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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

US08783607B2 UAV recovery system 有权
标题翻译：无人机恢复系统
公开(公告)号：US08783607B2
公开(公告)日：2014-07-22
申请号：US13204456
申请日：2011-08-05
申请人： Mark Cameron Allen , D'Milo Dean Hallerberg , Greg P. Timm
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。

3. 发明授权

US08511607B2 UAV launch attachment assembly and launch system 失效
标题翻译：无人机发射附件组装和发射系统
公开(公告)号：US08511607B2
公开(公告)日：2013-08-20
申请号：US12836496
申请日：2010-07-14
申请人： Andrew B. Robinson
发明人： Andrew B. Robinson
IPC分类号： B64F1/04
CPC分类号： B64F1/04 , B64C2201/021 , B64C2201/084 , B64F1/06
摘要： A UAV attachment assembly, used with a UAV launch assembly comprising a frame and a launch driver, comprises a base, a UAV support, a biasing element, a coupler, and a retainer. The base is operably coupled to the launch driver. The UAV support is mounted to the base and is placeable in vertically collapsed and vertically extended orientations. The biasing element biases the UAV support towards the collapsed orientation. The coupler releasably couples the UAV support to a UAV when the UAV support is in the extended orientation, the UAV support being free of the UAV when in the collapsed orientation. The retainer maintains the UAV support in the vertically extended orientation prior to launch and releases the UAV support at launch so that the biasing element can cause the UAV support to move towards the collapsed orientation and to disengage from the UAV.
摘要翻译：与包括框架和发射驱动器的UAV发射组件一起使用的UAV附件组件包括基座，UAV支撑件，偏置元件，联接器和保持器。基座可操作地联接到发射驱动器。无人机支撑安装在基座上，可放置在垂直折叠和垂直延伸的方向上。偏置元件使无人机支撑朝向折叠方向偏移。当UAV支撑处于延伸方向时，联接器将UAV支撑件可释放地耦合到UAV，UAV支撑在处于折叠方向时无UAV。保持架在启动之前将UAV支撑件保持在垂直延伸的方向，并在发射时释放UAV支撑，使得偏置元件可以使UAV支撑件朝向折叠方向移动并与UAV脱离接合。

4. 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。

5. 发明申请

US20120012695A1 UAV Launch Attachment Assembly and Launch System 失效
标题翻译：无人机启动附件组装和启动系统
公开(公告)号：US20120012695A1
公开(公告)日：2012-01-19
申请号：US12836496
申请日：2010-07-14
申请人： Andrew B. Robinson
发明人： Andrew B. Robinson
IPC分类号： B64F1/04
CPC分类号： B64F1/04 , B64C2201/021 , B64C2201/084 , B64F1/06
摘要： A UAV attachment assembly, used with a UAV launch assembly comprising a frame and a launch driver, comprises a base, a UAV support, a biasing element, a coupler, and a retainer. The base is operably coupled to the launch driver. The UAV support is mounted to the base and is placeable in vertically collapsed and vertically extended orientations. The biasing element biases the UAV support towards the collapsed orientation. The coupler releasably couples the UAV support to a UAV when the UAV support is in the extended orientation, the UAV support being free of the UAV when in the collapsed orientation. The retainer maintains the UAV support in the vertically extended orientation prior to launch and releases the UAV support at launch so that the biasing element can cause the UAV support to move towards the collapsed orientation and to disengage from the UAV.
摘要翻译：与包括框架和发射驱动器的UAV发射组件一起使用的UAV附件组件包括基座，UAV支撑件，偏置元件，联接器和保持器。基座可操作地联接到发射驱动器。无人机支撑安装在基座上，可放置在垂直折叠和垂直延伸的方向上。偏置元件使无人机支撑朝向折叠方向偏移。当UAV支撑处于延伸方向时，联接器将UAV支撑件可释放地耦合到UAV，UAV支撑在处于折叠方向时无UAV。保持架在启动之前将UAV支撑件保持在垂直延伸的方向，并在发射时释放UAV支撑，使得偏置元件可以使UAV支撑件朝向折叠方向移动并与UAV脱离接合。

6. 发明申请

US20130313357A1 UAV Launch Attachment Assembly and Launch System 有权
标题翻译：无人机启动附件组装和启动系统
公开(公告)号：US20130313357A1
公开(公告)日：2013-11-28
申请号：US13956225
申请日：2013-07-31
申请人： Arcturus UAV LLC
发明人： Andrew B. Robinson
IPC分类号： B64F1/04
CPC分类号： B64F1/04 , B64C2201/021 , B64C2201/084 , B64F1/06
摘要： A UAV attachment assembly, used with a UAV launch assembly comprising a frame and a launch driver, comprises a base, a UAV support, a biasing element, a coupler, and a retainer. The base is operably coupled to the launch driver. The UAV support is mounted to the base and is placeable in vertically collapsed and vertically extended orientations. The biasing element biases the UAV support towards the collapsed orientation. The coupler releasably couples the UAV support to a UAV when the UAV support is in the extended orientation, the UAV support being free of the UAV when in the collapsed orientation. The retainer maintains the UAV support in the vertically extended orientation prior to launch and releases the UAV support at launch so that the biasing element can cause the UAV support to move towards the collapsed orientation and to disengage from the UAV.
摘要翻译：与包括框架和发射驱动器的UAV发射组件一起使用的UAV附件组件包括基座，UAV支撑件，偏置元件，联接器和保持器。基座可操作地联接到发射驱动器。无人机支撑安装在基座上，可放置在垂直折叠和垂直延伸的方向上。偏置元件使无人机支撑朝向折叠方向偏移。当UAV支撑处于延伸方向时，联接器将UAV支撑件可释放地耦合到UAV，UAV支撑在处于折叠方向时无UAV。保持架在启动之前将UAV支撑件保持在垂直延伸的方向，并在发射时释放UAV支撑，使得偏置元件可以使UAV支撑件朝向折叠方向移动并与UAV脱离接合。

7. 发明申请

US20120032025A1 UAV RECOVERY SYSTEM 有权
标题翻译：无人机恢复系统
公开(公告)号：US20120032025A1
公开(公告)日：2012-02-09
申请号：US13204456
申请日：2011-08-05
申请人： Mark Cameron Allen , D'Milo Dean Hallerberg , Greg P. Timm
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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