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:
Dec. 21, 2021

Filed:

Aug. 21, 2018
Applicant:

Siemens Energy, Inc., Orlando, FL (US);

Inventors:

Kazim Ozbaysal, Charlotte, NC (US);

Ahmed Kamel, Orlando, FL (US);

Assignee:

Siemens Energy, Inc., Orlando, FL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B22F 5/04 (2006.01); B22F 7/06 (2006.01); B23K 1/00 (2006.01); B23K 35/30 (2006.01); B23P 6/00 (2006.01); B23K 35/02 (2006.01); B23K 101/00 (2006.01); B23K 1/20 (2006.01); B33Y 80/00 (2015.01);
U.S. Cl.
CPC ...
B22F 5/04 (2013.01); B22F 7/062 (2013.01); B23K 1/0004 (2013.01); B23K 1/0018 (2013.01); B23K 35/0244 (2013.01); B23K 35/304 (2013.01); B23P 6/005 (2013.01); B22F 2007/068 (2013.01); B23K 1/20 (2013.01); B23K 2101/001 (2018.08); B33Y 80/00 (2014.12);
Abstract

A method of repairing an airfoil is provided. The method includes providing an airfoil with a damaged section and removing the damaged section by machining or cutting an upper section of the airfoil. A replacement section is configured to mate with an upper surface of the airfoil. A presintered preform is provided to join the airfoil and the replacement sections through a resistance brazing process. The presintered preform is configured to mate with the upper surface of the airfoil and a lower surface of the replacement section and inserted between this upper surface and lower surface, creating a stacked airfoil comprising three mated sections in abutting contact. The stacked airfoil is resistance brazed such that only the braze material of the presintered preform melts and the upper surface of the airfoil and the lower surface of the replacement section remain below the grain boundary temperature of the material of the airfoil.


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