A seatback for an aircraft seat is described that includes an energy absorbing device for allowing the seatback to move from a first position to a second position when a force is applied to an upper region of the seatback. The seatback includes a guide for guiding movement of the seatback between a first position and a second position. A first connector for connecting the energy absorbing device to a seat back of an aircraft seat and a second connector for connecting the energy absorbing device to a frame or reclining mechanism of the aircraft seat are engaged by a destructible member, the destructible member is configured to be destructed when a predetermined force is applied to move the first connector away from the second connector. Seats and rows of seats including the seatback are also described.
本公开描述了一种用于飞机座椅的座椅靠背,其包括能量吸收装置,用于当力施加到座椅靠背的上部区域时允许座椅靠背从第一位置移动到第二位置。座椅靠背包括引导件,用于引导座椅靠背在第一位置和第二位置之间移动。用于将能量吸收装置连接到飞机座椅的座椅靠背的第一连接器和用于将能量吸收装置连接到飞机座椅的框架或倾斜机构的第二连接器通过可破坏构件接合,该可破坏构件构造成当施加预定力以使第一连接器远离第二连接器移动时破坏。还描述了包括座椅靠背的座椅和成排座椅。
Seat back comprising energy absorbing device
包括能量吸收装置的座椅靠背
2023-12-29
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |