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US Patent 10519013 Winch system for an airborne payload control system

Patent 10519013 was granted and assigned to Lockheed Martin on December, 2019 by the United States Patent and Trademark Office.

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Patent abstractTimelineTable: Further ResourcesReferences
Is a
Patent
Patent

Patent attributes

Patent Applicant
Lockheed Martin
Lockheed Martin
Current Assignee
Lockheed Martin
Lockheed Martin
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
10519013
Date of Patent
December 31, 2019
Patent Application Number
15444686
Date Filed
February 28, 2017
Patent Citations
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US Patent 10384782 Airborne payload control system
Patent Citations Received
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US Patent 12065225 Rapid aerial extraction systems
5
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US Patent 11945697 Multiple remote control for suspended load control equipment apparatus, system, and method
6
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US Patent 11992444 Apparatus, system, and method to control torque or lateral thrust applied to a load suspended on a suspension cable
7
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US Patent 12012188 Rapid aerial extraction systems
8
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US Patent 10934142 Motor-driven fairlead for assisting spooling or unspooling from a winch
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US Patent 11008198 Hoist and deployable equipment apparatus, system, and method
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US Patent 11026502 Portable electronic device leash and associated use thereof
‌
US Patent 11620597 Machine learning real property object detection and analysis apparatus, system, and method
13
...
Patent Primary Examiner
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Emmanuel M Marcelo
Patent abstract

A method for a winch system includes receiving, from a controller, instructions to spool a payload line, the payload line comprising a first end and a second end, the first end coupled to a main reel of the winch system and the second end configured to couple to a payload. The method further includes operating, based on the instructions, one or more of a first motor of the winch system and a second motor of the winch system, wherein the one or more of the first motor and the second motor are operated in order to control a position of the second end of the payload line.

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