Aerial arresting system for unmanned aerial vehicle

a technology for unmanned aerial vehicles and arresting systems, which is applied in the field of aerial arresting devices, can solve problems such as dangerous uav activities

Inactive Publication Date: 2017-12-14
THEISS UAV SOLUTIONS LLC
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

[0009]The preceding non-limiting aspects, as well as others, are more particularly described below. A more complete understanding of the processes and equipment can be obtained by reference to the accompanying drawings, which are not intended to indicate relative size and dimensions of the assemblies or components thereof. In t

Problems solved by technology

Although many of these uses are beneficial to society, some have found uses for drones that do not benefit the

Method used

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  • Aerial arresting system for unmanned aerial vehicle
  • Aerial arresting system for unmanned aerial vehicle
  • Aerial arresting system for unmanned aerial vehicle

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Embodiment Construction

[0045]The different configurations of the launch devices are indicated generally by the numeral 2 in the accompanying drawings. Launch devices 2 are carried by airborne vehicles 4 such as the fixed wing device depicted in FIGS. 1-3 or the rotor-type device depicted in FIGS. 4 and 6. Different vehicles can be used including manned aircraft or unmanned aircraft, fixed wing, rotorcraft, ducted-fan, ornithopter or orthopter, rocket / missile, and / or lighter-than-air. The rotor-type vehicle can be a multiple-rotor unmanned aerial vehicle (UAV) or drone which is controlled by a user through a controller 6 such as a radio frequency controller or a mobile computer such as a smart phone using cellular, WIFI, ZigBee®, Bluetooth®, WiMAX, communications protocols or a combination of both. The target 8 can be another airborne vehicle or a ground-based target. The ground-based target can be a vehicle, a person, or an animal. Launch device 2 is configured to be operated while vehicle 4 is airborne a...

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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.

Description

CROSS REFERENCE TO RELATED APPLICATIONS[0001]This application claims the benefit of U.S. Provisional Patent Applications 62 / 176,670 filed Feb. 26, 2015 and 62 / 262,264 filed Dec. 2, 2015; the disclosures of both are incorporated herein by reference.BACKGROUND OF THE DISCLOSURE1. Technical Field[0002]The disclosure generally relates to aerial arresting devices and methods for using the devices for eliminating or reducing an aerial device such as an unmanned aerial vehicle (UAV) or drone. More particularly, the disclosure relates to aerial arresting devices and methods that launch a device such as a net from one aerial vehicle to disrupt or discontinue the operation of another aerial vehicle. The disclosure relates to devices launched manually and automatically.2. Background Information[0003]Privately-owned aerial vehicles have increased in numbers especially unmanned aerial vehicles (UAVs) which are commonly referred to as drones. These vehicles have historically been for hobbyists wh...

Claims

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Application Information

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IPC IPC(8): F41H13/00
CPCF41H13/0006B64C39/024B64U70/30
Inventor THEISS, SHAWN M.ROGERS, MICHAEL E.SAHO, III, FRANKDRYDEN, JR., WILLIAM
Owner THEISS UAV SOLUTIONS LLC
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