<p>This study investigated the microstructure, mechanical properties, and fracture mechanism of a TiB/TA15 composite material. The TiB phase exhibited a quasi-continuous distribution at the grain boundaries of TiB/TA15, playing a role in pinning and grain refinement. The tensile strength of the material is greatly increased by 28.8% relative to that of TA15, from 875 to 1127&#xa0;MPa, and the fracture mechanism is mixed fracture. This study also conducted thermal cycling at 650 °C for 2&#xa0;h. After 1, 5, and 10 thermal cycles, the tensile strength decreased. However, it only decreased by 8.7% after 10 thermal cycles, which indicates that temperature fatigue had little effect on the mechanical properties.</p>

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Microstructure and Mechanical Properties of TiB/TA15 Composite Material for Aircraft Engines

  • Zhiyao Liu,
  • Chuman Rong,
  • Wei Zhang,
  • Yue Kou,
  • Lindi Wu,
  • Yanqing Wu,
  • Yang Li,
  • Sansan Ao

摘要

This study investigated the microstructure, mechanical properties, and fracture mechanism of a TiB/TA15 composite material. The TiB phase exhibited a quasi-continuous distribution at the grain boundaries of TiB/TA15, playing a role in pinning and grain refinement. The tensile strength of the material is greatly increased by 28.8% relative to that of TA15, from 875 to 1127 MPa, and the fracture mechanism is mixed fracture. This study also conducted thermal cycling at 650 °C for 2 h. After 1, 5, and 10 thermal cycles, the tensile strength decreased. However, it only decreased by 8.7% after 10 thermal cycles, which indicates that temperature fatigue had little effect on the mechanical properties.