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. 26, 2026

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); F16D 1/02 (2006.01); F16D 1/08 (2006.01); F01D 5/02 (2006.01); F01D 5/06 (2006.01); F04D 29/044 (2006.01); F04D 29/054 (2006.01); F16D 1/10 (2006.01); F16D 3/18 (2006.01);
U.S. Cl.
CPC ...
F02C 7/36 (2013.01); F16D 1/02 (2013.01); F16D 1/087 (2013.01); F01D 5/026 (2013.01); F01D 5/06 (2013.01); F04D 29/044 (2013.01); F04D 29/054 (2013.01); F05D 2240/60 (2013.01); F05D 2240/61 (2013.01); F16D 2001/103 (2013.01); F16D 3/185 (2013.01);
Abstract

An aircraft turbomachine, including a first shaft having external splines oriented parallel to an axis of rotation of the shaft, a second shaft having internal splines complementary to the external splines, this second shaft being fitted axially on the first shaft and these shafts rotating as one by engagement of their splines, and a system for axially locking the shafts with respect to one another, wherein the system includes screws that are oriented radially with respect to the axis, each of these screws being screwed into a first orifice in one of the shafts and having a free end for engaging a second orifice in the other of the shafts.


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