发明名称 Combustors with quench inserts
摘要 A combustor for a turbine engine is provided. The combustor includes a first liner having a first hot side and a first cold side; a second liner having a second hot side and a second cold side, the second hot side and the first hot side forming a combustion chamber therebetween, the combustion chamber configured to receive an air-fuel mixture for combustion therein; and an insert including a body portion extending through the first liner, a shoulder circumscribing the body portion and abutting the first hot side, and an inlet portion coupled to the body portion and abutting the first cold side such that the inlet portion and the shoulder capture the second liner therebetween to retain the insert.
申请公布号 EP2413036(A2) 申请公布日期 2012.02.01
申请号 EP20110174596 申请日期 2011.07.19
申请人 HONEYWELL INTERNATIONAL, INC. 发明人 RUDRAPATNA, NAGARAJA S.;LUDWIG, DANIEL;PAYNE, ART;SMALLEY, PHILIP;BISHOP, RICHARD
分类号 F23R3/06 主分类号 F23R3/06
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