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:
May. 19, 2015

Filed:

Jun. 06, 2012
Applicant:

John David Ward, Woodruff, SC (US);

Inventor:

John David Ward, Woodruff, SC (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G01L 1/22 (2006.01); G01N 29/04 (2006.01); G01N 3/08 (2006.01); F01D 21/00 (2006.01); F01D 21/12 (2006.01); G01M 15/14 (2006.01);
U.S. Cl.
CPC ...
G01N 3/08 (2013.01); F01D 21/003 (2013.01); F01D 21/12 (2013.01); G01M 15/14 (2013.01); F05D 2260/81 (2013.01); F05D 2260/83 (2013.01);
Abstract

A method and system for determining creep capability of turbine components is provided. A plurality of turbine components are manufactured from a material having known creep characteristics. Each of the plurality of turbine components is subjected to at least one of tensile stress, centrifugal stress and thermal stress, until a measurable amount of creep is acquired. The turbine components so tested are compared against known creep characteristics for the material used in the components. Components exhibiting an amount of creep greater than a predefined amount of creep will be separated from the plurality of turbine components and not placed into service.


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