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특허 상세정보

Off center combustor liner

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-001/00   
미국특허분류(USC) 060/752; 060/804
출원번호 US-0243122 (2008-10-01)
등록번호 US8056343 (2011-11-01)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Suthrland Asbill & Brennan LLP
인용정보 피인용 횟수 : 0  인용 특허 : 34
초록

The present application provides a liner for a combustor. The combustor liner may include a mouth, a passage for a flow of fuel, a passage for a flow of air, a first zone for mixing the flow of fuel and the flow of air, and the first zone having a constant diameter. The combustor liner may have at least one transition zone with first and second side walls angled substantially in the same direction, and an off center exit. This configuration will provide a more stable flow when exiting the combustor liner.

대표
청구항

We claim: 1. A gas turbine, comprising:a passage for a flow of fuel;a passage for a flow of air;a first zone for mixing the flow of fuel and the flow of air;the first zone having a constant diameter;at least one angled transition zones down stream of the first zone; andan off center exit down stream of the at least one angled transition zones; wherein the at least one angled transition zones being connected to the first zone by a first stepped side and a second stepped side; wherein the first stepped side and the second stepped side are angled substantia...

이 특허에 인용된 특허 (34)

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