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. 26, 2016

Filed:

Oct. 23, 2012
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Matthew Stephen Casavant, Greenville, SC (US);

Kenneth Damon Black, Travelers Rest, SC (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/20 (2006.01); F01D 9/02 (2006.01); F23R 3/00 (2006.01); F23R 3/60 (2006.01);
U.S. Cl.
CPC ...
F02C 7/20 (2013.01); F01D 9/023 (2013.01); F23R 3/002 (2013.01); F23R 3/005 (2013.01); F23R 3/60 (2013.01); F05D 2260/201 (2013.01); F23R 2900/00005 (2013.01); F23R 2900/00017 (2013.01); F23R 2900/03044 (2013.01);
Abstract

A deformable fastener assembly for use with a gas turbine engine. The deformable fastener may be used to fasten a component of the gas turbine that is subjected to high temperatures and thermal deformation, such as an impingement sleeve assembly, to a rigid portion, such as the inner turbine shell of the gas turbine engine. The deformable fastener assemblies may permit components to be fastened to a rigid portion of the gas turbine with a consistent load input to permit frictional transient sliding of the component relative to the rigid portion of the gas turbine engine.


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