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특허 상세정보

Gas turbine fuel system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-001/00   
미국특허분류(USC) 60/739 ; 60/742 ; 60/746 ; 138/114
출원번호 US-0255191 (1981-04-17)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 71  인용 특허 : 4
초록

A gas turbine engine is provided with an improved fuel system that features a fuel manifold with a primary and secondary fuel flowpath circumventing a combustor section of the engine. The manifold is formed with a double-walled construction for the purpose of withstanding high temperatures or fires around the combustor section and, additionally, to provide a secondary flowpath for draining any fuel leakage from the manifold. The two walls of the manifold include an inner wall that encloses the primary fuel flowpath through the fuel system. A concentric o...

대표
청구항

For a gas turbine engine having a combustor, a fuel-supply system for supplying fuel to the combustor and a plurality of fuel injectors for carrying fuel through a combustor outer casing to inject the fuel inside the combustor, an improved fuel-supply system comprising: a fuel manifold positionable around the combustor outer casing and including a primary fuel flowpath effective for providing fuel to said fuel injectors and a secondary fuel flowpath effective for collecting any leakage fuel that escapes said primary flowpath, wherein said fuel manifold i...

이 특허를 인용한 특허 피인용횟수: 71

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