Aerial launch and/or recovery for unmanned aircraft, and associated systems and methods

Patent metadata

Field	Value
Publication number	US-10836509-B2
Application number	US-201715839592-A
Country	US
Kind code	B2
Filing date	Dec 12, 2017
Priority date	Dec 13, 2016
Publication date	Nov 17, 2020
Grant date	Nov 17, 2020

Abstract

Aerial launch and/or recovery for unmanned aircraft, and associated systems and methods. A representative system includes a first, carrier aircraft having an airframe a propulsion system carried by the airframe and positioned to support the carrier aircraft in hover, and a capture line carried by the carrier aircraft and deployable to hang from the carrier aircraft. The capture line is sized to releasably engage with a capture device of a second, carried aircraft. The system further includes a retrieval device positioned to support the carried aircraft for detachment from the capture line.

First claim

We claim:

1. An unmanned aerial vehicle (UAV) system, comprising:
a first, carrier aircraft having:
an airframe;
a propulsion system carried by the airframe and positioned to support the carrier aircraft in hover; and
a capture line carried by the carrier aircraft and deployable to hang from the carrier aircraft, the capture line being sized to releasably engage with a capture device of a second, carried aircraft; and

a retrieval device detached from the carrier aircraft and positioned to support the carried aircraft for detachment from the capture line, the retrieval device including:
a boom; and
a line support element carried by the boom and positioned to engage with the capture line, the line support element including a pulley.

2. The system of claim 1 , further comprising at least one boom support attached to the boom and positioned to support the boom in an elevated position.

3. The system of claim 1 , further comprising a tension device couplable to the capture line.

4. The system of claim 1 , further comprising:
at least one boom support attached to the boom and positioned to support the boom in an elevated position;
a tension device couplable to the capture line;
a first container element configured to position the boom and the tension device in a deployed configuration;
a second container element releasably connectable to the first container element to position the at least one boom support in the deployed configuration and resist relative motion between the boom and the at least one boom support.

5. The system of claim 4 , wherein the first container element includes a container body, and wherein the second container element includes a container lid.

6. The system of claim 1 , further comprising a motion control element pivotably couplable to the boom and having an aperture positioned to receive the capture line and sized to engage with a portion of the carried aircraft, the motion control element being pivotable between a first, upwardly facing position and a second, downwardly facing position.

7. The system of claim 1 , wherein the propulsion system includes multiple rotors.

8. A method for capturing an unmanned aerial vehicle (UAV), the method comprising:
launching a first, carrier aircraft having a capture line;
engaging a second, carried aircraft with the capture line;
supporting the carried aircraft for disengagement from the capture line by engaging the capture line with a line support element carried by a boom positioned off-board the carrier aircraft;
disengaging the carried aircraft from the capture line; and
landing the carrier aircraft.

9. The method of claim 8 , further comprising:
deploying the boom and at least one boom support from at least a first container element;
connecting the at least one boom support to the boom;
supporting the boom with the first container element;
supporting the boom support with a second container element; and
connecting the first container element to the second container element to support the boom in an upright position.

10. The method of claim 8 , wherein disengaging the carried aircraft includes disengaging the carried aircraft while the capture line is engaged with the line support element.

11. The method of claim 10 , further comprising engaging the capture line with the line support element before launching the carrier aircraft.

12. The method of claim 10 , further comprising engaging the capture line with the line support element after launching the carrier aircraft.

13. The method of claim 8 , further comprising placing the carrier aircraft in a hover mode before engaging the carried aircraft with the capture line.

14. The method of claim 8 , wherein landing the carrier aircraft is performed before disengaging the carried aircraft from the capture line.

15. An unmanned aerial vehicle (UAV) system, comprising:
a first, carrier aircraft having:
an airframe;
a propulsion system carried by the airframe and positioned to support the carrier aircraft in hover; and
a capture line carried by the carrier aircraft and deployable to hang from the carrier aircraft, the capture line being sized to releasably engage with a capture device of a second, carried aircraft;

a retrieval device detached from the carrier aircraft and positioned to support the carried aircraft for detachment from the capture line, the retrieval device including:
a boom; and
a line support element carried by the boom and positioned to engage with the capture line; and

at least one boom support attached to the boom and positioned to support the boom in an elevated position.

16. The system of claim 15 , wherein the line support element includes a pulley.

17. The system of claim 15 , wherein the line support element includes a hook.

18. The system of claim 15 , further comprising a tension device couplable to the capture line.

19. The system of claim 15 , further comprising:
a first container element configured to position the boom in a deployed configuration;
a second container element releasably connectable to the first container element to position the at least one boom support in the deployed configuration and resist relative motion between the boom and the at least one boom support.

20. The system of claim 19 , wherein the first container element includes a container body, and wherein the second container element includes a container lid.

21. The system of claim 15 , further comprising a motion control element pivotably couplable to the boom and having an aperture positioned to receive the capture line and sized to engage with a portion of the carried aircraft, the motion control element being pivotable between a first, upwardly facing position and a second, downwardly facing position.

22. An unmanned aerial vehicle (UAV) system, comprising:
a first, carrier aircraft having:
an airframe;
a propulsion system carried by the airframe and positioned to support the carrier aircraft in hover;
a capture line carried by the carrier aircraft and deployable to hang from the carrier aircraft, the capture line being sized to releasably engage with a capture device of

a second, carried aircraft; and
a retrieval device detached from the carrier aircraft and positioned to support the carried aircraft for detachment from the capture line, the retrieval device including:
a boom; and
a line support element carried by the boom and positioned to engage with the capture line; and

a motion control element pivotably couplable to the boom and having an aperture positioned to receive the capture line and sized to engage with a portion of the carried aircraft, the motion control element being pivotable between a first, upwardly facing position and a second, downwardly facing position.

23. The system of claim 22 , wherein the line support element includes a pulley.

24. The system of claim 22 , further comprising a tension device couplable to the capture line.

25. The system of claim 22 , further comprising:
a first container element configured to position the boom in a deployed configuration;
a second container element releasably connectable to the first container element to position the at least one boom support in the deployed configuration and resist relative motion between the boom and the at least one boom support.

26. The system of claim 25 , wherein the first container element includes a container body, and wherein the secon

Assignees

• Insitu Inc

Inventors

• Mcgrew James Statelar
• Grubb Matthew David
• Dickson Andrew Keith
• Hayes Andrew Royds

Classifications

• B64U50/19

  using electrically powered motors · CPC title

• B64F1/0295 Primary

  aerodynamically or aerostatically supported, e.g. parafoil or balloon · CPC title

• B64F1/029 Primary

  using a cable or tether · CPC title

• B64F1/02

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

• B64D5/00

  Aircraft transported by aircraft, e.g. for release or reberthing during flight · CPC title