发明名称 |
COOLING AN APERTURE BODY OF A COMBUSTOR WALL |
摘要 |
An assembly is provided for a turbine engine. This turbine engine assembly includes a combustor wall, which includes a shell, a heat shield and an annular body. The body at least partially defines a first aperture through the shell and the heat shield. The body also defines one or more second apertures through which air is directed into the first aperture and provides non-uniform cooling to the body. |
申请公布号 |
WO2015147929(A3) |
申请公布日期 |
2015.11.19 |
申请号 |
WO2014US71573 |
申请日期 |
2014.12.19 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
KOSTKA, JR., STANISLAV;CUNHA, FRANK J. |
分类号 |
F23M5/08;F02C7/16;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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