| 发明名称 |
COOLING PATCH FOR HOT GAS PATH COMPONENTS |
| 摘要 |
The present application provides a cooling patch for use with a hot gas path component of a gas turbine engine. The cooling patch may include a base layer with a number of cooling channels extending therethrough, and a cover layer positioned on the base layer. The base layer and the cover layer may include a pre-sintered preform material. |
| 申请公布号 |
US2017122562(A1) |
申请公布日期 |
2017.05.04 |
| 申请号 |
US201514924742 |
申请日期 |
2015.10.28 |
| 申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
BERRY JONATHAN DWIGHT |
| 分类号 |
F23R3/06;F02C7/18;F23R3/00;B23K31/02;C21D9/00 |
主分类号 |
F23R3/06 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A cooling patch for use with a hot gas path component of a gas turbine engine, comprising:
a base layer; a plurality of cooling channels extending along the base layer; and a cover layer positioned on the base layer; wherein the base layer and the cover layer comprise a pre-sintered preform material. |
| 地址 |
Schenectady NY US |
