| 发明名称 |
GAS TURBINE ENGINE WALL ASSEMBLY WITH OFFSET RAIL |
| 摘要 |
A liner panel within a gas turbine engine includes a perimeter rail that defines a first height from a cold side. The liner panel also includes an intermediate rail that defines a second height from the cold side, where the second height is less than the first height. |
| 申请公布号 |
EP3066390(A1) |
申请公布日期 |
2016.09.14 |
| 申请号 |
EP20140857153 |
申请日期 |
2014.08.29 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
BANGERTER, JAMES P.;LOW, KEVIN J. |
| 分类号 |
F23R3/42;F02C3/14;F02C7/12;F23M5/04;F23R3/60 |
主分类号 |
F23R3/42 |
| 代理机构 |
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代理人 |
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| 主权项 |
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| 地址 |
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