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. 06, 2022

Filed:

Apr. 16, 2019
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Wangen Lin, S. Glastonbury, CT (US);

Gary J. Larson, Madison, CT (US);

Giovanni Whitman, Berlin, CT (US);

Scott Poeppel, New Hartford, CT (US);

Joseph Wilson, Granby, CT (US);

Assignee:

Raytheon Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B23K 26/342 (2014.01); F01D 5/00 (2006.01); F01D 9/04 (2006.01); B23P 6/00 (2006.01); B23K 26/32 (2014.01); B22F 5/00 (2006.01); B22F 7/06 (2006.01); B23K 26/144 (2014.01); F01D 25/24 (2006.01); B23K 101/00 (2006.01); C21D 9/50 (2006.01); B23K 103/08 (2006.01); C22C 19/05 (2006.01);
U.S. Cl.
CPC ...
B23K 26/342 (2015.10); B22F 5/009 (2013.01); B22F 7/062 (2013.01); B23K 26/144 (2015.10); B23K 26/32 (2013.01); B23P 6/007 (2013.01); F01D 5/005 (2013.01); F01D 9/041 (2013.01); F01D 25/24 (2013.01); B22F 2007/068 (2013.01); B22F 2999/00 (2013.01); B23K 2101/001 (2018.08); B23K 2103/08 (2018.08); C21D 9/50 (2013.01); C22C 19/057 (2013.01); F05D 2220/32 (2013.01); F05D 2230/10 (2013.01); F05D 2230/21 (2013.01); F05D 2230/31 (2013.01); F05D 2230/80 (2013.01); F05D 2300/17 (2013.01); F05D 2300/175 (2013.01); F05D 2300/177 (2013.01);
Abstract

A method of reworking an aerospace component includes removing a casting defect from a component manufactured of a non-fusion weldable base alloy to form a cavity. The cavity is then at least partially filled with a multiple of layers of discrete laser powder deposition spots of a filler alloy. A cast component for a gas turbine engine includes a cast component non-fusion weldable base alloy with a cavity filled with a multiple of layers of laser powder deposition spots of a filler alloy. The filler alloy may be different than the non-fusion weldable base alloy. A layer of non-fusion weldable base alloy is at least partially within the cavity and over the filler alloy.


Find Patent Forward Citations

Loading…