An energy absorbing assembly includes an attachment component configured to be coupled to a mounting structure. The energy absorbing assembly also includes an anchor that has a tip portion, a shaft, and a head. The anchor is configured to extend through the attachment component such that the head is disposed on a first side of the attachment component and the tip portion is disposed on a second side of the attachment component and is configured to be coupled to the mounting structure. The energy absorbing assembly also includes a deformable member configured to be positioned concentrically around the shaft of the anchor. The deformable member is configured to be retained between the first side of the attachment component and the head of the anchor.
Energy absorbing assembly for aircraft seat
2018-05-08
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |