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:
Oct. 21, 2025

Filed:

Sep. 16, 2022
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Mateusz Kesek, Nagawczyna, PL;

Tomasz Rozputynski, Hyżne, PL;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16C 3/02 (2006.01); F16D 1/076 (2006.01); B64C 11/02 (2006.01);
U.S. Cl.
CPC ...
F16C 3/023 (2013.01); F16D 1/076 (2013.01); B64C 11/02 (2013.01); F16B 2200/506 (2018.08);
Abstract

A propeller shaft assembly for an aircraft engine includes a shaft having a bore extending through the shaft at a front end thereof, the front end of the shaft having an outer surface facing radially outwardly from the shaft and an inner surface spaced apart from the outer surface and facing radially inwardly to the bore. The shaft has a front flange extending radially outwardly on the outer surface, the front flange having a base merging with the outer surface of the shaft. A sleeve is coupled to the shaft within the bore by an interference fit between the sleeve and the shaft, at least part of the sleeve axially aligned with the front flange. The sleeve axially extends from a front to a rear sleeve end, the rear sleeve end axially offset from the engine side surface of the front flange at the base of the front flange.


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