Multicopter-assisted system and method for launching and retrieving a fixed-wing aircraft

Patent metadata

Field	Value
Publication number	US-10836477-B2
Application number	US-201715432549-A
Country	US
Kind code	B2
Filing date	Feb 14, 2017
Priority date	Apr 2, 2013
Publication date	Nov 17, 2020
Grant date	Nov 17, 2020

Abstract

The present disclosure provides various embodiments of a multicopter-assisted launch and retrieval system generally including: (1) a multi-rotor modular multicopter attachable to (and detachable from) a fixed-wing aircraft to facilitate launch of the fixed-wing aircraft into wing-borne flight; (2) a storage and launch system usable to store the modular multicopter and to facilitate launch of the fixed-wing aircraft into wing-borne flight; and (3) an anchor system usable (along with the multicopter and a flexible capture member) to retrieve the fixed-wing aircraft from wing-borne flight.

First claim

The invention is claimed as follows:

1. A multicopter comprising:
a hub to which a fixed-wing aircraft is attachable, wherein the fixed-wing aircraft is attachable to an underside of the hub; and
first, second, third, and fourth arms each attachable to the hub and each including a rotor and a rotor motor drivingly engaged to the rotor;
wherein when the arms are attached to the hub, the arms are arranged so that when the fixed-wing aircraft is attached to the underside of the hub: (1) a nose of the fixed-wing aircraft is positioned between the first arm and the second arm; (2) a first connection between a fuselage of the fixed-wing aircraft and a first wing of the fixed-wing aircraft is positioned between the second arm and the third arm; (3) a tail of the fixed-wing aircraft is positioned between the third arm and the fourth arm; and (4) a second connection between the fuselage of the fixed-wing aircraft and a second wing of the fixed-wing aircraft is positioned between the fourth arm and the first arm.

2. The multicopter of claim 1 , wherein longitudinal axes of the first, second, third, and fourth arms are generally coplanar when the arms are attached to the hub.

3. The multicopter of claim 1 , wherein when the arms are attached to the hub, the first arm and the third arm are each generally transverse to both the second and fourth arms.

4. The multicopter of claim 3 , wherein the rotors are positioned such that, when the fixed-wing aircraft is attached to the hub, the rotors do not contact the fixed-wing aircraft.

5. The multicopter of claim 1 , which includes multiple landing gear attachable to the arms and positioned so when the fixed-wing aircraft is attached to the hub and the landing gear are attached to the arms, the landing gear do not contact the fixed-wing aircraft.

6. The multicopter of claim 5 , wherein when the arms are attached to the hub, the first arm and the third arm are each generally perpendicular to both the second and fourth arms.

7. The multicopter of claim 6 , wherein longitudinal axes of the first, second, third, and fourth arms are generally coplanar when the arms are attached to the hub.

8. The multicopter of claim 5 , wherein the rotors are positioned such that, when the fixed-wing aircraft is attached to the hub, the rotors do not contact the fixed-wing aircraft.

9. The multicopter of claim 1 , wherein the rotors are positioned such that, when the fixed-wing aircraft is attached to the hub, the rotors do not contact the fixed-wing aircraft.

10. A multicopter comprising:
a hub to which a fixed-wing aircraft is attachable, wherein the fixed-wing aircraft is attachable to an underside of the hub; and
four circumferentially spaced arms extending radially outward from the hub, each arm including a rotor and a rotor motor drivingly engaged to the rotor,
wherein the arms are arranged so when the fixed-wing aircraft is attached to the underside of the hub: (1) a nose of the fixed-wing aircraft is positioned between a first arm and a second arm; (2) a first connection between a fuselage of the fixed-wing aircraft and a first wing of the fixed-wing aircraft is positioned between the second arm and a third arm; (3) a tail of the fixed-wing aircraft is positioned between the third arm and a fourth arm; and (4) a second connection between the fuselage of the fixed-wing aircraft and a second wing of the fixed-wing aircraft is positioned between the fourth arm and the first arm.

11. The multicopter of claim 10 , wherein longitudinal axes of the arms are generally coplanar.

12. The multicopter of claim 11 , wherein the first arm and the third arm are each generally perpendicular to both the second and fourth arms.

13. The multicopter of claim 12 , wherein the rotors are positioned such that, when the fixed-wing aircraft is attached to the hub, the rotors do not contact the fixed-wing aircraft.

14. The multicopter of claim 11 , which includes multiple landing gear attached to the arms and positioned so when the fixed-wing aircraft is attached to the hub, the landing gear do not contact the fixed-wing aircraft.

15. The multicopter of claim 14 , wherein the first arm and the third arm are each transverse to both the second and fourth arms.

16. The multicopter of claim 11 , wherein longitudinal axes of the arms are generally coplanar, which includes multiple landing gear attached to the arms, wherein the first arm and the third arm are each transverse to both the second and fourth arms, and wherein the arms and the rotors are positioned so when the fixed-wing aircraft is attached to the hub, neither the landing gear nor the rotors contact the fixed-wing aircraft.

17. The multicopter of claim 11 , wherein the rotors are positioned such that, when the fixed-wing aircraft is attached to the hub, the rotors do not contact the fixed-wing aircraft.

18. The multicopter of claim 1 , wherein the hub to which the fixed-wing aircraft is attachable is configured to release an attached fixed-wing aircraft vertically from the hub into free flight.

19. The multicopter of claim 10 , wherein the hub to which the fixed-wing aircraft is attachable is configured to release an attached fixed-wing aircraft vertically from the hub into free flight.

20. A multicopter comprising:
a hub to which a fixed-wing aircraft is attachable;
first, second, third, and fourth arms each attachable to the hub and each including a rotor and a rotor motor drivingly engaged to the rotor, wherein each arm includes a first end attachable to the hub, and a second end opposite the first end and that extends radially beyond an outer radius of the corresponding rotor; and
first, second, third, and fourth landing gear attachable at the respective second ends of the first, second, third, and fourth arms opposite the hub,
wherein when the arms are attached to the hub, the arms are arranged so that when the fixed-wing aircraft is attached to the hub: (1) a nose of the fixed-wing aircraft is positioned between the first arm and the second arm; (2) a first wing of the fixed-wing aircraft is positioned between the second arm and the third arm; (3) a tail of the fixed-wing aircraft is positioned between the third arm and the fourth arm; and (4) a second wing of the fixed-wing aircraft is positioned between the fourth arm and the first arm.

21. A multicopter comprising:
a hub to which a fixed-wing aircraft is attachable;
four circumferentially spaced arms extending radially outward from the hub, each arm including a rotor and a rotor motor drivingly engaged to the rotor; and
four landing gear, wherein each landing gear has a first end and a second end opposite the first end, and is attached to one of the circumferentially spaced arms at an end opposite the hub, wherein both the first end and the second end of the landing gear is positioned radially outward from an outer radius of the rotor of the corresponding circumferentially spaced arm, and
wherein the arms are arranged so when the fixed-wing aircraft is attached to the hub: (1) a nose of the fixed-wing aircraft is positioned between a first arm and a second arm; (2) a first wing of the fixed-wing aircraft is positioned between the second arm and a third arm; (3) a tail of the fixed-wing aircraft is positioned between the third arm and a fourth arm; and (4) a second wing of the fixed-wing aircraft is positioned between the fourth arm and the first arm.

Assignees

• Hood Tech Corp

Inventors

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

Classifications

• B64U50/19

  using electrically powered motors · CPC title

• B64U2201/20

  Remote controls · CPC title

• B64U80/70

  in containers (B64U80/60 takes precedence) · CPC title

• B64U70/30

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

• B64C27/48 Primary

  Root attachment to rotor head · CPC title