# US 12,111,137 B2 · Aerial arresting system for unmanned aerial vehicle > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 12,111,137 B2 - Document ID: US12111137B2 - Status: Granted - Kind: B2 - Application number: 16/124,363 - Filed: 2018-09-07 - Published: 2019-03-14 - Granted: 2024-10-08 - Earliest claimed: 2015-02-26 - Applicants: Shawn M. Theiss; Michael E. Rogers - Inventors: Shawn M. Theiss; Michael E. Rogers - Web page: https://patentgrep.com/patent/US12111137B2 ## CPC - F41H 13/0006: {Ballistically deployed systems for restraining persons or animals, e.g. ballistically deployed nets} - B64C 39/024: {of the remote controlled vehicle type, i.e. RPV} - B64U 70/30: for capturing UAVs in flight by ground or sea-based arresting gear, e.g. by a cable or a net - B64U 10/16: with five or more distinct rotor axes, e.g. octocopters - B64U 10/25: Fixed-wing aircraft (VTOL aircraft B64U10/20) - B64U 2101/16: for controlling, capturing or immobilising other vehicles - B64U 2201/10: autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS] - B64U 2201/20: Remote controls - F41H: ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL - B64C: AEROPLANES; HELICOPTERS - B64U: UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR ## Abstract A device launcher can be carried and be used to launch a device by an airborne UAV against an airborne or ground target. The target can be a moving target with the device configured to slow or disable the movement of the target. The device can be triggered manually or through an automated targeting system. The launch apparatus can be configured to launch a single device or a plurality of devices. The device launched against the target can be separated from the launch vehicle or tethered to the launch vehicle. The device can be a net that entangles the rotors of a rotor-driven vehicle. The device can include a parachute to retard movement of target vehicle whether it is falling or if it continues to move. A method of patrolling a perimeter with an airborne vehicle includes the steps of moving the airborne vehicle within the perimeter to sense unauthorized targets and launching a device against those sensed targets. ## Claims ### Claim 1 A method of disabling a target unmanned aerial vehicle using another unmanned aerial vehicle while both are flying, the method comprising the steps of: mounting a net launch device on a first unmanned aerial vehicle in such a way that allows launching the net forward, backward, to either side, up, down, and combinations thereof; aiming the net launch device mounted on the first unmanned aerial vehicle at a target unmanned aerial vehicle; and launching a net from the net launch device at the target unmanned aerial vehicle with the entire body of the net moving away from the net launch device. ### Claim 2 (depends on 1) The method of claim 1, further comprising the step of activating the launching step manually by a remote user. ### Claim 3 (depends on 1) The method of claim 1, further comprising the step of launching the net through a remote controlled system. ### Claim 4 (depends on 1) The method of claim 1, further comprising the step of launching the net through an autopilot system. ### Claim 5 (depends on 1) The method of claim 1, further comprising the step of launching the net through a sensor system. ### Claim 6 (depends on 1) The method of claim 1, wherein the net is tethered to the first unmanned aerial vehicle and further comprising the step of releasing the net from the first unmanned aerial vehicle after the net has been launched. ### Claim 7 (depends on 6) The method of claim 6, wherein the step of releasing the net from the first unmanned aerial vehicle further comprises the step of releasing the net with an aerodynamic retardation system attached to the net. ### Claim 8 (depends on 1) The method of claim 1, further comprising the step of providing the first unmanned aerial vehicle in the form of a fixed wing aircraft. ### Claim 9 (depends on 1) The method of claim 1, further comprising the step of providing the first unmanned aerial vehicle in the form of a rotorcraft aircraft. ### Claim 10 (depends on 1) The method of claim 1, further comprising the step of providing the first unmanned aerial vehicle in the form of a ducted-fan aircraft. ### Claim 11 (depends on 1) The method of claim 1, further comprising the step of mounting a plurality of net launch devices to the first unmanned aerial vehicle. ### Claim 12 A method of disabling a target unmanned aerial vehicle using another unmanned aerial vehicle while both are flying, the method comprising the steps of: mounting a net launch device on a first unmanned aerial vehicle in such a way that allows launching the net forward, backward, to either side, up, down, and combinations thereof; aiming the net launch device mounted on the first unmanned aerial vehicle that is flying in a forward direction at a target unmanned aerial vehicle located in front of the first unmanned aerial vehicle; and launching a net from the net launch device at the target unmanned aerial vehicle with the entire body of the net moving away from the net launch device in a forward direction with respect to the first unmanned aerial vehicle. ### Claim 13 A method of disabling a target unmanned aerial vehicle using another unmanned aerial vehicle while both are flying, the method comprising the steps of: mounting a net launch device on a first unmanned aerial vehicle in such a way that allows launching the net forward, backward, to either side, up, down, and combinations thereof; aiming the net launch device mounted on the first unmanned aerial vehicle at a target unmanned aerial vehicle; launching a net from the net launch device at the target unmanned aerial vehicle with the entire body of the net moving away from the net launch device; capturing the target unmanned aerial vehicle with the net; and after the target unmanned aerial vehicle has been captured, continuing to fly the first unmanned aerial vehicle. ### Claim 14 (depends on 13) The method of claim 13, wherein the net is tethered to the first unmanned aerial vehicle and further comprising the step dragging and lifting the target unmanned aerial vehicle with the first unmanned aerial vehicle from one location to another location. ### Claim 15 (depends on 14) The method of claim 14, further comprising the step of releasing the net from the first unmanned aerial vehicle. ### Claim 16 (depends on 15) The method of claim 15, wherein the step of releasing the net from the first unmanned aerial vehicle further comprises the step of releasing the net with an aerodynamic retardation system attached to the net. ### Claim 17 A method of disabling a target unmanned aerial vehicle using another unmanned aerial vehicle while both are flying, the method comprising the steps of: mounting a net launch device on a first unmanned aerial vehicle; aiming the net launch device mounted on the first unmanned aerial vehicle that is flying in a forward direction at a target unmanned aerial vehicle located in front of the first unmanned aerial vehicle; launching a net from the net launch device at the target unmanned aerial vehicle with the entire body of the net moving away from the net launch device in the forward direction with respect to the first unmanned aerial vehicle; and wherein the net is tethered to the first unmanned aerial vehicle and further comprising the steps of capturing the target unmanned vehicle with the net and then dragging and lifting the target unmanned aerial vehicle with the first unmanned aerial vehicle from one location to another location. ### Claim 18 (depends on 17) The method of claim 17, further comprising the step of releasing the net from the first unmanned aerial vehicle after the target unmanned vehicle has been captured. ### Claim 19 (depends on 18) The method of claim 18, wherein the step of releasing the net from the first unmanned aerial vehicle further comprises the step of releasing the net with an aerodynamic retardation system attached to the net. ### Claim 20 (depends on 17) The method of claim 17, further comprising the step of activating the launching step through one of a remote controlled system, an autopilot system, a sensor system, and a manual system.