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