Gas turbine components and method for machining gas turbine components
The present technology relates to the problem that during diverse machining steps of application to the production or reconditioning of internally cooled gas turbine blades, an undesired effect may be had on sections of the gas turbine blades and proposes, as an improvement, to inject the cavity of...
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Main Author | |
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Format | Patent |
Language | English |
Published |
30.11.2010
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Subjects | |
Online Access | Get full text |
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Summary: | The present technology relates to the problem that during diverse machining steps of application to the production or reconditioning of internally cooled gas turbine blades, an undesired effect may be had on sections of the gas turbine blades and proposes, as an improvement, to inject the cavity of the gas turbine blades before the machining steps with a plastic material which can be removed without trace, such as polystyrene, which can be subsequently removed again, in particular by heat. |
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Bibliography: | Application Number: US20080196626 |