| 发明名称 |
CIRCUMFERENTIALLY RETAINED FAIRING |
| 摘要 |
<p>An assembly for a gas turbine engine includes a frame, a mount, and a fairing. The mount is attached to the frame and the fairing is connected to the mount. The fairing and mount have mating anti-deflection features that engage to prevent circumferential movement of the fairing relative to the frame.</p> |
| 申请公布号 |
EP2938833(A2) |
申请公布日期 |
2015.11.04 |
| 申请号 |
EP20130876268 |
申请日期 |
2013.12.16 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
CHUONG, CONWAY;SCOTT, JONATHAN ARIEL;BUDNICK, MATTHEW |
| 分类号 |
F01D9/04;F01D25/16;F01D25/28;F02C7/00;F02C7/20 |
主分类号 |
F01D9/04 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
|
| 地址 |
|
