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. 02, 2018

Filed:

Aug. 12, 2015
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Jacob Andrew Salm, Mauldin, SC (US);

Mark Carmine Bellino, Greenville, SC (US);

James Ryan Connor, Greenville, SC (US);

Gareth William David Lewis, Greenville, SC (US);

Keith Alan Lord, Taylors, SC (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/00 (2006.01); G05B 19/4099 (2006.01); G05B 15/02 (2006.01); B23P 6/00 (2006.01);
U.S. Cl.
CPC ...
F01D 5/005 (2013.01); G05B 15/02 (2013.01); G05B 19/4099 (2013.01); B23P 6/007 (2013.01); F05D 2220/30 (2013.01); F05D 2230/30 (2013.01); F05D 2230/80 (2013.01); G05B 2219/35128 (2013.01); G05B 2219/45147 (2013.01);
Abstract

A system for adaptively machining a shroud of a blade used in a turbomachine is provided. The system may include a computer system including a module(s) configured to: extract geometric location data from a 3D model of the shroud after use in the turbomachine, the 3D model created by digitizing using a digitizing device. The geometric location data includes geometric location data of a hard face plane of the shroud exposed to wear during turbomachine operation and of a non-worn surface adjacent to the hard face plane substantially unexposed to wear during turbomachine operation. Comparing the geometric location data of the non-worn surface from the three-dimensional model to a manufacturing model of the blade determines a change in position of the non-worn surface from use of the blade in the turbomachine. The change in position is used to modify a machining instruction used by a machining device to repair the hard face plane.


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