发明名称 |
Parachute landing velocity attenuator |
摘要 |
A gas-powered landing velocity attenuator for reducing the final descent velocity (and consequent ground impact load) of a parachutist or parachuted cargo. Immediately prior to impact, the gas source powers a device for drawing the load (either a parachutist or cargo) closer to the canopy of the paracute. In a first preferred embodiment, the load and the canopy are brought closer together by a single action piston and cable assembly powered by the gas source. A second embodiment uses an inflator assembly connected to an air bag or a braided tube to decrease the distance between the load and the parachute canopy. |
申请公布号 |
AU3448999(A) |
申请公布日期 |
1999.08.09 |
申请号 |
AU19990034489 |
申请日期 |
1999.01.26 |
申请人 |
SIMULA INC. |
发明人 |
LESLIE D. PETERSON;LANCE L. LABUN;A. GARY STUTHEIT;MYNOR J. CASTRO;MARVIN K. RICHARDS |
分类号 |
B64D1/14;B64D17/34;B64D17/36 |
主分类号 |
B64D1/14 |
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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