System and method of blade-tip facilitated aircraft capture

Patent metadata

Field	Value
Publication number	US-11667397-B2
Application number	US-202217582457-A
Country	US
Kind code	B2
Filing date	Jan 24, 2022
Priority date	Feb 28, 2017
Publication date	Jun 6, 2023
Grant date	Jun 6, 2023

Abstract

A method of capturing an aerial vehicle comprises rotating a first blade of the aerial vehicle, the first blade coupled to a hub of the aerial vehicle and having a contour configured to facilitate entanglement of a payload line of a winch system around the aerial vehicle. The method further comprises contacting, by a leading edge of the first blade, the payload line of the winch system and pulling the payload line towards the hub of the aerial vehicle, wherein the payload line is pulled towards the hub as the first blade continues to rotate and wherein continued rotation of the first blade causes the payload line to be tangled around the hub of the aerial vehicle.

First claim

What is claimed is:

1. An aerial vehicle comprising:
a propulsion system comprising one or more rotors, each of the one or more rotors comprising one or more blades, wherein:
each blade is coupled to a hub of its respective rotor;
each blade has a contour configured to facilitate entanglement of the aerial vehicle in a line of a winch system;
each blade of the aerial vehicle has a leading edge and a trailing edge, the leading edge configured to contact the payload line before the trailing edge contacts the payload line; and
the contour of each blade defines a feature towards the leading edge, the feature configured to hook the payload line, the feature being one or more of:
an indentation; and
a protrusion.

2. The aerial vehicle of claim 1 , wherein at least one blade of the aerial vehicle is counter-rotating to another blade of the aerial vehicle.

3. The aerial vehicle of claim 1 , wherein:
the aerial vehicle comprises at least one pre-existing wing and each blade is configured to couple to the at least one pre-existing wing.

4. The aerial vehicle of claim 1 , wherein the line of the winch system is pulled across the trailing edge of the blade towards its respective hub.

5. The aerial vehicle of claim 1 , wherein entanglement occurs after a pulling-in force on the line exceeds a tension force on the line.

6. The aerial vehicle of claim 1 , wherein each blade of the aerial vehicle is a fixed-pitch blade.

7. A system for capturing an airborne payload comprising:
a payload line comprising a first end and a second end, the second end of the payload line configured to couple to a payload;
a winch system operable to spool the payload line, the winch system comprising a main reel about which the first end of the payload line is wound; and
wherein the payload is an aerial vehicle comprising one or more rotors, each of the one or more rotors comprising one or more blades, wherein:
each blade is coupled to a hub of its respective rotor;
each blade has a contour configured to facilitate entanglement of the payload line around the aerial vehicle;
each blade of the aerial vehicle has a leading edge and a trailing edge, the leading edge configured to contact the payload line before the trailing edge contacts the payload line; and
the contour of each blade defines a feature towards the leading edge, the feature configured to hook the payload line, the feature being one or more of:
an indentation; and
a protrusion.

8. The system of claim 7 , wherein at least one blade of the aerial vehicle is counter-rotating to another blade of the aerial vehicle.

9. The system of claim 7 , wherein the payload line is pulled across the trailing edge of the blade towards its respective hub.

10. The system of claim 7 , wherein entanglement occurs after a pulling-in force on the payload line exceeds a tension force on the payload line.

11. An aerial vehicle comprising:
a fuselage; and
a propulsion system comprising one or more rotors, each of the one or more rotors comprising one or more blades, wherein:
each blade is coupled to a hub of its respective rotor;
each blade has a contour configured to facilitate entanglement of the aerial vehicle in a line of a winch system;
each blade of the aerial vehicle has a leading edge and a trailing edge, the leading edge configured to contact the payload line before the trailing edge contacts the payload line; and
the contour of each blade defines a feature towards the leading edge, the feature configured to hook the payload line, the feature being one or more of:
an indentation; and
a protrusion.

12. The aerial vehicle of claim 11 , wherein at least one blade of the aerial vehicle is counter-rotating to another blade of the aerial vehicle.

13. The aerial vehicle of claim 11 , wherein the aerial vehicle comprises at least one pre-existing wing and each blade is configured to couple to the at least one pre-existing wing.

14. The aerial vehicle of claim 11 , wherein the line of the winch system is pulled across the trailing edge of the blade towards its respective hub.

15. The aerial vehicle of claim 11 , wherein entanglement occurs after a pulling-in force on the line exceeds a tension force on the line.

Assignees

• Lockheed Corp

Inventors

• Gamble Dustin E
• Curran Matthew

Classifications

• B64F1/08 Primary

  using winches · CPC title

• B64F1/0295

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

• B64F1/029 Primary

  using a cable or tether · CPC title

• B64C11/46

  Arrangements of, or constructional features peculiar to, multiple propellers {(B64C11/306 takes precedence)} · CPC title