| 发明名称 |
GAS TURBINE ENGINE COMPONENT PROVIDING PRIORITIZED 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 having a non-gas path surface and a gas path surface, a cover plate positioned relative to the non-gas path surface and a cooling passage that extends between the cover plate and the non-gas path surface. At least one cooling entrance is formed through the cover plate and configured to bias the flow of a cooling fluid toward a prioritized location of the non-gas path surface. |
| 申请公布号 |
US2016194980(A1) |
申请公布日期 |
2016.07.07 |
| 申请号 |
US201414911285 |
申请日期 |
2014.08.13 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
THOMEN Seth J.;PIETRASZKIEWICZ Edward |
| 分类号 |
F01D25/12;F04D29/16;F04D29/54;F04D29/58;F01D9/04;F01D11/08 |
主分类号 |
F01D25/12 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A component for a gas turbine engine, comprising:
a platform having a non-gas path surface and a gas path surface; a cover plate positioned relative to said non-gas path surface; a cooling passage that extends between said cover plate and said non-gas path surface; and at least one cooling entrance formed through said cover plate and configured to bias the flow of a cooling fluid toward a prioritized location of said non-gas path surface. |
| 地址 |
Hartford CT US |
