发明名称 |
AIRCRAFT FRAME FOR TAILSTRIKE ANGLE ENHANCEMENT |
摘要 |
A wedge frame for an aircraft that provides tailstrike angle enhancement. The wedge frame has converging, non-parallel faceplanes that tilt a rear portion of the aircraft fuselage upward in order to prevent or reduce risk of the tail of the aircraft striking the ground during takeoff and landing. A method to prevent or reduce risk of the rear portion of an aircraft from striking the ground during takeoff and landing by using a wedge frame having converging, non-parallel faceplanes to tilt upward the rear portion of the aircraft. |
申请公布号 |
US2016311512(A1) |
申请公布日期 |
2016.10.27 |
申请号 |
US201414565892 |
申请日期 |
2014.12.10 |
申请人 |
The Boeing Company |
发明人 |
Sankrithi Mithra |
分类号 |
B64C1/06;B64C1/00 |
主分类号 |
B64C1/06 |
代理机构 |
|
代理人 |
|
主权项 |
1. A wedge frame for an aircraft that provides tailstrike angle enhancement, the wedge frame comprising an annular structure with non-parallel faceplanes formed by a forward distal edge and an aft distal edge of the annular structure. |
地址 |
Chicago IL US |