Microstructural investigation of high-velocity oxygen-fuel (HVOF) sprayed AlCoCrFeNi + 12 wt% CoCrFeNi composite coatings

Gas atomization produces predominantly spherical and chemically homogeneous powders with finer grains than those typically obtained through bulk preparation methods. This refined powder quality plays a crucial role in alloy development, where incorporating the larger atomic-sized element Al into high-plasticity FCC-structured CoCrFeNi medium-entropy alloys (MEAs) causes the formation of a harder AlCoCrFeNi high-entropy alloy (HEA) phase exhibiting a BCC/B2 crystal structure and reduced localized plasticity. Using the blend of gas atomized AlCoCrFeNi and CoCrFeNi powders in an 88:12 weight ratio, this microstructure-oriented study explores the potential to improve the balance between strength and localized plastic deformation in a composite coating deposited via high-velocity oxygen-fuel (HVOF) spraying. The resulting microstructure primarily consists of unmelted splats (USs), semi-molten splats (SMSs), and fully molten splats (FMSs). Relatively coarse, non-recrystallized, equiaxed dendritic grains are observed in USs and the central regions of SMSs, while dynamic recrystallization in the outer SMS layers leads to (ultra-)fine equiaxed/ribbon-like grains. In contrast, FMSs display fine, fully-(or near-)columnar grains formed through directional re-solidification. In addition to spinel-type in-flight oxides (IFOs) and Al-rich post-impact oxides (PIOs), minimal porosity is present. Consequently, the BCC/B2 AlCoCrFeNi and FCC CoCrFeNi splats, together with reinforcing oxides, indicate that the composite coating may achieve a more favorable combination of strength and localized plasticity than the individual AlCoCrFeNi or CoCrFeNi coatings. Multiple strengthening mechanisms, including BCC/FCC solid solution strengthening, order (B2-type) strengthening, and grain refinement, along with deformation mechanisms like both deformation and annealing twins, contribute to its superiority relative to laser cladded coatings of a similar composition. • AlCoCrFeNi/CoCrFeNi (88:12) blend provides a balance of strength and plasticity. • Al addition increases hardness in BCC/B2 AlCoCrFeNi splats. • Deformation twins appear in unmelted FCC CoCrFeNi splats. • Annealing twins form in dynamically recrystallized semi-molten FCC CoCrFeNi splats.

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Publication Details

Journal
Journal of Alloys and Compounds
Published
2026-04-01
DOI
https://doi.org/10.1016/j.jallcom.2026.187926
Primary Topic
High Entropy Alloys Studies
Type
article
Field-Weighted Citation Impact
0.00

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article

Microstructural investigation of high-velocity oxygen-fuel (HVOF) sprayed AlCoCrFeNi + 12 wt% CoCrFeNi composite coatings

Paul Munroe, Rasim Eriş, Ashok Meghwal, Christopher C. Berndt et al.
Journal of Alloys and Compounds
High Entropy Alloys Studies
article

Microstructural investigation of high-velocity oxygen-fuel (HVOF) sprayed AlCoCrFeNi + 12 wt% CoCrFeNi composite coatings

Paul Munroe, Rasim Eriş, Ashok Meghwal, Christopher C. Berndt, A.H-S. Ang
article en

Abstract

Gas atomization produces predominantly spherical and chemically homogeneous powders with finer grains than those typically obtained through bulk preparation methods. This refined powder quality plays a crucial role in alloy development, where incorporating the larger atomic-sized element Al into high-plasticity FCC-structured CoCrFeNi medium-entropy alloys (MEAs) causes the formation of a harder AlCoCrFeNi high-entropy alloy (HEA) phase exhibiting a BCC/B2 crystal structure and reduced localized plasticity. Using the blend of gas atomized AlCoCrFeNi and CoCrFeNi powders in an 88:12 weight ratio, this microstructure-oriented study explores the potential to improve the balance between strength and localized plastic deformation in a composite coating deposited via high-velocity oxygen-fuel (HVOF) spraying. The resulting microstructure primarily consists of unmelted splats (USs), semi-molten splats (SMSs), and fully molten splats (FMSs). Relatively coarse, non-recrystallized, equiaxed dendritic grains are observed in USs and the central regions of SMSs, while dynamic recrystallization in the outer SMS layers leads to (ultra-)fine equiaxed/ribbon-like grains. In contrast, FMSs display fine, fully-(or near-)columnar grains formed through directional re-solidification. In addition to spinel-type in-flight oxides (IFOs) and Al-rich post-impact oxides (PIOs), minimal porosity is present. Consequently, the BCC/B2 AlCoCrFeNi and FCC CoCrFeNi splats, together with reinforcing oxides, indicate that the composite coating may achieve a more favorable combination of strength and localized plasticity than the individual AlCoCrFeNi or CoCrFeNi coatings. Multiple strengthening mechanisms, including BCC/FCC solid solution strengthening, order (B2-type) strengthening, and grain refinement, along with deformation mechanisms like both deformation and annealing twins, contribute to its superiority relative to laser cladded coatings of a similar composition. • AlCoCrFeNi/CoCrFeNi (88:12) blend provides a balance of strength and plasticity. • Al addition increases hardness in BCC/B2 AlCoCrFeNi splats. • Deformation twins appear in unmelted FCC CoCrFeNi splats. • Annealing twins form in dynamically recrystallized semi-molten FCC CoCrFeNi splats.

Journal of Alloys and CompoundsVol. 1064
Australian Research Council (AU), UNSW Sydney (AU), Division of Materials Science and Engineering (AU), Swinburne University of Technology (AU)
Australian Research Council
Openalex Percentile: Top 14%
High Entropy Alloys Studies
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