公开(公告)号：US07849628B2

公开(公告)日：2010-12-14

申请号：US11856049

申请日：2007-09-16

申请人： John A. Condon ,  Timothy Brosseau ,  David Lyon

发明人： John A. Condon ,  Timothy Brosseau ,  David Lyon

IPC分类号： F41C27/06

CPC分类号： F41C27/06 ,  F41F3/04

摘要： A launcher system and method for an unmanned aerial vehicle (UAV), wherein the launcher system comprises a barrel comprising a prepackaged internal pusher cup configured behind the UAV housed within the barrel; an expansion chamber operatively connected around the barrel, wherein the barrel extends out of a first end of the expansion chamber; a muzzle adapter operatively connected to a second end of the expansion chamber, wherein the first end of the expansion chamber is positioned opposite to the second end of the expansion chamber; a rifle slip-fitted to the muzzle adapter; and a stand operatively connected to the expansion chamber, wherein a triggering of the rifle causes the internal pusher cup to push the UAV out of the barrel at a predetermined launch velocity in order to attain a predetermined self-propelled flight trajectory.

摘要翻译： 一种用于无人驾驶飞行器（UAV）的发射器系统和方法，其中所述发射器系统包括筒，所述筒包括配置在容纳在所述筒内的UAV后面的预先包装的内部推动器杯; 可操作地连接在所述筒周围的膨胀室，其中所述筒从所述膨胀室的第一端延伸出来; 枪口适配器可操作地连接到膨胀室的第二端，其中膨胀室的第一端与膨胀室的第二端相对定位; 枪口适配器上装有一个步枪; 以及可操作地连接到所述膨胀室的支架，其中所述步枪的触发导致所述内部推动器杯以预定的发射速度将所述UAV推出所述筒体，以便达到预定的自推进飞行轨迹。

公开(公告)号：US20100281745A1

公开(公告)日：2010-11-11

申请号：US11856049

申请日：2007-09-16

申请人： John A. Condon ,  Timothy Brosseau ,  David Lyon

发明人： John A. Condon ,  Timothy Brosseau ,  David Lyon

IPC分类号： F41C27/06

CPC分类号： F41C27/06 ,  F41F3/04

摘要： A launcher system and method for an unmanned aerial vehicle (UAV), wherein the launcher system comprises a barrel comprising a prepackaged internal pusher cup configured behind the UAV housed within the barrel; an expansion chamber operatively connected around the barrel, wherein the barrel extends out of a first end of the expansion chamber; a muzzle adapter operatively connected to a second end of the expansion chamber, wherein the first end of the expansion chamber is positioned opposite to the second end of the expansion chamber; a rifle slip-fitted to the muzzle adapter; and a stand operatively connected to the expansion chamber, wherein a triggering of the rifle causes the internal pusher cup to push the UAV out of the barrel at a predetermined launch velocity in order to attain a predetermined self-propelled flight trajectory.

摘要翻译： 一种用于无人驾驶飞行器（UAV）的发射器系统和方法，其中所述发射器系统包括筒，所述筒包括构造在容纳在所述筒内的UAV后面的预先包装的内部推动器杯; 可操作地连接在所述筒周围的膨胀室，其中所述筒从所述膨胀室的第一端延伸出来; 枪口适配器可操作地连接到膨胀室的第二端，其中膨胀室的第一端与膨胀室的第二端相对定位; 枪口适配器上装有一个步枪; 以及可操作地连接到所述膨胀室的支架，其中所述步枪的触发导致所述内部推动器杯以预定的发射速度将所述UAV推出所述筒体，以便达到预定的自推进飞行轨迹。