发明名称 |
TURBINE ENGINE COMBUSTOR HEAT SHIELD WITH MULTI-ANGLED COOLING APERTURES |
摘要 |
A combustor for a turbine engine is provided that includes a combustor wall. The combustor wall includes a shell and a heat shield, which is attached to the shell. One or more cooling cavities are defined between the shell and the heat shield, and fluidly couple a plurality of apertures defined in the shell with a plurality of apertures defined in the heat shield. The apertures in the heat shield include a first aperture and a second aperture. An angle of incidence between the first aperture and a surface of the heat shield is different than an angle of incidence between the second aperture and the surface. |
申请公布号 |
WO2015112221(A2) |
申请公布日期 |
2015.07.30 |
申请号 |
WO2014US63859 |
申请日期 |
2014.11.04 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
MOURA, DENNIS M.;PACHECO-TOUGAS, MONICA;EASTWOOD, JONATHAN J.;BOULDIN, LEE E. |
分类号 |
F23M5/08;F23M5/04;F23R3/42 |
主分类号 |
F23M5/08 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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