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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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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 15. Отображено 14.
16-01-2018 дата публикации

Exhaust-gas turbocharger

Номер: US0009869238B2
Принадлежит: BorgWarner Inc., BORGWARNER INC

An exhaust-gas turbocharger ( 1 ), with: a turbine housing ( 2 ) which has a turbine housing inlet ( 8 ) and a turbine housing outlet ( 9 ) for exhaust gas, and which has a wastegate duct between the turbine housing inlet ( 8 ) and the turbine housing outlet ( 9 ), and a flap arrangement ( 10 ) comprising a pivotable flap lever ( 12 ), a flap plate ( 11 ), which is connected to the flap lever ( 12 ), for opening and closing the wastegate duct, and having a spring element ( 17 ) which is arranged between the flap lever ( 12 ) and a disc ( 18 ) fastened to the flap plate ( 11 ). The spring element ( 17 ) has an outer circumferential region ( 23 ) which is supported on a sliding contact surface ( 20 ), which is of curved form, of the flap lever ( 12 ).

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11-02-2016 дата публикации

EXHAUST-GAS TURBOCHARGER

Номер: US20160040678A1
Принадлежит:

An exhaust-gas turbocharger () having a compressor () which has a compressor housing (); a turbine () which has a turbine housing (); and a compressor-side and/or turbine-side charge pressure regulating device () which has a shut-off element () which opens or closes a flow opening (). The shut-off element () is in the form of a slide which is mounted on a guide () so as to be longitudinally displaceable along a longitudinal central line (LM) of the guide (), and the flow opening () is arranged at least substantially at a right angle (α) with respect to the longitudinal central line (LM) of the guide (). 11. An exhaust-gas turbocharger () , having{'b': 2', '3, 'a compressor () which has a compressor housing ();'}{'b': 4', '5, 'a turbine () which has a turbine housing (); and'}{'b': 6', '7', '9, 'a compressor-side and/or turbine-side charge pressure regulating device () which has a shut-off element () which opens or closes a flow opening (), wherein'}{'b': 7', '8', '8, 'sub': '8', 'the shut-off element () is in the form of a slide which is mounted on a guide () so as to be longitudinally displaceable along a longitudinal central line (LM) of the guide (), and'}{'b': 9', '8, 'sub': '8', 'the flow opening () is arranged at least substantially at a right angle (a) with respect to the longitudinal central line (LM) of the guide ().'}271011. The exhaust-gas turbocharger as claimed in claim 1 , wherein the slide () has a slide head () which is connected to a slide rod ().3101312. The exhaust-gas turbocharger as claimed in claim 2 , wherein the slide head () is pot-shaped with a cylindrical guide and seal wall () that points into an interior space ().41014151615. The exhaust-gas turbocharger as claimed in claim 3 , wherein the slide head () is mounted on a cylindrical guide spigot () which has a cylindrical outer wall () and a face wall () that adjoins the outer wall ().5151013. The exhaust-gas turbocharger as claimed in claim 4 , wherein the outer wall () guides the slide ...

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02-03-2017 дата публикации

CONTROL ARRANGEMENT OF AN EXHAUST-GAS TURBOCHARGER

Номер: US20170058761A1
Принадлежит:

A control arrangement () of an exhaust-gas turbocharger () which has a charger housing (), the control arrangement () having a spindle () which has a first end region () arranged outside the charger housing () and a second end region () arranged within the charger housing () and having a valve disk () which is connected to the spindle (), wherein the valve disk () and the spindle () are separate components, and wherein the spindle () is connected by way of its second end region () to the valve disk () by means of a connecting means (). 11421. A control arrangement () of an exhaust-gas turbocharger () which has a charger housing () , the control arrangement () comprising:{'b': '15', 'a spindle () which has'}{'b': 24', '2, 'a first end region () arranged outside the charger housing () and'}{'b': 25', '2, 'a second end region () arranged within the charger housing (), and'}{'b': 18', '15', '33, 'a valve disk () which is connected to the spindle () and which interacts with a valve seat (), wherein'}{'b': 18', '15, 'the valve disk () and the spindle () are separate components, and'}{'b': 15', '25', '18', '26', '18', '33, 'the spindle () is connected by way of its second end region () to the valve disk () by means of a connecting means () after alignment of the valve disk () on the valve seat ().'}22627182515. The control arrangement as claimed in claim 1 , wherein the connecting means () has a fork-shaped fixing region () arranged on the valve disk () claim 1 , which fixing region engages around the second end region () of the spindle ().3252829303127. The control arrangement as claimed in claim 2 , wherein the second end region () has flattened abutment surfaces ( claim 2 , ) which bear against counterpart surfaces ( claim 2 , ) of the fork-shaped fixing region ().4263425. The control arrangement as claimed in claim 1 , wherein the connecting means () has a first spherical segment () which is connected to the second end region ().5253434. The control arrangement as ...

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15-03-2018 дата публикации

Exhaust-gas turbocharger

Номер: US20180073425A1
Принадлежит: BorgWarner Inc

An exhaust-gas turbocharger ( 1 ), with a turbine housing ( 2 ) which has a turbine housing inlet ( 8 ) and a turbine housing outlet ( 9 ) for exhaust gas, and which has a wastegate duct ( 45 ) between the turbine housing inlet ( 8 ) and the turbine housing outlet ( 9 ), and a flap arrangement ( 33 ) comprising a pivotable flap lever ( 35 ), a flap plate ( 34 ), which is connected to the flap lever ( 35 ), for opening and closing the wastegate duct, and having a spring element ( 37 ) which is arranged between the flap lever ( 35 ) and a disc ( 36 ) fastened to the flap plate ( 34 ). The spring element ( 17 ) has an outer circumferential region ( 23 ) which is supported on a sliding contact surface ( 42 ), which is of curved form, of the disc ( 36 ).

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16-04-2015 дата публикации

BYPASS VALVE, IN PARTICULAR COMPRESSOR BYPASS VALVE

Номер: US20150104341A1
Автор: Maue Fred, Ruh Matthias
Принадлежит: BORGWARNER INC.

A bypass valve (), in particular a compressor bypass valve, having a valve housing (); a valve guide body (), which is fixed in the valve housing (); and a valve disk (), which is guided between a closed position and an open position by the valve guide body () in the valve housing (). The the valve guide body () and the valve disk () are in the form of plastic parts. 11. A compressor comprising a bypass valve () , the bypass valve comprising{'b': '2', 'a valve housing ();'}{'b': 3', '2, 'a valve guide body (), which is fixed in the valve housing (); and'}{'b': 4', '3', '2, 'a valve disk (), which is guided between a closed position and an open position by the valve guide body () in the valve housing (), wherein'}{'b': 3', '4, 'the valve guide body () and the valve disk () are plastic parts.'}245. The compressor as claimed in claim 1 , wherein the valve disk () is provided with an O-ring groove ().35. The compressor as claimed in claim 2 , wherein an O-ring is molded into the O-ring groove ().446. The compressor bypass as claimed in claim 1 , wherein the valve disk () has a cast-in guide rod ().57686. The compressor as claimed in claim 4 , wherein the free end () of the guide rod () is provided with an assembly securing device () claim 4 , which is cast onto the guide rod ().69104. The compressor as claimed in claim 1 , wherein a spring guide device () is provided in an inner space () of the valve disk ().7999. The compressor valve as claimed in claim 6 , wherein the spring guide device () has a plurality of cast-on guide webs (A-G).812113. The compressor as claimed in claim 1 , wherein a spring guide device () is arranged in an inner space () of the valve guide body ().9121212. The compressor as claimed in claim 8 , wherein the spring guide device () has a plurality of cast-on guide webs (A-H).10613161720212425. The compressor as claimed in claim 1 , wherein the guide rod () is formed with a cruciform cross section and claim 1 , at the four free end regions (-) ...

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28-05-2015 дата публикации

EXHAUST-GAS TURBOCHARGER

Номер: US20150147162A1
Принадлежит: BORGWARNER INC.

An exhaust-gas turbocharger (), with: a turbine housing () which has a turbine housing inlet () and a turbine housing outlet () for exhaust gas, and which has a wastegate duct between the turbine housing inlet () and the turbine housing outlet (), and a flap arrangement () comprising a pivotable flap lever (), a flap plate (), which is connected to the flap lever (), for opening and closing the wastegate duct, and having a spring element () which is arranged between the flap lever () and a disc () fastened to the flap plate (). The spring element () has an outer circumferential region () which is supported on a sliding contact surface (), which is of curved form, of the flap lever (). 11. An exhaust-gas turbocharger () comprising:{'b': '2', 'a turbine housing ()'}{'b': 8', '9, 'which has a turbine housing inlet () and a turbine housing outlet () for exhaust gas, and'}{'b': 8', '9, 'which has a wastegate duct between the turbine housing inlet () and the turbine housing outlet (), and'}{'b': '10', 'a flap arrangement () comprising'}{'b': '12', 'a pivotable flap lever (),'}{'b': 11', '12, 'a flap plate (), which is connected to the flap lever (), for opening and closing the wastegate duct, and'}{'b': 17', '12', '18', '11, 'a spring element () which is arranged between the flap lever () and a disc () fastened to the flap plate (),'}wherein{'b': 17', '23', '20', '12, 'the spring element () has an outer circumferential region () which is supported on a sliding contact surface (), which is of curved form, of the flap lever ().'}21021112221122122. The exhaust-gas turbocharger as claimed in claim 1 , wherein the flap arrangement () has a first contact surface () on the flap plate () and a second contact surface () claim 1 , situated opposite the first contact surface () claim 1 , on the flap lever () claim 1 , wherein the two contact surfaces ( claim 1 , ) bear against one another only via a line of contact.3212221222122. The exhaust-gas turbocharger as claimed in claim 2 , ...

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12-07-2018 дата публикации

Method for assembling control arrangement of an exhaust-gas turbocharger

Номер: US20180193967A1
Принадлежит: BorgWarner Inc

A boost control device for a turbocharger, assembled at room temperature, may not be geometrically optimal at turbocharger operating temperature. The geometric deviation in the boost control device introduced by the heating of the turbocharger to operating temperature, or during welding of the boost control device, is corrected by producing a first turbocharger at room temperature, determining the geometry of the deviation at operating temperature, producing a distance element that will introduce an equal and opposite deviation, introducing the equal and opposite deviation via the distance element in second and subsequent turbochargers, whereby thermal deviation and corrective deviation offset so that the turbocharger is geometrically accurate at operating temperature.

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28-12-2017 дата публикации

MONO OR DUAL COAXIAL SLIDER VALVE FOR CONTROLLING A TWIN SCROLL TURBOCHARGER

Номер: US20170370279A1
Принадлежит: BORGWARNER INC.

A compact flow control valve capable of providing long service life in a very hostile environment. The valve is a mono or dual coaxial slider valve capable of controlling two different functions sequentially, at least one of the functions being controlled progressively. The flow control valve controls the fluid connection between two volutes () of a turbine housing () of a turbocharger as well as the fluid connection between the two volutes () of the turbine housing () of the turbocharger and a waste gate port (). 1. A turbocharger with a turbine housing having at least a first volute , a second volute , and a wastegate , and comprisinga valve housing defining at least one cylindrical space having a longitudinal axis, and having at least a first opening in communication with the first volute, a second opening in communication with the second volute, and third opening in communication with the wastegate;at least one piston slidable within said cylindrical space between a full closed and a full open position, and having a piston shaft,displacement means adapted to effect selective displacement of the at least one piston between the full closed and the full open position,wherein in the full closed position the first, second and third openings are blocked, andwherein as the at least one piston is moved out if the full closed position and in the direction of the full open position the openings are simultaneously or sequentially unblocked to allow communication between the unblocked openings.2. The turbocharger as in comprising a dual sequential coaxial slider valve claim 1 , the turbine housing having at least a first volute claim 1 , a second volute claim 1 , and a wastegate port claim 1 , and comprisinga valve housing defining at least one cylindrical space having a longitudinal axis, and having at least a first opening in communication with the first volute, a second opening in communication with the second volute, and third opening in communication with the wastegate ...

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02-01-2019 дата публикации

Method for assembling a control arrangement of an exhaust-gas turbocharger

Номер: EP3102804B1
Принадлежит: BorgWarner Inc

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26-10-2016 дата публикации

Exhaust-gas turbocharger

Номер: EP2917531A4
Принадлежит: BorgWarner Inc

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26-11-2019 дата публикации

Control arrangement of an exhaust-gas turbocharger

Номер: US10487724B2
Принадлежит: BorgWarner Inc

A control arrangement ( 1 ) of an exhaust-gas turbocharger ( 4 ) which has a charger housing ( 2 ), the control arrangement ( 1 ) having a spindle ( 15 ) which has a first end region ( 24 ) arranged outside the charger housing ( 2 ) and a second end region ( 25 ) arranged within the charger housing ( 2 ) and having a valve disk ( 18 ) which is connected to the spindle ( 15 ), wherein the valve disk ( 18 ) and the spindle ( 15 ) are separate components, and wherein the spindle ( 15 ) is connected by way of its second end region ( 25 ) to the valve disk ( 18 ) by means of a connecting means ( 26 ).

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03-10-2018 дата публикации

Control arrangement of an exhaust-gas turbocharger

Номер: EP3382177A1
Принадлежит: BorgWarner Inc

The invention relates to a control arrangement (1) of an exhaust-gas turbocharger (4) which has a charger housing (2), having a spindle (15) which has a first end region (24) arranged outside the charger housing (2) and which has a second end region (25) arranged within the charger housing (2); having a valve disk (18) which is connected to the spindle (15), wherein the valve disk (18) and the spindle (15) are separate components, and wherein the spindle (15) is connected by way of its second end region (25) to the valve disk (18) by means of a connecting means (26).

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12-11-2015 дата публикации

Control arrangement of an exhaust-gas turbocharger

Номер: CA2952169A1
Принадлежит: BorgWarner Inc

The invention relates to a control arrangement (1) of an exhaust-gas turbocharger (4) which has a charger housing (2), having a spindle (15) which has a first end region (24) arranged outside the charger housing (2) and which has a second end region (25) arranged within the charger housing (2); having a valve disk (18) which is connected to the spindle (15), wherein the valve disk (18) and the spindle (15) are separate components, and wherein the spindle (15) is connected by way of its second end region (25) to the valve disk (18) by means of a connecting means (26).

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01-08-2013 дата публикации

System and method for assembling a solar cell matrix

Номер: WO2013068982A4
Принадлежит: SOMONT GMBH

The invention refers to a system (11) for the formation of a matrix(13)of solar cells, having a unit (16) with an input area (17) and an output area(18). Between the input area (17) and the output area (18) the strings (12) are conveyed on the conveying unit (16)in a conveying direction(19). The system (11) further comprising means (31) for placing strings (12) on the input area(17) and rotating means (41, 51, 61) designed to lift a string (12) from the conveying unit (16), rotate that string about axes and lower it onto the same conveying unit (16).The invention refers further to a method using such a system (11).

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