Development of reliability criteria for rotor blades and guide vanes of contemporary gas turbines
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Results are presented for development of reliability criteria with respect to the microstructural state for alloy IN 792 rotor blades and guide vanes. The effect of prolonged aging and high-temperature overheating lasting 1 h on alloy structure and properties are evaluated.
Keywords
gas turbine rotor blades guide vanes overheating operational aging reliability criteria microstructure γ′-phasePreview
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© Springer Science+Business Media, Inc. 2012