System and method of blade-tip facilitated aircraft capture
AssigneeLockheed Martin Corporation
InventorsDustin E. Gamble, Matthew Curran
Life of this patent
Estimating the term…
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.
Claims15
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.
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.
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.
Dependencies are inferred from the claim text.