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 |
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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 |