| 发明名称 |
SUPERSONIC CARET INLET SYSTEM |
| 摘要 |
An engine inlet for efficient operation in both subsonic and supersonic flight wherein the inlet has a caret configuration is rotatable about an off-body axis for compression ramp angle and capture area variation and a diffuser is engaged to the inlet in a scrubbing relationship to maintain a seal upon rotation of the inlet. |
| 申请公布号 |
US2016273452(A1) |
申请公布日期 |
2016.09.22 |
| 申请号 |
US201514603666 |
申请日期 |
2015.01.23 |
| 申请人 |
The Boeing Company |
发明人 |
Huynh Thuy |
| 分类号 |
F02C7/042;B64D33/02;F02C7/057 |
主分类号 |
F02C7/042 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An engine inlet for efficient operation in both subsonic and supersonic flight, wherein the inlet has a caret configuration and is rotatable about an off-body axis for compression ramp angle and capture area variation. |
| 地址 |
Chicago IL US |
