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:
Aug. 09, 2016

Filed:

Jan. 16, 2014
Applicant:

Rolls-royce Plc, London, GB;

Inventors:

James Kell, Nottingham, GB;

Samantha Helen Davies, Manchester, GB;

Dragos Axinte, Nottingham, GB;

Mark Daine, Nottingham, GB;

Assignee:

ROLLS-ROYCE plc, Derby, GB;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B23P 6/00 (2006.01); F01D 5/00 (2006.01); B23K 26/36 (2014.01); B23K 26/40 (2014.01);
U.S. Cl.
CPC ...
B23P 6/002 (2013.01); B23K 26/0622 (2015.10); B23K 26/362 (2013.01); B23K 26/40 (2013.01); F01D 5/005 (2013.01); B23K 2201/001 (2013.01); B23K 2203/50 (2015.10); F05D 2230/13 (2013.01); F05D 2230/80 (2013.01); Y10T 29/49318 (2015.01);
Abstract

A repair method for repairing a component () of a gas turbine engine (). The method comprises first and second steps. The first step comprises directing an energy beam toward the component () to ablate a first region () of material to form a gap extending through the component () between a repair region () a base region () of the component, wherein subsequent to the first step the repair region () and base region () are joined by a connecting portion (). In the second step, an energy beam is direct toward the component () to ablate the repair region () to remove the repair region () from the component ().


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