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:
Jan. 30, 2024

Filed:

Feb. 10, 2023
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Samuel Panero, Montréal, CA;

Guy Lefebvre, Longueuil, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/00 (2006.01); B23P 6/00 (2006.01); B23K 26/21 (2014.01); B23K 15/00 (2006.01); B23K 101/00 (2006.01);
U.S. Cl.
CPC ...
F02C 7/00 (2013.01); B23K 15/0046 (2013.01); B23K 26/21 (2015.10); B23P 6/007 (2013.01); B23K 2101/001 (2018.08); F05D 2230/233 (2013.01); F05D 2230/234 (2013.01); F05D 2230/80 (2013.01);
Abstract

A method of repair for a metallic part of an aircraft engine includes detecting a defect inside a bore of the metallic part wherein the defect represents a departure from an intended geometry of the bore, the bore having a diameter and defining a longitudinal axis, and wherein the defect is located within the bore at a depth of at least greater than one diameter along the longitudinal axis. The method also includes measuring a geometry of the defect, preparing a patch with a complementary geometry to fill the geometry of the defect, placing the patch in the bore with the complementary geometry of the patch seated against the geometry of the defect, directing a welding beam from outside the bore, through the bore and onto the patch to weld the patch to the bore, and removing a portion of the patch to provide the intended geometry for the bore.


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