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