IP Library Granted Patent US 10,577,094
Granted Patent B2
US 10,577,094 · App. 15/433,686 · Granted Mar 3, 2020

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

Inventors: Andreas H. von Flotow (Hood River, OR); Corydon C. Roeseler (Hood River, OR)
Assignee: Hood Technology Corporation
B64C27/48B64C25/08B64C27/001B64C27/08B64C27/26B64C27/32B64C39/024B64D1/00B64D1/02B64D1/12B64D3/00B64D5/00B64D35/02B64F1/02B65D25/10B65D85/68B64C2027/003B64C2201/021B64C2201/024B64C2201/027B64C2201/042B64C2201/082B64C2201/108B64C2201/12B64C2201/146B64C2201/182B64C2201/201B65D2585/687
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Quick Facts
Patent No.
US 10,577,094
App. No.
15/433,686
Granted
Mar 3, 2020
Kind
B2
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 (29)

1. A rotorcraft-assisted system for retrieving an aircraft from flight, the system comprising:

a rotorcraft;

a flexible capture member having a first end and a second end, the first end attachable to the rotorcraft; and

an anchor system including a base, a breakaway device removably attachable to the base, and a flexible capture member payout and retract device rotatably attachable to the base,

wherein the second end of the flexible capture member is attachable to the flexible capture member payout and retract device,

wherein the flexible capture member is attachable to the breakaway device between the ends of the flexible capture member.

2. The rotorcraft-assisted system of claim 1 , wherein the flexible capture member includes a capture portion including two ends and a middle extending between the two ends, one of the two ends being thicker than the middle.

3. The rotorcraft-assisted system of claim 2 , wherein both ends of the capture portion are thicker than the middle.

4. The rotorcraft-assisted system of claim 3 , wherein the two ends of the capture portion each include a Brummel eye splice.

5. The rotorcraft-assisted system of claim 1 , wherein the flexible capture member includes an elastic portion near the first end.

6. The rotorcraft-assisted system of claim 5 , wherein the flexible capture member includes a capture portion and a retractable portion, the capture portion located between the elastic portion and the retractable portion.

7. The rotorcraft-assisted system of claim 6 , wherein the capture portion includes two ends and a middle extending between the two ends, one of the two ends being thicker than the middle.

8. The rotorcraft-assisted system of claim 7 , wherein both ends of the capture portion are thicker than the middle.

9. The rotorcraft-assisted system of claim 1 , wherein the flexible capture member includes an elastic portion near the first end, wherein the flexible capture member includes a capture portion and a retractable portion, the capture portion located between the elastic portion and the retractable portion, wherein the capture portion includes two ends and a middle extending between the two ends, wherein both ends of the capture portion are thicker than the middle, and wherein the two ends of the capture portion each include a Brummel eye splice.

10. The rotorcraft-assisted system of claim 1 , which includes a ring, the ring attachable to the flexible capture member to enable the flexible capture member to be attached to the breakaway device.

11. A flexible capture member for retrieving an aircraft from flight, the flexible capture member comprising:

an elastic portion including a compliant damper;

a retractable portion; and

a capture portion between the elastic portion and the retractable portion.

12. The flexible capture member of claim 11 , wherein the capture portion includes two ends and a middle extending between the two ends, one of the two ends being thicker than the middle.

13. The flexible capture member of claim 12 , wherein both of the ends of the capture portion are thicker than the middle.

14. The flexible capture member of claim 13 , wherein the two ends each include a Brummel eye splice.

15. The flexible capture member of claim 11 , wherein the retractable portion is non-elastic, and wherein the capture portion is non-elastic.

16. A flexible capture member for retrieving an aircraft from flight, the flexible capture member comprising:

an elastic portion;

a retractable portion including an elastic member; and

a capture portion between the elastic portion and the retractable portion.

17. The flexible capture member of claim 16 , wherein the retractable portion includes the elastic member and a non-elastic member, and wherein the elastic member is positioned inside the non-elastic member.

18. The flexible capture member of claim 16 , wherein the retractable portion includes the elastic member and a non-elastic member, and wherein the elastic member is positioned inside the non-elastic member, and wherein the capture portion is non-elastic.

Assignments (3)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 22, 2017
From: VON FLOTOW, ANDREAS H.
To: HOOD TECHNOLOGY CORPORATION
Reel/Frame 041343/0154 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 22, 2017
From: VON FLOTOW, ANDREAS H.; ROESELER, CORYDON C.
To: HOOD TECHNOLOGY CORPORATION
Reel/Frame 041343/0831 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 22, 2017
From: VON FLOTOW, ANDREAS H.; ROESELER, CORYDON C.
To: HOOD TECHNOLOGY CORPORATION
Reel/Frame 041346/0270 →
Continuity (8)
Continuation 15375909 · Dec 12, 2016
Continuation In Part 15144119 · May 2, 2016
Continuation 14597933 · Jan 15, 2015
Continuation In Part 14230454 · Mar 31, 2014
Provisional Application 62269629 · Dec 18, 2015
Provisional Application 61808392 · Apr 4, 2013
Provisional Application 61807508 · Apr 2, 2013
Related Publication 20170327226A1 · Nov 16, 2017
Cited By (1)
US 12,291,359