公开(公告)号：EP3093467B1

公开(公告)日：2018-09-26

申请号：EP16168488.1

申请日：2016-05-05

申请人： United Technologies Corporation

发明人： SHERIDAN, William G. ,  SUCIU, Gabriel L.

IPC分类号： F02C7/14 ,  B64C11/14 ,  F02C7/04 ,  F02C7/06 ,  F02C7/36 ,  F02K3/06

CPC分类号： F01D25/12 ,  B64C11/14 ,  F01D25/18 ,  F02C7/04 ,  F02C7/06 ,  F02C7/14 ,  F02C7/36 ,  F02K3/06 ,  F05D2220/32 ,  F05D2260/213 ,  F05D2260/40311 ,  F05D2260/98 ,  Y02T50/676

摘要： An oil cooling system is provided. The system may comprise an oil inlet, a manifold (142) fluidly coupled to the oil inlet, and a support strut (126) comprising internal tubing (132) fluidly coupled to the manifold (142). A heat exchanger (128) may be fluidly coupled to the internal tubing (132) of the support strut (126). A nose cone (130) may be disposed forward of the heat exchanger (128) and configured to rotate about an axis (A-A'). The heat exchanger (128) may be radially inward from a portion of the nose cone (130). A gas turbine engine (20) is also provided. The gas turbine engine (20) may comprise an epicyclic gear system (100) and fan (42) mechanically coupled to the epicyclic gear system (100). The fan (42) may be configured to rotate about an axis (A-A'). A nose cone (130) may be coupled to the fan (42) and configured to rotate about the axis (A-A'). A heat exchanger (128) may be forward of the fan (42) and in fluid communication with the epicyclic gear system (100).

公开(公告)号：EP3376011A1

公开(公告)日：2018-09-19

申请号：EP18157531.7

申请日：2018-02-20

申请人： Rolls-Royce plc

发明人： Pointon, James ,  Bradbrook, Stephen

IPC分类号： F02K3/06 ,  F02C7/36

CPC分类号： F02C7/36 ,  F01D25/24 ,  F02C9/18 ,  F02K3/06 ,  F05D2220/3216 ,  F05D2220/323 ,  F05D2240/60 ,  Y02T50/671

摘要： An aircraft gas turbine engine (10) includes a compressor system comprising a low pressure compressor (15) coupled to a low pressure shaft (23), and a high pressure compressor (16) coupled to a high pressure shaft (24). The engine includes an inner core casing (34) provided radially inwardly of compressor blades (42) of the compressor system, and an outer core casing arrangement provided radially outwardly of compressor blades (42) of the compressor system, the inner core casing and outer core casing arrangement defining a core working gas flow path (B) therebetween. The engine also includes a fan (13) coupled to the low pressure shaft (23) via a reduction gearbox (14); the outer core casing arrangement comprising a first outer core casing (48) and a second outer core casing (50) spaced radially outwardly from the first outer core casing (48). At an axial plane (E) of an inlet to the high pressure compressor (16), the second outer core casing (50) has an inner radius at least 1.4 times the inner radius of the first outer core casing (48).

公开(公告)号：EP3361057A2

公开(公告)日：2018-08-15

申请号：EP18156164.8

申请日：2018-02-09

申请人： Pratt & Whitney Canada Corp.

发明人： DUBREUIL, Jean ,  PLANTE, Ghislain ,  BEAUCHESNE-MARTEL, Philippe

IPC分类号： F01D15/10

CPC分类号： F02C7/32 ,  B64D27/10 ,  F01D15/00 ,  F01D15/10 ,  F01D15/12 ,  F02C3/10 ,  F02C3/103 ,  F02C3/107 ,  F02C3/145 ,  F02C6/20 ,  F02C6/206 ,  F02C7/36 ,  F04D29/053 ,  F04D29/321 ,  F05D2220/323 ,  F05D2220/324 ,  F05D2220/329 ,  F05D2240/60 ,  F05D2240/61 ,  F05D2260/4031

摘要： A method and a turbine rotor system for reducing over-speed potential of a turbine (21) of a gas turbine engine (10) involve mechanically connecting the turbine (21) to at least two mechanical loads (16, 22) via first and second mechanical drives (23a, 23b) extending in opposite directions from the turbine (21).

公开(公告)号：EP3353888A1

公开(公告)日：2018-08-01

申请号：EP16775109.8

申请日：2016-09-19

申请人： Voith Patent GmbH

发明人： MEHLICH, Andreas

IPC分类号： H02P9/06 ,  H02P9/10 ,  F01D15/10 ,  F02C7/36 ,  H02K49/04 ,  H02P3/04 ,  H02K7/108

CPC分类号： H02P9/06 ,  F01D15/10 ,  F02C7/36 ,  H02K7/108 ,  H02K49/04 ,  H02P3/04 ,  H02P9/10

摘要： Method and driveline used for stabilization of an electrical grid. The driveline for electricity generation comprises controllable power unit. Especially a gas motor or a gas turbine can be used as power unit. Further the driveline comprises a generator for electrical power generation. The generator is connectable to an electrical grid for feeding electrical power into the electrical grid. Between the generator and the power unit a torque limiting coupling is arranged in the driveline. To limit the torque the torque limiting coupling is slipping and a limited torque is provided to the generator.

公开(公告)号：EP3351825A1

公开(公告)日：2018-07-25

申请号：EP18152620.3

申请日：2018-01-19

申请人： Hamilton Sundstrand Corporation

发明人： LEMMERS, Glenn C. Jr.

IPC分类号： F16H3/66 ,  F01D15/00 ,  F02C7/36

CPC分类号： F16H3/66 ,  F01D15/00 ,  F02C7/36 ,  F05D2260/40311 ,  F16D7/00 ,  F16H2200/0039 ,  F16H2200/2007 ,  F16H2200/2038 ,  F16H2200/2041 ,  F16H2200/2066 ,  F16H2200/2069 ,  F16H2200/2082 ,  F16H2200/2084

摘要： A low speed spool multispeed transmission (100) includes an input shaft (101) configured to connect to a low pressure spool gearbox, a gear system (103) connected to the input shaft (101) and configured to convert an input speed (101) of the input shaft to an output speed within a predetermined speed range, wherein the gear system (103) includes a plurality of gear states to change the ratio between the input speed and the output speed, and an output shaft (105) connected to the gear system (103) to be rotated by the gear system (103) at the output speed, the output shaft (105) configured to connect to a generator. The input shaft (101) and the output shaft (105) can be coaxial.

公开(公告)号：EP2518279A3

公开(公告)日：2018-06-27

申请号：EP12166086.4

申请日：2012-04-27

申请人： United Technologies Corporation

发明人： Sheridan, William G.

IPC分类号： F01D25/16 ,  F02C7/36 ,  F02K3/06 ,  F16H57/08 ,  F16C23/04 ,  F16H57/04

CPC分类号： F16H1/28 ,  F01D25/16 ,  F02C7/36 ,  F16C23/045 ,  F16C2360/23 ,  F16H57/0427 ,  F16H57/082 ,  Y02T50/672 ,  Y10T29/49245

摘要： A fan gear drive system includes a torque frame (56) having a base (61) with integrated gear shafts (58) circumferentially spaced relative to one another. A fan shaft (34) is integrated with the base (61), such that the torque frame (56) provides rotational output from the fan gear drive system. Each shaft provides a shaft axis. A bearing assembly (60) is mounted on each of the gear shafts (58). The bearing assembly includes a spherical bearing (88) configured to permit angular movement of the bearing axis relative to the shaft axis.

公开(公告)号：EP3336334A1

公开(公告)日：2018-06-20

申请号：EP17207856.0

申请日：2017-12-15

申请人： United Technologies Corporation

发明人： SUCIU, Gabriel L. ,  MERRY, Brian ,  SHERIDAN, William G. ,  McCUNE, Michael E.

IPC分类号： F02C7/32 ,  F01D15/10 ,  F02C7/36

CPC分类号： F01D15/12 ,  F01D5/06 ,  F01D15/08 ,  F01D15/10 ,  F01D25/16 ,  F01D25/18 ,  F02C7/32 ,  F02C7/36 ,  F05D2220/32 ,  F05D2240/60 ,  F05D2260/402 ,  F05D2260/4031 ,  F05D2270/024 ,  F16H1/222 ,  F16H15/04 ,  F16H37/021

摘要： A gas turbine engine assembly includes, among other things, a turbine section having first and second turbines mounted for rotation about a common rotational axis (X) within an engine static structure, first and second turbine shafts (40, 50) coaxial with one another and to which the first and second turbines are respectively operatively mounted, an accessory drive gearbox (60) a first towershaft (68; 70) interconnecting the accessory drive gearbox (60) and the first or second turbine shaft (40; 50), and a multispeed transmission interconnecting the accessory drive gearbox (60) and at least one accessory component.

公开(公告)号：EP3093512B1

公开(公告)日：2018-06-20

申请号：EP16166119.4

申请日：2016-04-20

申请人： Rolls-Royce plc

发明人： Webster, John

IPC分类号： F16C17/02 ,  F16H57/04 ,  F16C3/02 ,  F16H57/08

CPC分类号： F16H57/08 ,  F02C7/36 ,  F05D2260/40311 ,  F16C3/02 ,  F16C17/02 ,  F16C2360/23 ,  F16C2361/61 ,  F16H1/28 ,  F16H57/0479 ,  F16H2057/085

摘要： A hollow cylindrical rotary bearing shaft for a planet gear of an epicyclic gear train, has a cylindrical outer surface accommodating the planet gear, and a wall thickness. The wall thickness of the bearing shaft varies circumferentially around a diameter of the bearing shaft so as to produce a pre-determined circumferential variation in the wall thickness.

公开(公告)号：EP3155234B1

公开(公告)日：2018-05-23

申请号：EP15732861.8

申请日：2015-06-11

申请人： SAFRAN AIRCRAFT ENGINES

发明人： LEPRETRE, Jean-Baptiste, Etienne, Bernard

IPC分类号： F01D25/16 ,  F02C7/32

CPC分类号： F01D15/12 ,  F01D15/08 ,  F01D15/10 ,  F01D25/04 ,  F01D25/16 ,  F01D25/20 ,  F01D25/24 ,  F02C7/32 ,  F02C7/36 ,  F05D2220/30 ,  F05D2220/50 ,  F05D2240/60 ,  F05D2260/96

公开(公告)号：EP3315716A1

公开(公告)日：2018-05-02

申请号：EP17182475.8

申请日：2017-07-21

申请人： Lee, Brent Wei-Teh

发明人： Lee, Brent Wei-Teh

IPC分类号： F01D1/32 ,  F02K7/00 ,  F02C3/16

CPC分类号： F02C3/165 ,  F01D1/32 ,  F01D5/02 ,  F01D13/02 ,  F02C5/04 ,  F02C7/16 ,  F02C7/22 ,  F02C7/36 ,  F02K7/005 ,  F05D2220/32 ,  F05D2220/76 ,  F05D2240/242 ,  F05D2240/35 ,  F05D2260/207 ,  F05D2260/40 ,  Y02T50/671 ,  Y02T50/675

摘要： A rotary device, comprising: a first central axle or shaft; an inlet configured to receive at least one fluid; and a first rotary disc in fluid communication with the inlet, configured to rotate around the first central axle or shaft, said rotary disc having a plurality of nozzles at a distal edge thereof, said nozzles being oriented to expel the fluid in a predetermined direction. Method of using the rotary device to produce mechanical energy.

摘要翻译： 一种旋转装置，包括：第一中心轴或轴; 构造成接收至少一种流体的入口; 以及与所述入口流体连通的第一旋转盘，所述第一旋转盘构造成围绕所述第一中心轴或轴旋转，所述旋转盘在其远端边缘处具有多个喷嘴，所述喷嘴定向成沿预定方向排出流体。 使用旋转装置产生机械能的方法。