| 发明名称 |
ENGINE INLET CONFIGURATION |
| 摘要 |
An engine inlet assembly includes an inlet duct having a first inlet duct leg and a second inlet duct leg, the first inlet duct leg and the second inlet duct leg extending toward a common inlet duct outlet located at an engine inlet. The first inlet duct leg and the second inlet duct leg are fixedly secured to an airframe of an aircraft at an air inlet. The duct outlet has a floating interface with the engine inlet. |
| 申请公布号 |
US2015291288(A1) |
申请公布日期 |
2015.10.15 |
| 申请号 |
US201414252236 |
申请日期 |
2014.04.14 |
| 申请人 |
Sikorsky Aircraft Corporation |
发明人 |
Bofill Steven;Chasen Scott A.;Simonetti Joseph Lawrence;Lamb, Jr. Donald William |
| 分类号 |
B64D33/02;B64C27/00 |
主分类号 |
B64D33/02 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An engine inlet assembly comprising:
an inlet duct including a first inlet duct leg and a second inlet duct leg, the first inlet duct leg and the second inlet duct leg extending toward a common inlet duct outlet disposed at an engine inlet; the first inlet duct leg and the second inlet duct leg fixedly secured to an airframe of an aircraft at an air inlet; and the duct outlet having a floating interface with the engine inlet. |
| 地址 |
Stratford CT US |
