| 发明名称 |
GAS TURBINE ENGINE CLEARANCE CONTROL |
| 摘要 |
A gas turbine engine includes first and second structures secured to one another at a bolted flange joint. A seal is supported by a third structure. A cover is arranged over the bolted flange joint and discrete from the first and second structures. The cover provides a seal land that engages the piston seal and protects the first structure from the adverse thermal environment. |
| 申请公布号 |
US2016146033(A1) |
申请公布日期 |
2016.05.26 |
| 申请号 |
US201514937397 |
申请日期 |
2015.11.10 |
| 申请人 |
United Technologies Corporation |
发明人 |
LeBlanc Ryan Edward;Wall Jordan T.;Bintz Matthew E. |
| 分类号 |
F01D11/08;F01D25/14;F02C3/00;F01D9/04;F01D11/00 |
主分类号 |
F01D11/08 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A gas turbine engine comprising:
first and second structures secured to one another at a bolted flange joint; a seal supported by a third structure; and a cover arranged over the bolted flange joint and discrete from the first and second structures, the cover provides a seal land that engages the seal. |
| 地址 |
Hartford CT US |
