首页|航空用超大规格TC18钛合金棒材的制备及组织性能研究

航空用超大规格TC18钛合金棒材的制备及组织性能研究

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经 3 次真空自耗电弧熔炼得到规格为φ720 mm的TC18 钛合金铸锭,再经 80 MN快锻机开坯锻造和多道次镦拔锻造,成功制备了航空用φ500 mm超大规格棒材,并对其组织均匀性及力学性能稳定性进行了评价分析.结果表明:TC18 钛合金铸锭头、中、尾不同部位的主元素极差在 0.1%以内,成分均匀性良好;TC18 钛合金棒材不同部位的低倍组织均匀模糊,高倍组织呈现出典型的双态组织,且组织均匀一致性良好;棒材不同部位的力学性能差异较小,具有良好的性能稳定性.
Study on Preparation,Microstructure and Mechanical Properties of Oversized TC18 Titanium Alloy Bar for Aviation
The TC18 titanium alloy ingot with diameter of 720 mm was prepared by three times vacuum consumable arc melting.The oversized φ500 mm TC18 titanium alloy bar for aviation was successfully prepared by 80 MN rapid forging machine via cogging,multiple pass upsetting and drawing.The uniformity of microstructure and the stability of mechanical properties were evaluated and analyzed.The results show that the range of main elements at different positions of TC18 titanium alloy ingot is less than 0.1%indicating well composition uniformity.The macrostructure of TC18 titanium alloy bar at different positions is uniform and fuzzy,and the microstructure presents a typical bimodal microstructure with good uniformity.The mechanical properties of the bar at different positions show well consistency and performance stability.

TC18 titanium alloyoversized barchemical compositionmicrostructuremechanical property

任晓龙、陈宇、张胜、杨晶、王涛、赵宁

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西部超导材料科技股份有限公司 特种钛合金材料制备技术国家地方联合工程实验室西安市特种钛合金制备及仿真技术重点实验室,陕西 西安 710018

TC18钛合金 超大规格棒材 化学成分 组织 力学性能

秦创原引用高层次创新创业人才项目

QCYRCXM-2023-003

2024

钛工业进展
中国有色金属工业协会钛锆铪分会 西北有色金属研究院

钛工业进展

CSTPCD
影响因子:0.2
ISSN:1009-9964
年,卷(期):2024.41(3)
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