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US Patent 11851178 Long range endurance aero platform system

Patent 11851178 was granted and assigned to The Aerospace Corporation on December, 2023 by the United States Patent and Trademark Office.

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Is a
Patent
Patent
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Patent attributes

Patent Applicant
The Aerospace Corporation
The Aerospace Corporation
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Current Assignee
The Aerospace Corporation
The Aerospace Corporation
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
118511780
Patent Inventor Names
Steven Beck0
Bernard Harris Jefferson, Jr.0
Jeffrey Lang0
Richard Welle0
John Morales0
Martin Panevsky0
Allyson Yarbrough0
Christopher Hartney0
...
Date of Patent
December 26, 2023
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Patent Application Number
167916050
Date Filed
February 14, 2020
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Patent Citations
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US Patent 7712701 Unmanned aerial vehicle with electrically powered, counterrotating ducted rotors
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US Patent 7794302 Directionally controllable, self-stabilizing, rotating flying vehicle
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US Patent 8113905 Directionally controllable flying vehicle and a propeller mechanism for accomplishing the same
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US Patent 8205820 Transforming unmanned aerial-to-ground vehicle
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US Patent 8251307 Airborne manipulator system
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US Patent 7032861 Quiet vertical takeoff and landing aircraft using ducted, magnetic induction air-impeller rotors
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US Patent 7484687 Propulsion device
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US Patent 7497759 Directionally controllable, self-stabilizing, rotating flying vehicle
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...
Patent Citations Received
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US Patent 12024285 Modular mobility system including thrusters movably connected to a support structure
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Patent Primary Examiner
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Medhat Badawi
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CPC Code
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B64C 2201/024
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B64D 27/24
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B64D 27/08
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B64D 2027/026
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Y02T 50/60
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B64C 2201/021
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B64C 27/22
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B64C 39/062
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Patent abstract

An unmanned aerial vehicle (UAV) that provides increased operational flight endurance and efficiency. The UAV includes a power generation system, which includes an internal combustion engine and one or more batteries (batteries). The power generation system is configured to generate power for propulsion of the UAV. The internal combustion engine is configured to power a lift propeller, generating vertical lift of the UAV, and the batteries are configured to power a micro-propeller assembly, propelling the UAV in a forward direction or multiple additional directions.

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