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.
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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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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