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:
Jul. 17, 2018

Filed:

Sep. 05, 2013
Applicant:

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

Inventors:

Trevor John Totten, Avon, IN (US);

Jonathan Michael Rivers, Indianapolis, IN (US);

Eric William Engebretsen, Zionsville, IN (US);

Matthew Joseph Kappes, Indianapolis, IN (US);

Assignee:

ROLLS-ROYCE CORPORATION, Indianapolis, IN (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/24 (2006.01); F01D 21/04 (2006.01); F01D 11/12 (2006.01); F02K 3/06 (2006.01);
U.S. Cl.
CPC ...
F01D 25/24 (2013.01); F01D 21/045 (2013.01); F01D 11/122 (2013.01); F02K 3/06 (2013.01); F05D 2220/36 (2013.01); F05D 2250/283 (2013.01); F05D 2300/702 (2013.01); Y02T 50/672 (2013.01);
Abstract

A containment system for a gas turbine engine includes a fan track assembly for use with a containment case. The fan track assembly includes a body of collapsible material that is positioned within a cavity of the fan case, and voids are provided for providing space in the event of a catastrophic blade failure. Various configurations of the fan track liner assembly are provided along with various mounting methodologies for securing the track liner assembly to the fan case of a gas turbine engine.


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