发明名称 COOLING HOLE WITH CURVED METERING SECTION
摘要 A gas turbine engine component having a cooling hole includes a first wall having a cooling hole inlet, a second wall generally opposite the first wall and having a cooling hole outlet, a metering section extending downstream from the inlet and having a hydraulic diameter (dh), and a diffusing section extending from the metering section to the outlet. The metering section includes a substantially convex first surface extending from a first end to a second end, a substantially concave second surface extending from a third end to a fourth end, and first and second curved portions connecting the ends of the first and second surfaces.
申请公布号 US2017081959(A1) 申请公布日期 2017.03.23
申请号 US201615008148 申请日期 2016.01.27
申请人 United Technologies Corporation 发明人 Lewis Scott D.;Zelesky Mark F.;Mongillo Dominic J.
分类号 F01D5/18;F01D9/02;F02C7/18;F01D11/08;F01D25/24;F01D25/12;F23R3/00;F01D5/22 主分类号 F01D5/18
代理机构 代理人
主权项 1. A gas turbine engine component having a cooling hole, the component comprising: a first wall comprising a cooling hole inlet; a second wall generally opposite the first wall and comprising a cooling hole outlet; a metering section extending downstream from the inlet and having a hydraulic diameter (dh), the metering section comprising: a substantially convex first surface extending from a first end to a second end;a substantially concave second surface extending from a third end to a fourth end;a first curved portion connecting the first end and the third end; anda second curved portion connecting the second end and the fourth end; and a diffusing section extending from the metering section to the outlet.
地址 Hartford CT US