发明名称 THREE-POSITION AIRCRAFT TAIL SKID MECHANISM AND METHOD OF ACTUATION
摘要 A system includes an aircraft having a fuselage with a tail portion. A tail skid is disposed in an opening of the tail portion. The tail skid includes a ground contact shoe and a mechanism configured to selectably move the ground contact shoe between respective ones of a stow position disposed within the opening, a landing position disposed below the opening, and a takeoff position different than the stow and landing positions. Before a takeoff or a landing, the ground contact shoe is moved to a corresponding one of the takeoff or landing positions. In the event of an over-rotation or an over-flaring of the aircraft during a takeoff or a landing, respectively, the ground contact shoe makes contact with the ground and a shock absorber of the system absorbs a shock of the contact and thereby prevents tail strike damage to the aircraft.
申请公布号 US2017057625(A1) 申请公布日期 2017.03.02
申请号 US201514834369 申请日期 2015.08.24
申请人 The Boeing Company 发明人 Mellor Mitchell L. R.
分类号 B64C25/52;B64C25/26 主分类号 B64C25/52
代理机构 代理人
主权项 1. A system, comprising: an aircraft having a fuselage with a tail portion; and a tail skid disposed in an opening of the tail portion, the tail skid comprising: a ground contact shoe; anda mechanism configured to selectably move the ground contact shoe between respective ones of a stow position disposed within the opening, a landing position disposed below the opening, and a takeoff position different than the stow and landing positions.
地址 Chicago IL US