Gas turbine components and method for machining gas turbine...

Metal working – Method of mechanical manufacture – Impeller making

Reexamination Certificate

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C219S121850, C427S259000, C416S09700R, C416S24100B, C416S232000

Reexamination Certificate

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07841084

ABSTRACT:
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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International Search Report corresponding to International Application Serial No. PCT/DE2007/000361, mailed Jul. 18, 2007.

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