Effect of hot isostatic pressing on the microstructure of turbine blade airfoil made of nickel-base superalloy

Chmiela B.; Kościelniak B.; Cwajna J.

doi:10.1515/amm-2017-0036

Archives of Metallurgy and Materials (Mar 2017)

Effect of hot isostatic pressing on the microstructure of turbine blade airfoil made of nickel-base superalloy

Chmiela B.,
Kościelniak B.,
Cwajna J.

Affiliations

Chmiela B.: Silesian University of Technology, Faculty of Materials Engineering and Metallurgy, Institute of Materials Science, 8 Krasinskiego Str., 40-019 Katowice, Poland
Kościelniak B.: Silesian University of Technology, Faculty of Materials Engineering and Metallurgy, Institute of Materials Science, 8 Krasinskiego Str., 40-019 Katowice, Poland
Cwajna J.: Silesian University of Technology, Faculty of Materials Engineering and Metallurgy, Institute of Materials Science, 8 Krasinskiego Str., 40-019 Katowice, Poland

DOI: https://doi.org/10.1515/amm-2017-0036
Journal volume & issue: Vol. 62, no. 1
pp. 241 – 245

Abstract

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Turbine blades are flight safety parts in the jet engine. Therefore they should be characterized by very good mechanical properties, especially high creep resistance and fatigue strength at high temperature. The mechanical properties of blades made of nickel-based superalloys depend on the microstructure of the casting and its porosity [1,2].

Published in Archives of Metallurgy and Materials

ISSN: 2300-1909 (Online)
Publisher: Polish Academy of Sciences
Country of publisher: Poland
LCC subjects: Technology: Mining engineering. Metallurgy; Technology: Electrical engineering. Electronics. Nuclear engineering: Materials of engineering and construction. Mechanics of materials
Website: https://journals.pan.pl/amm

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