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

Patent metadata

Field	Value
Publication number	US-10730615-B2
Application number	US-201715434745-A
Country	US
Kind code	B2
Filing date	Feb 16, 2017
Priority date	Apr 2, 2013
Publication date	Aug 4, 2020
Grant date	Aug 4, 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;
multiple arms attachable to the hub, each arm including a rotor and a rotor motor drivingly engaged to the rotor;
a first landing gear attachable to a first arm; and
a second landing gear attachable to a second arm, the second landing gear being shaped differently than the first landing gear.

2. The multicopter of claim 1 , wherein the second landing gear has a length, a maximum width, and a height, the length being greater than the maximum width and the height being greater than the length.

3. The multicopter of claim 2 , wherein the hub includes a component to which a fixed-wing aircraft is attachable.

4. The multicopter of claim 3 , wherein the second landing gear is oriented so when the fixed-wing aircraft is attached to the component, a plane that extends through the length of the body of the second landing gear is generally parallel to a roll axis of the fixed-wing aircraft.

5. The multicopter of claim 2 , wherein part of the second landing gear tapers from the maximum width to a minimum width from back to front.

6. The multicopter of claim 1 , wherein the second landing gear includes more surface area than the first landing gear.

7. The multicopter of claim 6 , wherein the first landing gear is a front landing gear and the second landing gear is a rear landing gear.

8. The multicopter of claim 1 , which includes a first landing gear extension attachable to the first arm and a second landing gear extension attachable to the second arm.

9. The multicopter of claim 8 , wherein the first landing gear is slidably receivable by or configured to slidably receive the first landing gear extension and the first landing gear extension is slidably receivable by or configured to slidably receive the first arm, and wherein the second landing gear is slidably receivable by or configured to slidably receive the second landing gear extension and the second landing gear extension is slidably receivable by or configured to slidably receive the second arm.

10. A multicopter comprising:
a hub;
first and second front arms attachable to the hub, each front arm including a rotor and a rotor motor drivingly engaged to the rotor;
first and second rear arms attachable to the hub, each rear arm including a rotor and a rotor motor drivingly engaged to the rotor;
first and second front landing gear respectively attachable to the first and second front arms; and
first and second rear landing gear respectively attachable to the first and second rear arms, the first and second rear landing gear being shaped differently than the first and second front landing gear.

11. The multicopter of claim 10 , wherein the first and second rear landing gear each have a length, a maximum width, and a height, the length being greater than the maximum width and the height being greater than the length.

12. The multicopter of claim 11 , wherein the hub includes a component to which a fixed-wing aircraft is attachable.

13. The multicopter of claim 12 , wherein the first and second rear landing gear are oriented so when the fixed-wing aircraft is attached to the hub, planes that extend through the lengths of the bodies of the first and second rear landing gear are generally parallel to a roll axis of the fixed-wing aircraft.

14. The multicopter of claim 11 , wherein the first and second rear landing gear generally taper from the maximum width to a minimum width from back to front.

15. The multicopter of claim 10 , wherein the first rear landing gear includes more surface area than the first front landing gear and the second rear landing gear includes more surface area than the second front landing gear.

16. The multicopter of claim 10 , which includes first and second front landing gear extensions respectively attachable to the first and second front arms and first and second rear landing gear extensions respectively attachable to the first and second rear arms.

17. The multicopter of claim 16 , wherein the first front landing gear is slidably receivable by or configured to slidably receive the first front landing gear extension and the first front landing gear extension is slidably receivable by or configured to slidably receive the first front arm, wherein the second front landing gear is slidably receivable by or configured to slidably receive the second front landing gear extension and the second front landing gear extension is slidably receivable by or configured to slidably receive the second front arm, wherein the first rear landing gear is slidably receivable by or configured to slidably receive the first rear landing gear extension and the first rear landing gear extension is slidably receivable by or configured to slidably receive the first rear arm, and wherein the second rear landing gear is slidably receivable by or configured to slidably receive the second rear landing gear extension and the second rear landing gear extension is slidably receivable by or configured to slidably receive the second rear arm.

Assignees

• Hood Tech Corp

Inventors

• Roeseler Corydon C
• Reiss Daniel Pepin

Classifications

• B64U80/70

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

• B64U80/82

  Airborne vehicles · CPC title

• B64C27/32 Primary

  Rotors · CPC title

• B64F1/029 Primary

  using a cable or tether · CPC title

• B64U60/50

  with landing legs · CPC title