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

• US 10,538,318 B2
• Filed: 02/14/2017
• Issued: 01/21/2020
• Est. Priority Date: 04/02/2013
• Status: Active Grant

• Current Assignee: Hood Technology Corporation
• Original Assignee: Hood Technology Corporation
• Inventors: von Flotow, Andreas H., Roeseler, Corydon C.
• Primary Examiner(s): Benedik, Justin M
• Application Number:
  US15/432,529
• Publication Number:
  US 20170327206A1
• Time in Patent Office: 1,071 Days
• CPC Class Codes: B64C 2027/003 mounted on rotor hub, e.g. a rotary force generator
• CPC Class Codes: B64C 25/08 non-fixed, e.g. jettisonable
• CPC Class Codes: B64C 27/001 Vibration damping devices
• CPC Class Codes: B64C 27/26 characterised by provision of fixed wings
• CPC Class Codes: B64C 27/32 Rotors
• CPC Class Codes: B64C 27/48 Root attachment to rotor head
• CPC Class Codes: B64D 1/00 Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight with respect to weapon sights devices F41G takes precedence, parachutes per se B64D17/00; ejectable seats B64D25/10; ejectable capsules B64D25/12; refuelling during flight B64D39/00; launching apparatus for projecting projectiles or missiles F41F1/00, F41F7/00; rocket or torpedo launchers F41F3/00
• CPC Class Codes: B64D 1/02 Dropping, ejecting, or releasing articles jettisonable fuel reservoirs B64D37/12
• CPC Class Codes: B64D 1/12 Releasing
• CPC Class Codes: B64D 3/00 Aircraft adaptations to facilitate towing or being towed B64D39/00 takes precedence
• CPC Class Codes: B64D 35/02 specially adapted for specific power plants
• CPC Class Codes: B64D 5/00 Aircraft transported by aircraft, e.g. for release or reberthing during flight flying units formed by separate aircraft B64C37/02
• CPC Class Codes: B64F 1/029 using a cable or tether
• CPC Class Codes: B64F 1/0295 aerodynamically or aerostatically supported, e.g. parafoil or balloon
• CPC Class Codes: B64U 10/10 Rotorcrafts
• CPC Class Codes: B64U 10/13 Flying platforms
• CPC Class Codes: B64U 10/14 with four distinct rotor axes, e.g. quadcopters
• CPC Class Codes: B64U 10/25 Fixed-wing aircraft VTOL aircraft B64U10/20
• CPC Class Codes: B64U 2101/00 UAVs specially adapted for particular uses or applications
• CPC Class Codes: B64U 2101/67 the UAVs comprising tethers for lowering the goods
• CPC Class Codes: B64U 2201/10 : autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS]
• CPC Class Codes: B64U 2201/104 : using satellite radio beacon positioning systems, e.g. GPS
• CPC Class Codes: B64U 2201/20 : Remote controls
• CPC Class Codes: B64U 30/20 : Rotors; Rotor supports
• CPC Class Codes: B64U 50/19 : using electrically powered motors
• CPC Class Codes: B64U 70/20 : for releasing or capturing UAVs in flight by another aircraft
• CPC Class Codes: B64U 70/30 : for capturing UAVs in flight by ground or sea-based arresting gear, e.g. by a cable or a net
• CPC Class Codes: B64U 80/70 : in containers B64U80/60 takes precedence
• CPC Class Codes: B65D 25/10 : Devices to locate articles in containers for protecting articles from mechanical damage B65D81/02
• CPC Class Codes: B65D 2585/687 : aircrafts
• CPC Class Codes: B65D 85/68 : for machines, engines or vehicles in assembled or dismantled form

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.

Claims

1. A multicopter comprising:

a hub;

multiple arms removably attachable to the hub, each arm including a rotor and a rotor motor drivingly engaged to the rotor; and

multiple landing gear, each landing gear removably attachable to one of the arms,

wherein for each arm, when one of the landing gear is attached to that arm, that landing gear is movable relative to that arm between a first position in which the rotor of that arm can contact that landing gear and a second position in which the rotor of that arm cannot contact that landing gear.

2. The multicopter of claim 1, which includes multiple landing gear extensions.

3. The multicopter of claim 2, wherein each landing gear extension is removably attachable to one of the arms and to one of the landing gear, and wherein each landing gear is removably attachable to one of the arms via one of the landing gear extensions.

4. The multicopter of claim 3, wherein each landing gear extension is slidably receivable in or configured to slidably receive one of the arms to attach that landing gear to that arm.

5. The multicopter of claim 4, wherein each landing gear is slidably receivable in or configured to slidably receive one of the landing gear extensions.

6. The multicopter of claim 4, wherein the first position is further radially inward toward the hub than the second position.

7. The multicopter of claim 1, which includes multiple landing gear extensions, wherein each landing gear extension is slidably receivable in or configured to slidably receive one of the arms to attach that landing gear to that arm, wherein the first position is further radially inward toward the hub than the second position, and wherein, for one of the landing gear, a longer portion of the landing gear extension to which that landing gear is attached is slidably received in or slidably receives the corresponding arm when the landing gear is in the first position than when the landing gear is in the second position.

8. A multicopter comprising:

a hub;

first, second, third, and fourth arms removably attachable to the hub, each arm including an upper rotor, an upper rotor motor drivingly engaged to the upper rotor, a lower rotor, and a lower rotor motor drivingly engaged to the rotor; and

first, second, third, and fourth landing gear respectively removably attachable to the first, second, third, and fourth arms,

wherein for each arm, when the respective landing gear is attached to that arm, that landing gear is movable between a first radial position in which the upper and lower rotors of that arm can contact that landing gear and a second radial position in which the upper and lower rotors of that arm cannot contact that landing gear.

9. The multicopter of claim 8, which includes first, second, third, and fourth landing gear extensions.

10. The multicopter of claim 9, wherein the first landing gear is removably attachable to the first arm via the first landing gear extension, the second landing gear is removably attachable to the second arm via the second landing gear extension, the third landing gear is removably attachable to the third arm via the third landing gear extension, and the fourth landing gear is removably attachable to the fourth arm via the fourth landing gear extension.

11. The multicopter of claim 10, wherein the first landing gear extension is slidably receivable in or configured to slidably receive the first arm to attach the first landing gear to the first arm, the second landing gear extension is slidably receivable in or configured to slidably receive the second arm to attach the second landing gear to the second arm, the third landing gear extension is slidably receivable in or configured to slidably receive the third arm to attach the third landing gear to the third arm, and the fourth landing gear extension is slidably receivable in or configured to slidably receive the fourth arm to attach the fourth landing gear to the fourth arm.

12. The multicopter of claim 9, wherein the first, second, third, and fourth landing gear are slidably receivable in or configured to slidably receive the first, second, third, and fourth landing gear extensions, respectively.

13. The multicopter of claim 12, wherein the first position is further radially inward toward the hub than the second position.

14. The multicopter of claim 13, wherein, for the first, second, third, and fourth landing gear, a longer portion of the landing gear extension to which that landing gear is attached is slidably received in or configured to slidably receive the respective arm when the that landing gear is in the first position than when that landing gear is in the second position.

15. A method of preventing complete rotation of multiple rotors of a multicopter, the method comprising:

for each of multiple arms of the multicopter, each arm including a rotor and a rotor motor drivingly engaged to the rotor, unlocking landing gear attached to that arm to enable that landing gear to move relative to that arm; and

for each of the landing gear, moving that landing gear relative to the arm to which that landing gear is attached from a first position in which the rotor of that arm cannot contact the landing gear to a second position in which the rotor of that arm can contact that landing gear.

16. The method of claim 15, wherein the second position is further radially inward toward a hub of the multicopter than the first position.

17. The method of claim 15, wherein each landing gear is attached to one of multiple landing gear extensions and each landing gear extension is slidably received in or configured to slidably receive a different one of the arms.

18. The method of claim 16, which includes, for each of the landing gear, moving that landing gear from the first position to the second position by sliding the landing gear extension to which that landing gear is attached further into the corresponding arm.

19. The method of claim 16, which includes, for each of the landing gear, moving that landing gear from the first position to the second position by sliding the corresponding arm further into the landing gear extension to which that landing gear is attached.

20. The method of claim 19, wherein the second position is further radially inward toward a hub of the multicopter than the first position.