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

Patent metadata

Field	Value
Publication number	US-11858631-B2
Application number	US-202017133055-A
Country	US
Kind code	B2
Filing date	Dec 23, 2020
Priority date	Oct 2, 2015
Publication date	Jan 2, 2024
Grant date	Jan 2, 2024

Abstract

Aerial launch and/or recovery for unmanned aircraft, and associated systems and methods. A representative unmanned aerial vehicle (UAV) comprises an airframe, a plurality of rotors, and a capture line. The rotors are coupled to the airframe and configured to support the UAV in hover. The capture line is carried by the UAV and is operatively coupled to an immersible anchor. The immersible anchor is configured to be immersed within a body of water during a capture operation involving the capture line.

First claim

What is claimed is:

1. An unmanned aerial vehicle (UAV) capture system, the system comprising:
a first UAV including:
an airframe, and
a plurality of rotors coupled to the airframe and configured to support the first UAV in hover;

a drag cable;
an immersible anchor configured to be immersed within a body of water; and
a capture line carried by the first UAV, wherein a first end of the capture line is coupled to the airframe, and wherein a second end of the capture line opposite the first end is coupled to the drag cable, the drag cable supporting the immersible anchor for capture of a second UAV in flight with the capture line.

2. The UAV capture system of claim 1 , wherein the drag cable extends between the immersible anchor and a waterborne vessel.

3. The UAV capture system of claim 2 , wherein the drag cable is operatively coupled to a winch, and wherein the winch is coupled to the waterborne vessel and configured to reel the drag cable in and out relative to the waterborne vessel.

4. The UAV capture system of claim 3 , wherein a first end of the drag cable is coupled to the winch, and wherein a second end of the drag cable opposite the first end of the drag cable is coupled to the immersible anchor.

5. The UAV capture system of claim 4 , wherein the second end of the drag cable is further coupled to a weighted mass, the weighted mass configured to maintain the drag cable in a stable orientation relative to the capture line and the waterborne vessel during the capture of the second UAV.

6. The UAV system of claim 5 , wherein the weighted mass extends from the drag cable at a first position of the drag cable and the immersible anchor extends from the drag cable at a second position of the drag cable different from the first position.

7. The UAV of claim 6 , further including a cable extending between the drag cable and the weighted mass.

8. The UAV capture system of claim 4 , wherein the winch is configured to reel in the drag cable, the immersible anchor, and the capture line toward the waterborne vessel when the first UAV carries the second UAV on the capture line when the second UAV is captured.

9. The UAV capture system of claim 1 , wherein the second end of the capture line is coupled to the drag cable via a ring.

10. The UAV system of claim 1 , wherein the drag cable is further coupled to a weighted mass, the weighted mass configured to maintain the drag cable in a stable orientation relative to the capture line during the capture of the second UAV.

11. The UAV system of claim 1 , wherein the first UAV is configured to capture the second UAV via the capture line, and wherein the first UAV is configured to carry the captured second UAV from a first location at which the capture occurred to a second location aboard a waterborne vessel.

12. A method, comprising:
commencing a flight of a first unmanned aerial vehicle (UAV) of a UAV system, the first UAV including:
an airframe;
a plurality of rotors coupled to the airframe and configured to support the first UAV in hover during the flight of the first UAV;
a drag cable;
an immersible anchor; and
a capture line carried by the first UAV, wherein a first end of the capture line is coupled to the airframe, and wherein a second end of the capture line opposite the first end is coupled to the drag cable, the drag cable supporting the immersible anchor; and

immersing the immersible anchor within a body of water for capture of a second UAV in flight with the capture line.

13. The method of claim 12 , wherein the drag cable extends between the immersible anchor and a waterborne vessel.

14. The method of claim 13 , wherein the second end of the capture line is coupled to the drag cable via a ring.

15. The method of claim 13 , wherein the drag cable is operatively coupled to a winch, and wherein the winch is coupled to the waterborne vessel and configured to reel the drag cable in and out relative to the waterborne vessel.

16. The method of claim 15 , wherein a first end of the drag cable is coupled to the winch, and wherein a second end of the drag cable opposite the first end of the drag cable is coupled to the immersible anchor.

17. The method of claim 16 , wherein the second end of the drag cable is further coupled to a weighted mass, the weighted mass maintaining the drag cable in a stable orientation relative to the capture line and the waterborne vessel during the capture of the second UAV.

18. The method of claim 16 , further comprising:
capturing the second UAV via the capture line of the first UAV; and
operating the winch to reel in the drag cable, the immersible anchor, and the capture line toward the waterborne vessel when the first UAV carries the second UAV on the capture line when the second UAV is captured.

19. The method of claim 12 , wherein the drag cable is further coupled to a weighted mass, the weighted mass maintaining the drag cable in a stable orientation relative to the capture line during the capture of the second UAV.

20. The method of claim 12 , further comprising:
capturing the second UAV via the capture line of the first UAV; and
carrying the second UAV when captured from a first location at which the second UAV became captured to a second location aboard a waterborne vessel.

Assignees

• Insitu Inc

Inventors

• Mcgrew James Statelar
• Kunz Peter Josef
• Rysdyk Rolf Theodoor

Classifications

• Y02T50/60

  Efficient propulsion technologies, e.g. for aircraft · CPC title

• B64U2201/10

  autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS] · CPC title

• B64U2101/60

  for transporting passengers; for transporting goods other than weapons · CPC title

• B64U30/294

  Rotors arranged in the UAV body · CPC title

• B64U50/35

  by wireless transmission, e.g. by induction · CPC title