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:
Apr. 28, 2020

Filed:

Aug. 31, 2018
Applicants:

Rolls-royce Corporation, Indianapolis, IN (US);

Rolls-royce North American Technologies Inc., Indianapolis, IN (US);

Inventors:

Aaron D. Sippel, Zionsville, IN (US);

Ted J. Freeman, Danville, IN (US);

Loic Fabries, West Lafayette, IN (US);

Assignees:

Rolls-Roye Corporation, Indianapolis, IN (US);

Rolls-Royce North American Technologies Inc., Indianapolis, IN (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/30 (2006.01); F04D 29/32 (2006.01); F01D 11/00 (2006.01); B23P 15/00 (2006.01);
U.S. Cl.
CPC ...
F01D 5/3069 (2013.01); B23P 15/006 (2013.01); F01D 5/3038 (2013.01); F01D 11/008 (2013.01); F04D 29/322 (2013.01); F05D 2220/323 (2013.01); F05D 2230/60 (2013.01); F05D 2240/30 (2013.01); F05D 2240/80 (2013.01); Y10T 29/49321 (2015.01);
Abstract

A wheel assembly for a gas turbine engine includes a disk, a plurality of blades, and a plurality of platforms. The disk is configured to rotate about an axis during operation of the gas turbine engine. The blades each include a circumferentially extending attachment feature that is received in the disk. The platforms each have an axially extending attachment feature that is received in the disk.


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