Rotorcraft-assisted system and method for launching and retrieving a fixed-wing aircraft into and from free flight

Patent metadata

Field	Value
Publication number	US-12384559-B2
Application number	US-202318170145-A
Country	US
Kind code	B2
Filing date	Feb 16, 2023
Priority date	Aug 17, 2016
Publication date	Aug 12, 2025
Grant date	Aug 12, 2025

Abstract

Various embodiments of the present disclosure provide a rotorcraft-assisted system and method for launching and retrieving a fixed-wing aircraft into and from free flight. The launch and retrieval system includes a modular multicopter, a storage and launch system, an anchor system, a flexible capture member, and an aircraft-landing structure. The multicopter is attachable to the fixed-wing aircraft to facilitate launching the fixed-wing aircraft into free, wing-borne flight. The storage and launch system is usable to store the multicopter (when disassembled) and to act as a launch mount for the fixed-wing aircraft by retaining the fixed-wing aircraft in a desired launch orientation. The anchor system is usable with the multicopter, the flexible capture member, and the aircraft-landing structure to retrieve the fixed-wing aircraft from free, wing-borne flight.

First claim

What is claimed is:

1. A method of retrieving a fixed-wing aircraft, said method comprising:
hoisting a flexible capture member having a first end coupled to a lifting device to a pre-determined altitude, wherein the flexible capture member is guided through an upper guiding component of an upwardly extending structure, wherein the lifting device is separate from the upper guiding component of the upwardly extending structure;
controlling the fixed-wing aircraft to intercept and engage a portion of the flexible capture member; and
lowering the flexible capture member with the fixed wing aircraft engaged to the portion of the flexible capture member such that the fixed-wing aircraft can contact the upwardly extending structure that is separate from the lifting device.

2. The method of claim 1 , which includes causing a tensioning device coupled to a second end of the flexible capture member to apply tension to the hoisted flexible capture member.

3. The method of claim 2 , wherein the tensioning device is a downhaul winch.

4. The method of claim 2 , which includes regulating the tensioning device.

5. The method of claim 4 , which includes regulating the tensioning device to hold the fixed-wing aircraft against gravity when the fixed-wing aircraft contacts the upwardly extending structure.

6. The method of claim 1 , wherein the upper guiding component includes a masthead.

7. The method of claim 1 , wherein the upper guiding component includes a castellated masthead.

8. The method of claim 1 , which includes maintaining the upper guiding component in a vertical position prior to the fixed-wing aircraft engaging the portion of the flexible capture member.

9. The method of claim 1 , which includes, when the upper guiding component moves from a vertical position prior to the fixed-wing aircraft engaging the portion of the flexible capture member, urging the upper guiding component to return to the vertical position.

10. The method of claim 1 , which includes, when the upper guiding component moves from a vertical position after the fixed-wing aircraft engages the portion of the flexible capture member, urging the upper guiding component to return to the vertical position.

11. The method of claim 1 , wherein the upwardly extending structure includes a padding, and which includes causing part of the fixed-wing aircraft that contacts the upwardly extending structure to contact the padding.

12. The method of claim 1 , wherein the lifting device is a multi-copter.

13. A method of retrieving a fixed-wing aircraft, said method comprising:
hoisting a flexible capture member having a first end coupled to a multi-copter to a pre-determined altitude, wherein the flexible capture member is guided through a masthead of an upwardly extending structure, wherein the multi-copter is separate from the upwardly extending structure;
controlling the fixed-wing aircraft to intercept and engage a portion of the flexible capture member; and
lowering the flexible capture member with the fixed-wing aircraft engaged to the portion of the flexible capture member such that the fixed-wing aircraft contacts the upwardly extending structure.

14. The method of claim 13 , which includes causing a tensioning device coupled to a second end of the flexible capture member to apply tension to the hoisted flexible capture member.

15. The method of claim 14 , wherein the tensioning device is a downhaul winch.

16. The method of claim 13 , which includes, when the masthead moves from a vertical position prior to the fixed-wing aircraft engaging the portion of the flexible capture member, urging the masthead to return to the vertical position.

17. The method of claim 13 , which includes, when the masthead moves from a vertical position after the fixed-wing aircraft engages the portion of the flexible capture member, urging the masthead to return to the vertical position.

18. The method of claim 13 , wherein the upwardly extending structure includes a padding, and which includes causing part of the fixed-wing aircraft that contacts the upwardly extending structure to contact the padding.

19. The method of claim 13 , wherein the lifting device is a multi-copter.

20. The method of claim 13 , wherein the masthead is a castellated masthead.

Assignees

• Hood Tech Corp

Inventors

• Von Flotow Andreas H
• Roeseler Corydon C
• Reiss Daniel Pepin
• Massong Jessie

Classifications

• B64U2201/20

  Remote controls · CPC title

• B64U20/94

  of rotors or rotor motors · CPC title

• B64U30/291

  Detachable rotors or rotor supports · CPC title

• B64U70/00

  Launching, take-off or landing arrangements · CPC title

• B64U20/80

  Arrangement of on-board electronics, e.g. avionics systems or wiring · CPC title