发明名称 INFLATION-CONTROLLED PARACHUTE
摘要 An inflation-controlled parachute comprises an extended flexible structure (10) for providing an aerodynamic drag-producing surface, and an inflation-control line (20) for controlling the rate at which the flexible structure (10) unfolds from a stowed configuration to an inflated configuration. One end of the inflation-control line (20) is secured to the flexible structure (10), and the remainder of the inflation-control line (20) is threaded through positioning rings (22) attached to the flexible structure (10) so that one segment of the inflation-control line (20) overlies another segment thereof in frictional engagement therewith. Frictional engagement of the two segments of the inflation-control line (20) occurs as the flexible structure (10) inflates, thereby controlling the rate of inflation of the flexible structure (10).
申请公布号 DE3462114(D1) 申请公布日期 1987.02.26
申请号 DE19843462114 申请日期 1984.06.15
申请人 LOCKHEED MISSILES & SPACE COMPANY, INC. 发明人 LINDGREN, MATTS J.;CULP, MURL F.
分类号 B64D17/34;(IPC1-7):B64D17/36 主分类号 B64D17/34
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