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US Patent 6932296 Cycloidal VTOL UAV

Patent 6932296 was granted and assigned to Information Systems Laboratories on August, 2005 by the United States Patent and Trademark Office.

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Patent
Patent
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Patent attributes

Patent Applicant
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Current Assignee
Information Systems Laboratories
Information Systems Laboratories
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
69322960
Patent Inventor Names
Glenn Martin Tierney0
Date of Patent
August 23, 2005
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Patent Application Number
106902840
Date Filed
October 21, 2003
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Patent Primary Examiner
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J. Woodrow Eldred
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Patent abstract

A system and method for moving an aerial vehicle along a flight path includes rotatable hubs mounted on opposite sides of the vehicle. Elongated airfoils are mounted on the hubs parallel to a common hub axis for rotation about the hub axis on a blade path. Each airfoil defines a chord line and the system includes a gear assembly changeable, during hub rotation, between a first modality wherein airfoil chord lines remain tangential to the blade path (curtate flight), and a second modality wherein airfoil chord lines remain parallel to the flight path of the vehicle (prolate flight). Also, rotation of the hub can be stopped and the airfoils used for fixed wing flight.

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