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:
Jun. 04, 2024

Filed:

Sep. 16, 2022
Applicants:

Safran Aircraft Engines, Paris, FR;

Safran Transmission Systems, Colombes, FR;

Inventors:

Paul Ghislain Albert Levisse, Moissy-Cramayel, FR;

Julien Fabien Patrick Becoulet, Moissy-Cramayel, FR;

Guillaume Pierre Mouly, Moissy-Cramayel, FR;

Patrice Jocelyn Francis Gedin, Moissy-Cramayel, FR;

Olivier Belmonte, Moissy-Cramayel, FR;

Assignees:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/36 (2006.01); F16H 1/36 (2006.01);
U.S. Cl.
CPC ...
F02C 7/36 (2013.01); F16H 1/36 (2013.01); F05D 2220/323 (2013.01); F05D 2220/36 (2013.01); F05D 2260/40311 (2013.01);
Abstract

An aircraft turbine engine includes a turbine shaft having a first axis of rotation, a propulsion propeller having a second axis of rotation parallel to and spaced from the first axis, and a mechanical reduction gear coupled to the turbine shaft and rotating the propeller. The reduction gear has a sun gear connected to the turbine shaft, a ring gear, and at least two planet gears, each including a first external toothing that is meshed with an external toothing of the sun gear. A second external toothing is located within the ring gear and is meshed with an internal toothing of the ring gear.


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