Abstract

Microstructural changes of the Inconel 718 and ATI 718Plus® base materials and the fusion zone caused by the isothermal hold at 760 °C for up to 500 h were investigated. The evaluation was performed using a scanning electron microscope with backscattered electrons detector and scanning transmission electron microscopy supported by energy-dispersive x-ray spectroscopy. Furthermore, to evaluate the effect of microstructural changes on mechanical properties Vickers microhardness measurements were performed. Exposure of welded joint at high temperature led to coarsening and/or dissolution of main strengthening phases’ particles and nucleation and growth of plate-like precipitates. In the interdendritic region of the fusion zone, the transformation of the Laves phase to a complex cluster of precipitates contained σ phase had taken place. Analysis of microstructure and microhardness measurements showed that ATI 718Plus has better mechanical properties and microstructural stability at elevated temperature than Inconel 718.

Highlights

  • Inconel 718 (IN718) is the most popular precipitationstrengthened nickel-based superalloy introduced by the Huntington Alloys Division of INCO in 1959 (Ref 1)

  • These modifications led to replacement of metastable c¢¢ main strengthening phase in IN718 with more stable c¢ phase in 718Plus that caused a increase in thermal stability up to 704 °C

  • The scanning electron microscope (SEM)-BSE investigations (Fig. 2a-c) and quantitative analysis of the microstructure of IN718 base material showed two major microstructural changes after heat treatment at 760 °C: formation and growth of d phase particles, and coarsening followed by dissolution of main strengthening phases particles (c¢¢ and c¢)

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Summary

Introduction

Inconel 718 (IN718) is the most popular precipitationstrengthened nickel-based superalloy introduced by the Huntington Alloys Division of INCO in 1959 (Ref 1). ATI 718PlusÒ (718Plus) is a precipitation-strengthened nickel-based superalloy which has been developed by ATI Allvac company at the beginning of the twenty-first century. The principal difference in 718Plus chemistry is lower Ti-to-Al ratio as well as lower amount of Fe, which is replaced by the addition of Co and W. These modifications led to replacement of metastable c¢¢ main strengthening phase in IN718 with more stable c¢ phase in 718Plus that caused a increase in thermal stability up to 704 °C. Other constituents of 718Plus microstructure are c matrix and precipitates of hexagonal gNi3Ti, g*-Ni6AlNb or Ni6(Al, Ti)Nb phases distributed mainly at the grain boundaries (Ref [6,7,8,9])

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