发明名称 |
Launch Tube Restraint System For Unmanned Aerial Vehicle (UAV) |
摘要 |
An unmanned aerial launch vehicle (UAV) launch apparatus is disclosed that includes a UAV (400) having an exterior surface, an aerial vehicle (AV) tab (510) extending from the exterior surface, a tube (440) containing the UAV (400), the tube (440) including a tab stop (515) configured to controllably hinder travel of the AV tab (510) past the tab stop (515), and a pair of opposing tab guides (700, 705) configured to position the AV tab (510) for travel over the tab stop (515). |
申请公布号 |
US2017029135(A1) |
申请公布日期 |
2017.02.02 |
申请号 |
US201615292908 |
申请日期 |
2016.10.13 |
申请人 |
AeroVironment, Inc. |
发明人 |
Su Guan H.;Rodriguez Marcos Henry |
分类号 |
B64F1/04;B64C39/02;F41B11/80 |
主分类号 |
B64F1/04 |
代理机构 |
|
代理人 |
|
主权项 |
1. An unmanned aerial launch vehicle (UAV) launch apparatus, comprising:
a UAV; a tube containing the UAV, wherein the tube has an open end; a cap positioned over the open end of the tube; and a strap extending through at least one strap guide and restraining the cap. |
地址 |
Monrovia CA US |