Device and method to intercept an aerial vehicle

Abstract

An airframe is provided that can be flown under the control of an operator or an automated sensor and feedback system. The airframe can be any of a variety of known configurations with multiple rotors, fixed or retractable wings, puller or pusher propellers, or jet engines. The airframe includes at least one arm that is used to intercept and disable another airborne vehicle. In some configurations, the arm is fixed and can include fingers at its outer end. In other configurations, the arm is movable from a closed condition to an open condition. A wire or net is connected between the arm and a portion of the airframe so that the wire or net is spread open when the arm is deployed to the open condition. The wire or net are configured to disable or capture a target such as another aerial vehicle.

1 . An airframe used to intercept another aerial vehicle in the air while flying; the airframe comprising:
 a body having a fixed arm projecting forward in a flight direction from the body; the arm being free of hinges.   
     
     
         2 . The airframe of  claim 1 , further comprising a plurality of fingers extending from the end of the fixed arm. 
     
     
         3 . The airframe of  claim 1 , further comprising a central body carried by the fixed arm; a plurality of fingers extending from the central body. 
     
     
         4 . An airframe used to intercept a target aerial vehicle in the air while flying; the airframe comprising:
 a body having an arm hinged to the body and movable between closed and open conditions with respect to the body;   a thin member connected to the arm and the body; the thin member being extended when the arm is in the open condition; and   the thin member being disposed in front of the hinged connection between the arm and the body when the arm is in the open condition; the thin member adapted to disable the target vehicle.   
     
     
         5 . The airframe of  claim 4 , wherein the thin member is releasable from the body and arm. 
     
     
         6 . The airframe of  claim 5 , further comprising a parachute connected to the thin member. 
     
     
         7 . The airframe of  claim 6 , wherein the parachute is carried by the body. 
     
     
         8 . An airframe used to intercept a target aerial vehicle in the air while flying; the airframe comprising:
 a body having a plurality of arms projecting forward in a flight direction from the body; and   at least one thin member carried by the arms; the thin member adapted to disable the target vehicle.   
     
     
         9 . The airframe of  claim 8 , wherein the arms are movable between a closed condition and an open condition with respect to the body. 
     
     
         10 . The airframe of  claim 9 , wherein the at least one thin member is in the form of a frame when the arms are in the open condition. 
     
     
         11 . The airframe of  claim 9 , wherein the at least one thin member is in the form of an X shape when the arms are in the open condition. 
     
     
         12 . The airframe of  claim 8 , wherein the thin member is releasable from the body. 
     
     
         13 . The airframe of  claim 12 , wherein the thin member is releasable from the arms. 
     
     
         14 . The airframe of  claim 13 , further comprising a parachute connected to the thin member. 
     
     
         15 . The airframe of  claim 12 , wherein the arms are releasable from the body with the thin member. 
     
     
         16 . The airframe of  claim 15 , further comprising a parachute connected to the thin member. 
     
     
         17 . The airframe of  claim 8 , wherein the thin member is carried by the arms in front of the body. 
     
     
         18 . The airframe of  claim 8 , wherein the thin member is a non-metal cord. 
     
     
         19 . The airframe of  claim 8 , wherein the thin member is a polymer fiber. 
     
     
         20 . The airframe of  claim 8 , wherein the thin member is a metal wire.