发明名称 |
FILM COOLED ENGINE COMPONENT FOR A GAS TURBINE ENGINE |
摘要 |
An engine component for a gas turbine engine includes a film-cooled wall having a hot surface facing hot combustion gas and a cooling surface facing a cooling fluid flow. The wall includes one or more film holes that have an outlet provided on the hot surface and a contoured inlet provided on the cooling surface. A contoured portion in the cooling surface encompasses the inlets for two or more film holes in the wall. |
申请公布号 |
WO2016099663(A3) |
申请公布日期 |
2016.08.11 |
申请号 |
WO2015US57718 |
申请日期 |
2015.10.28 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
BUNKER, RONALD, SCOTT;STONE, TIMOTHY, DERYCK |
分类号 |
F01D5/18;F23R3/00 |
主分类号 |
F01D5/18 |
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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