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公开(公告)号：US20250154902A1
公开(公告)日：2025-05-15
申请号：US18916983
申请日：2024-10-16
Applicant: ROLLS-ROYCE plc
Inventor： Michael C WILLMOT , Richard PEACE
IPC: F02C7/22 , F02C7/268 , H01M8/04082
Abstract: A propulsion system comprises a propulsive hydrogen-burning gas turbine engine, a first tank storing liquid hydrogen with an ullage and a first fuel line including a fuel pump and a vaporiser, the first fuel line providing gaseous hydrogen to the engine during operation of the system. A second tank storing gaseous hydrogen is coupled by a second fuel line to the first fuel line at a position thereon between the vaporiser and the engine, providing for engine start-up (when the vaporiser is inoperative) and power-boosting during operation of the system. A duct connects gaseous hydrogen within the second tank to the ullage in the first tank in order maintain pressure in the first tank as liquid hydrogen within it is depleted, preventing cavitation of liquid hydrogen within the fuel pump.
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公开(公告)号：US20200291866A1
公开(公告)日：2020-09-17
申请号：US16401225
申请日：2019-05-02
Applicant: ROLLS-ROYCE plc
Inventor： Richard PEACE , Robert GOULDS
Abstract: A gas turbine engine comprising: a compressor; a first turbine; and a first compressor bleed valve in fluid communication with the compressor and configured to release bleed air from the compressor; wherein the first compressor bleed valve is configured to release bleed air to a downstream location in the engine, the downstream location being downstream of the first turbine; wherein the first compressor bleed valve is configured to open wherein the first compressor bleed valve is configured to open to at least two positions, to thereby release a variable amount of bleed air from the compressor.
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公开(公告)号：US20190178106A1
公开(公告)日：2019-06-13
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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公开(公告)号：US20180010524A1
公开(公告)日：2018-01-11
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 , Y02T50/671
Abstract: A mounting bracket for mounting an accessory to a gas turbine engine comprises a space frame structure. The space frame structure comprises a plurality of struts joined to one another at nodes.
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公开(公告)号：US20130264110A1
公开(公告)日：2013-10-10
申请号：US13716300
申请日：2012-12-17
Applicant: ROLLS-ROYCE PLC
Inventor： Michael Christopher WILLMOT , John Philip RICHARDSON , Jason WATKISS , Paul BROUGHTON , Richard PEACE , Gary Alan SKINNER , Robin Charles KENNEA
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 including electrical raft having electrical conductors embedded in a rigid material is provided. The electrical assembly has an electrically conductive screen layer. The electrically conductive screen layer provides electromagnetic protection to the electrical conductors. The electrically conductive screen layer is electrically connected to a mounting fixture, which in turn may be electrically connected to an apparatus on which the electrical assembly may be mounted. The electrical raft is used to transport electrical signals (which may be, for example power and/or control signals), for example around a gas turbine engine.
Abstract translation: 提供了一种电气组件，其包括具有嵌入在刚性材料中的电导体的电筏。 电组件具有导电屏蔽层。 导电屏层为电导体提供电磁保护。 导电屏蔽层电连接到安装固定件，安装固定件又可电连接到可安装电气组件的装置。 电筏用于传输电信号（可能是例如功率和/或控制信号），例如在燃气涡轮发动机周围。
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Patent Agency Ranking
公开(公告)号：US20130160460A1
公开(公告)日：2013-06-27
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: F02C7/00
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：US20130160458A1
公开(公告)日：2013-06-27
申请号：US13716808
申请日：2012-12-17
Applicant: ROLLS-ROYCE PLC
Inventor： Michael Christopher WILLMOT , Paul BROUGHTON , Richard PEACE , Gary Alan SKINNER , Robin Charles KENNEA
IPC: F02C7/12
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 assembly for a gas turbine engine is provided. The raft assembly comprises a rigid electrical raft formed of a rigid material that includes an electrical system comprising electrical conductors embedded in the rigid material. The raft assembly further comprises an engine component that is mounted to the electrical raft. The electrical raft includes one or more integral cooling passages which guide a coolant fluid through the raft to cool the engine component
Abstract translation: 提供了一种用于燃气涡轮发动机的电动筏组件。 筏组件包括由刚性材料形成的刚性电筏，其包括包含嵌入刚性材料中的电导体的电气系统。 筏组件还包括安装到电筏的发动机部件。 电筏包括一个或多个整体冷却通道，其引导冷却剂流体通过筏以冷却发动机部件
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公开(公告)号：US20200290741A1
公开(公告)日：2020-09-17
申请号：US16401220
申请日：2019-05-02
Applicant: ROLLS-ROYCE plc
Inventor： Richard PEACE , Robert GOULDS
Abstract: A single-piece gas turbine engine bleed duct for a gas turbine engine including: a main airflow conduit configured to transmit a bleed flow to a location outside the gas turbine engine; a pressure regulating valve for regulating airflow through the main airflow conduit; a first inlet duct for directing airflow to the main airflow conduit and toward the pressure regulating valve, the first inlet duct including a non-return valve; and a second inlet duct for directing airflow to the main airflow conduit and toward the pressure regulating valve, the second inlet duct including a control valve; wherein each of the first and second inlet ducts are directly connectable to an engine casing of a gas turbine engine.
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公开(公告)号：US20200010208A1
公开(公告)日：2020-01-09
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：US20190259364A1
公开(公告)日：2019-08-22
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 , F02C7/24 , F01D25/24 , G10K11/172 , H02K5/24 , H02K7/18
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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