发明名称 Shock absorbing apparatus for aircraft seat
摘要 A shock absorbing apparatus for an aircraft seat that attenuates shock to passengers and crews includes; an airbag 11 being expanded in a plate shape in a state of less than maximum expansion; an upper flat plate 12 arranged on one side of the airbag 11; a lower flat plate 13 arranged on another side of the airbag 11; a gas supply device 15 for supplying a gas to the airbag 11; and a detector sending a signal to activate the gas supply device 15 by a preset condition. The shock is absorbed by expanding the airbag 11 before the shock is applied to the passenger.
申请公布号 US8573690(B2) 申请公布日期 2013.11.05
申请号 US200913057442 申请日期 2009.08.03
申请人 SHOJI HIROKAZU;KATAYAMA KAZUO;ENOMOTO NORIO;YUTANI HIROSHI;JAPAN AEROSPACE EXPLORATION AGENCY 发明人 SHOJI HIROKAZU;KATAYAMA KAZUO;ENOMOTO NORIO;YUTANI HIROSHI
分类号 B60N2/42 主分类号 B60N2/42
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