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Rotary valve multiple combustor pulse detonation engine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-005/02   
미국특허분류(USC) 60/3938 ; 60/3939 ; 60/3976 ; 60/3978
출원번호 US-0205505 (1994-03-04)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 70  인용 특허 : 0
초록

A pulse detonation engine is provided with at least one detonation combustor selectively coupled to an air inlet and fuel source. The detonation combustors are equipped with either active or passive means to dissipate the heat of detonation. Fuel, air, and an oxidizer can be fed to said detonation combustors either through a rotary valve or through a conically shaped injector head.

대표
청구항
▼

A rotary valve multiple combustor pulse detonation engine, comprising; at least two detonation chambers, each having an inlet end and an outlet end and further including means for preventing heat degradation of said chambers; a fuel manifold for supplying fuel from a fuel source to said at least two detonation chambers at said inlet ends; an inlet air duct manifold for supplying air to said at least two detonation chambers at said inlet ends; a means for initiating a pulsed supersonic shock wave-triggered detonation combustion wave in said at least two d...

이 특허를 인용한 특허 피인용횟수: 70

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