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. 10, 2024

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:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 35/025 (2024.01); B64C 11/48 (2006.01); B64C 27/12 (2006.01); F02C 7/36 (2006.01); B64D 35/022 (2024.01); F01D 15/12 (2006.01); F02C 7/32 (2006.01); F02K 5/00 (2006.01);
U.S. Cl.
CPC ...
F02C 7/36 (2013.01); B64C 11/48 (2013.01); B64C 27/12 (2013.01); B64D 35/022 (2024.01); B64D 35/025 (2024.01); F01D 15/12 (2013.01); F02C 7/32 (2013.01); F02K 5/00 (2013.01);
Abstract

The disclosure relates to an assembly for an aircraft turbomachine, having a speed reduction gear comprising an input pinion connected to a power shaft of the turbomachine and an output pinion connected to a propeller shaft of the turbomachine. According to the disclosure, the assembly includes two electric machines which are each configured to provide electrical power to the propeller shaft or to draw mechanical power from the propeller shaft, each electric machine comprising a rotor and a stator, the stator configured to be connected to a casing of the turbomachine. The speed reduction gear can include two substantially parallel intermediate transmission lines configured to transmit the torque from the input pinion to the output pinion, each rotor being driven in rotation respectively by a pinion of an intermediate line.


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