| 发明名称 |
GAS TURBINE ENGINE ATTACHMENT STRUCTURE AND METHOD THEREFOR |
| 摘要 |
An attachment structure for a gas turbine engine includes a frame that has a first annular case. A second annular case extends around the frame. The first annular case and the second annular case include a plurality of interlocks. Each of the interlocks includes a first member mounted on one of the first annular case or the second annular case and a corresponding second member mounted on the other of the first annular case or the second case. The first member is received in the second member such that the plurality of interlocks restricts relative circumferential and axial movement between the first annular case and the second annular case. |
| 申请公布号 |
US2016003104(A1) |
申请公布日期 |
2016.01.07 |
| 申请号 |
US201414768857 |
申请日期 |
2014.01.28 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Sander David J.;Duelm Shelton O. |
| 分类号 |
F01D25/26;F01D9/04 |
主分类号 |
F01D25/26 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An attachment structure for a gas turbine engine, comprising:
a frame including a first annular case; and a second annular case extending around the frame, the first annular case and the second annular case including a plurality of interlocks, each of the plurality of interlocks including a first member mounted on one of the first annular case or the second annular case and a corresponding second member mounted on the other of the first annular case or the second annular case, the first member being received in the second member such that the plurality of interlocks restrict relative circumferential and axial movement between the first annular case and the second annular case. |
| 地址 |
Hartford, CT US |
