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:
Sep. 26, 2017

Filed:

Nov. 18, 2014
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Zhaoli Hu, Greer, SC (US);

Abe Denis Darling, Laurens, SC (US);

Shamgar Elijah McDowell, Simpsonville, SC (US);

Douglas Anthony Serieno, Simpsonville, SC (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B23K 26/14 (2014.01); B23K 26/16 (2006.01); B23K 26/384 (2014.01); B23K 26/382 (2014.01); B23K 26/142 (2014.01); B23K 101/00 (2006.01);
U.S. Cl.
CPC ...
B23K 26/389 (2015.10); B23K 26/142 (2015.10); B23K 2201/001 (2013.01); F05D 2230/13 (2013.01);
Abstract

A system for forming a cooling hole in an airfoil includes a liquid-jet guided laser. The liquid-jet guided laser generates a laser beam confined within a fluid column. The fluid column/laser beam is directed at an outer surface of the airfoil. The system also includes a purge medium supply that is fluidly coupled to an aperture of the airfoil. The purge medium supply provides a purge medium into an inner cavity of the airfoil. The purge medium flow is oriented to flow in a flow direction that is substantially parallel to an inner surface of the cavity. A cooling hole is formed in the airfoil and extends through the outer surface and penetrates the inner surface of the cavity. A centerline of the cooling hole forms an acute angle with respect to the purge medium flow direction. The system described herein provides a method for manufacturing an airfoil.


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