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Synthesis mechanism and microstructure evolution of titanium matrix composites with a multiscale configuration

  • Shipeng Zhou
  • , Xin Chen*
  • , Shaocong Xiong
  • , Lujun Huang
  • , Delong Gong
  • , Guanghui Cong
  • , Lihua Cui
  • , Rui Zhang
  • , Xu Wang
  • , Jiayi Jin
  • , Shuai Wang
  • , Lin Geng
  • *Corresponding author for this work
  • Harbin Institute of Technology
  • Harbin Institute of Technology

Research output: Contribution to journalArticlepeer-review

Abstract

Configuration-structured titanium matrix composites (TMCs) are promising candidates for next-generation lightweight aero-engine hot-section components due to their excellent room- and high-temperature mechanical properties. In this work, a novel multiscale configuration was proposed and successfully constructed in Ti55 (Ti-5.5Al-4Sn-2Zr-1Mo-0.25Si-1Nd) matrix composites via powder metallurgy, achieving an excellent strength-ductility synergy. Network-distributed TiB and (Ti,Zr)₅Si₃ were tailored along the prior particle boundaries and α/β interfaces, while Nd5Sn3 nanoparticles were uniformly dispersed in the matrix. Moreover, a comprehensive statistical analysis was conducted on the size and spatial distribution characteristics of different phases at various sintering temperatures. As the temperature increased, TiB and Nd₅Sn₃ underwent a pronounced coarsening due to Ostwald ripening. Besides, the spatial distribution of Nd₅Sn₃ evolved from a network-like morphology to a uniform dispersion due to the secondary precipitation. Different from the transformation-independent coarsening process, (Ti,Zr)₅Si₃ exhibited obvious size refinement and redistribution from powder boundaries to α/β interfaces, which was governed by a transformation-induced dissolution and precipitation process. Meanwhile, the pinning effects of reinforcements resulted in an interesting staged coarsening process of the matrix. This work established a quantitative correlation between sintering temperature and microstructure evolution, which could provide valuable guidance for configuration design of advanced TMCs.

Original languageEnglish
Article number188409
JournalJournal of Alloys and Compounds
Volume1067
DOIs
StatePublished - 20 May 2026

Keywords

  • Microstructure evolution
  • Multiscale configuration
  • Powder metallurgy
  • Sintering temperature
  • Ti55 matrix composites

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