The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Aug. 15, 2023

Filed:

Nov. 02, 2018
Applicant:

Textron Systems Corporation, Hunt Valley, MD (US);

Inventors:

Sean Marshall Baity, Westminster, MD (US);

David D. Billingsley, Seven Valleys, PA (US);

Brad S. Galloway, Seven Valleys, PA (US);

Richard M. Chapman, Madison, WI (US);

Assignee:

Textron Systems Corporation, Hunt Valley, MD (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 29/00 (2006.01); B64C 39/10 (2006.01); B64C 1/26 (2006.01); B64C 11/44 (2006.01); B64C 11/46 (2006.01); B64C 39/02 (2023.01); B64D 27/24 (2006.01); G05D 1/08 (2006.01);
U.S. Cl.
CPC ...
B64C 29/0033 (2013.01); B64C 39/10 (2013.01); B64C 1/26 (2013.01); B64C 11/44 (2013.01); B64C 11/46 (2013.01); B64C 39/024 (2013.01); B64C 2039/105 (2013.01); B64C 2201/021 (2013.01); B64C 2201/024 (2013.01); B64C 2201/028 (2013.01); B64C 2201/042 (2013.01); B64C 2201/088 (2013.01); B64C 2201/104 (2013.01); B64C 2201/108 (2013.01); B64C 2201/165 (2013.01); B64C 2211/00 (2013.01); B64D 27/24 (2013.01); G05D 1/0858 (2013.01);
Abstract

An aircraft includes an airframe having a fixed-wing section and a plurality of articulated electric rotors, at least some of which are variable-position rotors having different operating configurations based on rotor position. A first operating configuration is a vertical-flight configuration in which the rotors generate primarily vertical thrust for vertical flight, and a second operating configuration is a horizontal-flight configuration in which the rotors generate primarily horizontal thrust for horizontal fixed-wing flight. Control circuitry independently controls rotor thrust and rotor orientation of the variable-position rotors to provide thrust-vectoring maneuvering. The fixed-wing section may employ removable wing panels so the aircraft can be deployed both in fixed-wing and rotorcraft configurations for different missions.


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