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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Main Authors | , |
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Format | Patent |
Language | English |
Published |
23.10.2012
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Subjects | |
Online Access | Get full text |
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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. |
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Bibliography: | Application Number: US20080969647 |