AERIAL PAYLOAD DEPLOYMENT SYSTEM

• US 20110147513A1
• Filed: 01/20/2010
• Published: 06/23/2011
• Est. Priority Date: 01/21/2009
• Status: Abandoned Application

• Current Assignee: Sofcoast, Inc.
• Original Assignee: Sofcoast, Inc.
• Inventors: SURMONT, JOHN STEVEN
• Application Number:
  US12/690,830
• Publication Number:
  US 20110147513A1
• Time in Patent Office: Days
• US Class Current: 244/33
• CPC Class Codes: B64B 1/10 Tail unit construction B64B1/12 takes precedence
• CPC Class Codes: B64B 1/14 Outer covering
• CPC Class Codes: B64B 1/20 provided with wings or stabilising surfaces tail unit construction B64B1/10; movable control surfaces B64B1/12
• CPC Class Codes: B64B 1/42 Construction or attachment of stabilising surfaces
• CPC Class Codes: B64B 1/50 Captive balloons

Abstract

A mobile aerial platform system is provided. The aerial platform system may lift a payload, such as a surveillance system or a communications repeater, into the lower atmosphere to assist in applications such as crowd control or disaster relief. The aerial platform system may be contained in a portable configuration and transported to the deployment site using a vehicle.

Claims

1. An aerial payload deployment system, comprising:

a frame configured to be disposed in a vehicle;

a gas cylinder disposed in the frame;

an aerial platform coupled to the vehicle by a tether and configured to be inflated using the gas from the gas cylinder; and

a payload configured to be carried by the aerial platform when the aerial platform is inflated.

2. The system of claim 1, wherein the aerial platform comprises a gas chamber coupled to a ram-air chamber, and wherein the aerial platform has an aerodynamic shape to provide lift.

3. The system of claim 2, wherein the aerial platform further comprises a plurality of helium chambers coupled to and alternating with a ram-air chamber.

4. The system of claim 2, wherein the aerial platform further comprises a biaxially-oriented polyethylene terephthalate polyester body, and wherein the gas chamber has a polyurethane lining for holding the gas.

5. The system of claim 1, further comprising an aerial platform deployment apparatus disposed on the vehicle to contain the aerial platform when deflated, and configured to open to allow egress of the aerial platform during inflation.

6. The system of claim 1, further comprising a winch coupled to the vehicle and the tether, and configured to control a vertical height of the aerial platform when inflated.

7. The system of claim 1, wherein the payload comprises a repeater.

8. The system of claim 1, wherein the payload comprises a surveillance system.

9. The system of claim 8, wherein the surveillance system comprises a video camera.

10. The system of claim 8, further comprising an electrical cable coupled to the tether to power the surveillance system and to allow the surveillance system to communicate with a base.

11. The system of claim 8, wherein the surveillance system communicates wirelessly with a base and is powered using a battery.

12. The system of claim 6, wherein the payload further comprises a positioning system.

13. The system of claim 12, wherein the positioning system comprises a global positioning system, an orientation sensor, and a height sensor.

14. The system of claim 13, wherein the positioning system provides position data to the surveillance system, wherein the surveillance system is configured to use the position data to determine a location of a predetermined surveillance area, and wherein the surveillance system is further configured to orient itself towards the predetermined surveillance area.

15. The system of claim 1, wherein the gas tank comprises a carbon fiber tank.

16. The system of claim 6, further comprising a pump coupled to the gas tank, wherein the winch is configured to lower the aerial platform while inflated, and wherein the pump is configured to deflate the aerial platform by pumping the helium from the aerial platform into the gas tank.

17. An aerial payload deployment vehicle apparatus, comprising:

a vehicle;

a gas cylinder disposed in the vehicle;

a winch configured to wind and unwind a tether;

wherein the tether is coupled to an aerial platform and the winch, the tether comprising a high strength material and a power cord;

wherein the aerial platform is coupled to the vehicle by the tether and is configured to be inflated using the gas from the gas cylinder; and

a payload configured to be carried by the aerial platform when the aerial platform is inflated, and configured to be powered by power from the power cord.

18. The apparatus of claim 17, wherein the aerial platform further comprises a gas chamber coupled to a ram-air chamber, and wherein the aerial platform has an aerodynamic shape to provide lift.

19. The system of claim 18, further comprising a pump coupled to the gas tank, wherein the winch is configured to lower the aerial platform while inflated, and wherein the pump is configured to deflate the aerial platform by pumping the helium from the aerial platform into the gas tank.

20. An aerial payload deployment system, comprising:

a frame configured to be disposed in a vehicle;

a gas cylinder disposed in the frame;

a winch configured to wind and unwind a tether;

wherein the tether is coupled to an aerial platform and the winch, the tether comprising a high strength material and a power cord;

wherein the aerial platform is coupled to the vehicle by the tether and is configured to be inflated using the gas from the gas cylinder, the aerial platform comprising a ram-air cell coupled to a gas cell and having an aerodynamic shape; and

a payload configured to be carried by the aerial platform when the aerial platform is inflated, and configured to be powered by power from the power cord, the payload comprising a surveillance system or a repeater.