PORTABLE UNMANNED AIRCRAFT FOR NEAR-INSTANT AERIAL SURVEILLANCE

• US 20140312164A1
• Filed: 01/18/2013
• Published: 10/23/2014
• Est. Priority Date: 01/18/2012
• Status: Abandoned Application

• Current Assignee: Joshua M. Gibson, Sagar Jasu Panara
• Original Assignee: Joshua M. Gibson, Sagar Jasu Panara
• Inventors: GIBSON, JOSHUA M., PANARA, SAGAR JASU
• Application Number:
  US13/745,322
• Publication Number:
  US 20140312164A1
• Time in Patent Office: Days
• US Class Current: 244/13
• CPC Class Codes: B64U 10/13 Flying platforms
• CPC Class Codes: B64U 10/80 UAVs characterised by their small size, e.g. micro air vehicles [MAV]
• CPC Class Codes: B64U 2101/30 for imaging, photography or videography
• CPC Class Codes: B64U 2101/31 for surveillance
• CPC Class Codes: B64U 2201/20 Remote controls
• CPC Class Codes: B64U 30/20 Rotors; Rotor supports
• CPC Class Codes: B64U 50/12 using turbine engines, e.g. turbojets or turbofans
• CPC Class Codes: B64U 50/14 ducted or shrouded
• CPC Class Codes: B64U 80/60 by wearable objects, e.g. garments or helmets

Abstract

A portable unmanned aerial vehicle or aircraft, capable of being easily carried by a single individual by means of a mounting device, which can be fastened on a belt or strap. The aerial vehicle comprises a wing attached at one end to a fan or turbine assembly. The fan or turbine assembly may be electrically driven, with power supplied by one or more batteries. In flight, the fan or turbine assembly causes the aerial vehicle to rotate around its center-of-mass (COM), with lift provided by the wing as it rotates. A camera is located on the aircraft at or near the COM.

Claims

1. An apparatus, comprising:

an unmanned aircraft; and

a mounting device, wherein the mounting device is adapted to enable the unmanned aircraft to be mounted and carried on a single individual.

2. The apparatus of claim 1, wherein the mounting device is mounted on a belt.

3. The apparatus of claim 1, wherein the mounting device is mounted on a strap.

4. The apparatus of claim 1, wherein the unmanned aircraft comprises a mono-wing.

5. The apparatus of claim 1, wherein the unmanned aircraft comprises at least one wing and at least one turbine or ducted fan propulsion system, and possesses a center of mass disposed between the at least one wing and at least one turbine or ducted fan propulsion system, wherein the unmanned aircraft rotates around the center of mass when in flight.

6. The apparatus of claim 5, further comprising a camera or imaging device located at the center of mass.

7. The apparatus of claim 6, further comprising a primary inertial navigation system located in the unmanned aircraft near the center of mass.

8. The apparatus of claim 7, further comprising a hiller extending from one side of the wing.

9. The apparatus of claim 8, wherein the hiller is disposed in the plane of rotation of the unmanned aircraft.

10. The apparatus of claim 7, further comprising a second inertial navigation system located in the mounting device.

11. The apparatus of claim 7, further comprising a wireless communication device located in the unmanned aircraft near the center of mass.

12. The apparatus of claim 7, wherein the camera or imaging device is positioned to take images below the aircraft when in flight.

13. The apparatus of claim 12, wherein the camera or imaging device captures an image each time the wing passes through a defined angular location with respect to the center of mass or center of rotation.

14. The apparatus of claim 13, wherein the image data is sent to a remote computing device, wherein the remote computing device aligns image data captured sequentially based upon the angular location.

15. The apparatus of claim 5, wherein the aircraft is powered by one or more batteries.

16. The apparatus of claim 5, wherein the wing is detachable.

17. The apparatus of claim 16, wherein the wing holds one or more batteries for powering the aircraft.

18. The apparatus of claim 5, further comprising a sound or light-based sensor on the front edge of the wing for detecting objects in the area of the aircraft.