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특허 상세정보

Gas turbine with a compressor for air

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F23R-003/42    F23R-003/54   
미국특허분류(USC) 060/772; 060/039.37; 060/751; 060/752
출원번호 US-0172016 (2002-06-17)
우선권정보 EP-0114599 (2001-06-18)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Harness, Dickey & Pierce, P.L.C.
인용정보 피인용 횟수 : 20  인용 특허 : 5
초록

In gas turbines, compressed air is supplied via an air duct to combustion chambers and is heated there. Pressure losses in the air duct should be minimized in order to ensure good overall efficiency. This is achieved by the compressed air flowing with approximately constant velocity in the air duct from the compressor to the inlet into the combustion chamber. This is supported by the effective cross section of the air duct being almost constant over this distance.

대표
청구항

In gas turbines, compressed air is supplied via an air duct to combustion chambers and is heated there. Pressure losses in the air duct should be minimized in order to ensure good overall efficiency. This is achieved by the compressed air flowing with approximately constant velocity in the air duct from the compressor to the inlet into the combustion chamber. This is supported by the effective cross section of the air duct being almost constant over this distance. second roller disposed and rotatably mounted within said second partial bore, and a third r...

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