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. 16, 2018

Filed:

Jan. 06, 2016
Applicant:

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

Inventors:

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

Jun Shi, Carmel, IN (US);

Emil R. DeJulio, Columbus, IN (US);

Assignee:

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 11/08 (2006.01); F16J 15/08 (2006.01); F01D 11/12 (2006.01); F01D 11/18 (2006.01); F01D 11/00 (2006.01);
U.S. Cl.
CPC ...
F01D 11/08 (2013.01); F01D 11/005 (2013.01); F01D 11/12 (2013.01); F01D 11/18 (2013.01); F16J 15/0887 (2013.01); F05D 2220/32 (2013.01); F05D 2230/60 (2013.01); F05D 2240/11 (2013.01); F05D 2240/24 (2013.01); F05D 2240/55 (2013.01); F05D 2250/75 (2013.01); F05D 2260/20 (2013.01); F05D 2300/20 (2013.01); F05D 2300/50212 (2013.01); F05D 2300/6033 (2013.01); Y02T 50/672 (2013.01);
Abstract

A turbine shroud for use in a gas turbine engine that includes a metallic carrier, a blade track, and a seal is disclosed. The seal is engaged with surfaces of the metallic carrier and the blade track to block ingress of hot gasses at the interface of the blade track and the metallic carrier.


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