| 发明名称 |
SYSTEM FOR DETACHABLY COUPLING AN UNMANNED AERIAL VEHICLE WITHIN A LAUNCH TUBE |
| 摘要 |
An unmanned aerial vehicle launch tube that has at least one layer of prepeg substrate disposed about an aperture to form a tube, a sabot disposed in an interior of said tube, said sabot having a first clasp tab, and a clasp detachably coupled to said first clasp tab and contacting an inner circumferential wall of said tube so that said clasp is rotationally constrained by the inner circumferential wall and said first clasp tab. |
| 申请公布号 |
US2016347476(A1) |
申请公布日期 |
2016.12.01 |
| 申请号 |
US201414561894 |
申请日期 |
2014.12.05 |
| 申请人 |
AEROVIRONMENT, INC. |
发明人 |
Andryukov Oleksandr |
| 分类号 |
B64F1/04;B64C39/02 |
主分类号 |
B64F1/04 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An unmanned aerial vehicle (UAV) launch tube apparatus, comprising:
at least one layer of prepeg substrate disposed about an aperture to form a tube; a sabot disposed in an interior of said tube, said sabot having a first clasp tab; and a clasp detachably coupled to said first clasp tab and contacting an inner circumferential wall of said tube; wherein said clasp is rotationally constrained by said inner circumferential wall and said first clasp tab. |
| 地址 |
Monrovia CA US |
