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US Patent 11472546 Fixed-wing short-takeoff-and-landing aircraft and related methods

Patent 11472546 was granted and assigned to Aurora Flight Sciences on October, 2022 by the United States Patent and Trademark Office.

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Contents

Is a
Patent
Patent

Patent attributes

Patent Applicant
Aurora Flight Sciences
Aurora Flight Sciences
Current Assignee
Aurora Flight Sciences
Aurora Flight Sciences
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
11472546
Date of Patent
October 18, 2022
Patent Application Number
16799393
Date Filed
February 24, 2020
Patent Citations
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US Patent 10543905 Battery shifting for center of gravity control
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US Patent 10252815 System and method for monitoring a cockpit of an aircraft
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US Patent 10273003 Multi-tank system for aerial firefighting aircraft
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US Patent 10533356 Latch system with position hold
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US Patent 10625852 Aerodynamically efficient lightweight vertical take-off and landing aircraft with pivoting rotors and stowing rotor blades
Patent Citations Received
‌
US Patent 12103669 Aerial vehicle such as high speed drone
0
‌
US Patent D997836 Aircraft
‌
US Patent 12091173 UAV with distributed propulsion and blown control surfaces
0
Patent Primary Examiner
‌
Brian M O'Hara
CPC Code
‌
B64C 39/08
‌
B64C 29/0025
‌
B64C 1/1407

Fixed-wing short-takeoff-and-landing aircraft and related methods. The aircraft comprise an airframe comprising a rear wing assembly and a forward wing assembly positioned forward of the rear wing assembly, a rear plurality of blowing rotor assemblies operatively coupled to the rear wing assembly that are configured to blow air across the rear wing assembly to induce lift in the rear wing assembly, and a forward plurality of blowing rotor assemblies that are operatively coupled to the forward wing assembly and configured to blow air across the forward wing assembly to induce lift in the forward wing assembly. The methods comprise inducing lift in a forward wing assembly by blowing air across the forward wing assembly with a forward plurality of blowing rotor assemblies and inducing lift in a rear wing assembly by blowing air across a rear wing assembly with a rear plurality of blowing rotor assemblies.

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