| 发明名称 |
Turbine Components with Bi-Material Adaptive Cooling Pathways |
| 摘要 |
The present application thus provides a turbine component for use in a hot gas path of a gas turbine engine. The turbine component may include an outer surface, an internal cooling circuit, an adaptive cooling pathway in communication with the internal cooling circuit and extending through the outer surface, and a cooling plug having two or more materials positioned within the adaptive cooling pathway. |
| 申请公布号 |
US2015198062(A1) |
申请公布日期 |
2015.07.16 |
| 申请号 |
US201414151859 |
申请日期 |
2014.01.10 |
| 申请人 |
General Electric Company |
发明人 |
Morgan Victor John;Fagan Joseph |
| 分类号 |
F01D25/12 |
主分类号 |
F01D25/12 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A turbine component for use in a hot gas path of a gas turbine engine, comprising:
an outer surface; an internal cooling circuit; an adaptive cooling pathway in communication with the internal cooling circuit and extending through the outer surface; and a cooling plug positioned within the adaptive cooling pathway; the cooling plug comprising two or more materials. |
| 地址 |
Schenectady NY US |
