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 |