Capture devices for unmanned aerial, vehicles, including track-borne capture lines, and associated systems and methods

Patent metadata

Field	Value
Publication number	US-10513350-B1
Application number	US-201815892701-A
Country	US
Kind code	B1
Filing date	Feb 9, 2018
Priority date	Nov 20, 2014
Publication date	Dec 24, 2019
Grant date	Dec 24, 2019

Abstract

Capture devices for unmanned aerial vehicles, including track borne capture lines, and associated systems and methods are disclosed. A representative system includes at least one support having an upright portion and at least one boom portion, a carriage track carried by the at least one boom portion, and a carriage carried by, and movable along, the carriage track. The system can further include a capture line carried by and extending downwardly from the at least one boom portion, or the carriage, or both the at least one boom portion and the carriage.

First claim

We claim:

1. An aircraft system, comprising:
at least one support having an upright portion and at least one boom portion;
a capture line carried by and extending downwardly relative to the at least one boom portion; and
a releasable restraint device coupled to the capture line to allow motion of the capture line in a first direction and to prevent motion of the capture line in a second direction opposite the first direction, wherein the restraint device includes a ratchet and a restraint line, the restraint line connected to the capture line.

2. The system of claim 1 wherein the ratchet is operatively coupled to the restraint line.

3. The system of claim 1 , further comprising:
a carriage track carried by the at least one boom portion; and
a carriage carried by and movable along the carriage track.

4. The system of claim 3 , wherein the restraint device is carried by and movable with the carriage.

5. The system of claim 3 wherein the restraint line is carried by the carriage.

6. The system of claim 3 wherein the capture line includes an engagement region positioned to engage with an engagement member of an aircraft, and wherein the restraint line is connected between the carriage and the capture line, the restraint line being connected to the capture line at a location above the engagement region.

7. An aircraft system, comprising:
at least one support having an upright portion and at least one boom portion;
a capture line carried by and extending downwardly relative to the at least one boom portion; and
a releasable restraint device coupled to the capture line to allow motion of the capture line in a first direction and to prevent motion of the capture line in a second direction opposite the first direction, the restraint device including:
a restraint line connected to the capture line;
a restraint support;
a locking pulley carried by the restraint support; and
a retraction member, wherein the restraint line is connected to the retraction member and engaged with the locking pulley between the capture line and the retraction member.

8. The system of claim 7 wherein the locking pulley is releasably carried by the restraint support, and wherein the restraint device further includes a winch coupled to the locking pulley to allow the locking pulley to move between a first position and a second position relative to the restraint support.

9. A method for arresting an unmanned aircraft in flight, comprising:
releasably engaging the unmanned aircraft with a downwardly extending, flexible capture line;
allowing motion of the capture line in a first direction as the unmanned aircraft decelerates;
preventing motion of the capture line in a second direction opposite the first direction, wherein the capture line is attached to a restraint line, and wherein preventing motion includes preventing motion of the restraint line; and
releasing the unmanned aircraft from the capture line.

10. The method of claim 9 wherein preventing motion of the capture line includes engaging a ratchet with a pulley about which the capture line passes.

11. The method of claim 9 wherein preventing motion of the capture line includes engaging a ratchet with a pulley about which the restraint line passes.

12. The method of claim 9 , further comprising:
absorbing energy imparted to the capture line by the unmanned aircraft; and
releasing at least a portion of the energy before releasing the unmanned aircraft from the capture line.

Assignees

• Insitu Inc

Inventors

• Kunz Peter
• Jackson Clifford
• Thomasian Craig Aram

Classifications

• B64C25/68

  Arrester hooks · CPC title

• B64F1/02 Primary

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

• B64U70/30

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

• B64F1/0297

  adjustable to align with aircraft trajectory · CPC title

• B64F1/029 Primary

  using a cable or tether · CPC title