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钛合金高速超声振动车削表面完整性及耐磨损性能试验研究

Experimental Study on Surface Integrity and Wear Resistance of Titanium Alloy During High-Speed Ultrasonic Vibration Cutting

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【作者】 彭振龙; 张翔宇; 王刚; 徐广涛; 赵明皞;

【Author】 PENG Zhenlong;ZHANG Xiangyu;WANG Gang;XU Guangtao;ZHAO Minghao;School of Mechanical and Power Engineering, Zhengzhou University;Henan Key Engineering Laboratory for Anti-Fatigue Manufacturing Technology;School of Mechanics and Safety Engineering, Zhengzhou University;Beijing Key Laboratory of Precision/Ultra-Precision Manufacturing Equipments and Control,Department of Mechanical Engineering, Tsinghua University;State Key Laboratory of Tribology in Advanced Equipment, Department of Mechanical Engineering,Tsinghua University;

【通讯作者】 张翔宇;

【机构】 郑州大学机械与动力工程学院; 抗疲劳制造技术河南省工程实验室; 郑州大学力学与安全工程学院; 清华大学机械工程系精密超精密制造装备及控制北京市重点实验室; 清华大学机械工程系高端装备界面科学与技术全国重点实验室;

【摘要】 在可替代性弱且常被用于制造航空发动机关键部件的前提下,钛合金等难加工材料的高效高质切削面临挑战。针对钛合金Ti–6Al–4V加工表面完整性不佳和使役性能有待提升难题,开展了钛合金Ti–6Al–4V的高速车削试验,分析了高速超声振动切削技术对钛合金Ti–6Al–4V表面完整性和已加工表面耐磨损性能的改善效果,进而为钛合金Ti–6Al–4V的高质量加工提供理论支撑。结果表明,相比于普通切削,高速超声振动切削有效降低了钛合金Ti–6Al–4V的表面粗糙度,提高了表面强度和表面残余压应力,以及增强了耐磨损性能。

【Abstract】 On the premise of weak substitutability and being often used to manufacture key components of aeroengine, high-efficient and high-quality machining of difficult-to-cut materials such as titanium alloys is facing challenges.Aiming at the problems of poor surface integrity and service performance of titanium alloy Ti–6Al–4V, high-speed cutting tests of titanium alloy Ti–6Al–4V were carried out, and the improvement of high-speed ultrasonic vibration cutting technology on the surface integrity and the wear resistance of machined surface was analyzed, thus providing theoretical support for high-quality machining of titanium alloy Ti–6Al–4V. The results show that compared with conventional cutting,high-speed ultrasonic vibration cutting effectively reduces the surface roughness, and improves surface strength, surface residual compressive stress and wear resistance of titanium alloy Ti–6Al–4V.

【基金】 国家自然科学基金(52005023)
  • 【文献出处】 航空制造技术 ,Aeronautical Manufacturing Technology , 编辑部邮箱 ,2024年09期
  • 【分类号】V263
  • 【下载频次】26
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