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:
Jul. 29, 2025

Filed:

Nov. 08, 2021
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Christophe Paul Jacquemard, Moissy-Cramayel, FR;

Xavier Jean Yves Alain Agneray, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/02 (2006.01); F02C 7/36 (2006.01); F16C 3/02 (2006.01);
U.S. Cl.
CPC ...
F01D 5/026 (2013.01); F02C 7/36 (2013.01); F05D 2240/60 (2013.01); F05D 2260/31 (2013.01); F16C 3/023 (2013.01); F16C 2360/23 (2013.01);
Abstract

Disclosed is a main shaft for an aircraft turbine engine drive line extending longitudinally from front to rear along an axis and having a rear portion configured for receiving a front portion of a rear shaft by interlocking, the main shaft having: —a front retaining member and a rear retaining member together defining a prison and each having a central opening, —a connecting ring, located in the prison, having a rear end configured to be screwed to a front end of the rear shaft extending into the central opening of the rear retaining member, the connecting ring having a gripping member formed on the inner surface and accessible from a front portion of the main shaft by a tool extending via the central opening of the front retaining member.


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