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Gas turbine engine fan cooled heat exchanger

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-003/02   
미국특허분류(USC) 60/2261 ; 60/266 ; 60/267
출원번호 US-0015243 (1993-02-05)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 71  인용 특허 : 0
초록
▼

A fan-jet gas turbine engine heat exchanger is cooled by fan air taken from the fan duct at a relatively high pressure region of the fan nozzle upstream of the fan nozzle\s throat and exhausted into a relatively low pressure region of the fan nozzle upstream of the throat. One embodiment provides a cooling air duct with a forward facing scoop at the duct\s inlet for capturing cooling air and providing greater dynamic pressure recovery. A diffuser is located upstream of the heat exchanger and a nozzle is located downstream of the heat exchanger with a noz...

대표
청구항
▼

A cooling apparatus for a heat exchanger used with an aircraft gas turbine engine having a fan duct including a fan nozzle and fan nozzle throat, said cooling apparatus comprising: a cooling air duct means, said cooling air duct means having a cooling duct inlet at a relatively high pressure region of the fan nozzle upstream of the fan nozzle throat and a cooling duct outlet at a relatively low pressure region of the fan nozzle upstream of the fan nozzle throat, a heat exchanger means disposed in the duct means between said cooling duct inlet and said co...

이 특허를 인용한 특허 피인용횟수: 71

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