发明名称 |
INCIDENCE TOLERANT ENGINE COMPONENT |
摘要 |
This disclosure relates to a gas turbine engine including a component having a leading edge, a pressure side and a suction side opposite the pressure side. The component includes a first group of showerhead holes in the leading edge and a second group of showerhead holes in one of the pressure side and the suction side. The component further includes a first core passageway and a second core passageway separate from the first core passageway. The first core passageway and the second core passageway are in communication with a respective one of the first group of showerhead holes and the second group of showerhead holes. |
申请公布号 |
US2016222794(A1) |
申请公布日期 |
2016.08.04 |
申请号 |
US201414917879 |
申请日期 |
2014.09.09 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Slavens Thomas N.;Zelesky Mark F.;Kohli Atul;Bradshaw Sean D.;Gautschi Steven Bruce |
分类号 |
F01D5/18;F01D9/04;F01D25/12;F04D29/08;F04D29/32;F04D29/58;F04D29/54;F01D5/14;F01D11/08 |
主分类号 |
F01D5/18 |
代理机构 |
|
代理人 |
|
主权项 |
1. A gas turbine engine, comprising:
a component having a leading edge, a pressure side and a suction side, the component including a first group of holes in the leading edge and a second group of holes in one of the pressure side and the suction side, the component including a first core passageway and a second core passageway separate from the first core passageway, the first core passageway and the second core passageway in communication with a respective one of the first group of holes and the second group of holes. |
地址 |
Hartford CT US |