| 发明名称 |
REVERSE CORE FLOW ENGINE MOUNTING ARRANGEMENT |
| 摘要 |
A mounting arrangement for an aircraft engine includes a mounting structure attached to an aircraft body and not directly connected to an engine core of the aircraft engine, a propulsor mounted to the mounting structure, and a thrust reverser mounted directly to either the propulsor or mounting structure. |
| 申请公布号 |
US2015121896(A1) |
申请公布日期 |
2015.05.07 |
| 申请号 |
US201414190162 |
申请日期 |
2014.02.26 |
| 申请人 |
United Technologies Corporation |
发明人 |
Suciu Gabriel L.;Chandler Jesse M.;Merry Brian D. |
| 分类号 |
F02C7/20;F02K1/54 |
主分类号 |
F02C7/20 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A mounting arrangement for an aircraft engine comprising:
a mounting structure attached to an aircraft body and not directly connected to an engine core of the aircraft engine; a propulsor mounted to the mounting structure; and a thrust reverser mounted directly to either the propulsor or mounting structure. |
| 地址 |
Hartford CT US |
