热处理工艺对TC11钛合金显微组织演变及硬度的影响研究

    Analysis on Effect of Heat Treatment on Microstructure Evolution and Hardness of TC11 Titanium Alloy

    • 摘要: 为优化TC11钛合金的热处理工艺,进行了不同工艺参数的固溶处理和固溶时效处理试验,研究固溶温度和冷却方式(空冷、炉冷)对其显微组织和硬度的影响规律。结果表明:固溶温度主导TC11合金的初生等轴α相含量,随着温度从940℃升至980℃,α相体积分数从69.8%降至37.3%;固溶冷却方式调控β转变组织形貌,空冷形成致密的片层状α组织,炉冷生成排列紧密且粗大的α相。硬度受固溶工艺协同作用显著,时效参数(530~800)℃×(1~24)h对TC11合金性能影响有限。980℃×1 h固溶+空冷、530℃×6 h时效+空冷时,TC11硬度最高,达到472.43 HV,较原始态提升23.1%;相同固溶温度下空冷工艺的硬度较炉冷的高。通过精准控制固溶温度与冷却方式可有效协调等轴α相含量与β转变组织形貌,为钛合金的性能优化提供新思路。

       

      Abstract: To optimize the heat treatment process of TC11 titanium alloy, the solid solution and solution+aging treatment tests with different process parameters were carried out, and the influence laws of solution temperature and cooling methods (air cooling/furnace cooling) on the microstructure and hardness were studied. The results show that the solution temperature dominates the content of primary equiaxed α phase in TC11 alloy. With the solution temperature increasing from 940 ℃ to 980 ℃, the volume fraction of α phase decreases from 69.8% to 37.3%. The cooling method regulates the morphology of β transformed structure: air cooling forms a dense lamellar α structure, while furnace cooling generates a dense and coarse α structure. Hardness is significantly affected by the synergistic effect of solution process, and aging parameters (530 ℃-800 ℃/1 h-24 h) have limited effects on the performance of TC11 alloy. When the alloy is treated with the process of 980 ℃×1 h solution+air cooling, 530 ℃×6 h aging+air cooling, the hardness of TC11 alloy is the highest of 472.43, which increases by 23.1% compared with the as-received state, and the hardness of the air-cooling process is higher than that of furnace cooling under the same solution temperature. Precise control of solution temperature and cooling method can effectively coordinate the content of equiaxial α phase and the morphology of β-transformed structure, providing new ideas for the performance optimization of titanium alloys.

       

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