The present invention provides a shock absorbing apparatus for an aircraft seat, that attenuates shock to passengers and crews. The apparatus 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
EP2311730(A4)
申请公布日期
2013.08.14
申请号
EP20090804707
申请日期
2009.08.03
申请人
JAPAN AEROSPACE EXPLORATION AGENCY;DAICEL CHEMICAL INDUSTRIES, LTD.