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Official PDF TranslationJournal of Mineral Metallurgy and Materials Science

Impact toughness, crack initiation and propagation mechanism of Ti6422 alloy with multi-level lamellar microstructure

Authors: Jie Shen; Zhihao Zhang; Jianxin Xie

DOI: 10.1007/s12613-025-3162-2Status: Verified Translated Edition
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Key Findings in This Report

• Extending furnace cooling time after solution treatment from 240 to 540 min increased impact toughness from 22.7 to 53.8 J/cm² by modifying αp lamella content and αs phase. • Raising aging temperature from 500 to 700°C reduced αs phase content and increased αp lamella/αs thickness, significantly improving impact toughness. • High αp lamellae content or large αs phase size leads to higher crack initiation and propagation energies. • Severe kinking of αp lamellae and multidirectional arrangement of α colonies deflect crack propagation, enhancing plastic deformation coordination and uniformity.