Abstract

Continuous fiber-reinforced TiAl-matrix composites are a potential structural material to satisfy the service requirements in space industry. Ta fiber with outstanding plasticity and toughness is regarded as a promising reinforcement. In this work, a 10 vol% Ta fiber-reinforced TiAl composite was prepared by combining slurry casting and vacuum hot pressing under condition of 1150 °C/ 35 MPa/ 2 h. Microstructure of interfacial reaction zone of the composite was investigated; meanwhile, thermodynamic calculation and theoretical analysis were conducted to explain the formation mechanisms of the reaction products. Three types of reaction products σ-Ta 2 Al, B2 and α 2 phases were formed between Ta fiber and TiAl matrix. σ phase was adjacent to Ta fiber with a fine grain structure, which was formed due to the lowest formation free energy. The aggregation of β stabilizers in Ti-rich region resulted in the formation of B2 phase that was close to σ phase. α 2 phase relied on B2 phase to nucleate and grow based on the Burgers relationship and their structure symmetry. Three-point bending tests show the fracture toughness (K IC ) of the Ta f /TiAl composite was 58% higher than that of pure TiAl matrix. The main toughening mechanism of the Ta f /TiAl composite was plastic deformation of the Ta fiber, meanwhile the interfacial debonding also had a contribution to toughening the TiAl alloy. The interfacial debonding location was mainly at the Ta / L I -σ interface due to the existence of thermal residual stress. • The interfacial reaction products from Ta fiber to TiAl matrix in turn were σ-Ta 2 Al, B2 and α 2 phases. • The fracture toughness (K IC ) of Ta f /TiAl composite has increased by 58% than that of pure TiAl matrix. • Plastic deformation of the Ta fiber was the main toughening mechanisms, and interfacial debonding also had a contribution to toughening TiAl alloy. • Interfacial debonding location was mainly at the Ta/L I -σ interface due to the existence of thermal residual stress.

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