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:
Dec. 23, 2025

Filed:

Jun. 09, 2023
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Eric S. Durocher, Boucherville, CA;

Michel Labrecque, Ste-Julie, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 35/021 (2024.01); F16H 1/28 (2006.01); F16H 37/04 (2006.01); F16H 57/038 (2012.01); F16H 57/02 (2012.01);
U.S. Cl.
CPC ...
B64D 35/021 (2024.01); F16H 1/28 (2013.01); F16H 37/041 (2013.01); F16H 57/038 (2013.01); F16H 2001/2872 (2013.01); F16H 2057/02043 (2013.01);
Abstract

An assembly for a propulsion system of an aircraft includes a gearbox, at least one accessory load assembly, a propulsor, and an electric motor. The gearbox module includes a gear assembly and an output shaft. The gear assembly is connected to the output shaft. The at least one accessory load assembly includes at least one accessory load coupled to the output shaft. The propulsor is coupled to the output shaft. The electric motor includes a rotor. The rotor is coupled to the gear assembly to drive rotation of the output shaft about a rotational axis. The rotation of the output shaft drives rotation of the propulsor and the at least one accessory load for each accessory load assembly of the at least one accessory load assembly.


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