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

Patent metadata

Field	Value
Publication number	US-10457389-B2
Application number	US-201715433697-A
Country	US
Kind code	B2
Filing date	Feb 15, 2017
Priority date	Apr 2, 2013
Publication date	Oct 29, 2019
Grant date	Oct 29, 2019

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;
an arm attachable to the hub, the arm including a rotor and a rotor motor drivingly engaged to the rotor, the rotor motor defining multiple cooling channels; and
a cooling fan attachable to the rotor motor, the cooling fan defining multiple radially oriented cooling channels,
wherein the cooling fan is positionable relative to the rotor motor so that the cooling channels of the cooling fan at least partially align with the cooling channels of the rotor motor.

2. The multicopter of claim 1 , wherein the cooling fan includes a body having inner and outer cylindrical side walls through which the multiple cooling channels of the cooling fan are defined.

3. The multicopter of claim 2 , wherein the rotor motor is partially positionable within a cavity defined by the inner side wall.

4. The multicopter of claim 3 , wherein the cooling fan includes an annular motor mounting shelf that extends radially inward from the inner side wall of the body of the cooling fan.

5. The multicopter of claim 4 , wherein the rotor motor is supportable by the motor mounting shelf.

6. The multicopter of claim 3 , wherein the rotor motor defines multiple radially oriented cooling channels.

7. The multicopter of claim 1 , which includes a collar configured to attach the cooling fan to the rotor motor.

8. The multicopter of claim 7 , wherein the cooling fan includes a collar connection lip extending upwardly from the body and radially outward.

9. The multicopter of claim 8 , wherein the collar defines a circumferentially extending lip retaining chamber sized to receive the collar connection lip of the cooling fan to attach the cooling fan to the rotor motor.

10. The multicopter of claim 9 , wherein the collar includes an inner cylindrical surface that defines multiple grooves sized to mate with corresponding grooves defined on an exterior surface of the rotor motor.

11. The multicopter of claim 1 , wherein the cooling fan is removably attached to the rotor motor.

12. A rotor motor cooling fan for a multicopter, the rotor motor cooling fan comprising:
a body having inner and outer cylindrical side walls through which multiple cooling channels are defined; and
an annular motor mounting shelf that extends radially inward from the inner side wall of the body,
wherein the inner side wall and the annular motor mounting shelf define a cavity sized to receive part of a motor.

13. A rotor motor assembly for a multicopter, the rotor motor assembly comprising:
a cooling fan including a body having inner and outer cylindrical side walls through which multiple cooling channels are defined and an annular motor mounting shelf that extends radially inward from the inner side wall of the body; and
a rotor motor attached to the cooling fan, partially positioned within a cavity defined by the inner side wall, and supported by the motor mounting shelf.

14. The rotor motor assembly of claim 13 , wherein the rotor motor includes multiple cooling channels and the rotor motor and the cooling fan are positioned relative to one another so the cooling channels of the rotor motor at least partially align with corresponding cooling channels of the cooling fan.

15. The rotor motor assembly of claim 13 , which includes a collar configured to attach the cooling fan to the rotor motor.

16. The rotor motor assembly of claim 15 , wherein the cooling fan includes a collar connection lip extending upwardly from the body and radially outward.

17. The rotor motor assembly of claim 16 , wherein the collar defines a circumferentially extending lip retaining chamber sized to receive the collar connection lip of the cooling fan to attach the cooling fan to the rotor motor.

18. The rotor motor assembly of claim 13 , wherein the cooling fan includes a collar connection lip extending upwardly from the body and radially outward, and which includes a collar configured to secure the cooling fan to the rotor motor, the collar including an inner cylindrical surface that defines multiple grooves sized to mate with corresponding grooves defined on an exterior surface of the rotor motor, the collar defining a circumferentially extending lip retaining chamber sized to receive the collar connection lip of the cooling fan to attach the cooling fan to the rotor motor.

Assignees

• Hood Tech Corp

Inventors

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

Classifications

• 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

• B64U50/19

  using electrically powered motors · CPC title

• B64D3/00

  Aircraft adaptations to facilitate towing or being towed · CPC title