| 发明名称 |
ACTIVE COOLING OF GROMMET BOSSES FOR A COMBUSTOR PANEL OF A GAS TURBINE ENGINE |
| 摘要 |
A liner assembly for a combustor of a gas turbine engine according to one disclosed non-limiting embodiment of the present disclosure includes a grommet with a multiple of grommet cooling passages. |
| 申请公布号 |
US2016025342(A1) |
申请公布日期 |
2016.01.28 |
| 申请号 |
US201414773990 |
申请日期 |
2014.03.11 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Erbas-Sen Nurhak;Hoke James B.;Tu John S.;Pacheco-Tougas Monica |
| 分类号 |
F23R3/00;F02C7/18 |
主分类号 |
F23R3/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A liner assembly for a combustor of a gas turbine engine comprising:
a grommet with a multiple of grommet cooling passages. |
| 地址 |
Hartford CT US |
