发明名称 |
FILM HOLE WITH PROTRUDING FLOW ACCUMULATOR |
摘要 |
A wall of a gas turbine engine is provided. The wall may comprise an external surface adjacent a gas path and an internal surface adjacent an internal flow path. A film hole may have an inlet at the internal surface and an outlet at the external surface. A flow accumulator adjacent the inlet may protrude from the internal surface. A method of making an engine component is also provided and comprises the step of forming a component wall comprising an accumulator on an internal surface and a film hole defined by the component wall. The film hole may include an opening adjacent the accumulator and defined by the internal surface. |
申请公布号 |
US2016108739(A1) |
申请公布日期 |
2016.04.21 |
申请号 |
US201514852896 |
申请日期 |
2015.09.14 |
申请人 |
United Technologies Corporation |
发明人 |
Musto Clifford J.;LoRicco Nicholas M.;Slavens Thomas N.;Jennings Timothy J.;Clum Carey;Moore Sasha M.;McBrien John;Quach San;Whitfield Christopher |
分类号 |
F01D5/18;B22C9/10 |
主分类号 |
F01D5/18 |
代理机构 |
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代理人 |
|
主权项 |
1. A gas turbine engine component, comprising
a component wall including a film hole comprising:
an inlet defined by an internal surface,an outlet defined by an external surface, a flow accumulator extending from the component wall adjacent the inlet, wherein the flow accumulator is in fluid communication with the inlet and the outlet. |
地址 |
Hartford CT US |