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公开(公告)号:US09759130B2
公开(公告)日:2017-09-12
申请号:US14033878
申请日:2013-09-23
Applicant: ROLLS-ROYCE PLC
Inventor: Ajith Appukuttan , Andrew Martin Rolt , Anthony John Moran
CPC classification number: F02C7/141 , F02C7/185 , F02C7/224 , F05D2260/213 , F05D2270/303 , Y02T50/671 , Y02T50/675 , Y02T50/676
Abstract: A cooling system for a gas turbine engine. The system includes a fuel air heat exchanger with a fuel passage that is in thermal contact with an engine cooling air passage. The system further includes a fuel deoxygenator located upstream of the fuel air heat exchanger and configured to deliver deoxygenated fuel to the fuel air heat exchanger fuel passage. The system also includes a valve configured to moderate engine cooling air flow to the engine cooling air passage.
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公开(公告)号:US09328978B2
公开(公告)日:2016-05-03
申请号:US13848530
申请日:2013-03-21
Applicant: ROLLS-ROYCE PLC
Inventor: Ajith Appukuttan , Yi Wang
CPC classification number: F28F27/02 , F02C7/14 , F02C7/224 , F05D2260/213 , F05D2260/80 , F28F2250/06
Abstract: The invention relates to a heat exchanger 10, comprising: a first unit 12 having a first conduit 16 for passing a flow of a first fluid through the first unit 12; a second unit 14 having a second conduit 28 for passing a flow of a second fluid through the second unit 28, wherein the flow of the first fluid is isolated from the second unit 14 and the flow of the second fluid is isolated from the first unit 12; and, a third conduit 40 connecting the first 12 and second 14 units, wherein the third conduit 40 is for carrying a flow of an intermediate fluid between the first 12 and second 14 units so as to transfer heat between the first fluid and the second fluid, when in use.
Abstract translation: 本发明涉及一种热交换器10,其包括:第一单元12,其具有用于使第一流体的流动通过第一单元12的第一导管16; 第二单元14具有用于使第二流体的流动通过第二单元28的第二导管28,其中第一流体的流动与第二单元14隔离,并且第二流体的流动与第一单元隔离 12; 以及连接第一12和第二单元14的第三导管40,其中第三导管40用于承载中间流体在第一12和第二单元14之间的流动,以便在第一流体和第二流体之间传递热量 在使用时。
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公开(公告)号:US09945247B2
公开(公告)日:2018-04-17
申请号:US14813755
申请日:2015-07-30
Applicant: ROLLS-ROYCE PLC
Inventor: Ajith Appukuttan , Benjamin Keeler , Paolo Vanacore
IPC: F01D25/02 , F01D9/02 , F01D15/08 , F01D17/10 , F01D25/10 , F02C7/141 , F02K3/115 , F02C7/047 , B64D13/06
CPC classification number: F01D25/02 , B64D2013/0607 , F01D9/02 , F01D15/08 , F01D17/105 , F01D25/10 , F02C7/047 , F02C7/141 , F02K3/115 , F05D2220/32 , F05D2240/10 , F05D2260/208 , Y02T50/675
Abstract: An anti-icing system for an engine section stator of a gas turbine engine. The system includes an environmental control system pre-cooler heat exchange system and a conduit. The environmental control system pre-cooler heat exchange system is configured to exchange heat between air bled from a compressor of the engine and bypass duct air. The conduit is configured to exchange heat from the pre-cooler heat exchange system to a heat transfer medium. The conduit is also configured to transfer the heat from the heat transfer medium to the engine section stator.
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