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 |
US2016265784(A1) |
申请公布日期 |
2016.09.15 |
申请号 |
US201415032354 |
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 |
F23R3/60;F02C7/12;F23R3/00 |
主分类号 |
F23R3/60 |
代理机构 |
|
代理人 |
|
主权项 |
1. A liner panel within a gas turbine engine, comprising:
a perimeter rail that defines a first height from a cold side; and an intermediate rail that defines a second height from the cold side, wherein the second height is less than the first height. |
地址 |
Farmington CT US |