发明名称 |
COOLING A QUENCH APERTURE BODY OF A COMBUSTOR WALL |
摘要 |
An assembly is provided for a turbine engine. A combustor wall of the turbine engine assembly includes a shell, a heat shield and an annular body engaged with the shell and the heat shield. The annular body extends through the combustor wall. The annular body at least partially defines a quench aperture along a centerline through the combustor wall. The annular body also at least partially defines a cooling aperture in fluid communication with the quench aperture. At least a portion of the cooling aperture extends radially outward from the quench aperture relative to the centerline. |
申请公布号 |
WO2015085065(A1) |
申请公布日期 |
2015.06.11 |
申请号 |
WO2014US68562 |
申请日期 |
2014.12.04 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
CUNHA, FRANK J.;KOSTKA, JR., STANISLAV |
分类号 |
F23M5/08;F02C7/12;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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