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:
Jan. 11, 2022

Filed:

Dec. 03, 2019
Applicants:

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

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

Inventors:

Shaling Starr, McCordsville, IN (US);

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

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

David J. Thomas, Brownsburg, IN (US);

Assignees:

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

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 11/08 (2006.01); F01D 25/24 (2006.01); F01D 11/00 (2006.01); F01D 25/00 (2006.01);
U.S. Cl.
CPC ...
F01D 25/246 (2013.01); F01D 11/08 (2013.01); F01D 11/005 (2013.01); F01D 25/005 (2013.01); F05D 2220/323 (2013.01); F05D 2230/60 (2013.01); F05D 2240/11 (2013.01); F05D 2260/30 (2013.01); F05D 2300/6033 (2013.01);
Abstract

A turbine shroud assembly includes a carrier, a blade track segment, and an attachment pin. The carrier is arranged to extend circumferentially at least partway around an axis. The blade track segment includes a runner that faces the axis to define a portion of a primary gas path of the gas turbine engine and an attachment flange that extends radially away from the runner. The attachment pin is configured to mount the blade track segment to the carrier.


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