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. 31, 2019

Filed:

Dec. 22, 2016
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Richard Gordon Rollings, Greer, SC (US);

Kevin Leon Bruce, Greer, SC (US);

William Scott Zemitis, Simpsonville, SC (US);

Assignee:

GENERAL ELECTRIC COMPANY, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/22 (2006.01); B23P 6/00 (2006.01); F01D 5/00 (2006.01);
U.S. Cl.
CPC ...
F01D 5/225 (2013.01); B23P 6/002 (2013.01); F01D 5/005 (2013.01); F05D 2230/10 (2013.01); F05D 2230/80 (2013.01); F05D 2240/11 (2013.01); F05D 2240/307 (2013.01); F05D 2250/192 (2013.01);
Abstract

A method for modifying an airfoil shroud located at a tip of an airfoil is provided. A locating step locates a reference location in a first end edge. The reference location includes a portion of a fillet. A seal rail extends circumferentially along a radially outer surface of the airfoil shroud. The fillet extends along the radially outer surface and is positioned directly adjacent to the seal rail. A forming step forms a compound relief cut in the fillet without performing a weld process on the airfoil shroud to remove the reference location. The compound relief cut has a first cut having a first radius extending from the seal rail towards the first end edge, and a second cut having a second radius extending from an end of the first cut to the first end edge. Modifying the airfoil shroud is complete following forming the compound relief cut.


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