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1. 发明申请

US20150001340A1 METHOD FOR RECOVERING A UAV 有权
标题翻译：无人机的恢复方法
公开(公告)号：US20150001340A1
公开(公告)日：2015-01-01
申请号：US14313350
申请日：2014-06-24
申请人： Arcturus UAV LLC
发明人： Mark Cameron Allen , D'Milo Dean Hallerberg , Greg P. Timm
IPC分类号： B64F1/02
CPC分类号： B64F1/02 , B64C2201/182 , B64F1/025
摘要： An unmanned aerial vehicle (UAV) recovery system comprises a base and a pneumatic capture net, including a set of upwardly extending, flexible, inflatable tubes, supported by a capture net support assembly. Drag forces are exerted on a UAV by the set of tubes when the UAV flies into them. In some examples the recovery system includes a plurality of decelerators, each decelerator having a supply of a restraint strap, connected to the pneumatic net, which can be pulled from the decelerator upon the application of a sufficient force so that movement of the pneumatic net is resistible by forces exertable by the decelerators on the pneumatic net.
摘要翻译：无人飞行器（UAV）回收系统包括基座和气动捕获网，其包括由捕获网支撑组件支撑的一组向上延伸的柔性可充气管。当无人机进入其中时，该组管子对无人机施加拖拉力。在一些示例中，回收系统包括多个减速器，每个减速器具有连接到气动网的约束带的供应，其可以在施加足够的力时从减速器拉动，使得气动网的移动为可抵抗由气动网上的减速器施加的力。

2. 发明授权

US09527603B2 Method for recovering a UAV 有权
标题翻译：无人机的恢复方法
公开(公告)号：US09527603B2
公开(公告)日：2016-12-27
申请号：US14313350
申请日：2014-06-24
申请人： Arcturus UAV LLC
发明人： Mark Cameron Allen , D'Milo Dean Hallerberg , Greg P. Timm
IPC分类号： B64F1/02
CPC分类号： B64F1/02 , B64C2201/182 , B64F1/025
摘要： An unmanned aerial vehicle (UAV) recovery system comprises a base and a pneumatic capture net, including a set of upwardly extending, flexible, inflatable tubes, supported by a capture net support assembly. Drag forces are exerted on a UAV by the set of tubes when the UAV flies into them. In some examples the recovery system includes a plurality of decelerators, each decelerator having a supply of a restraint strap, connected to the pneumatic net, which can be pulled from the decelerator upon the application of a sufficient force so that movement of the pneumatic net is resistible by forces exertable by the decelerators on the pneumatic net.
摘要翻译：无人飞行器（UAV）回收系统包括基座和气动捕获网，其包括由捕获网支撑组件支撑的一组向上延伸的柔性可充气管。当无人机进入其中时，该组管子对无人机施加拖拉力。在一些示例中，回收系统包括多个减速器，每个减速器具有连接到气动网的约束带的供应，其可以在施加足够的力时从减速器拉动，使得气动网的移动为可抵抗由气动网上的减速器施加的力。

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