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

Patent metadata

Field	Value
Publication number	US-10501176-B2
Application number	US-201715432483-A
Country	US
Kind code	B2
Filing date	Feb 14, 2017
Priority date	Apr 2, 2013
Publication date	Dec 10, 2019
Grant date	Dec 10, 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:
multiple arms each having a longitudinal axis;
a hub base to which the arms are attachable, wherein a first plane passes through the hub base and includes the longitudinal axes of the arms when the arms are attached to the hub base; and
a saddle attached to the hub base, wherein a second plane passes through the saddle, wherein part of the saddle is (i) movable relative to the hub base to vary an angle formed between the second plane and the first plane, (ii) attachable to a fixed-wing aircraft, and (iii) movable to set a pitch angle of the fixed-wing aircraft.

2. The multicopter of claim 1 , wherein the saddle is below the hub base.

3. The multicopter of claim 1 , wherein the part of the saddle is movable relative to the hub base between a first position and a second position.

4. The multicopter of claim 3 , wherein the angle is about 0 degrees when the part of the saddle is in the first position such that the second plane and the first plane are generally parallel.

5. The multicopter of claim 3 , wherein the angle is about 10 degrees when the part of the saddle is in the second position such that the second plane intersects the first plane.

6. The multicopter of claim 1 , which includes at least one locking device having a locked configuration in which part of the locking device contacts the part of the saddle to prevent the part of the saddle from moving relative to the hub base.

7. A multicopter comprising:
a hub base;
multiple arms each having a longitudinal axis and each being removably attachable to the hub base, wherein a first plane passes through the hub base and generally includes the longitudinal axes of the arms when the arms are attached to the hub base; and
a saddle having:
a first portion attached to the hub base; and
a second portion pivotably attached to the first portion, wherein a second plane passes through the second portion of the saddle, the second portion being pivotable relative to the first portion between a first position and a second position to vary an angle formed between the second plane and the first plane,
wherein the second portion is also (i) attachable to a fixed-wing aircraft and (ii) movable to set a pitch angle of the fixed-wing aircraft.

8. The multicopter of claim 7 , wherein the angle is about 0 degrees when the second portion of the saddle is in the first position such that the second plane and the first plane are generally parallel.

9. The multicopter of claim 7 , wherein the angle is about 10 degrees when the second portion of the saddle is in the second position such that the second plane intersects the first plane.

10. The multicopter of claim 7 , which includes at least one locking device having a locked configuration in which part of the locking device contacts the second portion of the saddle to prevent the second portion of the saddle from moving relative to the hub base.

11. The multicopter of claim 10 , wherein the second portion of the saddle is pivotably attached to the first portion of the saddle near one end of the second portion and is also attached to the first portion near an opposing end of the second portion via the at least one locking device.

12. The multicopter of claim 11 , which includes a first locking device and a second locking device.

13. The multicopter of claim 12 , wherein the first portion of the saddle includes two generally parallel, spaced apart first and second sides that respectively define first and second adjustment slots.

14. The multicopter of claim 13 , wherein a portion of the first locking device extends through the first adjustment slot and a portion of the second locking device extends through the second adjustment slot.

15. A method for preparing a multicopter for flight, the method comprising:
attaching multiple arms to a hub base of the multicopter;
pivoting part of a saddle relative to the hub base to establish a desired angle between a plane passing through the hub base and a plane passing through the saddle, wherein the plane passing through the hub base generally includes longitudinal axes of the arms, and wherein the part of the saddle is (i) attachable to a fixed-wing aircraft and (i) movable to set a pitch angle of the fixed-wing aircraft; and
locking the part of the saddle relative to the hub base.

16. The method of claim 15 , which includes attaching the arms to the hub base after pivoting the part of the saddle relative to the hub base.

17. The method of claim 15 , which includes attaching the fixed-wing aircraft to the part of the saddle.

18. The method of claim 17 , wherein the pitch angle of the fixed-wing aircraft is generally equal to a desired angle between the plane passing through the hub base and the plane passing through the saddle.

19. The method of claim 17 , which includes attaching the fixed-wing aircraft to the part of the saddle before attaching the arms to the hub base.

20. The method of claim 19 , which includes attaching the fixed-wing aircraft to the part of the saddle before pivoting the portion of the saddle relative to the hub base.

Assignees

• Hood Tech Corp

Inventors

• Von Flotow Andreas H
• Roeseler Corydon C

Classifications

• 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

• B64U80/70

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

• B64U2201/20

  Remote controls · CPC title

• B65D2585/687

  aircrafts · CPC title