| 发明名称 |
AIRCRAFT WITH FORWARD SWEEPING T-TAIL |
| 摘要 |
An aircraft includes a propulsor supported within an aft portion of the fuselage. A thrust reverser is supported proximate the propulsor for redirecting thrust forward to slow the aircraft upon landing. A tail extending from the aft portion of the fuselage is angled forward away from the aft portion and out of the discharge of airflow from the thrust reverser. |
| 申请公布号 |
US2015298794(A1) |
申请公布日期 |
2015.10.22 |
| 申请号 |
US201314440753 |
申请日期 |
2013.03.14 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Suciu Gabriel L.;Chandler Jesse M. |
| 分类号 |
B64C5/02;B64D41/00 |
主分类号 |
B64C5/02 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A thrust reversing system comprising:
a thrust reverser supported proximate a propulsor system for selectively redirecting thrust; and a vertical stabilizer that is proximate to the propulsor system and extending forwardly away from the thrust reverser, whereby discharge flow from the thrust reverser is configured for being directed away from the vertical stabilizer. |
| 地址 |
Hartford CT US |
