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:
Mar. 26, 2024

Filed:

Nov. 13, 2019
Applicant:

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

Inventors:

Anand A. Kulkarni, Charlotte, NC (US);

Kazim Ozbaysal, Charlotte, NC (US);

Ahmed Kamel, Orlando, FL (US);

Kyle I. Stoodt, Charlotte, NC (US);

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/28 (2006.01); B22F 1/10 (2022.01); B22F 3/10 (2006.01); B22F 3/26 (2006.01); B22F 5/04 (2006.01); B22F 10/16 (2021.01); B22F 10/18 (2021.01); B22F 10/38 (2021.01); B22F 10/40 (2021.01); B22F 10/68 (2021.01); B23K 1/00 (2006.01); B23K 35/30 (2006.01); B23K 101/00 (2006.01); B23P 6/00 (2006.01); C22C 19/05 (2006.01); F01D 5/00 (2006.01); F01D 25/00 (2006.01);
U.S. Cl.
CPC ...
F01D 5/28 (2013.01); B22F 1/10 (2022.01); B22F 3/1021 (2013.01); B22F 3/26 (2013.01); B22F 5/04 (2013.01); B22F 10/16 (2021.01); B22F 10/18 (2021.01); B22F 10/38 (2021.01); B23K 1/0018 (2013.01); B23K 35/3033 (2013.01); B23P 6/005 (2013.01); C22C 19/058 (2013.01); F01D 5/005 (2013.01); F01D 25/005 (2013.01); B22F 10/40 (2021.01); B22F 10/68 (2021.01); B22F 2301/15 (2013.01); B23K 2101/001 (2018.08); F05D 2230/237 (2013.01); F05D 2230/64 (2013.01); F05D 2230/80 (2013.01);
Abstract

A blade for a gas turbine includes a removed portion space, and further includes an airfoil portion defining the removed portion space, the airfoil portion formed from a base material, and a replacement component formed to fill the removed portion space. The replacement component is formed from a material that includes 50%-80% base material, 0%-30% braze material, and 0%-8% aluminum. A braze joint is formed between the airfoil portion and the replacement component to attach the replacement component to the airfoil portion and fill the removed portion space.


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