Unmanned aerial vehicle(UAV) recovery system

• US 20120187243A1
• Filed: 01/26/2011
• Published: 07/26/2012
• Est. Priority Date: 01/26/2011
• Status: Active Grant

• Current Assignee: Infoscitex
• Original Assignee: Infoscitex
• Inventors: Goldie, James, Vitale, Nicholas, Downey, George A., Leary, Kevin, Hafer, William
• Granted Patent: US 8,464,981 B2
• Time in Patent Office: Days
• US Class Current: 244/110.C
• CPC Class Codes: B64C 39/024 of the remote controlled vehicle type, i.e. RPV
• CPC Class Codes: B64F 1/027 using net or mesh
• 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 70/60 Take-off or landing of UAVs from a runway using their own power

Abstract

A UAV recovery system including a recovery cart; a guide mechanism for defining the path of the cart; a base station for capturing a UAV tailhook; a momentum transfer system driven by the inertia of the UAV through the arresting member to move the recovery cart along the guide mechanism away from the base station in the same direction as the UAV; an acceleration control device for converging the speeds and positions of the UAV and cart for enabling engagement of the cart and UAV as their relative speeds approach zero; and a brake system for stopping the recovery cart when the cart and UAV are engaged. Also disclosed is a UAV having a tailhook pivotably mounted on the UAV at the center of gravity of the UAV.

Claims

1. A UAV recovery system comprising:

a recovery cart;

a guide mechanism for defining the path of the cart;

a base station including an arresting member for capturing a UAV tailhook;

a momentum transfer system driven by the inertia of the UAV through said arresting member to move the recovery cart along the guide mechanism away from said base station in the same direction as the UAV;

an acceleration control device for converging the speeds and positions of the UAV and cart for enabling engagement of the cart and UAV as their relative speed approaches zero; and

a brake system for stopping the recovery cart when the cart and UAV are engaged.

2. The UAV recovery system of claim 1 in which said recovery system is installed on a ship.

3. The UAV recovery system of claim 2 in which said recovery system is installed cross-wise, between the starboard and port sides of the ship.

4. The UAV recovery system of claim 1 in which said cart includes a compliant surface for engaging the UAV.

5. The UAV recovery system of claim 4 in which said compliant surface includes a net.

6. The UAV recovery system of claim 1 in which said cart includes a damper system for cushioning the engagement of the UAV with said cart.

7. The UAV recovery system of claim 6 in which said damper system includes a compressible medium.

8. The UAV recovery system of claim 7 in which said compressible medium is within a vented deflatable enclosure.

9. The UAV recovery system of claim 4 in which said cart includes a collapsible recovery frame for supporting said compliant surface.

10. The UAV recovery system of claim 1 in which said cart includes wing support rigging.

11. The UAV recovery system of claim 1 in which said cart includes a main frame with wheels.

12. The UAV recovery system of claim 1 in which said guide mechanism includes at least one guide link extending between said base station and a remote ground mount and at least one follower on said cart for guiding on said guide link.

13. The UAV recovery system of claim 12 in which said guide link includes a cable.

14. The UAV recovery system of claim 1 in which said momentum transfer system includes a drive link connected with said arresting member around at least one direction changing mechanism in said base station and at least one direction changing mechanism in said remote ground mount and connected to said cart for drawing said cart forward away from said base station by the inertia of and in the same direction as the UAV.

15. The UAV recovery system of claim 14 in which said drive link includes a cable and said direction changing mechanism includes pulleys.

16. The UAV recovery system of claim 1 in which said arresting member includes a loop of cable.

17. The UAV recovery system of claim 1 in which said acceleration control device includes an adjustable brake mechanism on said cart for engaging said drive link.

18. The UAV recovery system of claim 17 in which said adjustable brake mechanism includes a reel and a brake member and a brake pad for bearing against said brake member to control release of said drive link.

19. The UAV recovery system of claim 18 in which said drive link includes a cable and said reel includes a cable reel.

20. The UAV recovery system of claim 1 in which said brake system includes a brake link connected to said cart and a reel and a brake member and a brake pad for bearing against said brake member to control release of said brake link.

21. The UAV recovery system of claim 20 in which said brake link includes a cable and said reel includes a cable reel.

22. The UAV recovery system of claim 1 in which said recovery system is installed on an airplane.

23. A UAV system including a UAV and a UAV recovery system comprising:

a UAV having a tailhook pivotably mounted on said UAV at the center of gravity of said UAV;

a recovery cart;

a guide mechanism for defining the path of the cart;

a base station including an arresting member for capturing a UAV tailhook;

a momentum transfer system driven by the inertia of the UAV through said arresting member to move the recovery cart along the guide mechanism away from said base station in the same direction as the UAV;

an acceleration control device for converging the speeds and positions of the UAV and cart for enabling engagement of the cart and UAV as their relative speeds approach zero; and

a brake system for stopping the recovery cart when the cart and UAV are engaged.