The present disclosure relates to an impact load distribution structure for a fuselage, the structure comprising: a floor frame defining a fuselage floor; a skid member fastened to a lower portion of the floor frame; and a crash box coupled to the skid member and extending to a lower portion of the floor frame, and configured to selectively deform in a crash load direction when an oblique crash occurs.
本公开涉及一种机身的碰撞载荷分布结构,该结构包括:底板框架,限定机身底板;滑橇构件,紧固到底板框架的下部;以及碰撞盒,联接到滑橇构件并延伸到底板框架的下部,并且被构造成在发生斜向碰撞时沿碰撞载荷方向选择性地变形。
Collision load distribution structure of fuselage
机身的碰撞载荷分布结构
2024-09-20
Patent
Electronic Resource
Chinese