毕运波/教授,博导
毕运波
教授、博导
办公电话:13067792747
通讯地址:紫金港校区开物苑3幢405室
电子邮件:zjubyb@zju.edu.cn
一、个人履历
1、教育背景
1997.09-2001.07 浙江大学机械制造及其自动化专业学士
2001.09-2007.09 浙江大学机械制造及其自动化专业博士
2、工作经历
2007.09-2009.12 浙江大学计算机科学与技术博士后流动站博士后
2009.12-2011.12 浙江大学机械工程学院制造工程及自动化研究所助理研究员
2012.01至今 浙江大学机械工程学院制造工程及自动化研究所副教授。
二、研究方向
长寿命装配连接技术
自动化钻铆技术及装备
复合材料加工与修复技术
研究概况:
围绕飞机制造和装配对先进制造工艺及装备的需求,从事飞机壁板装配变形定量预测与主动控制,装配连接过程物理建模、数字仿真与工艺优化,自动化钻铆技术、装备与系统,复合材料加工与修复等方面的研究和应用工作。近年来,主持国家科技支撑计划课题、民机专项课题、国家自然科学基金、浙江省自然科学基金等多项国家和省部级科研项目,发表SCI/EI论文30余篇,授权国家发明专利20余项,软件著作权2项。
三、奖励荣誉
飞机自动化装配成套工艺装备及集成应用, 中国机械工业科学技术奖一等奖, 2017, 3/15
面向国家重大战略需求的航空制造高层次工程人才培养模式探索与实践, 浙江省研究生教育学会教育成果奖, 2018, 3/15
2013-2014学年机械工程学系“我最喜爱的老师”提名奖
2014-2015学年机械工程学院“我最喜爱的老师”
2015-2016学年机械工程学院“我最喜爱的老师”
2017年浙江大学优秀“新生之友”
四、学术兼职
International Journal of Damage Mechanics,Assembly Automation,Proc.IMechE Part B: Journal of Engineering Manufacture,The Journal of Strain Analysis for Engineering Design,航空学报等国内外学术期刊审稿人
五、科研项目
国家自然科学基金面上项目,卧式双机联合自动钻铆系统压铆精度保障技术研究,2018.1至2021.12,主持
国家自然科学基金面上项目,机器人精确制孔基础理论与关键技术研究,2017.1至2020.12, 主参,排名3
国家自然科学基金面上项目,机器人精镗飞机交点孔的颤振机理及其稳定切削机制研究, 2016.1至2019.12, 主参,排名3
国家自然科学基金面上项目,基于局部刚度加强的大型飞机壁板装配变形控制及安全恢复技术研究, 2013.1至2016.12,主持
国家自然科学基金青年项目,机器人制孔过程中工件变形精确预测和单侧压紧力优化研究, 2013.1至2016.12,主参,排名3
中央高校基本科研业务费专项,大型飞机壁板装配变形控制技术研究,2013.1至2013.12,主持
浙江省自然科学基金面上项目,蜂窝复合材料加工固持与高速切削工艺优化研究,2010.1至2012.1,主持
此外,在国家科技支撑计划、工信部民机专项等国家级重大科研项目支持下,主参十余项飞机自动化装配系统项目,作为子项目负责人,具体承担柔性定位、机器人制孔、环形轨道制孔、专用机床制孔、自动化钻铆技术研究及系统开发任务,累计科研经费超千万元。
六、发表论文
发表SCI收录论文
Changyi Lei, Quan Chen, Yunbo Bi*, Jiangxiong Li and Yinglin Ke. An Effective Theoretical Model for Slug Rivet Assembly Based on Countersunk Hole Structure, International Journal of Advanced Manufacturing Technology, 2019, 101(1-4):1065-1074
Junxia Jiang, Chen Bian, Yunbo Bi* and Yinglin Ke. A new type of inner-side working head for automatic drilling and riveting system, Assembly Automation, 2019, 39(1):154-164
Jintong Liu, Heng Li, Yunbo Bi*, Huiyue Dong and Yinglin Ke. Influence of the deformation of riveting-side working head on riveting quality, International Journal of Advanced Manufacturing Technology, 2019,http://link.springer.com/article/10.1007/s00170-019-03504-9
Jintong Liu, Ze Zhao, Yunbo Bi* and Huiyue Dong. Prediction and compensation of force-induced deformation for a dual-machine-based riveting system using FEM and neural network, International Journal of Advanced Manufacturing Technology, 2019, accepted
Changyi Lei, Yunbo Bi*, Jiangxiong Li and Yinglin Ke. Slug Rivet Assembly Modeling and Effects of Procedure Parameters on the Quality of Riveted Lap Joints, Advances in Mechanical Engineering, 2018, 10(9):1687814018798397
Changyi Lei, Yunbo Bi*, Jiangxiong Li and Yinglin Ke. Experiment and numerical simulations of a slug rivet installation process based on different modeling methods, International Journal of Advanced Manufacturing Technology, 2018, 97(1-4):1481-1496
Dan Zhao, Yunbo Bi* and Yinglin Ke. An efficient error prediction and compensation method for coordinated five-axis machine tools under variable temperature. International Journal of Advanced Manufacturing Technology, 2018, 96(9-12):4431-4443
Dan Zhao, Yunbo Bi* and Yinglin Ke. Kinematic modeling and inverse kinematics solution of a new six-axis machine tool for oval holes drilling in aircraft wing assembly. International Journal of Advanced Manufacturing Technology, 2018, 96(5-8): 2231–2243
Dan Zhao, Yunbo Bi* and Yinglin Ke. A United Kinematic Calibration Method for a Dual-Machine System. Assembly Automation,2018,38(2): 226-238
Dan Zhao, Yunbo Bi* and Yinglin Ke. Kinematic modeling and base frame calibration of a dual-machine-based drilling and riveting system for aircraft panel assembly. International Journal of Advanced Manufacturing Technology, 2018, 94(5-8): 1873–1884
Dan Zhao, Yunbo Bi* and Yinglin Ke. An efficient error compensation method for coordinated CNC five-axis machine tools. International Journal of Machine Tools and Manufacture, 2017, 123:105-115
Changyi Lei, Yunbo Bi, Jiangxiong Li and Yinglin Ke.Effect of riveting parameters on the quality of riveted aircraft structures with slug rivet[J]. Advances in Mechanical Engineering, 2017, 9(11): 1687814017734710.
Changyi Lei, Cong Li, Yunbo Bi* and Jiangxiong Li. The optimal clamping force option for robotic drilling of stacked aluminum sheets based on shell theory[J]. Advances in Mechanical Engineering, 2017, 9(3): 1687814017695048.
Yunbo Bi, Weimiao Yan* and Yinglin Ke. Optimal placement of measurement points on large aircraft fuselage panels in digital assembly. Proceedings of the Institution of Mechanical Engineers, Part B: Journal of Engineering Manufacture, 2017, 231(1):73-84
Jiang Jiefeng and Bi Yunbo. Effect of parameters on local stress field in single-lap bolted joints with the interference fit[J]. Advances in Mechanical Engineering, 2016, 8(5): 1687814016647255.
Weimiao Yan, Yunbo Bi* and Mingjie Qiao. Effect of positioning errors of frames on fuselage panel assembly deformation. Advances in Mechanical Engineering, 2016, 8(5):1687814016650566.
Yunbo Bi*, Jifeng Jiang and Yinglin Ke. Effect of interference fit size on local stress in single lap bolted joints. Advances in Mechanical Engineering, 2015, 7(6):: 1687814015590307.
Yunbo Bi, Weimiao Yan and Yinglin Ke. Multi load-transmitting device based support layout optimization for large fuselage panels in digital assembly, Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science, 2015, 229(10):1792-1804
Jiefeng Jiang, Yunbo Bi*, Huiyue Dong, Yinglin Ke, Xintian Fan and Kunpeng Du. Influence of interference fit size on hole deformation and residual stress in hi-lock bolt insertion, Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science, 2014, 228(18): 3296-3305
Gang Liu, Wei Tang, Ying-LIN Ke, Qing-Liang Chen andYunbo Bi. Modeling of fast pre-joining processes optimization for skin-stringer panels, Assembly Automation, 2014, 34(4):323-332
Yunbo Bi*, Weimiao Yan and Yinglin Ke. Numerical study on predicting and correcting assembly deformation of a large fuselage panel during digital assembly, Assembly Automation, 2014, 34(2):204-216
Yun-bo Bi*, Qun-lin CHENG, Hui-yue DONG, Ying-lin KE. Machining distortion prediction of aerospace monolithic components, Journal of Zhejiang University:Science A, 2009, 10(5): 661-668.
七、授权发明专利
毕运波,程亮,曲巍崴,李江雄,柯映林,一种进给轴随AB轴摆动的五轴数控制孔机床正反解方法,ZL 201710108552.8 授权
毕运波,曲巍崴,程亮,柯映林,一种含双C轴的六轴自动化制孔锪窝机床的运动学反解方法,ZL 201710108540.5 实审
毕运波,王青,曲巍崴,董辉跃,方强,俞慈君,费少华,黄浦缙,李江雄,柯映林,一种飞机机翼数字化装配系统,ZL 201710416987.9 实审
毕运波,李江雄,王青,曲巍崴,柯映林,一种基于视觉测量及标定的AGV自动调姿定位方法,ZL 201710751564.2 实审
毕运波,柯臻铮,李江雄,柯映林,一种飞机翼盒转站用AVG车及其车载翼盒调姿定位系统,ZL 201710751427.9 实审
柯映林,毕运波,李江雄,曲巍崴,董辉跃,黄奇伟,一种飞机壁板卧式自动钻铆机的运动参数辨识方法,ZL 201610102623.9 实审
柯映林,毕运波,李江雄,曲巍崴,董辉跃,严伟苗,一种飞机壁板卧式自动钻铆机的基坐标系标定方法,ZL 201610101188.8 授权
蒋君侠,柯映林,黄奇伟,毕运波,柯臻铮,一种飞机壁板自动钻铆机的无头铆钉自动供钉系统,ZL 201610962618.5 授权
蒋君侠,柯映林,黄奇伟,毕运波,柯臻铮,一种飞机壁板自动钻铆机的有头铆钉自动供钉系统,ZL 201610962617.0 授权
柯映林,蒋君侠,毕运波,柯臻铮,曲巍崴,一种飞机壁板高度可调的自动钻铆机总体布局方法,ZL 201610977023.7 实审
柯映林,蒋君侠,毕运波,柯臻铮,曲巍崴,一种飞机壁板高度和转角可调的自动钻铆机总体布局方法,ZL 201610976161.3 实审
蒋君侠,柯映林,柯臻铮,毕运波,曲巍崴,一种用于飞机壁板卧式自动钻铆机的分离式铆接头,ZL 201610990058.4 授权
毕运波,柯映林,俞慈君,曲巍崴,一种飞机壁板卧式自动钻铆机空间相对位姿误差补偿方法,ZL 201610945832.X 授权
柯映林,方强,毕运波,费少华,一种自动钻铆机压脚气动控制方法,ZL 201611017412.1 授权
曲巍崴,黄奇伟,柯映林,毕运波,一种自动钻铆机排屑口吸力控制装置及方法,ZL 201611033108.6 授权
柯映林,方强,毕运波,费少华,一种自动钻铆机镦头高度控制方法,ZL 201611030666.7 授权
柯映林,方强,毕运波,费少华,一种自动钻铆机压铆力位移混合控制方法,ZL 201611030600.8 授权
毕运波,柯映林,王青,李江雄,柯臻铮,费少华,李文军,一种用于飞机壁板卧式自动钻铆机的末端精度重力补偿方法,ZL 201610101198.1 授权
毕运波,柯映林,俞慈君,曲巍崴,结合温度因素的飞机壁板卧式自动钻铆机空间相对位姿误差补偿方法,ZL 201610946457.0 授权
曲巍崴,黄奇伟,柯映林,毕运波,一种飞机壁板卧式自动钻铆机的工装夹具坐标系建站方法,ZL 201611056255.5 授权
柯映林,董辉跃,毕运波,曲巍崴,一种自动钻铆机的制孔法向修正方法,ZL 201611025556.1 授权
毕运波,严伟苗,柯映林,方伟,卢鹄,刘思仁,薛雷,汪西,王平,基于三轴数控定位器的飞机壁板装配变形的数字化校正方法,ZL 201410171706.4 授权
毕运波,严伟苗,柯映林,屠晓伟,姜丽萍,沈立恒,朱宇,邢宏文,周庆慧,基于六轴数控定位器的飞机壁板装配变形的数字化校正方法,ZL 201410171705.X 授权
朱伟东,曲巍崴,毕运波,柯映林,用于机器人制孔平台视觉测量系统的标定方法及装置,ZL 201410128629.4 授权
柯映林,严伟苗,毕运波,梁青霄,何胜强,杨国荣,一种基于局部刚度加强的大型飞机壁板变形控制及复位方法,ZL 201210232642.5 授权
毕运波,何胜强,柯映林,何丹青,程亮,王青,李江雄,俞慈君,黄鹏,金涨军,基于四个数控定位器、调姿平台和移动托架的飞机部件调姿、对接系统及方法, ZL 201010545364.X 授权
柯映林,黄小东,蒋君侠,杨国荣,樊新田,周启民,孙文博,赵安安,张洪双,邱宝贵,李江雄,方强,王青,毕运波,黄浦缙,飞机翼身大十字对接定位器布局方法,ZL 201010136786.1 授权
柯映林,杨卫东,蒋君侠,秦龙刚,贾叔仕,郭志敏,陈学良,黄浦缙,盖宇春,方强,余进海,刘刚,李江雄,俞慈君,毕运波,王青,球形铰接式三坐标柔性调姿单元,ZL 200810161658.5 授权
柯映林,杨卫东,李江雄,姚宝国,张斌,俞慈君,余进海,方强,蒋君侠,秦龙刚,毕运波,屠志明,贾叔仕,盖宇春,一种机翼水平位姿测量与评估方法,ZL 200810121357.X 授权
柯映林,杨卫东,李江雄,姚宝国,张斌,余进海,方强,秦龙刚,毕运波,屠志明,黄浦缙,飞机机翼、垂尾水平测量点打制系统及方法,ZL 200810121757.0 授权
柯映林,杨卫东,王青,李江雄,方强,蒋君侠,秦龙刚,毕运波,贾叔士,黄鹏,俞慈君,余进海,郭志敏,陈学良,黄浦缙,盖宇春,刘刚,一种飞机机身柔性化、自动化调姿方法,ZL 200810164117.8 授权
柯映林,杨卫东,方强,毕运波,李江雄,余进海,俞慈君,蒋君侠,秦龙刚,贾叔仕,郭志敏,张斌,基于三个定位器的飞机部件位姿调整协同控制方法,ZL 200810161669.3 授权
柯映林,杨卫东,方强,毕运波,李江雄,余进海,俞慈君,蒋君侠,秦龙刚,贾叔仕,郭志敏,张斌,基于四个定位器的飞机部件位姿调整协同控制方法, ZL 200810161667.4 授权
柯映林,杨卫东,李江雄,余进海,方强,毕运波,俞慈君,蒋君侠,秦龙刚,贾叔仕,郭志敏,张斌,一种基于四个定位器的飞机部件位姿调整系统及方法,ZL 200810161668.9 授权