发明名称 COUNTER-SWIRL DOUBLET COMBUSTOR WITH PLUNGED HOLES
摘要 An improved system, apparatus and method may comprise an inner liner and an outer liner extending circumferentially around an engine centerline axis thereby forming a combustion chamber therebetween. The system, apparatus, and method may include a front end extending between the inner and outer liners and having a plurality of fuel nozzle ports configured to each receive a fuel nozzle. First and second outer plunged inlet holes may be formed in the outer liner and extending in a first radial direction toward the engine centerline axis and into at least a portion of the combustion chamber. First and second inner plunged inlet holes may be formed in the inner liner and extending in a second radial direction away from the engine centerline axis and into at least a portion of the combustion chamber.
申请公布号 US2016169517(A1) 申请公布日期 2016.06.16
申请号 US201514964799 申请日期 2015.12.10
申请人 Rolls-Royce Corporation 发明人 Graves Charles B.;Moore Mindi D.;Woubshet Afework;Yount Randall E.
分类号 F23R3/06;F23R3/60;F02C3/04;F23R3/00 主分类号 F23R3/06
代理机构 代理人
主权项 1. An apparatus for providing combustion, comprising: an inner liner and an outer liner extending circumferentially around an engine centerline axis thereby forming a combustion chamber therebetween; a dome extending between the inner and outer liners and having a plurality of fuel nozzle ports configured to each receive a fuel nozzle, each fuel nozzle port having a port centerline axis extending axially therethrough; first and second outer plunged inlet holes formed in the outer liner and extending in a first radial direction toward the engine centerline axis and into at least a portion of the combustion chamber; and first and second inner plunged inlet holes formed in the inner liner and extending in a second radial direction away from the engine centerline axis and into at least a portion of the combustion chamber.
地址 Indianapolis IN US