IP Library Granted Patent US 11,851,211
Granted Patent B2
US 11,851,211 · App. 17/511,509 · Granted Dec 26, 2023

Expendable airborne fiber optic link

Inventors: Max Edward Klein (Huntsville, AL); David Porter (Huntsville, AL); Walter Thomas Castleberry (Hampton Cove, AL)
Assignee: Sanmina Corporation
B64F1/362B64C39/024B64U50/34G02B6/4292G02B6/4477H04B10/25H04B10/807B64U30/20B64U2201/20B64U2201/202G02B6/4457
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Quick Facts
Patent No.
US 11,851,211
App. No.
17/511,509
Granted
Dec 26, 2023
Kind
B2
Abstract

Aspects of the present disclosure are related unmanned aerial vehicles tethered to ground stations with an expendable airborne fiber-optic link. The tethers may be fiber-optic cables that can be used as a communications conduit between a ground station and a UAV for providing vehicle positioning/control information to the UAV as well as transmitting a large amount of information/data to the UAV. As the information being transmitted between to the UAV the ground station is critical, fiber-optic cables provide the bandwidth and transmission capabilities required with the added benefit of electromagnetic interference (EMI) and radio-frequency interference (RFI) immunity, making this an ideal solution for these applications.

Claims (52)

1. An unmanned aerial vehicle (UAV) system, the UAV system comprising:

an expendable airborne fiber-optic link;

a first UAV connected to a distal end of the expendable fiber-optic link;

a first fiber-optic dispenser connected to the first UAV;

a second UAV connected to the first UAV by a second fiber-optic link; and

a fixed ground station connected to a proximal end of the expendable fiber-optic link, the fixed ground station comprising:

a processing system configured to perform executable operational and application specific pre-programmed commands and instructions;

a first electro-optic converter connected to the processing system; and

a strain relief module, connected between the first fiber-optic dispenser and a length of the dispensed fiber, for preventing damage from an axially applied load and strain at a connection point to the first electro-optic converter.

2. The unmanned aerial vehicle (UAV) system of claim 1 , wherein the strain relief module is a mandrel used to wrap the expendable airborne fiber-optic link around.

3. The unmanned aerial vehicle (UAV) system of claim 1 , wherein the strain relief module is a section of the expendable airborne fiber-optic link adhered to a stationary fixture on the fixed ground station.

4. The unmanned aerial vehicle (UAV) system of claim 1 , wherein the strain relief module is a clamping mechanism radially encircling the expendable airborne fiber-optic link.

5. The unmanned aerial vehicle (UAV) system of claim 1 , further comprising a second electro-optic converter located on the distal end of the expendable airborne fiber-optic link.

6. The unmanned aerial vehicle (UAV) system of claim 1 , wherein the proximal end of the expendable airborne fiber-optic link is detachable from the UAV for transitioning to a battery powered free flight.

7. The unmanned aerial vehicle (UAV) system of claim 1 , further comprising:

a second fiber-optic dispenser connected to a distal end of the second fiber-optic link.

8. An unmanned aerial vehicle (UAV) system, the UAV system comprising:

a first expendable fiber-optic link;

a first fiber-optic dispenser connected to a proximal end of the first expendable fiber-optic link;

a first UAV connected to a distal end of the first expendable fiber-optic link;

a second UAV connected to the first UAV by a second expendable fiber-optic cable; and

a mobile ground station connected to a proximal end of the first expendable fiber-optic link, the mobile ground station comprising:

a processing system configured to perform executable operational and application specific pre-programmed commands and instructions;

an electro-optic converter connected to the processing system; and

a tension setting module, connected between the first fiber-optic dispenser and a length of the dispensed fiber-optic link, for controlling tension of the expendable fiber-optic link.

9. The unmanned aerial vehicle (UAV) system of claim 8 , further comprising a second fiber-optic dispenser connected to the distal end of the expendable fiber-optic link.

10. The unmanned aerial vehicle (UAV) system of claim 9 , wherein the second fiber optic dispenser is selected from an inside-payout dispenser with a tension brake, an outside-linear payout with a tension brake, and an outside-linear payout with an electrically controllable brake.

11. The unmanned aerial vehicle (UAV) system of claim 8 , further comprising:

a third fiber-optic dispenser connected to a proximal end of the second expendable fiber-optic cable; and

a fourth fiber-optic dispenser connected to a distal end of the second expendable fiber-optic cable.

12. The unmanned aerial vehicle (UAV) system of claim 11 , wherein the third fiber optic dispenser is selected from an inside-payout dispenser with a tension brake, an outside-linear payout with a tension brake, and an outside-linear payout with an electrically controllable brake.

13. The unmanned aerial vehicle (UAV) system of claim 11 , wherein the fourth fiber optic dispenser is selected from an inside-payout dispenser with a tension brake, an outside-linear payout with a tension brake, and an outside-linear payout with an electrically controllable brake.

14. The unmanned aerial vehicle (UAV) system of claim 8 , wherein the first fiber optic dispenser is selected from an inside-payout dispenser with a tension brake, an outside-linear payout with a tension brake, and an outside-linear payout with an electrically controllable brake.

15. The unmanned aerial vehicle (UAV) system of claim 14 , wherein the outside-linear payout with the electrically controllable brake comprises:

a fiber pack for storing and dispensing the fiber-optic link;

a rounded end-guide, for guiding the fiber-optic link, having a ball pin for restricting payout of fiber-optic link;

an axial flux motor, integrated into the rounded end-guide, having a layer of ferromagnetic nanoparticles embedded in an epoxy layer; and

a DC voltage applied to a stator of the axial flux motor for providing a constant resistive torque.

16. The unmanned aerial vehicle (UAV) system of claim 15 , wherein amplification of fiber tension applied to the fiber-optic link by the axial flux motor achieves desired tension at output of the fiber pack.

17. An unmanned aerial vehicle (UAV) system, the UAV system comprising:

a first expendable fiber-optic link;

a first UAV connected to a distal end of the expendable fiber-optic link; and

a mobile ground station connected to a proximal end of the first expendable fiber-optic link, the mobile ground station comprising:

a processing system configured to perform executable operational and application specific pre-programmed commands and instructions;

an electro-optic converter connected to the processing system; and

a tension setting module connected to the electro-optic converter for controlling tension of the expendable fiber-optic link; and

a first fiber-optic dispenser connected to the proximal end of the first expendable fiber-optic link;

a second fiber-optic dispenser connected to the distal end of the expendable fiber-optic link;

a second UAV connected to the first UAV by a second expendable fiber-optic cable;

a third fiber-optic dispenser connected to a proximal end of the second expendable fiber-optic cable; and

a fourth fiber-optic dispenser connected to a distal end of the second expendable fiber-optic cable.

18. The unmanned aerial vehicle (UAV) system of claim 17 , further comprising a remote controller communicatively coupled to the mobile ground station for receiving and responding to commands and instructions transmitted remotely.

Assignments (2)
SECURITY INTEREST Recorded Oct 28, 2025
From: SANMINA CORPORATION
To: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT
Reel/Frame 073363/0212 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 29, 2021
From: KLEIN, MAX EDWARD; PORTER, DAVID; CASTLEBERRY, WALTER THOMAS
To: SANMINA CORPORATION
Reel/Frame 057964/0680 →