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    • 98. 发明公开
    • SYSTEMS AND DEVICES FOR REMOTELY OPERATED UNMANNED AERIAL VEHICLE REPORT-SUPPRESSING LAUNCHER WITH PORTABLE RF TRANSPARENT LAUNCH TUBE
    • 用于远程操作的无人机空中车辆报告的系统和装置 - 具有便携式射频透明发射管的压载式发射机
    • EP3133019A1
    • 2017-02-22
    • EP16179915.0
    • 2010-09-09
    • AeroVironment, Inc.
    • Miralles, Carlos ThomasAndryukov, AlexanderSu, Guan H.McNeil, John
    • B64F1/04F41F3/04B64C13/20F42B39/14F41F1/00
    • B64F1/04B64C39/024B64C2201/08B64C2201/102B64C2201/146B64C2201/201B64F1/06F41A21/02F41F1/00F41F3/042F42B39/14
    • An unmanned aerial vehicle (UAV) launch tube (100) that comprises at least one inner layer of prepreg substrate (370) disposed about a right parallelepiped aperture (305), at least one outer layer of prepreg substrate (380) disposed about the right parallelepiped aperture (305), and one or more structural panels (341-344) disposed between the at least one inner layer of prepreg substrate (340) and the at least one outer layer of prepreg substrate (380). An unmanned aerial vehicle (UAV) launch tube (100) that comprises a tethered sabot (700,740) configured to engage a UAV within a launcher volume defined by an inner wall, the tethered sabot (700,740) dimensioned to provide a pressure seal at the inner wall and tethered to the inner wall, and wherein the tethered sabot (700,740) is hollow having an open end oriented toward a high pressure volume and a tether (740) attached within a hollow (910) of the sabot (700) and attached to the inner wall retaining the high pressure volume or attach to the inner base wall (1013). A system comprising a communication node (1500-1505) and a launcher (1520) comprising an unmanned aerial vehicle (UAV) in a pre-launch state configured to receive and respond to command inputs from the communication node (1500-1505).
    • 一种无人飞行器(UAV)发射管(100),其包括围绕直角平行六面体孔(305)布置的至少一个预浸料坯基底(370)的内层,至少一个预浸料坯基底 (305)以及设置在所述至少一个预浸料坯衬底(340)的内层和所述至少一个预浸料坯衬底(380)的外层之间的一个或多个结构面板(341-344)。 1。一种无人驾驶飞行器(UAV)发射管(100),其包括被配置成在由内壁限定的发射器体积内接合UAV的系留弹底(700,740),所述系留弹壳(700,740)的尺寸被设计成在内部提供压力密封 (700,740)是中空的,具有朝向高压容积的开口端和连接在弹壳(700)的中空部(910)内并连接到所述内壁的系绳(740) 内壁保持高压容积或附接到内部基壁(1013)。 一种包括通信节点(1500-1505)和启动器(1520)的系统,所述通信节点(1500-1505)和启动器(1520)包括处于预启动状态的无人飞行器(UAV),其被配置为接收并响应来自通信节点(1500-1505)的命令输入。