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
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