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    白争锋
    点击:2865次  添加时间:2012/05/28  作者:不详

    白争锋

    工学博士

    副教授、博士生导师

    电子邮件:zfbai@hitwh.edu.cn

    教育背景

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    2001.09-2005.07 哈尔滨工业大学  航天学院   本科

    2005.09-2007.07 哈尔滨工业大学  航天学院    硕士

    2007.09-2011.07 哈尔滨工业大学  航天学院    博士

    研究领域

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    多体系统动力学、结构动力学、机械系统可靠性分析与寿命预测

    代表性成果

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    1. Zheng Feng Bai, Jun Chen, Yi Sun. Effects of contact force model on dynamics characteristics of mechanical system with revolute clearance joints.IJST - Transactions of Mechanical Engineering. 2014 (Accepted)   (SCI; EI)

    2. Zheng Feng Bai, Hui Bo Zhang, Yi Sun. Wear prediction for dry revolute joint with clearance in multibody system by integrating dynamics model and wear model. Latin American Journal of Solids and Structures. 2014 (Accepted)  (SCI; EI)

    3. Zheng Feng Bai, Yang Zhao, Jun Chen. Dynamics analysis of planar mechanical system considering revolute clearance joint wear. Tribology International. 2013, 64:85-95 (SCI; EI)

    4. Zheng Feng Bai, Yang Zhao, Xing Gui Wang. Wear analysis of revolute joints with clearance in multibody systems. SCIENCE CHINA Physics, Mechanics & Astronomy. 2013,56(8): 1581-1590    (SCI; EI)

    5. Zheng Feng Bai, Yang Zhao, A Hybrid Contact Model of Revolute Joint with Clearance for Mechanical Systems. International Journal of Non-Linear Mechanics. 2013,(48):15-36  (SCI; EI)

    6. Zheng Feng Bai, Yang Zhao, Xing Gui Wang. A nonlinear contact force model for revolute joint with clearance. Journal of Mechanics. 2013,(29)04: 653-660   (SCI; EI)

    7. Zheng Feng Bai, Yang Zhao, Dynamics modeling and quantitative analysis of multibody systems including revolute clearance joint. Precision Engineering. 2012, 36:554-567   (SCI; EI)

    8. Zheng Feng Bai, Yang Zhao. Dynamic behaviour analysis of planar mechanical systems with clearance in revolute joints using a new hybrid contact force model. International Journal of Mechanical Sciences. 2012, 54, 190-205  (SCI; EI)

    9.Zheng Feng Bai, Yang Zhao, Attitude Motion of Spacecraft during Oblique Solar Panel Deployment. Aircraft Engineering and Aerospace Technology. 2012,84(2):109-114   (SCI; EI)

    10. Li Xin Zhang, Zheng Feng Bai, Yang Zhao, Xi Bin Cao. Dynamic Response of Solar Panel Deployment on Spacecraft System Considering Joint Clearance. Acta Astronautica. 2012, 81:174-185   (SCI; EI)

    11. Yang Zhao, Zheng Feng Bai. Dynamics Analysis of Space Robot Manipulator with Joint Clearance.  Acta Astronautica. 2011,68:1147-1155   (SCI; EI)

    12. Yang Zhao, ZhengFeng Bai. Effects of Clearance on Deployment of Solar panels on Spacecraft System. Transactions of the Japan Society for Aeronautical and Space Sciences, 2011,53(182):291-295  (SCI; EI)

    13. Zheng Feng Bai, Yang Zhao, Jun Chen. Dynamics analysis of dual-axis positioning mechanism of satellite antenna with joint clearance. Multidiscipline Modeling in Materials and Structures, 2014, 10(1):59-74   (EI)

    14. Zheng-feng Bai, Bin-jiu Yang Yi Sun. Investigation on Dynamics of Mechanical System with Clearance Joint.  The Open Mechanical Engineering Journal. 2014:8, 224-229   (EI)

    15. Zheng Feng Bai, Xing Gui Wang, Yang Zhao, Investigation on dynamics characteristics of real manipulator with multiple clearance joints. Applied Mechanics and Materials. 2013, 251: 152-157  (EI)

    16. Li Xin Zhang, Zheng Feng Bai, Yang Zhao XiBin Cao. Parameter Computation of Equivalent Mechanical Models of Liquid Sloshing in Spacecraft Container. Applied Mechanics and Materials. 2013, 397:209-212  (EI)

    17. 白争锋赵阳,赵志刚. 考虑运动副间隙的机构动态特性研究. 振动与冲击. 2011, 30(11):17-20,41    (EI)

    代表性项目

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    1. 考虑运动副间隙与摩擦磨损效应的柔性航天机构耦合动力学研究(国家自然科学基金,编号:51305093)负责人

    2. 航天机构可靠性动力学基础研究973计划课题,编号:2013CB733004

    主要研究人员,排名第4

    3. 考虑运动副间隙、摩擦磨损和构件柔性的航天机构动力学研究(山东省自然科学基金,编号:ZR2013EEQ004)  负责人

    4. 基于区间域的含间隙参数变化航天机构动力学研究(哈尔滨工业大学创新基金,编号: HIT.NSRIF.2013122)负责人

    5. 考虑运动副非规则磨损间隙和构件弹性的机构动力学研究 (中国博士后科学基金面上资助,编号:2012M520723) 负责人

    6. 考虑多间隙的航天机构非线性动力学分析与优化设计研究(中国博士后科学基金特别资助,编号: 2014T70317) 负责人