinder includes a generally vertical, rotatable shaft having at least one set of cutter blades driven thereby and a fan assembly mounted on the shaft below the cutter blades in position to receive output therefrom. The fan assembly includes a fan disc secured to the shaft and rotatable therewith. A plurality of fan blades are secured to the fan disc in a generally radial orientation. Each fan blade includes a bottom flange secured to a top surface of the fan disc, a web extending upwardly from the bottom flange and a top flange extending outwardly from the web in a direction of rotation of the fan disc. The fan blades are preferably moveably mounted to the fan disc such that the angle of the fan blades relative to a true radial orientation can be adjusted. 1. A grinder comprising:a rotatable shaft with at least one grinding means;a fan assembly mounted on the shaft, said fan assembly including a) a fan disc secured to the shaft and rotatable therewith, said fan disc having a direction of rotation and b) at least one fan blade.2. The grinder according to claim 1 , wherein claim 1 ,a) said at least one fan blade includes a plurality of fan blades that form a web;b) each of said fan blades includes a fan disc, the web extending in a first direction from said fan disc; andc) each of said fan blades includes a top flange extending in a second direction from said web.3. The grinder according to claim 2 , a) each of said fan blades includes a base flange,', 'b) said web is connected to said base flange along an edge of said base flange oriented in a direction of rotation of said fan disc; and', 'c) said top flange is connected to said web along a top edge thereof., 'wherein,'}4. The grinder according to claim 2 , wherein the position of each of said fan blades is adjustable relative to said fan disc.5. The grinder according to claim 4 , wherein each of said fan blades is connected to said fan disc by at least one fastener.6. The grinder according to claim 5 , wherein ...

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27-03-2014 дата публикации

Impeller and Electric-Motor Driven Water Pump Having the Same

Номер: US20140086767A1
Автор: Kenya Takarai
Принадлежит: HITACHI AUTOMOTIVE SYSTEMS LTD

An impeller is comprised of a hub configured to be rotated on a central axis, a shroud formed to be opposed to the hub in a direction of the central axis and having a central opening serving as a fluid inlet, and a plurality of circumferentially-equidistant spaced blades interleaved between the hub and the shroud. When a mating face of the shroud with each of the blades is divided into a radially inward region and a radially outward region, and a mating face of each of the blades with the shroud is divided into a radially inward region and a radially outward region, a given weld range is set only in the radially inward region of the mating face of the shroud with each of the blades and the radially inward region of the mating face of each of the blades with the shroud.

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10-04-2014 дата публикации

Bi-Directional Compression Fan Rotor for a Gas Turbine Engine

Номер: US20140096507A1
Автор: Sohail Mohammed
Принадлежит: United Technologies Corp

A fan rotor has a hub, and a plurality of axial flow fan blades extending radially outwardly of the hub. A radial compressor impeller is positioned radially inwardly of the fan blades. The radial compressor impeller has an upstream inlet which extends generally in an axial direction defined by an axis of rotation of the hub. The radial flow compressor impeller has an outlet that extends radially outwardly of the inlet, and into a supply passage for supplying air to a core engine. An engine is also disclosed.

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10-04-2014 дата публикации

Fan blade system with multiple spaced layers of blades and centrifugal fan using same

Номер: US20140099207A1
Автор: Meihua Yuan
Принадлежит: Asia Vital Components Shenzhen Co Ltd

A fan blade system with multiple spaced layers of blades and a centrifugal fan using same are disclosed. The centrifugal fan includes a housing, in which the fan blade system is mounted. The fan blade system includes a hub, and a first and a second blade group outward extended from a circumferential wall of the hub to axially space from each other. The housing includes a main housing portion and a secondary housing portion integrally formed on one side of the main housing portion. When the fan blade system is mounted in the housing, the two blade groups are separately located in the main housing portion and the secondary housing portion to produce higher airflow pressure and more air volume. With these arrangements, the centrifugal fan can have upgraded performance and be manufactured with reduced labor, time and material costs.

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05-01-2017 дата публикации

BLOWER FILTER DEVICE, RESPIRATORY PROTECTION DEVICE, OPERATIONAL INFRASTRUCTURE AND METHOD

Номер: US20170001048A1
Принадлежит:

A blower filter device includes a blower unit that draws and delivers ambient air; a filter unit that filters a harmful substance, or a filter coupling to couple and uncouple the filter unit. A control unit is configured to actuate the blower unit, to determine an operating state of the blower filter device and/or other respirator system components and/or a respirator system () as a whole and to generate an alarm if a determined operating state indicates a disturbance. An output unit is configured to receive the alarm from the control unit and to output the alarm. A communication interface () is configured for wireless network integration and to transmit the alarm via the network (). A respirator system () with such a blower filter device, an operational infrastructure () with such a respirator system, as well as a method of blower filter operation and operational infrastructure monitoring are provided. 1. A blower filter device for a respirator system , the blower filter device comprising:a blower unit configured to draw in and deliver ambient air;a filter unit configured to filter at least one harmful substance out of the ambient air drawn in and delivered, or a filter coupling for coupling and uncoupling such a filter unit,a control unit configured to actuate the blower unit, to determine an operating state of the blower filter device or to determine an operating state of other components of the respirator system or to determine an operating state of the respirator system as a whole or to determine an operating state of any combination of the blower filter device other components of the respirator system and the respirator system as a whole and to generate an alarm based on a determined operating state indicating a disturbance;an output unit configured to receive the alarm from the control unit and to output the alarm;a communication interface configured to be wirelessly integrated in a network and to transmit the alarm to other participants of the network.2. A ...

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06-01-2022 дата публикации

ROTOR ASSEMBLY

Номер: US20220003237A1
Принадлежит:

The disclosure relates to a high-speed radial fan and to a rotor assembly () for a high-speed radial fan, comprising a bearing tube () which is axially open in the interior and in which a shaft () carrying a fan wheel () is mounted with a rotor (), wherein the rotor () of the rotor assembly () is mounted in a cylindrical separating can (). 1102040305050103. A rotor assembly () for a high-speed radial fan , comprising a bearing tube () which is axially open in the interior and in which a shaft () carrying a fan wheel () is mounted with a rotor () , wherein the rotor () of the rotor assembly () is mounted in a cylindrical separating can ().211023. The radial fan () with a rotor assembly () according to claim 1 , characterized in that the radial fan has a fan housing () claim 1 , which is formed as a single piece with the separating can ().31204050403. The radial fan () according to claim 1 , characterized in that the bearing tube () with the shaft () and the rotor () mounted on the shaft () is arranged in the separating can () claim 1 , which is closed around the circumference.41322a. The radial fan () according to claim 2 , characterized in that the separating can () extends away from a substantially flat housing base plate () of the fan housing () in the axial direction.5150515033a. The radial fan () according to claim 1 , characterized in that an air gap is formed between the rotor () and a stator () surrounding the rotor () claim 1 , and the separating can () with its cylindrical separating can walls () is arranged within the air gap.613. The radial fan () according to claim 1 , characterized in that the material of the separating can () is an isolator or has a contact resistance greater than 10 Ohm.7140242025203050. The radial fan () according to claim 1 , characterized in that the shaft () claim 1 , on a first bearing () arranged in the bearing tube () and a second bearing () arranged in the bearing tube () spaced apart in the axial direction as relates to the ...

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06-01-2022 дата публикации

Pump Assembly

Номер: US20220003241A1
Принадлежит:

A pump assembly () for pumping boiling water to a dispenser in a drinking water dispensing system, the pump assembly () comprising: a pump housing () having an inlet () for the boiling water and an outlet () arranged in fluid communication with the inlet (); an impeller () disposed in the pump housing () for rotation about a central axis () for driving the water from the inlet () to the outlet (), wherein the inlet () is arranged on the central axis (); and an inducer () arranged in the inlet () to the pump housing () and operatively connected to the impeller () for rotation therewith about the central axis () to induce the water at the inlet () towards the impeller () and raise the inlet pressure. 1. A pump assembly for pumping boiling water to a dispenser in a drinking water dispensing system , the pump assembly comprising:a pump housing having an inlet for the boiling water and an outlet arranged in fluid communication with the inlet;an impeller disposed in the pump housing for rotation about a central axis for driving the water from the inlet to the outlet, wherein the inlet is arranged on the central axis; andan inducer arranged in the inlet to the pump housing and operatively connected to the impeller for rotation therewith about the central axis to induce the water at the inlet towards the impeller and raise the inlet pressure.2. A pump assembly according to claim 1 , wherein the impeller and the inducer are mounted on a common shaft comprised of a ceramic.3. A pump assembly according to claim 1 , wherein the inducer comprises a generally elongate stem which extends along the central axis away from the impeller into the inlet claim 1 , and at least one blade or flight that extends in a helical or screw formation on an outer periphery of the stem.4. A pump assembly according to claim 4 , wherein an upstream end of the inducer stem terminates in a tapered or rounded cap or nose to promote laminar flow through the inlet.5. A pump assembly according to claim 1 , ...

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07-01-2021 дата публикации

DYNAMIC BALANCING OF ADDITIVELY MANUFACTURED IMPELLERS

Номер: US20210001539A1
Принадлежит:

A method of manufacturing an impeller for a thermal management device includes partially curing a curable liquid in a curable liquid bath to form a first stage rotor, removing the first stage rotor from the curable liquid bath, the first stage rotor having excess curable liquid on a surface thereof, rotating the first stage rotor to displace the excess curable liquid radially outward from a rotational axis to compensate for imbalances in the first stage rotor, and fully curing the first stage rotor and at least a portion of the excess curable liquid to produce a second stage rotor that is more rotationally balanced than the first stage rotor. 1. A method for manufacturing an impeller for a thermal management device , the method comprising:partially curing a curable liquid in a curable liquid bath to form a first stage rotor;removing the first stage rotor from the curable liquid bath, the first stage rotor having excess curable liquid on a surface thereof;rotating the first stage rotor to displace the excess curable liquid radially outward from a rotational axis to compensate for imbalances in the first stage rotor; andfully curing the first stage rotor and at least a portion of the excess curable liquid to produce a second stage rotor that is more rotationally balanced than the first stage rotor.2. The method of claim 1 , wherein partially curing the curable liquid comprises exposing the curable liquid to a particular wavelength of light.3. The method of claim 1 , wherein fully curing the first stage rotor and at least a portion of the excess curable liquid comprises fully curing the first stage rotor and at least a portion of the excess curable liquid while rotating the first stage rotor and at least a portion of the excess curable liquid.4. The method of claim 1 , wherein fully curing the curable liquid includes exposing the curable liquid to a thermal energy source.5. The method of claim 1 , wherein fully curing the curable liquid includes exposing the curable ...

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07-01-2016 дата публикации

ROTATION PART OF ROTARY MACHINE AND METHOD OF MANUFACTURING THE SAME

Номер: US20160001406A1
Автор: AHN Jongkee
Принадлежит:

There is provided a rotation part of a rotary machine, the rotation part including: a base unit including a surface constituting fluid channels; a plurality of blade units protruding from the base unit; a plurality of shroud segment support units connected to the plurality of blade units and extending in a parallel direction to the surface of the base unit; a shroud segment disposed between and bonded to adjacent shroud segment support units of the plurality of shroud segment support units; and a first reinforcing unit provided on an intersection portion between a blade unit of the plurality of blade units and a shroud segment support unit of the plurality of shroud segment support units, wherein a distance from a protruding direction center line of the blade unit to an end portion of the shroud segment support unit is greater than a maximum distance from the protruding direction center line of the blade unit to an end portion of the first reinforcing unit. 1. A rotation part of a rotary machine , the rotation part comprising:a base unit comprising a surface constituting fluid channels;a plurality of blade units protruding from the base unit;a plurality of shroud segment support units connected to the plurality of blade units and extending in a parallel direction to the surface of the base unit;a shroud segment disposed between and bonded to adjacent shroud segment support units of the plurality of shroud segment support units; anda first reinforcing unit provided on an intersection portion between a blade unit of the plurality of blade units and a shroud segment support unit of the plurality of shroud segment support units,wherein a distance from a protruding direction center line of the blade unit to an end portion of the shroud segment support unit is greater than a maximum distance from the protruding direction center line of the blade unit to an end portion of the first reinforcing unit.2. The rotation part of a rotary machine of claim 1 , wherein a first step ...

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04-01-2018 дата публикации

MANUFACTURING METHOD AND MANUFACTURING DEVICE FOR RESIN FAN

Номер: US20180001524A1
Автор: MATSUDA Masao
Принадлежит: MATSUDAKANAGATAKOGYO CO., LTD.

A resin fan includes a semi-molded article in which a first circular plate and blades are integrated. While the semi-molded article is retained, a composite mold is moved to a secondary molding side, a second mold is put in a first position and a third mold is moved to the first position and inserted into the first mold. An intermediate part extends over the inner surface-side of a large-bend part, and causes the end of the third mold to engage with the first mold. Next, resin is poured into a secondary forming mold, and a second circular plate is integrally molded continuous with the blades of the semi-molded article, and a fan is molded. Together with the opening of the second mold and the composite mold, the third mold and the composite mold are opened, each of the molds is moved to a second position. 16-. (canceled)7. A method of manufacturing a resin fan that includes a multitude of blades arranged radially from the center and held securely between a first circular plate and a second circular plate aligned at the center with each other , said resin fan being molded with resin by using a two-stage molding process , the method comprising forming a resin fan on a primary forming mold and a secondary forming mold , both of which will be described below , wherein (a) said blades are so formed as to be bent and that the bend so formed has a convex surface in the direction of one complete revolution;', {'sub': 01', '0 2', '01, '(b) said blade is molded such that it has a height of Hon the side of the outer peripheral edge thereof, said height increasing gradually toward the inner peripheral side, and that it has a height of H(>H) on the side of the inner peripheral edge thereof; and'}, '(c) said first circular plate includes a first central opening portion;, '(1) said resin fan is molded into a particular shape in the following way in which'} (a) a first circular plate forming mold for molding the outer side and the outer peripheral edge on said first circular plate ...

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01-01-2015 дата публикации

TECHNIQUES FOR IMPROVED VOLUMETRIC RESISTANCE BLOWER APPARATUS, SYSTEM AND METHOD

Номер: US20150003007A1
Принадлежит:

Embodiments of an apparatus, system, method and techniques are described for an improved volumetric resistance blower and rotor. An apparatus may comprise, for example a motor, a casing having one or more inlets and one or more outlets, and a cylindrical rotor to create a volumetric resistance inside the casing, at least a portion of the rotor comprising a porous material. Other embodiments are described. 1. A blower , comprising:a motor;a casing having one or more inlets and one or more outlets; anda cylindrical rotor to create a volumetric resistance inside the casing, at least a portion of the rotor comprising a porous material.2. The blower of claim 1 , the porous material comprising one or more of foam claim 1 , fabric claim 1 , stamped or cut metal claim 1 , porous paper claim 1 , woven materials claim 1 , screens claim 1 , or porous plastics.3. The blower of claim 1 , the porous material comprising a plurality of bristles arranged in a random or pseudo-random pattern and coupled to a hub arranged to support the rotor and to couple the rotor to the motor.4. The blower of claim 3 , the bristles comprising a plastic or metal material having rigidity selected such that the bristles are self-supporting.5. The blower of claim 1 , the rotor comprising a plurality of blades and the porous material arranged around at least a portion of one or more of the plurality of blades.6. The blower of claim 5 , the plurality of blades coupled on a first end to a hub arranged to support the rotor and to couple the rotor to the motor and on a second end to an outer ring of the rotor claim 5 , the porous material arranged in one or more of a space between one or more of the plurality of blades claim 5 , a space between the hub and the outer ring and a space between a top side and a bottom side of the outer ring.7. The blower of claim 1 , the rotor comprising a porous material arranged between a top plate and a bottom plate claim 1 , the porous material arranged to continuously ...

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05-01-2017 дата публикации

MULTI-STAGE ELECTRIC CENTRIFUGAL COMPRESSOR AND SUPERCHARGING SYSTEM FOR INTERNAL COMBUSTION ENGINE

Номер: US20170002727A1
Принадлежит: MITSUBISHI HEAVY INDUSTRIES, LTD.

An object is to provide a multi-stage electric centrifugal compressor and a supercharging system for an internal combustion engine with a driving unit of a rotational shaft that can be readily controlled when a single-shaft and two-stage centrifugal compressor is employed. A multi-stage electric centrifugal compressor includes: an electric motor; and a pair of centrifugal compressors coupled to either side of the electric motor, the pair of centrifugal compressors comprising a low-pressure stage compressor and a high-pressure stage compressor connected in series. The low-pressure stage compressor and the high-pressure stage compressor are formed to have different pressure ratios from each other. 16-. (canceled)7. A multi-stage electric centrifugal compressor for pressurizing intake air to be supplied to an internal combustion engine , comprising:an electric motor; anda pair of centrifugal compressors coupled to either side of the electric motor, the pair of centrifugal compressors comprising a low-pressure stage compressor and a high-pressure stage compressor connected in series,wherein the low-pressure stage compressor and the high-pressure stage compressor are formed to have different pressure ratios from each other, andwherein the multi-stage electric centrifugal compressor further comprisesa map defining a relationship of a rotation speed of the electric motor to a discharge pressure or a discharge flow rate of the multi-stage electric centrifugal compressor;a matching unit configured to match the map with an intake pressure or an intake flow rate required for the multi-stage centrifugal compressor by an engine controller configured to control operation of an internal combustion engine to derive a required rotation speed of the electric motor; anda motor controller configured to control the rotation speed of the electric motor to achieve the required rotation speed derived by the matching unit.8. The multi-stage electric centrifugal compressor according to claim ...

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05-01-2017 дата публикации

BALANCE PISTON WITH A SEALING MEMBER

Номер: US20170002825A1
Принадлежит: DRESSER-RAND COMPANY

A balance piston for a compressor is provided. The balance piston may include an annular body and a seal extending from an axial surface of the annular body. The annular body may be configured to be disposed about and coupled with a rotary shaft of the compressor. The seal may be configured to form a sealing engagement with at least one component of the compressor to prevent a flow of a process fluid from an impeller of the compressor to a seal cavity of the compressor. 1. A balance piston for a compressor , comprising:an annular body configured to be disposed about and coupled with a rotary shaft of the compressor; anda seal extending from an axial surface of the annular body and configured to form a sealing engagement with at least one component of the compressor to prevent a flow of a process fluid from an impeller of the compressor to a seal cavity of the compressor.2. The balance piston of claim 1 , wherein the annular body is integral with an impeller of the compressor.3. The balance piston of claim 1 , wherein the seal comprises a protrusion extending from the axial surface of the annular body.4. The balance piston of claim 3 , wherein the protrusion is configured to form a sealing engagement with a shaft seal assembly of the compressor to prevent the flow of the process fluid from the impeller to the seal cavity.5. The compressor of claim 4 , wherein the protrusion is configured to form the sealing engagement with a labyrinth seal of the shaft seal assembly.6. The compressor of claim 5 , wherein the protrusion and the labyrinth seal define a tortuous path therebetween.7. The compressor of claim 3 , wherein the protrusion extends annularly about the axial surface of the annular body.8. The compressor of claim 3 , wherein an inner radial surface and an outer radial surface of the protrusion are substantially parallel with one another.9. The compressor of claim 3 , wherein an inner radial surface of the protrusion is arcuate.10. The compressor of claim 3 , ...

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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

BLADE OF CROSS-FLOW FAN

Номер: US20170002827A1
Автор: UDA Masafumi
Принадлежит:

A blade of a cross-flow fan including leading and trailing edge portions arranged on inner and outer peripheral sides of the cross-flow, and a base portion formed between the edge portions. The edge portions are arc shaped. The base portion has a pressure surface and a suction surface. A radius of the leading-edge portion is greater than a radius of the trailing-edge portion. A maximum thickness is at a position of maximum thickness that is closer to the leading-edge portion than to the trailing-edge portion. A first thickness is at an intermediate position on a blade chord. A second thickness is at a position set apart from an outer-peripheral end of the blade chord by 5% of the chord length. A value obtained by dividing the first thickness by the maximum thickness that is greater than a value obtained by dividing the second thickness by the first thickness. 1. A blade of a cross-flow fan comprising:a leading-edge portion arranged on an inner-peripheral side of the cross-flow fan, the leading-edge portion being formed in an arc shape;a trailing-edge portion arranged on an outer-peripheral side of the cross-flow fan, the trailing-edge portion being formed in an arc shape; and a pressure surface configured and arranged to generate positive pressure, and', 'a suction surface configured and arranged to generate negative pressure,, 'a base portion formed between the leading-edge portion and the trailing-edge portion, the base portion having'}the leading-edge portion and the trailing-edge portion being formed such that a radius of the leading-edge portion is greater than a radius of the trailing-edge portion, and a maximum thickness at a position of maximum thickness that is closer to the leading-edge portion than to the trailing-edge portion,', 'a first thickness at an intermediate position on a blade chord,', 'a second thickness at a position set apart from an outer-peripheral end of the blade chord by 5% of the chord length, and, 'the base portion being formed so as ...

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05-01-2017 дата публикации

MULTI-VOLUTE SIROCCO FAN

Номер: US20170002829A1

Disclosed is a multi-volute sirocco fan (multiblade fan). The present invention relates to a multi-volute sirocco fan configured to discharge fluid into several directions while using one motor and one fan. The sirocco fan according to the present invention comprises: a driving motor; a fan connected to a rotation shaft of the driving motor to thus be rotated therewith, the fan having a plurality of vanes arranged and installed in a cylindrical shape along the circumferential direction thereof; and at least two stacked volutes in the center of which the fan is arranged and installed and which guide the fluid while the cross-sectional area formed by the upper and lower surfaces, side surfaces thereof and the outer circumferential surface of the fan is linearly increased. 1. A multi-volute sirocco fan comprising:a driving motor;a fan connected to a rotation shaft of the driving motor to be rotated therewith, and having a plurality of vanes arranged and installed in a cylindrical shape along a circumferential direction thereof; andat least two stacked volutes in a center of which the fan is arranged and installed and which guide a fluid while a cross-sectional area thereof formed by upper and lower surfaces, side surfaces thereof and an outer circumferential surface of the fan is linearly increased.2. The multi-volute sirocco fan of claim 1 , wherein a lower surface of a lowermost one of the volutes is closed.3. The multi-volute sirocco fan of claim 1 , wherein a rounded guide for guiding the fluid is provided at an end of an upper surface central introduction port of an uppermost one of the volutes.4. The multi-volute sirocco fan of claim 1 , wherein the volutes are stacked claim 1 , and then contact surfaces thereof are welded and fixed.5. The multi-volute sirocco fan of claim 1 , wherein a plurality of diameter reduction protruding portions of which diameters are reduced and which protrude are provided at an upper surface central introduction port of a lower one of ...

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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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05-01-2017 дата публикации

MODULAR FAN BLADE

Номер: US20170002833A1
Принадлежит:

A modular fan blade includes a first fan blade and a second fan blade. The first fan blade includes a hub and plural first vanes, and the hub has an external periphery, and the first vane is combined with the external periphery, and a flange is formed at the external periphery and a retaining space is formed on a surface of the flange; and the second fan blade includes a fan frame and plural second vanes, and the fan frame is installed at the flange of the hub, sheathed on the hub, and installed in the retaining space, so as to achieve the effects of increasing the wind output of the fan effectively and replacing the blades conveniently. 1. A modular fan blade , comprising:a first fan blade, including a hub and a plurality of first vanes, and the hub having an external periphery, and the first vanes being combined to the external periphery, and the external periphery having a flange formed thereon, and a retaining space formed on a surface of the flange; anda second fan blade, including a fan frame, and a plurality of second vanes connected to the external periphery of the fan frame, and the fan frame being disposed at the flange of the hub, engaged with the hub, and installed in the retaining space.2. The modular fan blade as claimed in claim 1 , wherein the hub has a plurality of latch slots formed on the flange claim 1 , and the fan frame having a plurality of hooks corresponsive to the plurality of latch slots respectively claim 1 , and the second fan blade is latched to the latch slots through the hooks and combined with the hub.3. The modular fan blade as claimed in claim 1 , wherein the second vanes are partially disposed on the first vanes.4. The modular fan blade as claimed in claim 3 , wherein each of the first vanes has a groove formed on a side proximate to the hub claim 3 , and an end of some of the second vanes is disposed in the groove of the first vanes.5. The modular fan blade as claimed in claim 1 , wherein the fan frame has an inner peripheral ...

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05-01-2017 дата публикации

FAN HAVING A BLADE ASSEMBLY WITH DIFFERENT CHORD LENGTHS

Номер: US20170002836A1
Принадлежит:

A fan includes an impeller having blades of varying chord lengths. The fan includes a fan housing surrounding the impeller. The fan housing includes a protruding region, or throat, separated from each passing blade by a clearance, or throat gap, that varies according to the chord length. During rotation of the impeller, the impeller blades rotate about a rotational axis, passing the protruding region defining a minimum radial gap to the protruding region. Due to their different chord lengths, the impeller blades pass the throat region at different throat gaps. Shorter blades are likely to have lower amplitude static pressures and lower air velocities resulting at the blade tip, and are hence likely to generate a lower amplitude acoustic pulse at the protruding region. The variety of chord lengths modulate the amplitude of the pressure to spread acoustic sound across multiple frequencies thereby reducing peak amplitude of the acoustic sound. 1. A fan assembly suitable for use in a consumer electronic device , the fan assembly comprising:an impeller; anda plurality of impeller blades secured with the impeller, the plurality of impeller blades configured to rotate with the impeller in response to a rotational force applied to the impeller, wherein the plurality of impeller blades include blades of different chord lengths that follow a pattern that spreads an acoustic tonal output generated while the impeller is rotating to reduce a perception of the acoustic tonal output.2. The fan assembly of claim 1 , wherein the pattern comprises a periodic pattern.3. The fan assembly of claim 2 , wherein the periodic pattern is a sinusoidal pattern.4. The fan assembly of claim 3 , wherein adjacent impeller blades of the plurality of impeller blades comprise an equal angular spacing.5. The fan assembly of claim 1 , wherein the plurality of impeller blades comprises a first impeller blade having a longest blade length of the plurality of impeller blades and a second impeller blade ...

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01-01-2015 дата публикации

LOW-NOISE BLOWER

Номер: US20150003966A1
Автор: Duquette Steven
Принадлежит:

A low-noise blower has an impeller with an impeller plate and a plurality of blades each attached to the impeller plate. Each blade has a tip and a leading surface with a first portion that is proximate to the tip and has a first radius that is within a range of 0.03-0.20 inch. 1. A blower comprising: an impeller plate; and', 'a plurality of blades each attached to the impeller plate and comprising, 'an impeller comprisinga tip and a leading surface that comprises a first portion proximate to the tip,the first portion having a first radius that is within a range of 0.03-0.20 inch.2. The blower of claim 1 , wherein the first radius is within a range of 0.14-0.16 inch.3. The blower of claim 1 , wherein:the impeller plate comprises an outside edge with a second radius;the tip is coincident with the outside edge of the impeller plate;the leading surface comprises a second portion disposed between the tip and the first portion; andthe second portion of the leading surface comprises the second radius.4. The blower of claim 3 , further comprising a housing comprising:an impeller cavity, wherein the impeller plate is disposed within the impeller cavity;a collector; anda slot between the impeller cavity and the collector, the slot having an upper edge and a lower edge each comprising a third radius that is within a range of 0.01-0.30 inch.5. The blower of claim 4 , wherein:the impeller cavity further comprises an upper inner surface;each blade comprises a top surface; anda gap between the top surface at the tip of the respective blade and the upper inside surface of the impeller cavity is within a range of 0.005-0.050 inch.6. The blower of claim 3 , wherein:the housing comprises an inside wall that is proximate to the outside edge; anda gap between the inside wall and the outside edge is in a range of 0.035-0.110 inch when the impeller is stationary.7. The blower of claim 1 , wherein:the housing comprises a shelf;the impeller plate further comprises a bottom surface ...

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05-01-2017 дата публикации

AIR-CONDITIONING INDOOR MACHINE

Номер: US20170003038A1
Автор: UDA Masafumi
Принадлежит:

A wall-mounted air-conditioning indoor machine includes a cross-flow fan, a casing and a heat exchanger. The casing includes a stabilizer and a rear guider. The stabilizer is divided into top and bottom parts with a tongue part in between. The stabilizer, rear guider, and cross-flow fan are arranged so that three expressions, (θa−θ)><(θb−θ)<, and θb≧θa, are satisfied. A reference angle (θ) is formed by a fan-referencing horizontal line and a scroll-referencing line. A first angle (θa) is formed by the fan-referencing horizontal line and a first straight line connecting a fan center point and a front-surface-side closest point of the stabilizer. A second angle (θb) is formed by the fan-referencing horizontal line and a second straight line connecting the fan center point and a back-surface-side closest point of the rear guider. 1. A wall-mounted air-conditioning indoor machine , comprising:a cross-flow fan arranged and configured to generate an air flow, the cross-flow fan having a plurality of blades aligned along a circumference thereof;a casing including a stabilizer on a front-surface side and a rear guider on a back-surface side, the stabilizer being divided into a top part and a bottom part with a tongue part in between, a blown air channel being formed in the casing by the stabilizer and the rear guider, and the blown air channel having a scroll shape through which air flows from the cross-flow fan to a blow-out port; anda heat exchanger including a front-surface-side heat exchange section and a back-surface-side heat exchange section, the heat exchanger being arranged on an airflow-upstream side of the cross-flow fan; a horizontal line through a fan center point, which is a rotational center of the cross-flow fan, being a fan-referencing horizontal line,', 'a line designated as a scroll-referencing line being a straight line, which of any straight line tangent to a circle connecting outer ends of the plurality of fan blades of the cross-flow fan and adjoining ...

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07-01-2016 дата публикации

FAN, MOLDING DIE, AND FLUID FEEDER

Номер: US20160003256A1
Принадлежит: SHARP KABUSHIKI KAISHA

A fan includes a plurality of blade portions arranged spaced apart from each other in a circumferential direction, each blade portion having a blade surface including a pressure surface disposed on a rotational direction side of the fan and a suction surface disposed on a back side of the pressure surface. The plurality of blade portions include a first blade portion and a second blade portion different from each other in at least one of an outer peripheral blade tip angle and an inner peripheral blade tip angle, and are provided such that a discrepancy angle is equal among a plurality of the blade portion. 1. A fan comprising a plurality of blade portions arranged spaced apart from each other in a circumferential direction , each blade portion having a blade surface including a pressure surface disposed on a rotational direction side of the fan and a suction surface disposed on a back side of said pressure surface , whereinwhen cut along a plane orthogonal to a rotation axis of the fan, said blade portion has an inner edge portion at which a center line between said pressure surface and said suction surface intersects an inner peripheral-side blade tip, and an outer edge portion at which the center line intersects an outer peripheral-side blade tip,as the fan is rotated, a fluid flow is produced on said blade surface to flow between said inner edge portion and said outer edge portion,when an angle between a straight line passing through a rotational center of the fan and said outer edge portion and a tangent of said center line at said outer edge portion is defined as an outer peripheral blade tip angle, an angle between a straight line passing through the rotational center of the fan and said inner edge portion and a tangent of said center line at said inner edge portion is defined as an inner peripheral blade tip angle, and an angle between a chord line in contact with the inner peripheral-side and outer peripheral-side blade tips on said pressure surface side, ...

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07-01-2016 дата публикации

METHOD FOR MAKING AN IMPELLER FROM SECTOR SEGMENTS

Номер: US20160003257A1
Принадлежит: Nuovo Pignone Srl

A manufacturing technique for impellers for a centrifugal rotating machine is provided. The impeller is made by composition of single vanes pieces that fit to the hub or directly to the rotor shaft by welding, friction welding or a mechanical locking system. The manufacturability of the segments is easy fast and cheap and make it possible to use advanced manufacturing technologies like additive manufacturing of the type of Direct Metal Laser Melting. 1. A method for manufacturing an impeller for a centrifugal rotating machine comprising a substantially disk shaped main body comprising a front surface and a rear surfaces , a shroud comprising a front surface and a rear surfaces arranged spaced from the front surface of the main body , a plurality of blades , attached to the front surface of the main body joining the main body with the shroud wherein side surfaces of the blades , the front surface of the body , and the rear surface of the shroud form flow passages for compressing air , the method comprisingmaking a single segments of the impeller comprising a single blade, a section of the main body and the corresponding section of the shroud; andsuccessively joining together the plurality of segments to form the impeller.2. The method according to claim 1 , wherein the segments are joined together by welding claim 1 , or friction welding.3. The method according to claim 1 , wherein the impeller is attached to a hub that is attached to a rotor shaft of the machine claim 1 , or is attached directly to the rotor shaft.4. The method according to claim 3 , wherein the impeller is attached to the hub or directly to the rotor shaft by Cold Metal Transfer (CMT) deposition.5. The method according to claim 1 , wherein the single segments are attached to the hub or directly to the rotor shaft of the machine.6. The method according to claim 3 , wherein the segments are attached to the hub or to the rotor shaft by welding claim 3 , friction welding claim 3 , or by a mechanical ...

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07-01-2016 дата публикации

Pump including a shield for protecting a pump wheel against a coolant leak along the hub of the wheel

Номер: US20160003262A1
Автор: Olivier Philippart
Принадлежит: AREVA NP

A pump is provided. The pump includes a flow chamber for the heat-transport fluid, a pump wheel which is placed entirely in the flow chamber and which comprises a hub, a shaft for rotating the pump wheel, having an axial end section rigidly connected to the pump wheel and fitted in the hub of the pump wheel, a motor for rotating the shaft around its axis, and means for causing a coolant for cooling the driveshaft to flow, at a temperature lower than that of the heat-transport fluid, along the driveshaft. The pump also includes a shield for protecting the pump wheel against a coolant leak along an outer peripheral surface of the hub of the pump wheel, the protective shield being attached to the pump wheel.

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07-01-2016 дата публикации

METHOD FOR ASSEMBLING COMPRESSOR, AND BUNDLE GUIDE DEVICE

Номер: US20160003263A1

A method for assembling a compressor comprises: a bundle arrangement step in which a bundle is arranged behind the opening of a casing in the insertion direction; a first insertion step in which the front end of the bundle is inserted into the casing by moving the bundle by means of both an outside traveling device and an intermediate traveling device; and a second insertion step in which the intermediate traveling device is removed from the bundle and the bundle is inserted further inward into the casing by moving the bundle by means of both an inside traveling device and the outside traveling device. 1. A method for assembling a compressor including a bundle having a rotor therein , a casing into which the bundle is inserted , and an inside traveling device supporting the front end of the bundle in the direction of the insertion into the casing and capable of traveling in the insertion direction on the inner peripheral surface of the casing , and an outside traveling device supporting the rear end of the bundle in the insertion direction and capable of traveling in the insertion direction on a base surface disposed outside the casing and an intermediate traveling device supporting the intermediate portion of the bundle between the inside traveling device and the outside traveling device in the insertion direction and capable of traveling on the base surface being removable from the compressor , comprising:a bundle arrangement step in which the bundle is arranged behind an opening of the casing in the insertion direction;a first insertion step in which the front end of the bundle is inserted into the casing by moving the bundle by means of both the outside traveling device and the intermediate traveling device; anda second insertion step in which the intermediate traveling device is removed from the bundle and the bundle is inserted further inward into the casing by moving the bundle by means of both the inside traveling device and the outside traveling device.2. ...

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04-01-2018 дата публикации

IMPELLER FOR ROTARY MACHINE, COMPRESSOR, SUPERCHARGER, AND METHOD FOR PRODUCING IMPELLER FOR ROTARY MACHINE

Номер: US20180002812A1
Принадлежит: MITSUBISHI HEAVY INDUSTRIES, LTD.

An impeller for a rotary machine includes: a base material of the impeller comprising Al or an Al alloy; a surface layer for the impeller formed by an electroless plating layer comprising a Ni—P based alloy; and an under layer disposed between the base material and the surface layer, the under layer having a smaller Vickers hardness than the surface layer. 116-. (canceled)17. An impeller for a rotary machine , comprising:a base material of the impeller comprising Al or an Al alloy;a surface layer for the impeller formed by an electroless plating layer comprising a Ni—P based alloy; andan under layer disposed between the base material and the surface layer, the under layer having a smaller Vickers hardness than the surface layer,wherein the surface layer has a P content rate of not less than 4 wt % and not more than 10 wt %.18. The impeller for a rotary machine according to claim 17 , wherein the surface layer has an amorphous structure.19. An impeller for a rotary machine claim 17 , comprising:a base material of the impeller comprising Al or an Al alloy;a surface layer for the impeller formed by an electroless plating layer comprising a Ni—P based alloy; andan under layer disposed between the base material and the surface layer, the under layer having a smaller Vickers hardness than the surface layer,wherein the under layer comprises a plating layer containing Ni.20. The impeller for a rotary machine according to claim 19 , wherein the plating layer serving as the under layer comprises a Ni—P based alloy having an amorphous structure claim 19 , the Ni—P based alloy having a P content rate of not less than 10 wt % and not more than 13 wt % in the under layer.21. The impeller for a rotary machine according to claim 19 , wherein the Ni plating layer serving as the under layer is an electrolytic plating layer having a Vickers hardness of not more than 350 HV.22. The impeller for a rotary machine according to claim 17 , wherein the under layer is a plating layer ...

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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

Multi-stage impeller assembly for pump

Номер: US20180003182A1
Принадлежит: LITENS AUTOMOTIVE PARTNERSHIP

In an aspect, there is provided a pump impeller assembly that includes a first impeller portion arranged to drive a fluid through a fluid conduit, a second impeller portion movable between a more-rotationally engaged position in which the second impeller portion has a first amount of rotational engagement with the first impeller portion, and a less-rotationally engaged position in which the second impeller portion has a second amount of rotational engagement with the first impeller portion that is less than the first amount of rotational engagement, and an actuator operatively connected to the second impeller portion and configured to drive movement of the second impeller portion between the more-rotationally engaged position and the less-rotationally engaged position based on a fluid property

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04-01-2018 дата публикации

Centrifugal Fan

Номер: US20180003188A1
Принадлежит:

There is provided a centrifugal fan that effectively cools an electronic component with a simple structure. The centrifugal fan comprises an impeller having a plurality of pins extending in an axial direction, a rotor yoke formed with a plurality of through-holes through which the pins penetrate, the rotor yoke being joined to the impeller as the pins penetrate through the through-holes, and a circuit board arranged in a state having a gap with respect to the rotor yoke , wherein an end ′ of the pin protrudes from the rotor yoke to a side of the circuit board, and the plurality of pins are arranged with uneven pitch in a circumferential direction of the impeller. 1. A centrifugal fan comprising:an impeller having a plurality of pins extending in an axial direction;a rotor yoke formed with a plurality of through-holes through which the pins penetrate, the rotor yoke being joined to the impeller as the pins penetrate through the through-holes; anda circuit board arranged in a state having a gap with respect to the rotor yoke,whereinan end of the pin protrudes from the rotor yoke to a side of the circuit board, andthe plurality of pins are arranged with uneven pitch in a circumferential direction of the impeller.2. The centrifugal fan according to claim 1 , wherein an electronic component on the circuit board and a part of the pin protruding to the side of the circuit board are positioned to overlap with each other when viewed from a direction perpendicular to a rotation axis. This application claims the benefit of Japanese Patent Application No. 2016-130804, filed Jun. 30, 2016, which is hereby incorporated by reference in its entirety.The present invention relates to a centrifugal fan characterized by a function of cooling a built-in electronic component.Centrifugal fans have been widely used for purposes including cooling, ventilation, air conditioning of various equipment including home electrical equipment, OA equipment, and industrial equipment, or for air ...

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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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02-01-2020 дата публикации

METHOD FOR MANUFACTURING TURBO FAN

Номер: US20200003062A1
Автор: ISHII Fumiya, ODA Shuzo
Принадлежит:

A method for manufacturing a turbo fan unit includes a step for preparing multiple fan blades and an other-side side plate, and a step for connecting each of the multiple fan blades to the other-side side plate by a welding process. In the preparing step, one of the fan blade and the side plate is prepared, in which a connecting-surface forming portion having a connecting surface and a welding projection protruded from the connecting surface is formed. The connecting surface connects one of the fan blade and the side plate to the other one of the fan blade and the side plate. In the connecting step, the welding projection is melted down and the connecting surface is connected to an opposing surface, which is the surface of one of the fan blade and the side plate and which is opposing to the connecting surface. 1. A method for manufacturing a turbo fan unit to be used in a blower device , wherein the turbo fan unit comprises:multiple fan blades arranged around a fan center line;a shroud ring connected to one side of each fan blade in an axial direction of the fan center line and forming an air suction port through which air is sucked;an other-side side plate connected to the other side of each fan blade in the axial direction of the fan center line; andan air-flow guide portion located at a position inside of the other-side side plate in a fan radial direction for guiding an air flow sucked from the air suction port in a direction from an inside to an outside of the fan radial direction,wherein the air-flow guide portion has an air guide surface, which is formed in the air-flow guide portion on the one side of the axial direction and which guides the air flow sucked from the air suction port,wherein the other-side side plate has a plate-side guide surface, which faces blade passages respectively formed between neighboring fan blades of the multiple fan blades, and which guides an air flow passing through the blade passages,wherein the method for manufacturing the ...

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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

Shaft Seal

Номер: US20200003221A1
Автор: Sixsmith Paul
Принадлежит:

A shaft seal for an exhaust fan. The seal limits leakage from within an exhaust fan housing around an exhaust fan drive shaft that extends between a rotational power source exterior to the exhaust fan housing and a position within the exhaust fan housing. The seal comprises a plenum generally positioned about the exhaust fan drive shaft at the point where the shaft extends into the fan housing; an auxiliary blower comprising a housing, an internal blade driven by an auxiliary blower drive shaft, and an auxiliary blower drive to rotate the drive shaft where the auxiliary blower drive is operatively associated with the rotational power source such that operation of the rotational power sources causes a rotation of the exhaust fan drive shaft and the auxiliary blower drive shaft; and a duct fluidly connecting the auxiliary blower housing to the plenum. 117-. (canceled)18. A shaft seal for an exhaust fan , the shaft seal for limiting the leakage of a fluid from within an exhaust fan housing around an exhaust fan drive shaft that extends between a position exterior to the exhaust fan housing and a position within the exhaust fan housing , the shaft seal comprising:a plenum generally positioned about the exhaust fan drive shaft at the point where the exhaust fan drive shaft extends into the exhaust fan housing;an auxiliary blower comprising an auxiliary blower housing, an internal auxiliary blower blade or impeller driven by an auxiliary blower drive shaft, and an auxiliary blower drive to rotate the auxiliary blower drive shaft, said auxiliary blower drive comprising a first pulley mounted to said auxiliary blower drive shaft, said first pulley rotated by a belt driven by a second pulley mounted to either the exhaust fan drive shaft or to a rotating shaft of an exhaust fan motor; anda duct fluidly connecting said auxiliary blower housing to said plenum,said auxiliary blower mounted upon a track such that the position of said first pulley relative to said second pulley ...

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