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:
Jan. 06, 2026

Filed:

Jan. 30, 2024
Applicant:

Safran Transmission Systems, Colombes, FR;

Inventors:

Maxime Fernandez, Moissy-Cramayel, FR;

Yohan Douy, Moissy-Cramayel, FR;

Boris Pierre Marcel Morelli, Moissy-Cramayel, FR;

Jordane Emile André Peltier, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/36 (2006.01); B64C 11/30 (2006.01); B64D 35/024 (2025.01); F01D 15/10 (2006.01); F16H 1/22 (2006.01);
U.S. Cl.
CPC ...
F02C 7/36 (2013.01); B64C 11/306 (2013.01); B64D 35/024 (2024.01); F01D 15/10 (2013.01); F16H 1/22 (2013.01); F05D 2260/4031 (2013.01);
Abstract

An aircraft turbomachine includes a speed reduction gear having an input pinion connected to a power shaft and an output pinion connected to a propeller shaft. An electric machine is integrated into the speed reduction gear and is configured to provide electrical power to the propeller shaft or to take mechanical power from the propeller shaft. The electric machine has a rotor driven in rotation about an axis coaxial with a longitudinal axis of the turbomachine and a stator connected to a casing. The input pinion includes an input shaft offset from an axis of the output pinion, and the speed reduction gear has two parallel intermediate transmission lines configured to transmit the torque from the input pinion to the output pinion to drive the rotor in rotation.


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