Unmanned Aerial Surveillance Device

• US 20100282897A1
• Filed: 08/16/2006
• Published: 11/11/2010
• Est. Priority Date: 08/17/2005
• Status: Abandoned Application

• Current Assignee: Chang Industry, Inc.
• Original Assignee: Chang Industry, Inc.
• Inventors: de la Torre, Samuel
• Application Number:
  US11/464,973
• Publication Number:
  US 20100282897A1
• Time in Patent Office: Days
• US Class Current: 244/49
• CPC Class Codes: B64C 39/024 of the remote controlled vehicle type, i.e. RPV
• CPC Class Codes: B64U 10/25 Fixed-wing aircraft VTOL aircraft B64U10/20
• CPC Class Codes: B64U 10/50 Glider-type UAVs, e.g. with parachute, parasail or kite for landing B64U70/83
• CPC Class Codes: B64U 20/65 Composite materials
• CPC Class Codes: B64U 20/87 Mounting of imaging devices, e.g. mounting of gimbals
• CPC Class Codes: B64U 2101/30 for imaging, photography or videography
• CPC Class Codes: B64U 2101/31 for surveillance
• CPC Class Codes: B64U 2201/10 autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS]
• CPC Class Codes: B64U 2201/20 Remote controls
• CPC Class Codes: B64U 30/12 Variable or detachable wings, e.g. wings with adjustable sweep
• CPC Class Codes: B64U 30/14 detachable
• CPC Class Codes: B64U 30/40 Empennages, e.g. V-tails foldable or collapsible UAVs B64U20/50
• CPC Class Codes: B64U 50/13 using external fans or propellers
• CPC Class Codes: B64U 50/19 using electrically powered motors
• CPC Class Codes: B64U 80/60 by wearable objects, e.g. garments or helmets
• CPC Class Codes: B64U 80/70 in containers B64U80/60 takes precedence

Abstract

An aerial surveillance device is provided, comprising an image capturing device capable of being supported by an airframe structure above the ground. The airframe structure includes a body portion defining a longitudinal axis and configured to support the image-capturing device. A tail portion having control surfaces is operably engaged with the body portion along the axis. Transversely-extending wing portions are directly engaged with the body portion. Each wing portion is defined by longitudinally-opposed spars extending from a spaced-apart disposition at the body portion to a common connection distally from the body portion. The spars have a fabric extending therebetween to provide a wing surface. A support member extends along an aerodynamic center, transversely to the body portion, of each wing portion, to tension and rigidify the wing portions so as to provide a positive camber for the wing portions and to form an airfoil.

Claims

1. An unmanned aerial surveillance device, comprising:

an image capturing device;

an airframe structure having the image-capturing device operably engaged therewith and configured to be capable of supporting the image-capturing device at an above-ground altitude, said airframe structure including;

an elongate body portion defining a longitudinal axis;

a tail portion operably engaged with the body portion along the axis and comprising a rudder control surface and an elevator control surface;

a pair of transversely-opposed wing portions directly and operably engaged with the body portion and extending substantially transversely thereto, each wing portion being defined by longitudinally-opposed spars extending from a spaced-apart disposition at the body portion to a common connection disposed distally with respect to the body portion, the spars having a fabric extending therebetween so as to provide a wing surface; and

a support member extending along an aerodynamic center, transversely to the body portion, of each wing portion, the support members being configured to tension and rigidify the wing portions so as to provide a positive camber for each wing portion and to form an airfoil.

2. A device according to claim 1 wherein each support member extends from the common connection of each wing portion to engage at least one of the body portion and each other, so as to rigidify the wing portions.

3. A device according to claim 1 further comprising a tensioning member extending between the common connections of the transversely-opposed wing portions and configured to provide a tension therebetween so as to rigidify the wing portion and form a dihedral.

4. A device according to claim 1 further comprising a tensioning member extending between each common connection of the transversely-opposed wing portions and the body portion, the tensioning members being configured to provide a tension between each common connection and the body portion so as to rigidify the respective wing portion and form a dihedral.

5. A device according to claim 1 wherein the image capturing device is at least partially housed by the airframe structure.

6. A device according to claim 1 wherein the image-capturing device is configured to at least one of pan, tilt, and zoom with respect to the airframe structure.

7. A device according to claim 1 wherein the image capturing device is stabilized with respect to the airframe structure.

8. A device according to claim 1 wherein the image capturing device is gyroscopically stabilized.

9. A device according to claim 1 further comprising a propulsion device operably engaged with the body portion of the airframe structure for providing forward propulsion for the airframe structure.

10. A device according to claim 9 wherein the propulsion device further comprises a propeller member having a plurality of blades and being configured to be rotated by a motor so as to provide the forward propulsion for the airframe structure, the blades of the propeller member being foldable to extend substantially parallel to the axis.

11. A device according to claim 9 further comprising a power source operably engaged with at least one of the image-capturing device and the propulsion device and configured to provide power therefor, the power source being supported by the airframe structure.

12. A device according to claim 1 further comprising a controller device operably engaged with and configured to control at least one of the image-capturing device, the propulsion device, the rudder control surface, and the elevator control surface.

13. A device according to claim 12 wherein the controller device is at least partially housed by the body portion of the airframe structure and is configured to be remotely actuated.

14. A device according to claim 13 further comprising an actuator device configured to be in wireless communication with the controller device and to remotely actuate the controller device, so as to allow the at least one of the image-capturing device, the propulsion device, the rudder control surface, and the elevator control surface to be remotely controlled as the airframe structure is at the above-ground altitude.

15. A device according to claim 12 further comprising a navigation device operably engaged with at least the controller device, the controller device being responsive to the navigational device to direct the at least one of the image-capturing device, the propulsion device, the rudder control surface, and the elevator control surface to guide the airframe structure from a first location to a second location and the image-capturing device to capture at least one image at a waypoint between and including the first and second locations.

16. A device according to claim 1 further comprising an extension member operably engaged between the body portion and the tail portion so as to separate the tail portion from the body portion along the axis.

17. A device according to claim 1 further comprising an explosive device releasably engaged with the airframe structure and configured to be selectively released while the airframe structure is at the above-ground altitude.

18. A device according to claim 1 further comprising an audio-capturing device operably engaged with the airframe structure so as to be supported thereby.

19. A device according to claim 1 wherein the tail portion and each of the wing portions is configured to be foldable toward and along the axis such that, when folded, the airframe structure is configured to be received by a tubular storage container.

20. A device according to claim 1 wherein the wing portions are configured to be removable from the airframe structure, and wherein the wing portions and the tail portion are foldable such that, when folded, the wing portions and the airframe structure are configured to be received by a tubular storage container.

21. A device according to claim 1 further comprising a selectively actuatable controlled descent and recovery system operably engaged with the airframe structure and configured to slow a descent thereof.

22. A device according to claim 21 wherein the controlled descent and recovery system further comprises a selectively deployable parachute device.

23. A device according to claim 1 further comprising an aileron member operably engaged with the common connection of each wing portion, the aileron members being controllable to affect the roll of the device.

24. A device according to claim 1 further comprising at least one spreader member operably engaged between the longitudinally-opposed spars of each wing portion so as to separate the spars into the spaced-apart disposition.

25. A device according to claim 24 wherein the support member of each wing portion is operably engaged with the at least one spreader member of that wing portion such that, upon the support member being deployed to tension and rigidify that wing portion, the support member deploys the at least one spreader member to separate the spars into the spaced-apart disposition.