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:
Mar. 19, 2024

Filed:

Nov. 02, 2021
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Paul Ghislain Albert Levisse, Moissy-Cramayel, FR;

Olivier Belmonte, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/36 (2006.01); F01D 25/18 (2006.01); F02C 3/06 (2006.01);
U.S. Cl.
CPC ...
F02C 7/36 (2013.01); F01D 25/183 (2013.01); F02C 3/06 (2013.01); F05D 2220/323 (2013.01); F05D 2230/70 (2013.01); F05D 2240/55 (2013.01); F05D 2240/60 (2013.01); F05D 2260/40 (2013.01); F05D 2260/98 (2013.01);
Abstract

An aircraft turbomachine having a longitudinal axis includes a high-pressure (HP) body, a low-pressure (LP) body, a fan, and a reduction gear having an epicyclic gear train. The turbomachine includes three modules: a first module having the LP turbine and the LP shaft, a second module having the LP compressor and a journal secured to the rotor of the LP compressor, and a third module having an input shaft of the reduction gear, this input shaft having an upstream end for coupling to a sun gear of the reduction gear and a downstream end comprising first splines that are oriented parallel to the axis and are configured to be engaged in second complementary splines of said second module.


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