| 发明名称 |
GAS TURBINE ENGINE COMBUSTOR LINER PANEL |
| 摘要 |
A liner panel is provided for a combustor of a gas turbine engine. The liner panel includes a multiple of heat transfer augmentors. At least one of the multiple of heat transfer augmentors includes a depression, where the depression includes an entrance to at least one passage through the liner panel. |
| 申请公布号 |
WO2015050592(A3) |
申请公布日期 |
2015.06.11 |
| 申请号 |
WO2014US42130 |
申请日期 |
2014.06.12 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
DRAKE, CHRISTOPHER;CUNHA, FRANK J.;KOSTKA, STANISLAV |
| 分类号 |
F23M5/00;F02C7/12;F23M5/04;F23R3/42 |
主分类号 |
F23M5/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
|
| 地址 |
|
