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 |
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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