发明名称 |
GAS TURBINE ENGINE COMPONENT WITH COMBINED MATE FACE AND PLATFORM COOLING |
摘要 |
A component for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a platform that axially extends between a leading edge and a trailing edge, circumferentially extends between a first mate face and a second mate face, and includes a gas path surface and a non-gas path surface. The component defines at least one cavity that extends at least partially inside of the component. A first plurality of cooling holes extends from the at least one cavity to at least one of the first mate face and the second mate face and a second plurality of cooling holes extends from either the at least one cavity or the non-gas path surface to the gas path surface. |
申请公布号 |
EP2956627(A2) |
申请公布日期 |
2015.12.23 |
申请号 |
EP20140797049 |
申请日期 |
2014.02.07 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
LEWIS, SCOTT D.;RAPP, BRANDON M.;BEATTIE, JEFFREY S.;HOUGH, MATTHEW ANDREW;TELLER, BRET M.;JACQUES, JEFFREY MICHAEL;ASTERLIN, MAX |
分类号 |
F01D5/18;F01D5/08;F01D11/24;F01D25/12;F02C7/18;F04D29/58 |
主分类号 |
F01D5/18 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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