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Computational modeling and interpretability analysis of manufacturing parameters in titanium matrix composites

  • Beijing Institute of Technology

科研成果: 期刊稿件文章同行评审

摘要

The design of high-performance titanium matrix composites (TMCs) often faces the challenge of complex, nonlinear interactions between multi-scale processing parameters and mechanical properties. To overcome the limitations of traditional empirical methods, this study establishes a comprehensive data-driven computational framework to predict and optimize the performance of TMCs. To address the challenge of small-sample generalization, a diversity-oriented independent validation strategy was employed, strictly separating model training from a heterogeneous hold-out test set. Among various evaluated algorithms, the gradient boosting (GB) model demonstrated superior fidelity, achieving high predictive accuracy on the unseen independent datasets (R2 up to 0.88 for strength). To ensure model transparency, a synergistic interpretability framework was implemented, integrating Pearson correlation, feature importance screening, SHapley Additive exPlanations (SHAP), and individual conditional expectation (ICE) plots. This multi-level approach quantitatively identified reinforcement characteristics, hot rolling reduction, and sintering pressure as the primary mechanical descriptors. Crucially, the model captured distinct, non-linear optimization regimes, identifying optimal property windows at lower pressures (40–50 MPa) for spark plasma sintering (SPS) and higher pressures (300–500 MPa) for hot-pressing, both in synergy with 70–75% rolling reductions. Experimental validation on a 2.0 wt% MXene/Ti composite confirmed the model's high-fidelity strength prediction with errors <2%. This ML-driven strategy provides a computationally efficient paradigm for defining tailored processing envelopes, offering new insights into the inverse design of high-performance metal matrix composites.

源语言英语
文章编号114624
期刊Computational Materials Science
268
DOI
出版状态已出版 - 5 4月 2026

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