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특허 상세정보

Low emissions combustion system for a gas turbine engine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-003/14    F02K-003/32    F02K-003/36   
미국특허분류(USC) 60/737 ; 60/748 ; 60/756 ; 60/742 ; 239/405 ; 239/433 ; 239/434
출원번호 US-0182966 (1998-10-08)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Miller
인용정보 피인용 횟수 : 102  인용 특허 : 11
초록

A low emissions combustion system for a gas turbine engine, including a generally annular combustor with a plurality of tangential fuel injectors to introduce a fuel/air mixture. The annular combustor includes a skirt shaped flow control baffle from the inner liner and air dilution holes in the inner liner underneath the flow control baffle and also in the cylindrical outer liner. The fuel injectors extend through the recuperator housing and into the combustor through an angled tube and then through a tangential guide in the cylindrical outer liner of th...

대표
청구항

[ We claim:] [1.] A fuel injector for a gas turbine engine combustor, comprising:an elongated straight cylindrical constant diameter injector tube having an outer end and a discharge end and having an elongation axis;a fuel inlet tube;a generally cylindrical coupler having a central bore therethrough, the outer end of said elongated straight cylindrical constant diameter injector tube mounted over one end of said generally cylindrical coupler and, said fuel inlet tube extending through the central bore of said generally cylindrical coupler from the other...

이 특허를 인용한 특허 피인용횟수: 102

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