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특허 상세정보

Radial inlet swirler with twisted vanes for fuel injector

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-003/14   
미국특허분류(USC) 60/748 ; 60/740 ; 239/400 ; 239/406
출원번호 US-0947593 (1997-10-09)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Friedland
인용정보 피인용 횟수 : 89  인용 특허 : 12
초록

The fuel injector for a combustor of a gas turbine engine of the high shear design type is configured to include two swirlers with passages where the vanes in the inner swirler of the inner swirler in the passage which is closest to the centerline of the fuel nozzle includes a judiciously located twist and together with the proper flow ratio between the two swirl passages and the proper swirl angle of the flow stream in each of the passages provide an enhanced fuel injector with improved lean blowout and high altitude relight characteristics while assuri...

대표
청구항

[ I claim:] [1.] A high shear designed fuel injector for a combustor of a gas turbine engine comprising a fuel nozzle supported at an inlet of said combustor, a first radial inlet swirler mounted on said fuel nozzle and including a first passage for flowing air into the combustor and being coaxially disposed relative to said fuel nozzle, a second radial inlet swirler mounted adjacent to said first radial swirler and including a second passage for flowing additional air into the combustor and being concentrically disposed relative to said first passage, s...

이 특허를 인용한 특허 피인용횟수: 89

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