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

Patent metadata

Field	Value
Publication number	US-11299264-B2
Application number	US-202016906339-A
Country	US
Kind code	B2
Filing date	Jun 19, 2020
Priority date	Apr 2, 2013
Publication date	Apr 12, 2022
Grant date	Apr 12, 2022

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;
a fixed-wing aircraft engager extending from the hub;
multiple arms attachable to the hub, each arm including a rotor and a rotor motor drivingly engaged to the rotor; and
one or more vertical stabilizers configured to orient the multicopter into airflow about the yaw axis.

2. The multicopter of claim 1 , wherein the one or more vertical stabilizers include a fin.

3. The multicopter of claim 1 , wherein the one or more vertical stabilizers include a plurality of spaced apart fins.

4. The multicopter of claim 1 , wherein the one or more vertical stabilizers also function as rear landing gear of the multicopter.

5. The multicopter of claim 1 , wherein the fixed-wing aircraft engager is configured to releasably engage a fixed-wing aircraft.

6. The multicopter of claim 1 , wherein the fixed-wing aircraft engager is configured to releasably engage a fixed-wing aircraft, wherein the one or more vertical stabilizers are configured to provide yaw stability to the multicopter during forward movement at a predetermined altitude, and wherein the fixed-wing aircraft engager is configured to release the fixed-wing aircraft into free wingborne flight with a fuselage of the fixed-wing aircraft aligned with airflow in the direction of forward movement of the multicopter.

7. The multicopter of claim 6 , wherein the one or more vertical stabilizers are fin-shaped rear landing gear of the multicopter.

8. A method of launching a fixed-wing aircraft comprising:
releasably engaging a fixed-wing aircraft to a fixed-wing aircraft engager of a multicopter;
ascending the combined multicopter and fixed-wing aircraft to a predetermined height;
achieving, by the combined multicopter and fixed-wing aircraft, forward airspeed with yaw stability provided by one or more vertical stabilizers of the multicopter; and
releasing the fixed-wing aircraft into free wingborne flight, wherein the fixed-wing aircraft is aligned with airflow around the combined multicopter and fixed-wing aircraft.

9. The method of claim 8 , wherein the one or more vertical stabilizers include a fin, and which includes achieving the forward airspeed with yaw stability provided by the fin.

10. The method of claim 8 , wherein the one or more vertical stabilizers include a plurality of spaced apart fins, and which includes achieving the forward airspeed with yaw stability provided by the plurality of spaced apart fins.

11. The method of claim 8 , wherein the one or more vertical stabilizers function as rear landing gear of the multicopter, and which includes achieving the forward airspeed with yaw stability provided by the rear landing gear of the multicopter.

12. The method of claim 8 , wherein the one or more vertical stabilizers are fin-shaped rear landing gear of the multicopter, and which includes achieving the forward airspeed with yaw stability provided by the fin-shaped rear landing gear of the multicopter.

13. A multicopter comprising:
a hub;
a fixed-wing aircraft engager extending from the hub;
four arms attachable to the hub, each arm including a rotor and a rotor motor drivingly engaged to the rotor;
a first vertical stabilizer attached to a first arm of the four arms; and
a second vertical stabilizer attached to a second arm of the four arms,
wherein the first and second vertical stabilizers are configured to orient the multicopter into airflow about the yaw axis.

14. The multicopter of claim 13 , wherein:
a first end of the first arm is attached to the hub, and a second end of the first arm is attached to the first vertical stabilizer, and
a first end of the second arm is attached to the hub, and a second end of the second arm is attached to the second vertical stabilizer.

15. The multicopter of claim 13 , which includes
a first leg attached to a third arm of the four arms; and
a second leg attached to the fourth arm of the four arms.

16. The multicopter of claim 15 , wherein the first, second, third, and fourth arms are positioned relative to the hub such that during forward movement of the multicopter, the first and second vertical stabilizers are configured to orient the multicopter into airflow such that the first and second vertical stabilizers are at a rear of the multicopter, and the first and second legs are at a front of the multicopter.

Assignees

• Hood Tech Corp

Inventors

• Roeseler Corydon C
• Reiss Daniel Pepin

Classifications

• B64U80/82

  Airborne vehicles · CPC title

• B64U80/70

  in containers (B64U80/60 takes precedence) · 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