UNMANNED GYROKITE AS SELF-POWERED AIRBORNE PLATFORM FOR ELECTRONIC SYSTEMS

• US 20110186687A1
• Filed: 01/29/2010
• Published: 08/04/2011
• Est. Priority Date: 01/29/2010
• Status: Abandoned Application

• Current Assignee: Raytheon Company (Rtx Corporation)
• Original Assignee: Raytheon Company (Rtx Corporation)
• Inventors: Elder, Steven J.
• Application Number:
  US12/696,389
• Publication Number:
  US 20110186687A1
• Time in Patent Office: Days
• US Class Current: 244/155.A
• CPC Class Codes: B64C 31/06 Kites toy aspects A63H27/08; airborne towed targets, e.g. kites F41J9/10
• CPC Class Codes: B64C 39/022 Tethered aircraft
• CPC Class Codes: B64U 10/11 Autogyros
• CPC Class Codes: B64U 10/60 Tethered aircraft
• CPC Class Codes: B64U 2101/20 for use as communications relays, e.g. high-altitude platforms
• CPC Class Codes: B64U 2101/31 for surveillance
• CPC Class Codes: B64U 2201/20 Remote controls
• CPC Class Codes: F03D 13/20 Arrangements for mounting or supporting wind motors; Masts or towers for wind motors
• CPC Class Codes: F03D 5/00 Other wind motors controlling thereof F03D7/00
• CPC Class Codes: F05B 2240/917 attached to cables
• CPC Class Codes: F05B 2240/921 kept aloft due to aerodynamic effects

Abstract

Embodiments of an unmanned gyrokite for use in conjunction with a tether are provided. In one embodiment, the unmanned gyrokite includes an airframe configured to be attached to the tether, an autogyro rotor assembly mounted to the airframe and configured to generate lift when deployed in winds aloft, and a generator mechanically coupled to the autogyro rotor assembly and configured to be driven thereby. An electronic system coupled to the airframe is configured to be powered by the generator.

Claims

1. An unmanned gyrokite for use in conjunction with a tether, the unmanned gyrokite comprising:

an airframe configured to be attached to the tether;

an autogyro rotor assembly mounted to the airframe and configured to generate lift when deployed in winds aloft;

a generator mechanically coupled to the autogyro rotor assembly and configured to be driven thereby; and

an electronic system coupled to the airframe and configured to be powered by the generator.

2. An unmanned gyrokite according to claim 1 wherein the autogyro rotor assembly comprises:

a rotor hub rotatably coupled to the airframe; and

a plurality of rotor blades extending radially outward from the rotor hub.

3. An unmanned gyrokite according to claim 2 wherein the generator is housed, at least partially, within the rotor hub.

4. An unmanned gyrokite according to claim 2 further comprising a scanning device having at least one antenna integrated into the autogyro rotor assembly.

5. An unmanned gyrokite according to claim 4 wherein the scanning device is selected from the group consisting of a vertical scanning radar and a direction finder.

6. An unmanned gyrokite according to claim 4 further comprising a rotor sensor coupled to the autogyro rotor assembly and configured to monitor an operational parameter thereof.

7. An unmanned gyrokite according to claim 6 wherein the rotor sensor comprises a tachometer configured to monitor the rotational speed of the rotor hub and plurality of rotor blades.

8. An unmanned gyrokite according to claim 2 wherein each of the plurality of rotor blades comprises a parafoil.

9. An unmanned gyrokite according to claim 1 further comprising:

a controller electrically coupled to the generator; and

a tether release mechanism mounted to the airframe and operatively coupled to the controller, the tether release mechanism configured to disengage the airframe and the tether when actuated by the controller.

10. An unmanned gyrokite according to claim 8 wherein the unmanned gyrokite is configured to be utilized in conjunction with a Ground Control Station, and wherein the unmanned gyrokite further comprises a wireless transceiver operatively coupled to the controller and configured to enable bi-directional communication between the controller and the Ground Control Station.

11. An unmanned gyrokite according to claim 1 wherein the electronic system comprises a camera.

12. An unmanned gyrokite according to claim 1 wherein the electronic system comprises a targeting system.

13. An unmanned gyrokite according to claim 1 wherein the electronic system comprises a telecommunication repeater.

14. An unmanned gyrokite according to claim 1 wherein the electronic system comprises a cellular site.

15. An unmanned gyrokite according to claim 1 wherein the electronic system comprises an electronic beacon.

16. An unmanned gyrokite for use in conjunction with a tether and an electronic system, the unmanned gyrokite comprising:

an airframe configured to be attached to the tether;

an autogyro rotor assembly mounted to the airframe and configured to generate lift when the unmanned gyrokite is deployed in winds aloft;

a package bay coupled to the airframe and to support the electronic system; and

a generator mechanically coupled to the autogyro rotor assembly and configured to be driven thereby, the generator supplying power to electronic system when installed within the package bay.

17. An unmanned gyrokite according to claim 16 further comprising:

a controller operatively coupled to the generator; and

a tether release mechanism operatively coupled the controller and mechanically coupled between the tether and the airframe, the tether release mechanism configuration to disengage the airframe from the tether when actuated by the controller.

18. An unmanned gyrokite according to claim 17 further comprising a scanning device operatively coupled to the controller and integrated into the autogyro rotor assembly.

19. An unmanned gyrokite for use in conjunction with a tether, the unmanned gyrokite comprising:

an airframe configured to be attached to the tether;

an autogyro rotor assembly mounted to the airframe and configured to generate lift when the unmanned gyrokite is deployed in winds aloft;

a generator mechanically coupled to the autogyro rotor assembly and configured to be driven thereby;

a surveillance sensor coupled to the airframe and configured to be powered by the generator; and

a transmitter operatively coupled to the surveillance sensor and configured to transmit data received therefrom.

20. An unmanned gyrokite according to claim 19 wherein the surveillance sensor is selected from the group consisting of a camera and a synthetic aperture radar.