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. 02, 2019

Filed:

Feb. 03, 2016
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Herbert Chidsey Roberts, Middletown, OH (US);

David Scott Diwinsky, West Chester, OH (US);

Wayne R. Grady, Hamilton, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B23P 6/04 (2006.01); B23K 26/03 (2006.01); B23K 26/08 (2014.01); F01D 5/00 (2006.01); B23K 26/342 (2014.01); B23K 26/70 (2014.01); B23K 26/144 (2014.01); B23K 101/00 (2006.01); B23K 103/18 (2006.01);
U.S. Cl.
CPC ...
F01D 5/005 (2013.01); B23K 26/032 (2013.01); B23K 26/0884 (2013.01); B23K 26/144 (2015.10); B23K 26/342 (2015.10); B23K 26/702 (2015.10); B23P 6/045 (2013.01); B23K 2201/001 (2013.01); B23K 2203/26 (2015.10); F05D 2230/80 (2013.01); F05D 2230/90 (2013.01); F05D 2260/83 (2013.01);
Abstract

A method for remotely stopping a crack in a component of a gas turbine engine is provided. The method can include inserting an integrated repair interface attached to a cable delivery system within a gas turbine engine; positioning the tip adjacent to a defect within a surface of the component; temporarily attaching the tip adjacent to the defect within the surface on the component; supplying a new material to the area to fill the defect; and heating the new material to fuse the new material to the component within the defect.


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