System for shipboard launch and recovery of unmanned aerial vehicle (UAV) aircraft and method therefor

• US 8,028,952 B2
• Filed: 03/31/2008
• Issued: 10/04/2011
• Est. Priority Date: 03/31/2008
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Urnes, James M. Sr.
• Primary Examiner(s): Dinh; Tien
• Assistant Examiner(s): KREINER, MICHAEL B
• Application Number:
  US12/059,389
• Publication Number:
  US 20090242693A1
• Time in Patent Office: 1,282 Days
• Field of Search: 244/110.C, 244/110.F, 244/110.G, 244/110.R, 244/116, 244/63
• US Class Current: 244/63
• CPC Class Codes: B63B 35/50 Vessels or floating structures for aircraft aircraft carriers B63G11/00; flying-boat hulls, other flotation means for aircraft B64
• CPC Class Codes: B64C 39/024 of the remote controlled vehicle type, i.e. RPV
• CPC Class Codes: B64F 1/06 using catapults
• CPC Class Codes: B64U 10/25 Fixed-wing aircraft VTOL aircraft B64U10/20
• CPC Class Codes: B64U 70/30 for capturing UAVs in flight by ground or sea-based arresting gear, e.g. by a cable or a net
• 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

Abstract

A system to launch and recover an Unmanned Aerial Vehicle (UAV) aircraft has a pole member attached to a deck of a ship. An arm member is attached to the pole member and extends away from the pole member in an approximately horizontal direction. The arm member is able to move rotationally and vertically on the pole member. An attachment mechanism is attached to a distal end of the arm member for holding and capturing the UAV aircraft. Momentum of the UAV aircraft causes the arm member to move rotationally around and vertically on the pole member when the UAV aircraft is coupled to the attachment mechanism.

Claims

1. A system to launch and recover an Unmanned Aerial Vehicle (UAV) aircraft comprising:

a pole member attached to a deck of a ship;

an arm member attached to the pole member and extending away from the pole member in an approximately horizontal direction, the arm member being able to move rotationally around the pole member and vertically up and down the pole member; and

an attachment mechanism attached to a distal end of the arm member for releasably holding, launching, and capturing the UAV aircraft;

wherein momentum of the UAV aircraft causes the arm member to move rotationally around and vertically on the pole member when the UAV aircraft is coupled to the attachment mechanism.

2. A system to launch and recover an Unmanned Aerial Vehicle (UAV) aircraft in accordance with claim 1 further comprising a capture assembly attached to the UAV aircraft to aid in the attachment mechanism capturing the UAV aircraft.

3. A system to launch and recover an Unmanned Aerial Vehicle (UAV) aircraft in accordance with claim 2 wherein the capture assembly is attached to the UAV aircraft and positioned near a center of gravity of the UAV aircraft.

4. A system to launch and recover an Unmanned Aerial Vehicle (UAV) aircraft in accordance with claim 2 further comprising a pivot boom coupled to the capture assembly to extend a capture area of the UAV aircraft by the attachment device.

5. A system to launch and recover an Unmanned Aerial Vehicle (UAV) aircraft in accordance with claim 1 further comprising a track formed on the pole member for guiding movement of the arm member coupled to the track.

6. A system to launch and recover an Unmanned Aerial Vehicle (UAV) aircraft in accordance with claim 5 wherein the track runs spirally from a top section to a bottom section of the pole member.

7. A system to launch and recover an Unmanned Aerial Vehicle (UAV) aircraft in accordance with claim 1 wherein the arm member further comprises a sleeve inserted onto the pole member, the sleeve slidably and rotatably connected to the pole member, the arm member attached to the sleeve and extending away from the sleeve in an approximately horizontal direction.

8. A system to launch and recover an Unmanned Aerial Vehicle (UAV) aircraft in accordance with claim 7 further comprising a track formed on the pole member, the sleeve positioned in the track, the track guiding movement of the arm member coupled to sleeve.

9. A system to launch and recover an Unmanned Aerial Vehicle (UAV) aircraft in accordance with claim 1 wherein the pole member is located approximately on a centerline of the ship.

10. A method for launching an Unmanned Aerial Vehicle (UAV) aircraft comprising:

attaching the UAV aircraft to an approximately horizontal arm member, the approximately horizontal arm moveably coupled to an approximately vertical pole member;

moving the horizontal arm vertically in a spiral direction up the approximately vertical pole member; and

releasing the UAV aircraft from the approximately horizontal arm member when the UAV aircraft reaches launch airspeed.

11. The method of claim 10 wherein moving the horizontal arm in a spiral direction further comprising activating a propulsion system of the UAV aircraft to move the horizontal arm in the spiral direction on the approximately vertical pole member.

12. The method of claim 10 further comprising adjusting flight control surfaces of the UAV aircraft to minimize stress on a surface of the UAV aircraft attached to the approximately horizontal arm member.

13. The method of claim 10 further comprising adjusting an angle of attack of the UAV aircraft to sustain the launch airspeed at release from the arm member.

14. The method of claim 10 wherein attaching the UAV aircraft to an approximately horizontal arm member further comprising positioning the UAV aircraft to a location approximately 90 degrees to a centerline of a main deck and is approximately perpendicular to the arm member during a ship launch of the UAV aircraft.

15. A method of recovering an Unmanned Aerial Vehicle (UAV) aircraft comprising:

rotating an arm member on an approximately vertical pole member to a positioned approximately 90 degrees from a centerline of a deck, and at a top section of the approximately vertical pole member;

capturing the UAV aircraft at a distal end of the arm member; and

descending the arm member in a circular spiral down the vertical pole to reduce airspeed of the UAV aircraft.

16. The method of claim 15 further comprising extending a capture assembly on the UAV aircraft on a pivot boom to increase capture area of the UAV aircraft.

17. The method of claim 16 further comprising activating a visual sensor on the UAV aircraft to monitor and update relative position of the capture assembly to the attachment arm member.

18. The method of claim 15 further comprising reducing airspeed of the UAV aircraft prior to capturing the UAV aircraft at a distal end of the arm member.

19. The method of claim 18 further comprising controlling the UAV aircraft to fly a sharp flare pull-up while commanding idle thrust prior to capturing the UAV aircraft at a distal end of the arm member to reduce airspeed.

20. The method of claim 15 further comprising controlling an approach flight path of the UAV to synchronize with a motion of a capture device located on the arm member.