The Investigation of the Chemical Composition, Structure, and Mechanical Properties of EP648 Alloy at Different Stages of Additive Manufacturing


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Abstract

The chemical composition of a nickel heat-resistant alloy of the EP648 brand at different stages of additive manufacturing, as well as the structure and mechanical properties of the synthesized material in comparison with a material obtained via a traditional deformation method, is investigated. It is shown that the application of additive technologies in the manufacture of EP648 nickel heat-resistant alloy leads to a significant increase in the concentration of gases (O and N) in the alloy, formation of a fine-grain structure, and increased porosity. Here, an increase in the strength properties and a decrease in the impact strength, low cycle fatigue, and plasticity are characteristic of such a material. The time to failure of the synthesized specimens in a creep rupture test exceeds that of sheet specimens but is inferior to that of deformed bars.

About the authors

P. G. Min

All-Russian Scientific Research Institute of Aviation Materials

Author for correspondence.
Email: viamlab3@mail.ru
Russian Federation, Moscow, 105005

V. E. Vadeev

All-Russian Scientific Research Institute of Aviation Materials

Email: viamlab3@mail.ru
Russian Federation, Moscow, 105005

A. M. Rogalev

All-Russian Scientific Research Institute of Aviation Materials

Email: viamlab3@mail.ru
Russian Federation, Moscow, 105005

A. E. Knyazev

All-Russian Scientific Research Institute of Aviation Materials

Email: viamlab3@mail.ru
Russian Federation, Moscow, 105005


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