Abstract
Ti matrix composites reinforced with 1–5 wt% graphene oxide (GO) were prepared by hot-pressed sintering in argon atmosphere. The effect of sintering temperature on the microstructures and mechanical properties of the composite was also evaluated. The results show that TiC nanoparticles were formed in situ as interfacial products via the reaction between Ti and GO during sintering. With increases in GO content and sintering temperature, the amount of TiC increased, improving the mechanical properties of the composites. GO was also partly retained with a lamellar structure after sintering. The composite reinforced with 5 wt% GO exhibited a hardness of 457 HV, 48.4% higher than that of pure Ti at 1473 K. The Ti-2.5 wt% GO composite sintered at 1473 K achieved a maximum yield stress of 1294 MPa, which was 62.7 % higher than that of pure Ti. Further increasing the GO content to 5 wt% led to a slight decrease in yield stress owing to GO agglomeration. The fracture morphology of the composite reinforced with GO exhibited a quasi-cleavage fracture, whereas that of the pure Ti matrix showed a ductile fracture. The main strengthening mechanism included grain refinement, solution strengthening, and dispersion strengthening of TiC and GO.
Highlights
The increasing demand for lightweight and highperformance materials for the aerospace industry in recent years has led to the development of metal matrix composites (MMCs)
The following conclusions are drawn: (1) graphene oxide (GO) is uniformly distributed in the matrix when the content is lower than 5 wt%
TiC measuring 20–200 nm is formed in situ as an interfacial product by the reaction between Ti and GO during sintering
Summary
The increasing demand for lightweight and highperformance materials for the aerospace industry in recent years has led to the development of metal matrix composites (MMCs). The TiC formed in situ can improve the interfacial bonding between the Ti matrix and GO and enhance the mechanical properties of the composite.
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