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특허 상세정보

Combustion air control system for a gas turbine engine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-009/18   
미국특허분류(USC) 600/392.3 ; 600/392.9
출원번호 US-0085626 (1998-05-27)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Cain
인용정보 피인용 횟수 : 78  인용 특허 : 2
초록

Systems for controlling the combustion air to be used with a gas turbine engine for control the products of combustion and reducing emissions emitted therefrom have been used in the past. The present system includes a compressed air plenum being divided into a combustion air supply portion and a dilution or cooling air supply portion. A variable geometry system is positioned between the compressor section and the compressed air plenum. The variable geometry system is movably between an open position and a closed position. Movement of the variable geometr...

대표
청구항

[ What is claimed is:] [1.] A gas turbine engine having a compressor section establishing a flow of compressed air, a source of fuel and a combustion section; said gas turbine engine comprising: a fuel injector, a compressed air plenum being divided into a combustion air supply portion and a dilution or cooling air supply portion; a variable geometry system that includes a control mechanism being connected to a divider mechanism having a plurality of holes or openings positioned therein, said system being positioned between said compressor section and sa...

이 특허를 인용한 특허 피인용횟수: 78

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