发明名称 UAV recovery system II
摘要 A UAV recovery system is disclosed. In the illustrative embodiment for UAV recovery over water, the system includes ship-based elements and UAV-based elements. The UAV-based elements include a mass, such as ball, that is coupled to cord, which is in turn coupled to the tail of a UAV. The ship-based elements include a capture plate and a boom, wherein the boom is pivotably coupled to the deck of a ship. For use in recovery operations, the boom is rotated so that it extends over the side of the ship. A UAV is flown over the boom toward the capture plate at an altitude such that the mass that is attached to the tail of the UAV hangs lower than the capture plate. With continued forward motion, the cord that hangs from the UAV is captured by a grooves in the capture plate. The capture plate geometrically constrains the mass, thereby assuring positive capture of the UAV.
申请公布号 US2007158498(A1) 申请公布日期 2007.07.12
申请号 US20060327616 申请日期 2006.01.06
申请人 LOCKHEED MARTIN CORPORATION 发明人 SNEDIKER JOHN
分类号 B64F1/02 主分类号 B64F1/02
代理机构 代理人
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