Apparatus for rebuilding gas turbine engines

A method for repairing a turbine blade for a gas turbine engine is provided. The method includes securing the blade into a clamping fixture, obtaining a zero reference from a gauging surface on the clamping fixture, coupling the clamping fixture to a grinding machine, and grinding the blade based on...

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Bibliographic Details
Main Authors POWERS JOHN MATTHEW, DORREL BRIAN DUDLEY
Format Patent
LanguageEnglish
Published 23.10.2012
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Summary:A method for repairing a turbine blade for a gas turbine engine is provided. The method includes securing the blade into a clamping fixture, obtaining a zero reference from a gauging surface on the clamping fixture, coupling the clamping fixture to a grinding machine, and grinding the blade based on the zero reference.
Bibliography:Application Number: US20080969647