| 发明名称 |
Lightweight air vehicle and pneumatic launcher |
| 摘要 |
<p>A portable unmanned air vehicle and launcher system including a foldable unmanned air vehicle with a pressure tube; a launch gas reservoir for holding launch gas; a launch tube operatively connected to the launch gas reservoir and having a free end that is positioned in the pressure tube of the air vehicle; a free piston positioned within the launch tube; and a free piston stop to prevent the free piston from leaving the launch tube. A first portion of the launch gas in the launch gas reservoir is released into the launch tube and forces the free piston from an initial position to an end position at which the free piston is stopped by the free piston stop.</p> |
| 申请公布号 |
AU2004270608(A1) |
申请公布日期 |
2005.03.17 |
| 申请号 |
AU20040270608 |
申请日期 |
2004.02.19 |
| 申请人 |
AAI CORPORATION |
发明人 |
STEPHEN W. MILLER;MATTHEW T. VELAZQUEZ |
| 分类号 |
B64B;B64B1/00;B64C3/56;B64C39/02;B64F1/04;B64F1/06;(IPC1-7):B64B1/00 |
主分类号 |
B64B |
| 代理机构 |
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代理人 |
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