UAV take-off method and apparatus

Patent metadata

Field	Value
Publication number	US-9708077-B2
Application number	US-201514610847-A
Country	US
Kind code	B2
Filing date	Jan 30, 2015
Priority date	Jan 30, 2014
Publication date	Jul 18, 2017
Grant date	Jul 18, 2017

Abstract

A method and apparatus for launching unmanned air vehicles (UAVs) includes supporting the unmanned air vehicle on a surface vehicle, such as a dolly cart, for riding along a surface such as ground or water. A towline is connected to the surface vehicle and the towline is pulled to force the unmanned air vehicle in a forward direction at a speed sufficient for take-off. The towline may be pulled by a winch system. In some embodiments the UAV is positioned with a nose down angle on the surface vehicle. The nose down angle permits overspeed of the UAV and cart as it is pulled along the ground, as well as controlled take-off.

First claim

What is claimed is:

1. A method of launching an unmanned air vehicle, comprising:
supporting the unmanned air vehicle on a surface vehicle, the surface vehicle adapted to travel on a ground surface, the surface vehicle supporting the unmanned air vehicle in a nose down position wherein a nose of the unmanned air vehicle is oriented downwardly with respect to the ground surface;
connecting a towline to the surface vehicle;
pulling the towline to force the unmanned air vehicle in a forward direction at a speed sufficient for take-off, wherein the nose down position of the unmanned air vehicle has sufficient incline to produce a negative angle of attack to provide a negative lift at lift surfaces of the unmanned air vehicle as the unmanned air vehicle moves in the forward direction, and wherein the surface vehicle is configured to prevent rearward movement of the unmanned air vehicle relative to the surface vehicle while permitting the unmanned air vehicle to move relative to the surface vehicle in at least one non-rearward direction; and
after the unmanned air vehicle has reached the speed sufficient for take-off, adjusting lift surfaces of the unmanned air vehicle to counteract the negative lift and launch the unmanned air vehicle from the surface vehicle.

2. The method of claim 1 , in which at least a part of the towline is resilient to reduce an impact of initial towline tension.

3. The method of claim 1 , in which the surface vehicle comprises a dolly cart having surface-engaging members.

4. The method of claim 1 , in which the unmanned air vehicle is retained on the surface vehicle during initial towline tension impact by retainers on the surface vehicle arranged to contact trailing edges of the wings of the unmanned air vehicle and prevent rearward movement of the unmanned air vehicle relative to the surface vehicle.

5. The method of claim 1 , in which the unmanned air vehicle is supported on the surface vehicle by wings of the unmanned air vehicle resting on side walls of the surface vehicle.

6. The method of claim 1 , in which supporting the unmanned air vehicle comprises supporting a fuselage of the unmanned air vehicle between two sidewalls of the surface vehicle.

7. The method of claim 6 , in which the sidewalls comprise vertical slides and the unmanned air vehicle comprises a pair of laterally opposed guides at sides of the fuselage, the slides obstructing rearward motion of the guides relative to the surface vehicle.

8. The method of claim 1 , in which pulling the towline comprises driving a winch to pull the towline.

9. The method of claim 1 , further comprising operating a propulsion apparatus of the unmanned air vehicle after take-off from the surface vehicle.

10. The method of claim 1 , wherein at least a pair of retainers are provided on the surface vehicle, each retainer being positioned rearwardly of an associated contact point on the unmanned air vehicle and configured to prevent rearward movement of the unmanned air vehicle relative to the surface vehicle while permitting the unmanned air vehicle to move relative to the surface vehicle in the at least one non-rearward direction.

11. The method of claim 10 , in which each of the retainers comprises a wing retainer projecting upwardly from an associated side wall of the surface vehicle and configured to engage a rear surface of an associated lift surface.

12. The method of claim 10 , in which each of the retainers comprises a slide coupled to an associated sidewall of the surface vehicle, wherein the unmanned air vehicle includes a pair of guides projecting from a fuselage of the unmanned air vehicle, each guide being sized to engage an associated slide.

13. The method of claim 12 , in which each slide is oriented substantially vertically to permit vertical movement of the unmanned air vehicle relative to the surface vehicle.

14. Apparatus for launching an unmanned air vehicle, comprising:
a towline;
a surface vehicle including surface riding units for traveling over a ground surface, the surface vehicle configured to releasably support the unmanned air vehicle in a nose down position wherein a nose of the unmanned air vehicle is oriented downwardly with respect to the ground surface, the surface vehicle having a coupling for connecting the towline to the surface vehicle;
a drive for pulling the towline, thereby to advance the surface vehicle in a forward direction;
wherein the unmanned air vehicle in the nose down position has an incline sufficient to produce a negative angle of attack to provide a negative lift at lift surfaces of the unmanned air vehicle as the unmanned air vehicle moves in the forward direction at a speed sufficient for take-off; and
wherein at least a pair of retainers are provided on the surface vehicle, each retainer being positioned rearwardly of an associated contact point on the unmanned air vehicle and configured to prevent rearward movement of the unmanned air vehicle relative to the surface vehicle while permitting the unmanned air vehicle to move relative to the surface vehicle in at least one non-rearward direction.

15. The apparatus of claim 14 , in which the surface vehicle further comprises supports arranged to support the unmanned air vehicle in the nose down position as the surface vehicle travels on the ground surface.

16. The apparatus of claim 14 , in which the surface vehicle comprises a dolly cart.

17. The apparatus of claim 14 , in which the drive comprises a winch.

18. The apparatus of claim 14 , in which each of the retainers comprises a wing retainer projecting upwardly from an associated side wall of the surface vehicle and configured to engage a rear surface of an associated lift surface.

19. The apparatus of claim 14 , in which each of the retainers comprises a slide coupled to an associated sidewall of the surface vehicle, wherein the unmanned air vehicle includes a pair of guides projecting from a fuselage of the unmanned air vehicle, each guide being sized to engage an associated slide.

20. The apparatus of claim 19 , in which each slide is oriented substantially vertically to permit vertical movement of the unmanned air vehicle relative to the surface vehicle.

Assignees

• Boeing Co

Inventors

• Criado Alfredo
• Kawiecki Grzegorz M
• Lemus Martin Jose L
• Ferreyra Eduardo G
• Pereira Mayan Sergio

Classifications

• B64C39/024

  of the remote controlled vehicle type, i.e. RPV · CPC title

• B64F1/08 Primary

  using winches · CPC title

• B64F1/10

  using self-propelled vehicles · CPC title

• B64C2201/08

  Operations & Transport · mapped topic

• B64U70/70

  Launching or landing using catapults, tracks or rails (launching from storage containers B64U70/50) · CPC title