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

Patent metadata

Field	Value
Publication number	US-10967987-B2
Application number	US-201916533251-A
Country	US
Kind code	B2
Filing date	Aug 6, 2019
Priority date	Jun 27, 2016
Publication date	Apr 6, 2021
Grant date	Apr 6, 2021

Abstract

Locking line capture devices for unmanned aircraft are disclosed. An example line capture device is configured to be attached to a wing of an unmanned aerial vehicle (UAV). The example line capture device includes a body having a line capture slot. The line capture slot has an open end and a closed end. The example line capture device further includes a retainer having a first lobe, a second lobe, and a third lobe. The retainer is movable relative to the body between a first position in which the first and third lobes are positioned on opposite sides of the line capture slot and the second lobe is positioned over the line capture slot, and a second position in which the first and second lobes are positioned over the line capture slot and the third lobe is positioned clear of the line capture slot.

First claim

What is claimed is:

1. A line capture device configured to be attached to a wing of an unmanned aerial vehicle (UAV), the line capture device comprising:
a body having a line capture slot, the line capture slot having an open end and a closed end; and
a retainer having a first lobe, a second lobe, and a third lobe, the retainer being movable relative to the body between a first position in which the first and third lobes are positioned on opposite sides of the line capture slot and the second lobe is positioned over the line capture slot, and a second position in which the first and second lobes are positioned over the line capture slot and the third lobe is positioned clear of the line capture slot.

2. The line capture device of claim 1 , wherein the retainer is pivotable relative to the body between the first and second positions.

3. The line capture device of claim 1 , further comprising a biasing device coupled between the body and the retainer, the biasing device configured to bias the retainer away from the second position and toward the first position.

4. The line capture device of claim 1 , wherein the retainer is configured to be positioned in the first position prior to the retainer being engaged by a recovery line.

5. The line capture device of claim 4 , wherein the retainer is configured to be positioned in the second position in response to the retainer being engaged by a first portion of the recovery line.

6. The line capture device of claim 5 , wherein the first lobe is configured to block access to the open end of the line capture slot when the retainer is in the second position.

7. The line capture device of claim 5 , wherein the first lobe is configured to prevent a second portion of the recovery line from being captured within the line capture slot when the retainer is in the second position.

8. The line capture device of claim 1 , wherein the retainer is configured to capture a recovery line in the line capture slot between the first lobe and the closed end in response to the retainer being engaged by the recovery line.

9. The line capture device of claim 1 , wherein the retainer is configured to capture a recovery line in the line capture slot between the second lobe and the closed end in response to the retainer being engaged by the recovery line.

10. The line capture device of claim 1 , wherein the retainer is further movable to a third position in which the first lobe is positioned over the line capture slot and the second and third lobes are clear of the line capture slot.

11. The line capture device of claim 10 , wherein the retainer is configured to enable a recovery line captured in the line capture slot to be moved past the second lobe and toward the open end when the retainer is in the third position.

12. The line capture device of claim 10 , wherein the retainer is pivotable relative to the body between the second and third positions.

13. An unmanned aerial vehicle (UAV), comprising
a wing; and
a line capture device attached to the wing, the line capture device including:
a body having a line capture slot, the line capture slot having an open end and a closed end; and
a retainer having a first lobe, a second lobe, and a third lobe, the retainer being movable relative to the body between a first position in which the first and third lobes are positioned on opposite sides of the line capture slot and the second lobe is positioned over the line capture slot, and a second position in which the first and second lobes are positioned over the line capture slot and the third lobe is positioned clear of the line capture slot.

14. The UAV of claim 13 , wherein the retainer is pivotable relative to the body between the first and second positions.

15. The UAV of claim 13 , wherein the line capture device further includes a biasing device coupled between the body and the retainer, the biasing device configured to bias the retainer away from the second position and toward the first position.

16. The UAV of claim 13 , wherein the retainer is configured to be positioned in the first position prior to the retainer being engaged by a recovery line.

17. The UAV of claim 13 , wherein the retainer is further movable to a third position in which the first lobe is positioned over the line capture slot and the second and third lobes are clear of the line capture slot.

18. A method, comprising:
moving a retainer of a line capture device relative to a body of the line capture device from a first position to a second position, the line capture device being coupled to a wing of an unmanned aerial vehicle (UAV), the body having a line capture slot including an open end and a closed end, the retainer having a first lobe, a second lobe, and a third lobe, wherein the first and third lobes are positioned on opposite sides of the line capture slot and the second lobe is positioned over the line capture slot when the retainer is in the first position, and wherein the first and second lobes are positioned over the line capture slot and the third lobe is positioned clear of the line capture slot when the retainer is in the second position.

19. The method of claim 18 , wherein moving the retainer from the first position to the second position includes pivoting the retainer relative to the body.

20. The method of claim 18 , further comprising biasing the retainer away from the second position and toward the first position via a biasing device coupled between the body and the retainer.

Assignees

• Insitu Inc

Inventors

• Grubb Matthew

Classifications

• B64U80/84

  Waterborne vehicles · CPC title

• B64U70/30 Primary

  for capturing UAVs in flight by ground or sea-based arresting gear, e.g. by a cable or a net · CPC title

• B64U70/00

  Launching, take-off or landing arrangements · CPC title

• B64F1/02 Primary

  for arresting aircraft, e.g. nets or cables · CPC title

• B64F1/029 Primary

  using a cable or tether · CPC title