Change in the Microstructure of Ni Alloy Disk Workpieces for Gas Turbine Engines Produced by the HIP + Deformation Method


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Abstract

Abstract—The changes in the microstructure during thermomechanical treatment under different regimes of a new granulated heat-resistant alloy based on VZh178P nickel obtained by the method of hot isostatic pressing and subsequent hot deformation (HIP + deformation) are studied. The change in the grain size of the γ matrix after the main operations of the technological conversion is shown; the dynamics of their growth in hardening below and above the temperature of total dissolution of the γ' phase and the microstructure after the total thermal treatment are shown.

About the authors

A. A. Shestakova

All-Russian Scientific Research Institute of Aviation Materials

Author for correspondence.
Email: lab3@viam.ru
Russian Federation, Moscow

M. N. Letnikov

All-Russian Scientific Research Institute of Aviation Materials

Email: lab3@viam.ru
Russian Federation, Moscow

M. M. Bakradze

All-Russian Scientific Research Institute of Aviation Materials

Email: lab3@viam.ru
Russian Federation, Moscow

M. V. Bubnov

All-Russian Scientific Research Institute of Aviation Materials

Email: lab3@viam.ru
Russian Federation, Moscow

A. V. Skugorev

All-Russian Scientific Research Institute of Aviation Materials

Email: lab3@viam.ru
Russian Federation, Moscow


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