公开(公告)号：EP3712387A1

公开(公告)日：2020-09-23

申请号：EP20162219.8

申请日：2020-03-10

申请人： United Technologies Corporation

发明人： ROBERGE, Gary D.

IPC分类号： F01D11/24 ,  F01D17/20 ,  F01D25/12 ,  F01D19/00 ,  F01D11/12

摘要： A compressor case (62) for a gas turbine engine (20) includes an annular body that extends circumferentially around a center axis (A) and extends axially along the center axis (A). A first bleed manifold (70) is formed on an outer surface of the annular body and encloses a first plenum (71). A second bleed manifold (72) is formed on the outer surface of the annular body and is axially aft of the first bleed manifold (70). The second bleed manifold (72) encloses a second plenum (73). A bleed inlet (74) extends through the annular body and into the first bleed manifold (70). Cooling passages (76) are formed in the annular body, and each of the cooling passages (76) extends from the first plenum (71) to the second plenum (73) and fluidically connects the first plenum (71) to the second plenum (73).

公开(公告)号：EP3670850A1

公开(公告)日：2020-06-24

申请号：EP19203223.3

申请日：2019-10-15

申请人： United Technologies Corporation

发明人： PARNIN, Francis

IPC分类号： F01D17/20 ,  F01D25/20 ,  F16K17/00

摘要： A two-tier lubrication system (100) may comprise an oil nozzle (118) located in a bearing compartment (120). A main oil system (101) may be configured to provide oil to the oil nozzle (118). A scavenge system (130) may be configured to collect oil from the bearing compartment (120). A valve (160) may be fluidly coupled between the main oil system (101) and the scavenge system (130). The valve (160) may be configured to actuate between a main flow position and a scavenge flow position.

公开(公告)号：EP2522813B1

公开(公告)日：2019-01-16

申请号：EP12166283.7

申请日：2012-05-01

申请人： Rolls-Royce plc

发明人： Foster, Peter Frederick William

IPC分类号： F01D17/02 ,  F01D17/20 ,  F01D25/08 ,  F01D25/12 ,  F02C7/12 ,  F02C7/18 ,  F02C9/16 ,  F02C9/18

公开(公告)号：EP3109167B1

公开(公告)日：2018-10-03

申请号：EP16176139.0

申请日：2016-06-24

申请人： Pratt & Whitney Canada Corp.

发明人： ULLYOTT, Richard ,  JONES, Anthony ,  JULIEN, Andre ,  THOMASSIN, Jean

IPC分类号： B64D41/00 ,  B64C13/40 ,  F01C1/22 ,  F01C21/00 ,  F01D17/20 ,  F01D25/18 ,  F02B33/40 ,  F02B41/10 ,  F02B55/00 ,  F02C7/06 ,  F02C7/32 ,  F02C7/36 ,  F02B63/04

CPC分类号： B64D41/00 ,  B64D13/06 ,  B64D33/08 ,  B64D2013/0611 ,  B64D2013/0618 ,  B64D2041/002 ,  F01C1/22 ,  F01C21/008 ,  F01C21/06 ,  F01C21/08 ,  F01D5/06 ,  F01D15/10 ,  F01D17/20 ,  F01D25/18 ,  F02B33/40 ,  F02B41/10 ,  F02B55/00 ,  F02B63/042 ,  F02C7/06 ,  F02C7/32 ,  F02C7/36 ,  F04D27/009 ,  F04D29/286 ,  F04D29/321 ,  F04D29/462 ,  F04D29/563 ,  F04D29/582 ,  F05D2220/50 ,  F05D2220/76 ,  F05D2260/211 ,  Y02T10/163 ,  Y02T10/17 ,  Y02T50/44 ,  Y02T50/53

摘要： An auxiliary power unit (10) for an aircraft, having a compressor (18), an intercooler (26) including first conduit(s) having an inlet in fluid communication with the compressor outlet (180) and second conduit(s) configured for circulation of a coolant therethrough, an engine core (12) having an inlet (12i) in fluid communication with an outlet of the first conduit(s), and a bleed conduit (74) in fluid communication with the outlet of the first conduit(s) through a bleed air valve. The auxiliary power unit may include a generator (14) in driving engagement with the shaft of the engine core (12) to provide electrical power for the aircraft. A method of providing compressed air and electrical power to an aircraft is also discussed.

公开(公告)号：EP3187696A1

公开(公告)日：2017-07-05

申请号：EP16205159.3

申请日：2016-12-19

申请人： General Electric Company

发明人： MONIZ, Thomas Ory ,  ROSE, Joseph George ,  ORLANDO, Robert Joseph ,  CHOU, Chenyu Jack

IPC分类号： F01D17/16 ,  F01D17/20

CPC分类号： F01D17/145 ,  F01D15/08 ,  F01D17/105 ,  F01D17/162 ,  F01D17/20 ,  F04B9/02 ,  F04B43/0081 ,  F04B43/04 ,  F04B53/10 ,  F04B53/16 ,  F04D29/522 ,  F05D2220/32 ,  F05D2240/12 ,  F05D2270/80

摘要： An actuator (402) includes a pump (705) including a first cavity (708) and a diaphragm (704) coupled in flow communication with the first cavity. The diaphragm is configured to pressurize a fluid contained in the first cavity. The pump further includes a first valve (706) coupled in flow communication with the first cavity. The first valve is configured to release fluid from the first cavity when the first cavity is pressurized. The actuator also includes a piston assembly (712,713) operatively coupled to the pump.

摘要翻译： 致动器（402）包括泵（705），该泵包括与第一腔流动连通的第一腔（708）和隔膜（704）。 隔膜被构造成对包含在第一腔体中的流体加压。 泵还包括与第一腔流动连通的第一阀（706）。 第一阀构造成当第一腔被加压时从第一腔释放流体。 致动器还包括可操作地联接到泵的活塞组件（712,713）。

公开(公告)号：EP3106631A1

公开(公告)日：2016-12-21

申请号：EP15768319.4

申请日：2015-03-26

申请人： Mitsubishi Hitachi Power Systems, Ltd. ,  Mitsubishi Hitachi Power Systems Europe, Ltd.

发明人： MATSUMOTO Kazunari ,  SUZUKI Jumpei ,  RUBIO Elvio ,  RATIA Pablo ,  DANIEL Carlos Mora

IPC分类号： F01K23/10 ,  F01D17/00 ,  F01D17/20 ,  F02C9/28 ,  F02C9/42

摘要： In a method for operating a multi-shaft combined cycle plant, a low load mode for adjusting the output of the multi-shaft combined cycle plant by adjusting only the output of a gas turbine, and a high load mode in which the output of the multi-shaft combined cycle plant can be adjusted by adjusting the output of both the gas turbine and a steam turbine, are switched according to the required load (S15). In the low load mode, the steam turbine is supplied with steam at a standby flow rate amount at which the steam turbine can maintain a predetermined initial load, and the initial load is imposed on the steam turbine (S21 to 23).

公开(公告)号：EP3052769A4

公开(公告)日：2016-11-09

申请号：EP14856933

申请日：2014-09-12

申请人： UNITED TECHNOLOGIES CORP

发明人： SMITH DARREN M

IPC分类号： F01D11/22 ,  F01D17/02 ,  F01D17/20 ,  F02C7/36

CPC分类号： F01D11/22 ,  F01D17/02 ,  F01D17/20 ,  F02C7/36

摘要： A first actuator moves a compressor rotor and compressor blades along a rotational axis of the compressor rotor. A turbine rotor includes a plurality of turbine blades each extending radially outwardly from the turbine rotor to an outer tip. A turbine housing surrounds each of the turbine blade tips. The turbine housing has an inner surface, and a turbine tip clearance is defined between each of the turbine blade tips and the inner surface of the turbine housing. A second actuator moves the turbine rotor and the turbine blades along a rotational axis of the turbine rotor. A control controls the first actuator of the compressor rotor, and the second actuator of the turbine rotor to control the compressor tip clearance and the turbine tip clearance.

摘要翻译： 第一致动器沿着压缩机转子的旋转轴线移动压缩机转子和压缩机叶片。 涡轮转子包括多个涡轮机叶片，每个涡轮叶片从涡轮机转子径向向外延伸到外部末端。 涡轮机壳体围绕每个涡轮机叶片尖端。 涡轮机壳体具有内表面，并且涡轮机顶端间隙被限定在每个涡轮机叶片尖端和涡轮机壳体的内表面之间。 第二致动器沿着涡轮机转子的旋转轴线移动涡轮转子和涡轮机叶片。 控制器控制压缩机转子的第一致动器和涡轮转子的第二致动器以控制压缩机顶端间隙和涡轮机顶端间隙。

公开(公告)号：EP2876261B1

公开(公告)日：2016-11-09

申请号：EP14194132.8

申请日：2014-11-20

申请人： Rolls-Royce Deutschland Ltd & Co KG

发明人： Homeyer, Christian

IPC分类号： F01D17/08 ,  F01D17/20 ,  F01D21/00 ,  F01D25/26 ,  F01D25/28

CPC分类号： F01D21/003 ,  F01D17/085 ,  F01D17/20 ,  F01D25/26 ,  F01D25/28 ,  F05D2220/32 ,  F05D2230/60 ,  F05D2230/64 ,  F05D2270/303 ,  F05D2270/80 ,  Y10T29/4932

公开(公告)号：EP3039253A1

公开(公告)日：2016-07-06

申请号：EP14753387.1

申请日：2014-07-31

申请人： Siemens Energy, Inc.

发明人： BEVLY, Alex J. III ,  MCCONKEY, Joshua S.

IPC分类号： F01D17/20 ,  F01D21/00 ,  F01D17/02

CPC分类号： H04Q9/14 ,  F01D17/02 ,  F01D17/20 ,  F01D21/003 ,  H04Q2209/40 ,  Y02T50/672

摘要： In a telemetry system (100) in a high-temperature environment of a combustion turbine engine (10), a wireless power-receiving coil assembly (116) may be affixed to a movable component (104) of the turbine engine. Power-receiving coil assembly (116) may include a radio-frequency transparent housing (130) having an opening (132). A lid (134) may be provided to close the opening of the housing. Lid (134) may be positioned to provide support against a surface (120) of the movable component. An induction coil (133) is disposed in the housing distally away from the lid and encased between a first layer (136) and a last layer (140) of a potting adhesive. Lid (134) is arranged to provide vibrational buffering between the surface (120) of the movable component (104) and the layers encasing the induction coil.

公开(公告)号：EP2930315A1

公开(公告)日：2015-10-14

申请号：EP14164187.8

申请日：2014-04-10

申请人： Siemens Aktiengesellschaft

发明人： Gericke, Frank

IPC分类号： F01D17/20 ,  F01D25/24

CPC分类号： F01D17/20 ,  F01D25/243 ,  F05D2220/31 ,  H01R13/52

摘要： Die Erfindung betrifft eine Steckverbindung (20) für zwei elektrische Messignalleitungen (18, 19) in einer Dampfturbine (5), wobei die Steckverbindung (20) im Dampfraum (4) zwischen Innengehäuse (2) und Aussengehäuse (3) der Dampfturbine angeordnet ist und eine geeignete dampfdichte Ummantelung (23) aufweist, um die Steckverbindung (20) vor den hohen Dampfparametern zu schützen.

摘要翻译： 本发明涉及在内部壳体（2）和所述外部壳体的蒸汽涡轮机（3）被布置和之间的蒸气空间（4）中的蒸汽涡轮机（5）的插塞连接（20），用于两个电Messignalleitungen（18，19），其中，所述连接器（20） 具有合适的防汽鞘（23），以保护从高蒸汽参数的连接器（20）。