4.0 Article

Comprehensive and Comparative Heat Treatment of Additively Manufactured Inconel 625 Alloy and Corresponding Microstructures and Mechanical Properties

Journal

Publisher

MDPI
DOI: 10.3390/jmmp6050107

Keywords

Inconel 625; additive manufacturing techniques; post-process heat treatment; microstructures; microindentation hardness; tensile properties

Funding

  1. NASA [80NSSC22PA055]
  2. NASA Marshall Space Flight Center

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This study examines and compares the microstructures, mechanical properties, and Vickers microindentation hardnesses for additively manufactured samples built by different AM processes. The study finds that high-temperature heat treatment of AM process-built samples can improve their microstructures and mechanical properties. The heat-treated samples exhibit similar grain structures and hardnesses, independent of the AM process used.
This study examines and compares the microstructures, Vickers microindentation hardness, and mechanical properties for additively manufactured (AM) samples built by a variety of AM processes: wire arc AM (WAAM), electron beam powder bed fusion (EB-PBF), laser wire direct energy deposition (LW-DED), electron beam direct energy deposition (EB-DED), laser-powered direct energy deposition (LP-DED), and laser powder bed fusion (L-PBF). These AM process samples were post-processed and heat-treated by stress relief annealing at 1066 degrees C, HIP at 1163 degrees C, and solution annealing treatment at 1177 degrees C. The resulting microstructures and corresponding microindentation hardnesses were examined and compared with the as-built AM process microstructures and hardnesses. Fully heat-treated AM process samples were mechanically tested to obtain tensile properties and were also evaluated and compared. Principal findings in this study were that high-temperature heat treatment >1100 degrees C of AM process-built samples was dominant and exhibited recrystallized, equiaxed grains containing fcc {111} annealing twins and second phase particles independent of the AM process, in contrast to as-built columnar/dendritic structures. The corresponding yield stress values ranged from 285 MPa to 371 MPa, and elongations ranged from 52% to 70%, respectively. Vickers microindentation hardnesses (HV) over this range of heat-treated samples varied from HV 190 to HV 220, in contrast to the as-built samples, which varied from HV 191 to HV 304.

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