Deployment system and method for subsurface launched unmanned aerial vehicle

• US 20080111021A1
• Filed: 11/15/2006
• Published: 05/15/2008
• Est. Priority Date: 11/15/2006
• Status: Active Grant

• Current Assignee: The United States of America Naval Undersea Warefare Center
• Original Assignee: The United States of America Naval Undersea Warefare Center
• Inventors: Heaston, Jeremy R., Toth, David E.
• Granted Patent: US 7,472,866 B2
• Time in Patent Office: Days
• US Class Current: 244/63
• CPC Class Codes: B63G 8/28 Arrangement of offensive or defensive equipment
• CPC Class Codes: B64F 1/04 for launching aircraft
• CPC Class Codes: B64U 70/70 Launching or landing using catapults, tracks or rails launching from storage containers B64U70/50
• CPC Class Codes: B64U 80/84 Waterborne vehicles
• CPC Class Codes: F41F 3/07 Underwater launching-apparatus

Abstract

A launch system is provided in which an unmanned aerial vehicle is secured to a platform in a watertight tube adapted to be launched from a submerged platform. Once launched, side panels on the tube are jettisoned and a flotation device is deployed to bring the tube to the surface. The flotation device maintains the tube in a vertical position when rising to and at the surface. After surfacing, a top-sealing cap of the tube is opened. A lifting mechanism within the tube raises the vertically oriented platform assembly up within the tube. Guide rails maintain the vertical orientation of the assembly during lifting. At the topmost point of travel, the assembly is raised clear of the tube and is disengaged from the guide rails, allowing the assembly to pivot about its attachment to the lifting mechanism and assume an orientation favorable for launching the UAV.

Claims

1. A system for deploying an Unmanned Aerial Vehicle (UAV) from a platform submerged in a medium, the system comprising:

a capsule enclosing the UAV in a watertight manner when submerged;

a floatation device attached to said capsule, said floatation device providing buoyancy to said capsule to bring said capsule to a surface of the medium after launch of said capsule from the submerged platform;

a hatch forming an opening in said capsule to allow the UAV to exit said capsule, said hatch opening after said capsule reaches the surface of the medium;

a lifting means within said capsule for moving the UAV from within said capsule, through said hatch and to a position exterior to said capsule; and

a cradle for releasably supporting the UAV, said cradle and the UAV rotating between an interior orientation and a launch orientation when the UAV reaches the position exterior to said capsule.

2. The system of claim 1 further comprising a guide means to maintain said interior orientation of the cradle and UAV during movement of the UAV within said capsule by said lifting means.

3. The system of claim 2 wherein said guide means comprises:

at least one rail fixed within said capsule; and

at least one extension of said cradle slidably mating with said guide rail.

4. The system of claim 3 wherein said guide means comprises bearings to facilitate sliding movement between said at least one extension and said at least one rail.

5. The system of claim 4 wherein said bearings comprise linear bearings.

6. The system of claim 1 wherein said floatation device forms a collar at least partially surrounding said capsule when said floatation device is inflated, said collar being offset from a center of gravity of the capsule to maintain a longitudinal axis of said capsule in a substantially vertical position when said capsule reaches the surface.

7. The system of claim 6 wherein said floatation device comprises a plurality of chambers.

8. The system of claim 6 further comprising removable panels covering said floatation device, said panels conforming to a shape of said capsule.

9. The system of claim 1 wherein said lifting means comprises:

a motorized winch; and

a cable attached at one end to said winch and at a distal end to said cradle, wherein said cable is wound on the winch to move said cradle and the UAV within said capsule.

10. The system of claim 1 wherein said lifting means is selected from a group of lifting means including a winch and cable system, a hydraulic piston, rack and pinion gearing, a screw drive and a chain drive.

11. The system of claim 1 further comprising:

a power source within said capsule for providing power for operation of said system;

controls for controlling operation of said system; and

sensors for obtaining measurements of ambient conditions at least one of which within and exterior to the capsule.

12. The system of claim 11 wherein said sensors measure a depth of the medium for determining when said floatation device is activated.

13. The system of claim 11 wherein said sensors measure sea state conditions exterior to said capsule when said capsule reaches the surface for determining when said hatch is to be opened.

14. The system of claim 1 wherein said system comprises:

a ramp structure on the cradle for releasably attaching a fixed-wing UAV such that a launch orientation of the fixed-wing UAV slopes upward away from the surface; and

a launching mechanism for assisting the fixed-wing UAV in moving up said ramp structure during launch.

15. The system of claim 1 wherein lifting surfaces of the fixed-wing UAV are stored in a folded position within the capsule.

16. A system for deploying an Unmanned Aerial Vehicle (UAV) from a submerged platform, the system comprising:

a watertight elongated cylindrical capsule enclosing the UAV;

a floatation device providing buoyancy to said capsule to bring said capsule to a surface after launch of said capsule from the submerged platform, the floatation device maintaining a longitudinal axis of said capsule to be substantially vertical;

a lifting means within said capsule for moving the UAV vertically within said capsule;

a removable cap forming an opening in said capsule, said lifting means moving the UAV through opening; and

a cradle for releasably supporting the UAV, said cradle and UAV rotating between a vertical interior orientation and a substantially horizontal launch orientation upon the UAV passing through the opening.

17. The system of claim 16 further comprising:

at least one guide rail fixed within said capsule;

at least one extension of the cradle slidably mating with said guide rail; and

bearings to facilitate sliding movement between said at least one extension and said at least one rail.

18. The system of claim 18 wherein the lifting means comprises:

a motorized winch; and

a cable attached at one end to said winch and at a distal end to said cradle, wherein said cable is wound on the winch to move the cradle and the UAV within said capsule.