Apparatus and method for launching a fixed-wing aircraft into free flight

Patent metadata

Field	Value
Publication number	US-11639236-B2
Application number	US-201916568978-A
Country	US
Kind code	B2
Filing date	Sep 12, 2019
Priority date	Sep 6, 2017
Publication date	May 2, 2023
Grant date	May 2, 2023

Abstract

Various embodiments of the present disclosure provide a parasail-assisted system for launching a fixed-wing aircraft into free flight and for retrieving a fixed-wing aircraft from free flight.

First claim

The invention claimed is:

1. A method of launching a fixed-wing aircraft into wing-borne flight, the method comprising:
releasably attaching an aircraft hoisting device to the fixed-wing aircraft, wherein the aircraft hoisting device is attached to the fixed-wing aircraft using (a) a front engager of the aircraft hoisting device movable between a front engaged position and a front disengaged position, and (b) a rear engager of the aircraft hoisting device movable between a rear engaged position and a rear disengaged position, and such that the front engager contacts a first leading edge of a first wing of the fixed-wing aircraft and a second leading edge of a second wing of the fixed-wing aircraft;
lifting the aircraft hoisting device to a desired altitude; and
causing the aircraft hoisting device to release the fixed-wing aircraft into free flight.

2. The method of claim 1 , wherein attaching the aircraft hoisting device to the fixed-wing aircraft includes causing the front engager to contact the first wing of the fixed-wing aircraft adjacent to a first connection between the first wing and a fuselage of the fixed-wing aircraft.

3. The method of claim 2 , wherein attaching the aircraft hoisting device to the fixed-wing aircraft includes causing the front engager to contact the second wing of the fixed-wing aircraft adjacent to a second connection between the second wing and the fuselage of the aircraft.

4. The method of claim 1 , wherein attaching the aircraft hoisting device to the fixed-wing aircraft includes causing the rear engager to contact a first trailing edge of the first wing of the fixed-wing aircraft.

5. The method of claim 4 , wherein attaching the aircraft hoisting device to the fixed-wing aircraft includes causing the rear engager to contact a second trailing edge of the second wing of the fixed-wing aircraft.

6. The method of claim 1 , wherein attaching the aircraft hoisting device to the fixed-wing aircraft includes causing the rear engager to contact the first wing of the fixed-wing aircraft adjacent to a first connection between the first wing and a fuselage of the fixed-wing aircraft.

7. The method of claim 6 , wherein attaching the aircraft hoisting device to the fixed-wing aircraft includes causing the rear engager to contact the second wing of the fixed-wing aircraft adjacent to a second connection between the second wing and the fuselage of the fixed-wing aircraft.

8. The method of claim 1 , wherein causing the aircraft hoisting device to release the fixed-wing aircraft into free flight includes moving the front engager from the front engaged position to the front disengaged position.

9. The method of claim 8 , wherein moving the front engager from the front engaged position to the front disengaged position causes the first leading edge of the first wing of the fixed-wing aircraft to be forced away from the aircraft hoisting device.

10. The method of claim 1 , wherein causing the aircraft hoisting device to release the fixed-wing aircraft into free flight includes moving the rear engager from the rear engaged position to the rear disengaged position.

11. The method of claim 10 , wherein moving the rear engager from the rear engaged position to the rear disengaged position causes a first trailing edge of the first wing of the fixed-wing aircraft to be forced away from the aircraft hoisting device.

12. The method of claim 1 , wherein the front engager and the rear engager are connected by a linking mechanism, and wherein causing the aircraft hoisting device to release the fixed-wing aircraft into free flight includes moving the front engager from the front engaged position to the front disengaged position such that the linking mechanism causes the rear engager to move from the rear engaged position to the rear disengaged position.

13. The method of claim 1 , wherein the front engager and the rear engager are connected by a linking mechanism, and wherein causing the aircraft hoisting device to release the fixed-wing aircraft into free flight includes moving the rear engager from the rear engaged position to the rear disengaged position such that the linking mechanism causes the front engager to move from the front engaged position to the front disengaged position.

14. The method of claim 1 , wherein the front engager is movable from the front engaged position to the front disengaged position by rotating, and wherein the rear engager is movable from the rear engaged position to the rear disengaged position by rotating.

15. A fixed-wing aircraft launching system comprising:
a lifting device; and
an aircraft hoisting device affixed to the lifting device, the aircraft hoisting device including:
a saddle base;
a front engager couplable with the fixed-wing aircraft and movable between a front engaged position and a front disengaged position;
a rear engager couplable with the fixed-wing aircraft and movable between a rear engaged position and a rear disengaged position; and
a linking mechanism connected to the front engager and the rear engager, wherein the linking mechanism is configured to cause the front engager and the rear engager to simultaneously move from an engaged position to a disengaged position.

16. The system of claim 15 , wherein when in the front engaged position, the front engager is configured to contact a first wing of the fixed-wing aircraft.

17. The system of claim 16 , wherein when in the rear engaged position, the rear engager is configured to contact the first wing of the fixed-wing aircraft.

18. The system of claim 15 , wherein the saddle base includes a first side bracket and a second side bracket.

19. The system of claim 18 , wherein the front engager is rotatably coupled to the first side bracket and is rotatably coupled to the second side bracket.

20. The system of claim 18 , wherein the rear engager is rotatably coupled to the first side bracket and is rotatably coupled to the second side bracket.

21. The system of claim 15 , which includes a servo motor coupled to the front engager to move the front engager from the front engaged position to the front disengaged position.

22. The system of claim 15 , wherein the front engager includes a first leading edge engager and a second leading edge engager.

23. The system of claim 22 , wherein the first leading edge engager includes a first triangular base rotatably attached to the saddle base, and wherein the second leading edge engager includes a second triangular base rotatably attached to the saddle base.

24. The system of claim 23 , wherein the first triangular base defines a first contoured leading edge engaging surface shaped to engage a first leading edge of a first wing of the fixed-wing aircraft, and wherein the second triangular base defines a second contoured leading edge engaging surface shaped to engage a second leading edge of a second wing of the fixed-wing aircraft.

25. The system of claim 24 , wherein the first leading edge engaging surface is shaped to engage the first leading edge of the first wing adjacent to a first connection between the first wing and a fuselage of the fixed-wing aircraft, and wherein the second leading edge engaging surface is shaped to engage the second leading edge of the second wing adjacent to a second connection between the second wing and a fuselage of the fixed-wing aircraft.

26. The system of claim 22 , further comprising a shaft coupling the first leading edge enga

Assignees

• Hood Tech Corp

Inventors

• Von Flotow Andreas H
• Roeseler Corydon C

Classifications

• B64F1/04 Primary

  for launching aircraft · CPC title

• B64U70/30 Primary

  for capturing UAVs in flight by ground or sea-based arresting gear, e.g. by a cable or a net · CPC title

• B64U60/50

  with landing legs · CPC title

• B64U70/83

  using parachutes, balloons or the like · CPC title

• B64U80/50

  the UAVs being disassembled · CPC title