Launch and recovery system for unmanned aerial vehicles

• US 8,517,306 B2
• Filed: 08/28/2006
• Issued: 08/27/2013
• Est. Priority Date: 07/23/1999
• Status: Expired due to Fees

• Current Assignee: Advanced Aerospace Technologies Incorporated
• Original Assignee: Advanced Aerospace Technologies Incorporated
• Inventors: McDonnell, William R., Baker, Charles H.
• Primary Examiner(s): Sanderson, Joseph W
• Application Number:
  US11/510,920
• Publication Number:
  US 20070108345A1
• Time in Patent Office: 2,556 Days
• Field of Search: 244/63, 244/110.R, 244/110.C, 244/110.F, 244/110.G
• US Class Current: 244/110.C
• CPC Class Codes: B64C 25/68 Arrester hooks
• CPC Class Codes: B64C 39/024 of the remote controlled vehicle type, i.e. RPV
• CPC Class Codes: B64D 3/00 Aircraft adaptations to facilitate towing or being towed B64D39/00 takes precedence
• CPC Class Codes: B64F 1/02 for arresting aircraft, e.g. nets or cables
• CPC Class Codes: B64F 1/04 for launching aircraft
• CPC Class Codes: B64F 1/10 using self-propelled vehicles
• CPC Class Codes: B64U 10/25 Fixed-wing aircraft VTOL aircraft B64U10/20
• CPC Class Codes: B64U 30/10 Wings
• CPC Class Codes: B64U 50/13 using external fans or propellers
• 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 method of launching and retrieving a UAV (Unmanned Aerial Vehicle) (10). The preferred method of launch involves carrying the UAV (10) up to altitude using a parasail (8) similar to that used to carry tourists aloft. The UAV is dropped and picks up enough airspeed in the dive to perform a pull-up into level controlled flight. The preferred method of recovery is for the UAV to fly into and latch onto the parasail tow line (4) or cables hanging off the tow line and then be winched back down to the boat (2).

Claims

1. In combination, an aircraft and a capturing apparatus adapted for capturing the aircraft,

the aircraft comprising

a) a hook attached to an outboard portion of a wing of said aircraft, said hook comprising an inboardly-extending forward part defining a forward side of an outboardly-extending passageway, the passageway having an inboardly-facing mouth, said hook being constructed and proportioned to intercept an arrestment line and reliably and releasably attach said aircraft to said arrestment line with a line retaining mechanism, and

b) lateral deflecting structure constructed and arranged to reliably deflect the arrestment line laterally into engagement and attachment with the hook, the lateral deflecting structure comprising a leading edge of the wing of said aircraft,

the capturing apparatus comprising

c) the arrestment line, and

d) a flexible support structure supported by a base, the flexible support structure being constructed to absorb energy by bending without breaking, the flexible support structure supporting the arrestment line across a flight path of the aircraft in a generally vertical orientation for capture of the hook, said support for said arrestment line being kept clear of the intended flight path of the aircraft,

the capturing apparatus being so constructed and proportioned that elastic deformation of components of the capturing apparatus absorbs most of the energy during arrestment of the forward velocity of the aircraft.

2. The combination of claim 1 wherein elastic deformation of components of the capturing apparatus comprises bending of the support and elastic deformation of the arrestment line.

3. The combination of claim 2 wherein elastic deformation of components of the capturing apparatus further comprises elastic deformation of other structures coupled to the arrestment line.

4. The combination of claim 3 wherein the other structures comprise at least one stretchable line coupled to the support structure and to the base, said stretchable line being designed to stretch to absorb aircraft arrestment energy.

5. The combination of claim 4 wherein the stretchable line angles horizontally and significantly up from a connection to the base toward a point on the arrestment line support structure.

6. The combination of claim 1 wherein the base is the ground.

7. The combination of claim 1 wherein a restraint is attached to a lower end of the arrestment line.

8. The combination of claim 7 wherein said restraint attached to a lower end of the arrestment line comprises a connection to the base.

9. The combination of claim 8 wherein the lower end of the arrestment line is connected to the base through the support structure.

10. The combination of claim 1 wherein a leading edge of said lateral deflecting structure is swept at least fifteen degrees at an inboard point on the wing.

11. The combination of claim 1 wherein said arrestment line is positioned such that during a successful arrestment it is possible for said arrestment line to contact one side of the aircraft, with said aircraft in a level attitude, without the other side of the aircraft contacting a second arrestment line.

12. The combination of claim 1 further comprising tension structures coupled to the arrestment line above and below an intended point of capture of said aircraft, the tension structures deforming elastically in response to deflection of the arrestment line.

13. The combination of claim 1 wherein the hook has an open entrance and a closed end, the line retaining mechanism comprising at least one obstruction that makes it easier for said line to move toward the closed end of the hook than to move back toward the open entrance.

14. The combination of claim 1 wherein the support structure extends down to said base on only one side of the intended flight path.

15. The combination of claim 1 wherein said capturing apparatus is designed to capture said aircraft from wingborne flight.

16. The combination of claim 1 wherein said hook and line retaining mechanism are the primary mechanisms that secure the aircraft to the capturing apparatus during the arrestment.

17. The combination of claim 1 wherein said flexible support structure includes a pole.

18. The combination of claim 1 wherein the arrestment line lacks discrete stops for preventing the aircraft from sliding down the arrestment line.

19. The combination of claim 1 wherein the passageway is closed at its outboard end, the open mouth of the passageway lying adjacent the leading edge of the wing, and the line retaining mechanism comprising at least one obstruction that makes it easier for said line to move toward the closed end of the hook than to move back toward the open entrance.

20. The combination of claim 1 wherein the forward part of the hook includes a portion that extends outboard relative to the aircraft then extends forward relative to the aircraft and then extends inboard relative to the aircraft to form the inboardly-facing mouth of said hook adjacent a leading edge of the wing, said hook being positioned such that a portion of the hook that extends inboard relative to the aircraft is in front of a line described by the leading edge of the wing just inboard of the mouth of the hook.

21. In combination, an aircraft and a capturing apparatus adapted for capturing the aircraft,

the aircraft comprising

a) a hook attached to an outboard portion of a wing of said aircraft, said hook comprising an inboardly-extending forward part defining a forward side of an outboardly-extending passageway, the passageway having an inboardly-facing mouth, said hook being constructed and proportioned to intercept an arrestment line and reliably and releasably attach said aircraft to said arrestment line with a line retaining mechanism, and

b) lateral deflecting structure constructed and arranged to reliably deflect the arrestment line laterally into engagement and attachment with the hook, the lateral deflecting structure comprising a leading edge of the wing of said aircraft,

the capturing apparatus comprising

c) the arrestment line, and

d) an arrestment line support structure supported by a base,

the arrestment line being designed to deflect when contacted by said aircraft, the arrestment line being suspended at its upper end by said support structure across a flight path of the aircraft in an orientation which is generally perpendicular to said leading edge of said wing at an intended point of interception of said aircraft, and being connected at its lower end to the base,

said support structure being kept clear of the intended flight path of the aircraft and extending down to said base on only one side of the intended flight path.

22. The combination of claim 21 wherein a leading edge of said lateral deflecting structure is swept at least fifteen degrees at an inboard point on the wing.

23. The combination of claim 21 wherein said arrestment line is positioned such that during a successful arrestment it is possible for said arrestment line to contact one side of the aircraft, with said aircraft in a level attitude, without the other side of the aircraft contacting a second arrestment line.

24. The combination of claim 21 wherein said arrestment line is connected to the base through said support structure.

25. The combination of claim 21 wherein said arrestment line is suspended in a generally vertical orientation.

26. The combination of claim 21 wherein said capturing apparatus is designed to capture said aircraft from wingborne flight.

27. The combination of claim 21 wherein said hook and line retaining mechanisms are the primary mechanisms that secure the aircraft to the capturing apparatus during the arrestment.

28. The combination of claim 21 wherein said arrestment line support structure includes a pole.

29. The combination of claim 21 wherein the arrestment line lacks discrete stops for preventing the aircraft from sliding down the arrestment line.

30. The combination of claim 21 wherein the capturing apparatus further comprises at least one stretchable line coupled to the support structure and to the base, said stretchable line being designed to stretch to absorb aircraft arrestment energy.

31. The combination of claim 21 wherein the passageway is closed at its outboard end, the open mouth of the passageway lying adjacent the leading edge of the wing, and the line retaining mechanism comprising at least one obstruction that makes it easier for said line to move toward the closed end of the hook than to move back toward the open entrance.