发明名称 Gliding decelerator including an assembly for improving the lift to drag ratio associated therewith
摘要 A gliding decelerator and an assembly for use therein for improving the lift to drag ratio associated therewith. In a preferred embodiment, the gliding decelerator includes a ram-air canopy shaped to include a plurality of half-cells, each half-cell having an open leading end and a closed tailing end. Inflatable bladders are secured within the respective half-cells of the canopy, the inflatable bladders being appropriately dimensioned so that, when inflated soon after the canopy has been opened, each bladder fills its respective half-cell in such a way as to stiffen the half-cell both along its length and at its open leading end. The inflatable bladders may be inflated simultaneously or in stages, the inflation means comprising a gas source, a flexible manifold connecting the gas source to the half-cells and valve means for controlling the output of the gas source. Control of the valve means may be automatic, e.g., a timer, a remote control unit, or may be controlled by a parachutist, e.g., completion of an electric circuit. The inflation means may be mounted within the wing-shaped canopy or may be externally mounted.
申请公布号 US5303883(A) 申请公布日期 1994.04.19
申请号 US19930094671 申请日期 1993.07.16
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE ARMY 发明人 BREWER, JOHN C.;SADECK, JAMES E.
分类号 B64D17/02;(IPC1-7):B64D17/02 主分类号 B64D17/02
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