| 发明名称 |
GAS TURBINE ENGINE COMBUSTOR LINER PANEL WITH SYNERGISTIC COOLING FEATURES |
| 摘要 |
A liner panel for a combustor of a gas turbine engine includes a multiple of heat transfer augmentors. At least one of the multiple of heat transfer augmentors includes a cone shaped pin. |
| 申请公布号 |
US2017003027(A1) |
申请公布日期 |
2017.01.05 |
| 申请号 |
US201515106032 |
申请日期 |
2015.01.30 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Kostka Stanislav;Cunha Frank J.;Hoke James B.;Snyder Timothy S.;Cheung Albert K.;Adamopoulos Christos |
| 分类号 |
F23R3/00;F02C7/18;F23R3/06 |
主分类号 |
F23R3/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A liner panel for a combustor of a gas turbine engine, comprising:
a multiple of heat transfer augmentors, at least one of the multiple of heat transfer augmentors including a cone shaped pin. |
| 地址 |
Hartford CT US |
