公开(公告)号：US20140151508A1

公开(公告)日：2014-06-05

申请号：US13689853

申请日：2012-11-30

Applicant: WB Electronics S.A.

Inventor： WOJCIECH SZUMINSKI ,  Ryszard Jurecki ,  Grzegorz Krupa ,  Adam Bartosiewicz ,  Piotr Wojciechowski

IPC: B64D1/08

CPC classification number: B64D1/08 ,  B60V1/00 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/127 ,  B64C2201/185 ,  B64C2201/187

Abstract: The mode of landing of an unmanned aerial vehicle driven by an electric engine, containing main power supply batteries, control systems of the surveillance head, transmitting and receiving systems, a flight control system, and a container equipped with a surveillance head with a looking down lens, placed in a recess situated in the lower part of the fuselage by which the vehicle is lightened at the last stage of flight shortly before landing, which means the container placed in the recess is detached, then moved outside the vehicle's body and descended by means of a parachute into a desired location, and the lightened vehicle lands in some other place. The recess in the fuselage contains an electrically controlled lock which fixes detachably the container equipped with at least one parachute placed at the bottom section of the container, on the side of the surveillance head.

Abstract translation: 由电动发动机驱动的无人驾驶飞机的模式，包含主电源电池，监视头的控制系统，发射和接收系统，飞行控制系统和装备有俯视监视头的集装箱 透镜放置在位于机身下部的凹部中，车辆在着陆前不久的最后阶段减轻，这意味着放置在凹槽中的容器被分离，然后移动到车身的外部并且下降 降落伞进入所需位置的方式，轻型车辆落在其他地方。 机身中的凹槽包含一个电控锁，其可拆卸地固定装备有至少一个放置在容器底部的降落伞的容器，在监视头的一侧。