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公开(公告)号:US11808216B1
公开(公告)日:2023-11-07
申请号:US17837749
申请日:2022-06-10
Inventor: Paul K. Johnson , Andrew J. Eifert , Richard Peace , Richard Young , Robert T. Duge
CPC classification number: F02C9/18 , F02C6/08 , F05D2220/323 , F05D2260/605 , F05D2260/606 , F05D2270/3061
Abstract: A propulsion system includes two gas turbine engines and an air-provisioning system. The air-provisioning system includes a first ejector, a second ejector, a plenum fluidically connected with the first ejector and the second ejector, and a first propulsor. The air-provisioning system is configured to bleed and mix air from each gas turbine engine in the ejectors so as to provide selectively a flow of plenum air from the plenum to the first propulsor at a desired pressure and a desired flow rate to power the first propulsor.
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公开(公告)号:US09713202B2
公开(公告)日:2017-07-18
申请号:US13716503
申请日:2012-12-17
Applicant: ROLLS-ROYCE PLC
Inventor: Paul Broughton , Richard Peace , Gary Alan Skinner , Robin Charles Kennea
IPC: F02C7/12 , F02C7/20 , H05B3/28 , B23P6/00 , H02G3/04 , H01R12/00 , H02G3/32 , B60R16/02 , B64C3/34 , F02C7/141 , B60R16/08 , F02C7/16 , H01R12/57 , H01R12/59 , H01R12/51 , H01R12/61 , H02G3/00 , B60R16/00 , B64D29/08 , F02C7/00 , F02C7/32 , H02G1/00 , H02G3/02 , F02C7/047 , F02C7/224 , F24H1/10 , H05B1/02 , H05K7/20
CPC classification number: H05B3/28 , B23P6/005 , B60R16/00 , B60R16/02 , B60R16/0207 , B60R16/0215 , B60R16/08 , B64C3/34 , B64D29/08 , F02C7/00 , F02C7/047 , F02C7/12 , F02C7/141 , F02C7/16 , F02C7/20 , F02C7/224 , F02C7/32 , F05D2260/30 , F05D2300/603 , F16M13/02 , F24H1/105 , H01R12/00 , H01R12/51 , H01R12/515 , H01R12/57 , H01R12/59 , H01R12/592 , H01R12/61 , H02G1/00 , H02G3/00 , H02G3/02 , H02G3/04 , H02G3/0487 , H02G3/32 , H05B1/0236 , H05K1/0393 , H05K7/20 , H05K2201/029 , Y02T50/672 , Y10T29/49002 , Y10T29/49117 , Y10T29/49234 , Y10T29/49236 , Y10T29/49238 , Y10T156/10
Abstract: The present invention provides a gas turbine engine part which has a primary purpose in the engine which is structural and/or aerodynamic. The part is formed of rigid composite material, and has an electrical system comprising electrical conductors permanently embedded in the composite material. This provides advantages in terms of weight, complexity, and build time.
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公开(公告)号:US11527228B2
公开(公告)日:2022-12-13
申请号:US16266411
申请日:2019-02-04
Applicant: ROLLS-ROYCE plc
Inventor: Richard Peace , Oliver C. Taylor-Tibbott , John G. Marshall
IPC: G10K11/168 , F01D25/24 , F02C7/24 , G10K11/172 , H02K5/24 , H02K7/18 , F02K1/82 , F02C7/045
Abstract: A fairing for a power generation machine, the fairing comprising: a first layer comprising a metallic material; a second layer comprising a composite; and a third layer positioned between the first layer and the second layer, the third layer being configured to attenuate acoustic waves over a predetermined frequency range.
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公开(公告)号:US11383853B2
公开(公告)日:2022-07-12
申请号:US16437263
申请日:2019-06-11
Applicant: ROLLS-ROYCE plc
Inventor: Richard Peace , Adam Newman
Abstract: An electric propulsion unit (102) for an aircraft is shown. A fan (202) produces a pressured airflow (P) by raising the pressure of an incident airflow (I). An electric machine (201) is arranged to drive the fan and is located within a casing (204). A primary cooling circuit (205) is located within the casing, and includes the electric machine and a first pass of a fluid-fluid heat exchanger (208), thereby placing the electric machine and the fluid-fluid heat exchanger in thermal communication. A secondary cooling circuit includes a second pass of the fluid-fluid heat exchanger and an air-fluid heat exchanger (210) located within the pressurised airflow produced by the fan, thereby placing the fluid-fluid heat exchanger and the air-fluid heat exchanger in thermal communication.
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公开(公告)号:US09456472B2
公开(公告)日:2016-09-27
申请号:US13716244
申请日:2012-12-17
Applicant: ROLLS-ROYCE PLC
Inventor: Justin Dalton , Paul Broughton , Richard Peace , Gary Alan Skinner , Robin Charles Kennea
IPC: B23P6/00 , B60R16/02 , F02C7/00 , F02C7/047 , F02C7/12 , F02C7/20 , F02C7/224 , F02C7/32 , F24H1/10 , H01R12/00 , H02G1/00 , H02G3/02 , H02G3/32 , H02G1/02 , H05B3/28 , B64C3/34 , B60R16/08 , F02C7/141 , F02C7/16 , H02G3/04 , H05B1/02
CPC classification number: H05B3/28 , B23P6/005 , B60R16/00 , B60R16/02 , B60R16/0207 , B60R16/0215 , B60R16/08 , B64C3/34 , B64D29/08 , F02C7/00 , F02C7/047 , F02C7/12 , F02C7/141 , F02C7/16 , F02C7/20 , F02C7/224 , F02C7/32 , F05D2260/30 , F05D2300/603 , F16M13/02 , F24H1/105 , H01R12/00 , H01R12/51 , H01R12/515 , H01R12/57 , H01R12/59 , H01R12/592 , H01R12/61 , H02G1/00 , H02G3/00 , H02G3/02 , H02G3/04 , H02G3/0487 , H02G3/32 , H05B1/0236 , H05K1/0393 , H05K7/20 , H05K2201/029 , Y02T50/672 , Y10T29/49002 , Y10T29/49117 , Y10T29/49234 , Y10T29/49236 , Y10T29/49238 , Y10T156/10
Abstract: The present invention provides a rigid raft formed of rigid composite material. The raft has an electrical system and/or a fluid system embedded therein. The raft further has a tank for containing liquid integrally formed therewith. The tank can be formed of the rigid composite material. The tank can be for a gas turbine engine.
Abstract translation: 本发明提供由刚性复合材料形成的刚性筏。 筏具有嵌入其中的电气系统和/或流体系统。 筏还具有用于容纳与其一体形成的液体的罐。 罐可以由刚性复合材料形成。 该罐可用于燃气涡轮发动机。
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公开(公告)号:US10072583B2
公开(公告)日:2018-09-11
申请号:US15622419
申请日:2017-06-14
Applicant: ROLLS-ROYCE PLC
Inventor: Richard Peace , Rong Yang , Joshua Lee , Liam Kelly
CPC classification number: F02C7/32 , F01D25/24 , F01D25/28 , F05D2220/32 , F05D2230/30 , F05D2250/75 , H05K999/99 , Y02T50/671
Abstract: A mounting bracket for mounting an accessory to a gas turbine engine, the mounting bracket including a space frame structure. The space frame structure including a plurality of struts joined to one another at nodes.
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公开(公告)号:US09699833B2
公开(公告)日:2017-07-04
申请号:US13716439
申请日:2012-12-17
Applicant: ROLLS-ROYCE PLC
Inventor: Paul Broughton , Richard Peace , Gary Alan Skinner , Robin Charles Kennea
IPC: F02C7/32 , H05B3/28 , F02C7/12 , F02C7/20 , B23P6/00 , H02G3/04 , H01R12/00 , H02G3/32 , B60R16/02 , B64C3/34 , F02C7/141 , B60R16/08 , F02C7/16 , H01R12/57 , H01R12/59 , H01R12/51 , H01R12/61 , H02G3/00 , B60R16/00 , B64D29/08 , F02C7/00 , H02G1/00 , H02G3/02 , F02C7/047 , F02C7/224 , F24H1/10 , H05B1/02 , H05K7/20
CPC classification number: H05B3/28 , B23P6/005 , B60R16/00 , B60R16/02 , B60R16/0207 , B60R16/0215 , B60R16/08 , B64C3/34 , B64D29/08 , F02C7/00 , F02C7/047 , F02C7/12 , F02C7/141 , F02C7/16 , F02C7/20 , F02C7/224 , F02C7/32 , F05D2260/30 , F05D2300/603 , F16M13/02 , F24H1/105 , H01R12/00 , H01R12/51 , H01R12/515 , H01R12/57 , H01R12/59 , H01R12/592 , H01R12/61 , H02G1/00 , H02G3/00 , H02G3/02 , H02G3/04 , H02G3/0487 , H02G3/32 , H05B1/0236 , H05K1/0393 , H05K7/20 , H05K2201/029 , Y02T50/672 , Y10T29/49002 , Y10T29/49117 , Y10T29/49234 , Y10T29/49236 , Y10T29/49238 , Y10T156/10
Abstract: An electrical assembly 600 comprising an electrical raft 200 and an electronic unit 300 is provided to a gas turbine engine 10. The electrical raft 200 has electrical conductors 252 embedded in a rigid material 220, which may be a rigid composite material. The electrical conductors 252 are in electrical contact with the electronic unit 300. When the electronic unit 300 is installed, at least a part 310 of it forms a part of a gas-washed surface of the engine 10. The electronic unit 300 is then easily accessible from the engine 10, and potentially complex and/or heavy access doors/panels may not be required.
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公开(公告)号:US09426844B2
公开(公告)日:2016-08-23
申请号:US13716516
申请日:2012-12-17
Applicant: ROLLS-ROYCE PLC
Inventor: Paul Broughton , Richard Peace , Gary Alan Skinner , Robin Charles Kennea , Michael Christopher Willmot , Philip Summerfield
IPC: H05B3/28 , F02C7/12 , F02C7/20 , B23P6/00 , H02G3/04 , H01R12/00 , H02G3/32 , B60R16/02 , B64C3/34 , F02C7/141 , H01R12/57 , H01R12/59 , H01R12/51 , H01R12/61 , H02G3/00 , B60R16/08 , F02C7/16 , B60R16/00 , B64D29/08 , F02C7/00 , F02C7/32 , H02G1/00 , H02G3/02 , F02C7/047 , F02C7/224 , F24H1/10 , H05B1/02
CPC classification number: H05B3/28 , B23P6/005 , B60R16/00 , B60R16/02 , B60R16/0207 , B60R16/0215 , B60R16/08 , B64C3/34 , B64D29/08 , F02C7/00 , F02C7/047 , F02C7/12 , F02C7/141 , F02C7/16 , F02C7/20 , F02C7/224 , F02C7/32 , F05D2260/30 , F05D2300/603 , F16M13/02 , F24H1/105 , H01R12/00 , H01R12/51 , H01R12/515 , H01R12/57 , H01R12/59 , H01R12/592 , H01R12/61 , H02G1/00 , H02G3/00 , H02G3/02 , H02G3/04 , H02G3/0487 , H02G3/32 , H05B1/0236 , H05K1/0393 , H05K7/20 , H05K2201/029 , Y02T50/672 , Y10T29/49002 , Y10T29/49117 , Y10T29/49234 , Y10T29/49236 , Y10T29/49238 , Y10T156/10
Abstract: An electrical raft 200 is provided that has electrical conductors 252 embedded in a rigid material 220. The electrical raft 200 may have other embedded components, such as embedded fluid pipes 210. The electrical raft 200 is provided with a raft map 400 that indicates the location and/or path of components embedded in the electrical raft 200. The raft map 400 can be used to identify the positions of the embedded components, and may also be provided with active elements, such as LEDs, which may be used to indicate an operating state of the systems/components embedded in the electrical raft 200. The raft map 400 may be useful in assembly, repair and fault diagnosis, for example.
Abstract translation: 提供电筏200,其具有嵌入刚性材料220中的电导体25.电筏200可以具有其它嵌入的部件,例如嵌入式流体管道210.电筏200设置有筏图400,其指示位置 和/或嵌入电筏200中的部件的路径。筏图400可以用于识别嵌入式部件的位置,并且还可以设置有活动元件,例如LED,其可以用于指示操作 嵌入在电动筏200中的系统/组件的状态。例如,筏图400可用于组装,修理和故障诊断。
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公开(公告)号:US09259808B2
公开(公告)日:2016-02-16
申请号:US13716648
申请日:2012-12-17
Applicant: ROLLS-ROYCE PLC
Inventor: Paul Broughton , Richard Peace
CPC classification number: B23P6/005 , F02C7/32 , F05D2230/60 , F05D2230/70 , F05D2230/72 , Y02T50/672 , Y10T29/49238
Abstract: A gas turbine engine 10 is provided with rigid raft assemblies 290, which may be electrical harness raft assemblies 290 comprising electrical conductors embedded in a rigid composite material. The rigid raft assemblies 290 can be provided with engine dressings, such as pipework and ECUs to produce an electrical raft assembly. In order to assemble or dress the gas turbine engine 10, the rigid raft assemblies can be pre-prepared to incorporate at least a part of at least one gas turbine engine system/component before being installed on the gas turbine engine 10. During maintenance, whole raft assemblies can be removed and replaced with corresponding, pre-prepared assemblies. This can save considerable time during engine build and maintenance.
Abstract translation: 燃气涡轮发动机10设置有刚性筏组件290,其可以是包括嵌入刚性复合材料中的电导体的电气筏组件290。 刚性筏组件290可以设置有发动机敷料,例如管道和ECU,以产生电筏组件。 为了组装或装饰燃气涡轮发动机10,可以预先准备刚性筏组件以在安装在燃气涡轮发动机10上之前并入至少一个燃气涡轮发动机系统/部件的至少一部分。在维护期间, 整个筏组件可以拆下并用相应的预先准备的组件替换。 这可以在发动机制造和维护期间节省大量时间。
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公开(公告)号:US11339684B2
公开(公告)日:2022-05-24
申请号:US16197557
申请日:2018-11-21
Applicant: ROLLS-ROYCE plc
Inventor: Richard Peace , Oliver C. Taylor-Tibbott
Abstract: A fairing for a power generation machine, the fairing comprising: a first layer comprising a metallic material and defining a first surface and a second opposite surface, the first layer being configured to enable the fairing to be coupled to the power generation machine; and a second layer comprising a composite material and defining a first surface and a second opposite surface, the second layer being coupled to the first layer, the second surface of the second layer defining an external surface of the fairing.
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