V. Sh. Sufiiarov

TL;DR: In this article, it is shown that transitions in microstructure, texture, and properties in fabricated Inconel 718 functionally graded components can be obtained at relatively small or large length scales, depending upon the functional gradient desired in a particular application.

TL;DR: In this article, the microstructural design of Inconel 718 specimens produced by selective laser melting (SLM) was adjusted through process parameters manipulation and post-process heat treatment, and the effects of heat treatment on microstructure, process induced defects, deformation behaviour and failure mechanisms were studied.

TL;DR: In this article, the correlation between powder layer thickness and relative density, microstructure and mechanical properties of nickel-based superalloy produced by selective laser melting is presented, and it is shown that the size of columnar dendritic cells depends on the layer thickness used during SLM.

TL;DR: In this paper, the results of an evaluation of mechanical properties of the samples made of Ti-6Al-4V and VT6 titanium-based alloys and Inconel 718 refractory nickel alloy in various directions are presented.

TL;DR: Inconel 718 is a nickel-based superalloy commonly used in aircraft engine and nuclear applications, where components experience severe mechanical stresses Due to the typical high temperature applications, Thermo-Mechanical Fatigue (TMF) and creep tests are common benchmarks for such applications.