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특허 상세정보

Combustion chamber for gas turbine engine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-003/14    F02C-007/00   
미국특허분류(USC) 60/723 ; ; 60/737
출원번호 US-0449752 (1995-05-25)
우선권정보 DE-4426351 (1994-07-25)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 65  인용 특허 : 3
초록

In a combustion chamber consisting of a first stage (1) and a second stage (2) arranged downstream in the direction of flow, a mixer (100) is arranged on the head side of the first stage (1), which mixer (100) forms a fuel/air mixture (19). Acting on the outflow side of this mixer (100) is a catalyzer (3) in which the said mixture (19) is completely burnt, the mixing being selected in such a way that an adiabatic flame temperature of between 800°and 1100°C. arises. Positioned on the outflow side of this catalyzer (3) are vortex generators (200) which pro...

대표
청구항

A combustion chamber for a gas turbine apparatus, which comprises a wall enclosing a duct having a longitudinal flow direction along a duct axis, the combustion chamber being divided into a: a first stage having a mixer mounted on a head side for forming a fuel/air mixture, a catalyzer downstream of the mixer for combustion of the fuel/air mixture, a plurality of vortex generators mounted on an interior wall segment downstream of the catalyzer, and a venturi-shaped duct section downstream of the vortex generators and means for injecting at least one of a...

이 특허를 인용한 특허 피인용횟수: 65

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