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:
Jun. 02, 2020

Filed:

Dec. 03, 2014
Applicants:

Lei Chen, South Windsor, CT (US);

Zhiwei Yang, South Windsor, CT (US);

William J. Brindley, Hebron, CT (US);

Monika D. Kinstler, Manchester, CT (US);

Bruce R. Saxton, West Suffield, CT (US);

Inventors:

Lei Chen, South Windsor, CT (US);

Zhiwei Yang, South Windsor, CT (US);

William J. Brindley, Hebron, CT (US);

Monika D. Kinstler, Manchester, CT (US);

Bruce R. Saxton, West Suffield, CT (US);

Assignee:

RAYTHEON TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/28 (2006.01); C25D 5/50 (2006.01); C25D 3/66 (2006.01); C25D 3/56 (2006.01); C22C 19/05 (2006.01); C25D 3/12 (2006.01); C25D 5/40 (2006.01); C25D 7/00 (2006.01); F01D 9/02 (2006.01); F01D 25/00 (2006.01); C25D 5/18 (2006.01);
U.S. Cl.
CPC ...
F01D 5/288 (2013.01); C22C 19/058 (2013.01); C25D 3/12 (2013.01); C25D 3/562 (2013.01); C25D 3/665 (2013.01); C25D 5/40 (2013.01); C25D 5/50 (2013.01); C25D 7/00 (2013.01); F01D 9/02 (2013.01); F01D 25/005 (2013.01); F01D 25/007 (2013.01); C25D 5/18 (2013.01); F05D 2220/30 (2013.01); F05D 2230/30 (2013.01); F05D 2230/80 (2013.01); F05D 2230/90 (2013.01); F05D 2300/132 (2013.01); F05D 2300/175 (2013.01); F05D 2300/177 (2013.01);
Abstract

A nickel-chromium (Ni—Cr) alloy and a method for electrodepositing the Ni—Cr alloy on a turbine engine component for dimensionally restoring the engine component are described. The engine component is restored by re-building wall thickness with the Ni—Cr alloy including from 2 to 50 wt % chromium balanced with nickel. The turbine component coated with the Ni—Cr alloy is heat-treated at a high temperature to homogenize composition of the alloy to mimic the base alloy and to restore materials lost during repair of the turbine component.


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