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:
Feb. 27, 2018

Filed:

Aug. 17, 2015
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Matthew Troy Hafner, Honea Path, SC (US);

Victor John Morgan, Simpsonville, SC (US);

Frederic Woodrow Roberts, Simpsonville, SC (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 11/22 (2006.01); F01D 25/04 (2006.01); F01D 25/00 (2006.01); F01D 25/08 (2006.01); F01D 11/20 (2006.01); F01D 11/14 (2006.01);
U.S. Cl.
CPC ...
F01D 11/22 (2013.01); F01D 11/20 (2013.01); F01D 25/005 (2013.01); F01D 25/04 (2013.01); F01D 25/08 (2013.01); F01D 11/14 (2013.01); F05D 2220/32 (2013.01); F05D 2240/11 (2013.01); F05D 2260/52 (2013.01); F05D 2260/96 (2013.01); F05D 2300/17 (2013.01); F05D 2300/171 (2013.01); F05D 2300/502 (2013.01); F05D 2300/6033 (2013.01);
Abstract

A turbine shroud assembly is disclosed including an inner shroud having a surface adjacent to a hot gas path, an outer shroud, a damper block disposed between the inner shroud and the outer shroud, a first biasing apparatus, and a second biasing apparatus. The first biasing apparatus provides a first biasing force to the inner shroud, biasing the inner shroud a first deflection distance in a direction toward the hot gas path and away from the outer shroud. The second biasing apparatus provides a second biasing force to the damper block, biasing the damper block a second deflection distance in a direction toward the hot gas path and away from the outer shroud. The second deflection distance is greater than the first deflection distance.


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