| 发明名称 |
GAS TURBINE ENGINE COMBUSTOR LINER PANEL |
| 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 hemi-spherical protuberance. |
| 申请公布号 |
WO2015002686(A2) |
申请公布日期 |
2015.01.08 |
| 申请号 |
WO2014US34009 |
申请日期 |
2014.04.14 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
DRAKE, CHRISTOPHER;KOSTKA, STANISLAV, JR.;CUNHA, FRANK J. |
| 分类号 |
F23M5/00;F02C3/14;F02C7/12;F02C7/24;F23M5/08;F23R3/42 |
主分类号 |
F23M5/00 |
| 代理机构 |
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