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 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