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:
Oct. 07, 2025

Filed:

Apr. 02, 2024
Applicant:

Textron Innovations Inc., Providence, RI (US);

Inventors:

Jonathan Andrew Knoll, Burleson, TX (US);

George Matthew Thompson, Lewisville, TX (US);

Charles Hubert Speller, Flower Mound, TX (US);

Grant Michael Beall, Arlington, TX (US);

Assignee:

Textron Innovations Inc., Providence, RI (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 29/00 (2006.01); B64C 27/28 (2006.01); B64U 30/297 (2023.01); B64U 50/19 (2023.01);
U.S. Cl.
CPC ...
B64C 29/0033 (2013.01); B64C 27/28 (2013.01); B64U 30/297 (2023.01); B64U 50/19 (2023.01);
Abstract

A rotor system for an aircraft includes a rotor assembly comprising a plurality of rotor blades connected to a rotor mast, wherein the rotor assembly is tiltable relative to a wing of the aircraft between a first position corresponding to an airplane mode of the aircraft and a second position corresponding to a helicopter mode of the aircraft; and a drive system for providing rotational energy to the rotor assembly via the rotor mast. The drive system includes at least one electric motor for generating rotational energy to a motor shaft; and a gearbox connected to receive rotational energy from the at least one electric motor via the motor shaft and to provide rotational energy to the rotor mast via a rotor shaft, wherein the at least one electric motor is fixed relative to the wing of the aircraft.


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