| 发明名称 |
SUPPORT ASSEMBLY FOR A GAS TURBINE ENGINE |
| 摘要 |
A support assembly for a gas turbine engine includes at least one inner support that extends about a circumferential axis and defines a cavity for receiving a control ring. At least one cover plate is attached to at least one inner support to enclose the cavity. At least one of the inner support and the cover plate includes a rail and the other of the inner support and the cover plate includes a groove for engaging the rail. |
| 申请公布号 |
US2016341062(A1) |
申请公布日期 |
2016.11.24 |
| 申请号 |
US201514719634 |
申请日期 |
2015.05.22 |
| 申请人 |
United Technologies Corporation |
发明人 |
Jenkins Decari S.;Bauer Steven J. |
| 分类号 |
F01D11/14;F01D25/28 |
主分类号 |
F01D11/14 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A support assembly for a gas turbine engine comprising:
at least one inner support extending about a circumferential axis defining a cavity for receiving a control ring; and at least one cover plate attached to the at least one inner support enclosing the cavity, wherein at least one of the inner support and the cover plate includes a rail and the other of the inner support and the cover plate includes a groove for engaging the rail. |
| 地址 |
Hartford CT US |
