Abstract

We report the synthesis and characterization of two different types of Ni-based laminated composites (Types I and II). In Type-I composites, layers of Ni and Ti3SiC2 (Ni–Ti3SiC2) were interleaved with Ni, whereas in Type-II composites, Ni–Ti3SiC2 layers were interleaved with Al and Ni. The laminate thickness and Ti3SiC2 content in the individual Ni–Ti3SiC2 layers were systematically varied in both the composites. Detailed SEM studies showed that Ti3SiC2 particulates are well distributed in the Ni-matrix with little or no interfacial reactions with interparticle porosity. However, there were interfacial reactions between Ni and Al in Type II composites. In general, Type I multilayered composites had higher ultimate compressive strength (UCS) in parallel orientation as compared to perpendicular orientation (layers are aligned parallel or perpendicular to the wear surface then it will be referred to as parallel or perpendicular orientation). Comparatively, in Type II composites, the UCS was greater in perpendicular orientation as compared to parallel due to the presence of Al layers as bonding layers. Both the composite designs showed triboactive behavior against alumina disks and sensitivity to laminate thickness and orientation. In Type-I composites, the decrease in µ and wear rate (WR) with laminate thickness was more pronounced in the perpendicular orientation as compared to the parallel orientation. Comparatively, Ni–Ti3SiC2/Al/Ni composites showed that the parallel orientation was more effective in enhancing the triboactive performance. SEM analysis of tribosurfaces showed signs of triboxidation and abrasion, which led to the formation of O-rich tribofilms.

Highlights

  • There is a critical need for designing lightweight, high-performance materials with high strength and toughness for automotive, aerospace, bioengineering, and construction applications

  • Ti3 SiC2 particulates were well dispersed in the Ni-layers and the layers were uniform in thickness, interparticle porosity was observed

  • The ultimate compressive strength (UCS) of these composites was sensitive to Ti3SiC2 content, and it with the increase in Ti3 SiC2 content was more prominent in perpendicular orientation as compared to decreased as the concentration of Ti3SiC2 was increased in the composites

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Summary

Introduction

There is a critical need for designing lightweight, high-performance materials with high strength and toughness for automotive, aerospace, bioengineering, and construction applications. Further For of composites of MAX phases with metals have shown many promising properties [10,11,12,13,14,15,16,17,18,19,20,21,22]. Showed that composites of pure reinforced with 40 vol % Ti3AlC2 had twice yield strength than pure aluminum [14]. AlC had twice yield strength than pure aluminum [14] This group proved that Ti3AlC2 particulates can efficiently reinforce the Al-matrix.

Laminate Design
SiC23SiC
Calculation of Ti3SiC2 Concentration in Composite
Slurry Design and Tape Casting
Mechanical and Tribological Testing
Results and Discussion
Microstructure Analysis
Mechanical Performance of Ni-Matrix Composites
Composites layer thickness Behavior was varied from3SiC
Tribological Behavior of Ni–Ti3 SiC2 Composites
SiC3SiC
Comparison with Other Solid Lubricants
Conclusions
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