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 |
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代理人 |
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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 |