| 发明名称 |
COMMON JOINT FOR A COMBUSTOR, DIFFUSER, AND TOBI OF A GAS TURBINE ENGINE |
| 摘要 |
An assembly for a gas turbine engine is disclosed. The gas turbine engine may have a combustor, a diffuser, and a tangential onboard injector. The assembly may include a common joint between the combustor, the diffuser, and the tangential onboard injector. |
| 申请公布号 |
US2016017755(A1) |
申请公布日期 |
2016.01.21 |
| 申请号 |
US201314759700 |
申请日期 |
2013.01.29 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Low Kevin Joseph |
| 分类号 |
F01D25/28;F01N3/20;F01D25/24;F02C3/04 |
主分类号 |
F01D25/28 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An assembly for a gas turbine engine, comprising:
a combustor; a diffuser surrounding the combustor; a tangential onboard injector downstream of the diffuser; and a common joint joining the combustor, the diffuser, and the tangential onboard injector. |
| 地址 |
Hartford CT US |
