公开(公告)号：US09175934B1

公开(公告)日：2015-11-03

申请号：US13680597

申请日：2012-11-19

Applicant: Lockheed Martin Corporation

Inventor： James C Kilian

IPC: F41G9/00 ,  F41H13/00 ,  G05D1/12 ,  B64D47/08

CPC classification number: F41H13/00 ,  B64C2201/121 ,  B64D47/08 ,  F41H11/02 ,  G05D1/12

Abstract: An injector device configured to mount to a predatory unmanned aerial vehicle (UAV) for non-destructively disabling and controlling a threat UAV comprises a rigid housing having a hollow interior. A controllable mount structure attaches the rigid housing to the predatory UAV and aligns the housing opening with the fuselage or payload of the threat UAV. A rigid penetrator rod disposed in the interior of the housing is configured to pierce the fuselage and hence payload of the threat UAV. A conduit coupled to the penetrator rod enables a disabling substance to be conveyed through the penetrator rod and into the payload of the threat UAV. An ejector propels the penetrator rod from the housing and into the payload of the threat UAV in response to a trigger when the threat UAV is within a predetermined range.

Abstract translation: 配置成安装到掠夺式无人驾驶飞行器（UAV）用于非破坏性地禁用和控制威胁无人机的喷射器装置包括具有中空内部的刚性壳体。 可控制的安装结构将刚性壳体连接到掠夺式无人机，并将壳体开口与威胁无人机的机身或有效载荷对准。 设置在壳体内部的刚性穿透杆配置成刺穿机身并因此穿过威胁无人机的有效载荷。 连接到穿透杆的导管使得能够将致残物质输送通过穿透杆并进入威胁无人机的有效载荷。 当威胁UAV在预定范围内时，喷射器响应于触发器将穿透杆从壳体推进到威胁无人机的有效载荷中。