Locking line capture devices for unmanned aircraft, and associated systems and methods

• US 10,407,181 B2
• Filed: 06/27/2016
• Issued: 09/10/2019
• Est. Priority Date: 06/27/2016
• Status: Active Grant

• Current Assignee: Insitu Incorporated (The Boeing Co.)
• Original Assignee: Insitu Incorporated (The Boeing Co.)
• Inventors: Grubb, Matthew
• Primary Examiner(s): Wang, Michael H
• Application Number:
  US15/194,492
• Publication Number:
  US 20170369185A1
• Time in Patent Office: 1,170 Days
• CPC Class Codes: B64F 1/029 using a cable or tether
• CPC Class Codes: B64U 70/00 Launching, take-off or landing arrangements
• 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 80/84 Waterborne vehicles

Abstract

Locking line capture devices for unmanned aircraft, and associated systems and methods are disclosed herein. A representative system includes a line capture body having a line slot with an open end and closed end, and a retainer positioned proximate the line slot and movable between first position in which the retainer blocks access to the line slot and a second position in which the retainer allows access to the line slot. A locking device is operably coupled between the capture body and the retainer and is movable between an unlocked position to allow movement of the retainer between the first and second positions, and a locked position to block such movement. A release device is operably coupled to the locking device and movable between a secured position with the locking device secured in the locked position, and a released position with the locking device movable between the locked and unlocked positions.

Claims

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

a line capture body having a line slot, the line slot having an open end and a closed end;

a retainer positioned proximate the line slot and rotatable relative to the line capture body and a wing of the UAV system between a first position in which the retainer blocks access to the line slot and a second position in which the retainer allows access to the line slot, the retainer positioned in the first position prior to the retainer being engaged by a recovery line;

a locking device operably coupled between the line capture body and the retainer, and moveable between at least one unlocked position in which the locking device allows movement of the retainer from the first position to the second position, and a locked position in which the locking device blocks movement of the retainer from the first position to the second position, the locking device including a line strike device positioned across the line slot to make contact with the recovery line, and a locking element positioned to engage with the retainer when the locking device is in the locked position; and

a release device operably coupled to the locking device and moveable between a secured position with the locking device secured in the locked position, and a released position with the locking device movable between the locked position and the unlocked position.

2. The system of claim 1 wherein the retainer includes a flat portion that extends over the line slot when the retainer is in the first position, and wherein the system further comprises a spring coupled between the retainer and the line capture body, with the spring biasing the retainer to the first position.

3. The system of claim 1 wherein the locking device is slideable between the locked and unlocked positions.

4. The system of claim 1 wherein the locking element is slideable between the locked and unlocked positions, and wherein the line strike device is operably coupled to both the line capture body and the locking element, the line strike device being movable between an unstruck position with the locking device in the unlocked position, and a struck position with the locking device in the locked position.

5. The system of claim 1 wherein the line strike device includes an elongated wire positioned across the line slot.

6. The system of claim 1 wherein the line strike device includes a flat portion positioned across the line slot.

7. The system of claim 1 wherein the retainer includes a flat portion that extends over the line slot when the retainer is in the first position, the flat portion including a notch, and wherein the locking element of the locking device is positioned in the notch when the locking device is in the locked position, and is positioned out of the notch when the locking device is in the unlocked position.

8. The system of claim 1, wherein the line capture body is rigidly attached to the wing, and the retainer is rotatable relative to the line capture body.

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

a line capture body having a line slot, the line slot having an open end and a closed end;

a retainer positioned proximate the line slot and movable relative to a wing of the UAV system between a first position in which the retainer blocks access to the line slot and a second position in which the retainer allows access to the line slot;

a locking device operably coupled between the line capture body and the retainer, and moveable between at least one unlocked position in which the locking device allows movement of the retainer from the first position to the second position, and a locked position in which the locking device blocks movement of the retainer from the first position to the second position, the locking device including a wire having a line strike portion positioned across the line slot to make contact with a recovery line, and a locking portion positioned to engage with the retainer when the locking device is in the locked position; and

a release device operably coupled to the locking device and moveable between a secured position with the locking device secured in the locked position, and a released position with the locking device movable between the locked position and the unlocked position.

10. The system of claim 9 wherein the retainer includes a notch, and wherein the locking portion of the locking device is positioned in the notch when the locking device is in the locked position, and is positioned out of the notch when the locking device is in the unlocked position.

11. The system of claim 9 wherein the locking device and the release device are both portions of a single unitary wire.

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

a UAV having a wing;

a line capture body attached to the wing and having a line slot, the line slot having an open end and a closed end, the line capture body further having a lock groove;

a retainer having a flat portion with a notch, the retainer being positioned proximate the line slot and movable between a first position in which the flat portion is positioned over the line slot to block access to the line slot and a second position in which the flat portion is rotated away from the first position to allow access to the line slot;

a locking device operably coupled between the line capture body and the retainer, the locking device including;

a locking element positioned in the lock groove and slideable between an unlocked position in which the locking device allows movement of the retainer from the first position to the second position, and a locked position in which the locking device blocks movement of the retainer from the first position to the second position, the locking element further including a protrusion that is positioned in the notch when the locking device is in the locked position, and is positioned out of the notch when the locking device is in the unlocked position; and

a line strike device positioned across the line slot, and operably coupled to both the line capture body and the locking element, the line strike device being movable between an unstruck position with the locking element in the unlocked position, and a struck position with the locking element in the locked position; and

a release device operably coupled to the locking device and moveable between a secured position with the locking element secured in the locked position, and a released position with the locking element movable between the locked position and the unlocked position.

13. The system of claim 12 wherein the line strike device includes a wire pivotably coupled between the line capture body and the locking element.

14. The system of claim 12 wherein the locking device and the release device are both portions of a single unitary wire.

15. A method for capturing an unmanned aerial vehicle (UAV), the method comprising:

directing the UAV toward a recovery line;

engaging a line capture device carried by the UAV with the recovery line by moving at least one of the UAV and the recovery line relative to the other, causing a portion of the recovery line to enter a line slot of the capture device and move a retainer of the capture device from a first position to a second position;

after the recovery line has entered the line slot, engaging a locking device with the retainer to prevent the retainer from moving from the first position to the second position; and

after the UAV has been captured, releasing the UAV from the recovery line by moving a release device from a secured position, with the locking device secured in the locked position, to a released position, with the locking device movable between the locked position and the unlocked position.

16. The method of claim 15 wherein the portion of the recovery line is a first portion, and wherein the retainer, in the second position, prevents a second portion of the recovery line from entering the line slot.

17. The method of claim 15 wherein the recovery line rotates the retainer from the first position to the second position.

18. The method of claim 15 wherein engaging the locking device includes sliding the locking device.

19. The method of claim 15 wherein engaging the locking device includes moving a portion of the locking device from a position beneath the retainer.

20. The method of claim 15 wherein engaging the locking device includes moving a portion of the locking device into a notch of the retainer.

21. The method of claim 15 wherein causing the portion of the recovery line to move the retainer includes causing the portion of the recovery line to strike a line strike device coupled to the retainer.

22. The method of claim 21 wherein the line strike device includes a flat portion positioned across the line slot.

23. The method of claim 21 wherein the line strike device includes a portion of a wire.

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

a line capture body having a line slot, the line slot having an open end and a closed end;

a retainer positioned proximate the line slot and movable relative to a wing of the UAV system between a first position in which the retainer blocks access to the line slot and a second position in which the retainer allows access to the line slot; and

a locking device operably coupled between the line capture body and the retainer, and moveable between at least one unlocked position in which the locking device allows movement of the retainer from the first position to the second position, and a locked position in which the locking device blocks movement of the retainer from the first position to the second position, the locking device including a wire having a line strike portion positioned across the line slot to make contact with a recovery line, and a locking portion positioned to engage with the retainer when the locking device is in the locked position.