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. 17, 2023

Filed:

Sep. 09, 2021
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Mateusz Kesek, Debica, PL;

Wojciech Durak, Rzeszow, PL;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/02 (2006.01); F02C 6/20 (2006.01); F02C 7/06 (2006.01); F02C 7/36 (2006.01); F16D 1/076 (2006.01);
U.S. Cl.
CPC ...
F01D 5/025 (2013.01); F01D 5/026 (2013.01); F02C 6/206 (2013.01); F02C 7/06 (2013.01); F02C 7/36 (2013.01); F16D 1/076 (2013.01); F05D 2220/325 (2013.01); F05D 2240/61 (2013.01);
Abstract

An apparatus for a gas turbine engine includes a shaft base, a flange and a plurality of lobes. The shaft base extends axially along an axis between a shaft first end and a shaft second end. The flange is connected to the shaft base at the shaft first end. The flange projects radially out from the shaft base. The flange includes a plurality of fastener apertures, and the fastener apertures include a first fastener aperture. The lobes are arranged circumferentially about the axis. Each of the lobes is connected to and projects radially away from the shaft base. Each of the lobes is connected to and projects axially out from the flange. The lobes include a first lobe and a second lobe. The first fastener aperture is arranged circumferentially between the first lobe and the second lobe. The second lobe radially overlaps the first fastener aperture.


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