Launch and recovery system for unmanned aerial vehicles

• US 8,167,242 B2
• Filed: 09/29/2010
• Issued: 05/01/2012
• 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.
• Primary Examiner(s): Michener, Joshua J
• Application Number:
  US12/893,407
• Publication Number:
  US 20110011974A1
• Time in Patent Office: 580 Days
• Field of Search: 244/110.R, 244/110.C, 244/110.F, 244/110.G
• US Class Current: 244/110.G
• 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. An aircraft and an aircraft recovery system designed to recover said aircraft, said aircraft recovery system having an arrestment line and an arrestment line support, said aircraft including a line capturing and retaining device located off centerline of said aircraft, said line capturing and retaining device having a passageway with an open entrance and a closed end, said passageway having at least two obstructions the line passes during recovery, each of said obstructions increasing the force required to move the line back past the obstruction toward the open entrance of said passageway relative to the force required to move the line initially past the obstruction toward the closed end of the passageway, a first of said at least two obstructions being closer to the open entrance than a second of said at least two obstructions.

2. The combination of claim 1 wherein the first obstruction comprises a spring-loaded latch.

3. The combination of claim 1 wherein the aircraft is an unmanned aerial vehicle.

4. The combination of claim 1 wherein the aircraft comprises at least one wing, the capturing and retaining device being mounted on said wing.

5. The combination of claim 4 wherein a leading edge of said wing is swept at least fifteen degrees at an inboard point on said wing.

6. The combination of claim 5 wherein the arrestment line is positioned to contact a leading edge of the wing and to slide along the leading edge of the wing to the capturing and retaining device.

7. The combination of claim 6 wherein the arrestment line is positioned to contact the leading edge of the wing in an orientation generally perpendicular to the leading edge of the wing.

8. The combination of claim 6 wherein the open entrance of the capturing and retaining device forms a smooth continuation of a leading edge of said wing.

9. An aircraft designed to be recovered by an aircraft recovery system having an arrestment line and an arrestment line support, said aircraft including a line capturing and retaining hook mounted to a wing of the aircraft and located off centerline of said aircraft, said hook having an open entrance forming a smooth continuation of a leading edge of said wing, a closed end outboard of the open entrance, and, between the open entrance and closed end, an inner throat, an outer throat, and a first obstruction which requires less force for the line to enter the outer throat than to exit the outer throat through the open entrance and a second obstruction between said inner throat and outer throat which requires less force during the arrestment for the line to pass from the outer throat to the inner throat than from the inner throat to the outer throat.

10. The aircraft of claim 9 wherein the first obstruction comprises a spring-loaded latch.

11. The aircraft of claim 9 wherein the aircraft is an unmanned aerial vehicle.

12. The aircraft of claim 9 wherein said leading edge of said wing is swept at least fifteen degrees at an inboard point on said wing.

13. The aircraft of claim 9 wherein the inner throat is smaller than the diameter of the line.

14. A method of capturing an aircraft with an aircraft recovery system, said aircraft recovery system having an arrestment line and an arrestment line support, said aircraft comprising at least one wing, and a capturing and retaining device mounted on said wing off centerline of the aircraft, the method comprising flying said aircraft into said arrestment line to cause the arrestment line to slide along a leading edge of said wing into an open entrance of a passageway in said capturing and retaining device, said passageway having a closed end, said passageway having at least two obstructions the line passes during recovery, each of said at least two obstructions increasing the force required to move the line back past the obstruction toward the open entrance of said passageway relative to the force required to move the line initially past the obstruction toward the closed end of the passage way, a first of said at least two obstructions being closer to the open entrance than a second of said at least two obstructions.

15. The method of claim 14 wherein the first obstruction comprises a spring-loaded latch.

16. The method of claim 14 wherein the aircraft is an unmanned aerial vehicle.

17. The method of claim 14 wherein a leading edge of said wing is swept at least fifteen degrees at an inboard point on said wing.

18. The method of claim 14 wherein a portion of the passageway between the second obstruction and the closed end is smaller than the diameter of the line.

19. A method of capturing an aircraft with an aircraft recovery system, said aircraft recovery system having an arrestment line and an arrestment line support, said aircraft comprising at least one wing, and a capturing and retaining device mounted on said wing and located off centerline of said aircraft, the method comprising flying said aircraft into said arrestment line to cause the arrestment line to slide along a leading edge of said wing into an open entrance of said capturing and retaining device, the open entrance forming a smooth continuation of the leading edge, past a first obstruction in the capturing and retaining device into an outer throat of the capturing and retaining device, the first obstruction requiring less force during arrestment for the line to enter the outer throat than to exit the outer throat through the open entrance, and past a second obstruction into an inner throat of the capturing and retaining device, the second obstruction requiring less force during arrestment for the line to pass from the outer throat to the inner throat than from the inner throat to the outer throat, the inner throat having a closed end outboard of the open entrance, the line being retained in the inner throat.