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:
May. 30, 2023

Filed:

Dec. 20, 2018
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Arnaud Nicolas Negri, Moissy-Cramayel, FR;

Julien Fabien Patrick Becoulet, Moissy-Cramayel, FR;

Michel Gilbert Roland Brault, Moissy-Cramayel, FR;

Guillaume Patrice Kubiak, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16D 1/10 (2006.01); F01D 5/02 (2006.01); F02C 7/36 (2006.01);
U.S. Cl.
CPC ...
F16D 1/101 (2013.01); F01D 5/026 (2013.01); F02C 7/36 (2013.01); F16D 2001/103 (2013.01);
Abstract

A shaft assembly () for an aircraft turbine engine (), comprising a first outer shaft () and a second inner shaft (), the first outer shaft being intended to be engaged axially on the second shaft and comprising inner longitudinal splines () for coupling with outer longitudinal splines () of the second shaft, characterised in that, when the first and second shafts are in the coupling position, the inner and outer splines are engaged in one another and cooperate with each other in an axial coupling area (Z), the inner and outer teeth being situated outside this coupling area.


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