李朝峰

发布时间:2019-10-15浏览次数:240

一、个人简介:

李朝峰,男,中共党员,副教授,博士生导师,硕士生导师。20101月毕业于东北大学机械设计及理论专业,获工学博士学位并留校任教。为东北大学闻邦椿院士课题组核心成员,航空动力装备振动及控制教育部重点实验室(B)主要成员。 2011年至2014年在沈阳鼓风机集团透平研究院做在职博士后工作;2016年至2017年在加拿大约克大学做公派访问学者。近几年主持国家自然科学基金2项,教育部科研费项目5项、其它省部级及校企合作横向项目3项。曾参与多个国家自然科学基金重点项目、973项目的科研工作。目前担任中国机械工程学会高级会员,中国振动工程学会高级会员,中国转子动力学理事会理事,中国故障诊断学会理事,辽宁省振动工程学会理事会理事。参编著作2部,获批发明专利5项。在Journal of Sound and VibrationNonlinear DynamicsInternational Journal of Mechanical SciencesThin-Walled StructuresApplied Mathematical ModellingMechanical Systems and Signal ProcessingJournal of Vibration and Control、机械工程学报、振动工程等SCI/EI收录的期刊上等发表学术论文60余篇,SCI检索20余篇,EI检索50余篇;授权及申请国家发明专利近10项,软件著作权10余项。目前兼任Nonlinear DynamicsJournal of Sound and VibrationJournal of Vibration and ControlJournal of Mechanical Science and Technology、机械工程学报、北京航空航天大学学报等著名国内外期刊审稿专家。

  

二、教育经历:

2007/03–2010/01,东北大学,机械设计及理论专业,工学博士;

2005/09–2007/07,东北大学,机电一体化专业,工学硕士;

2000/09–2004/07,鞍山科技大学,机械工程及自动化专业,工学学士。

  

三、工作经历:

2014/01–至今,东北大学,机械工程与自动化学院,副教授;

2016/12–2017.12,加拿大York University,机械工程系,访问学者;

2010/10–2014/10,沈阳鼓风机集团有限公司,博士后;

2010/01–2013/12,东北大学,机械工程与自动化学院,讲师;

  

四、研究方向:

(1) 航空发动机转动部件耦合结构动力学;

(2) 旋转机械振动噪声分析与故障诊断研究;

(3) 复合材料及智能材料结构动力学;

(4) 基于虚拟仪器技术的振动测试与控制。

  

五、讲授课程:

本科生课程:《有限元及计算机辅助分析》、《机械工程创新训练》、《人生哲学方法论》

研究生课程:《机械系统动力学》、《机械产品动态优化设计》、《振动利用工程》

  

六、发表论文:

目前共发表学术论文70余篇,其中第1作者或通讯作者50余篇,部分论文如下:

[1].Li Chaofeng*, Tang Qiansheng, Xi Chenyang, Zhong Bingfu, Wen Bangchun. Coupling vibration behaviors of drum-disk-shaft structures with elastic connection. International Journal of Mechanical Sciences, 2019,155(5): 392-404.

[2].Li Chaofeng *, Zhong Bingfu , Shen Zengchuang, Zhang Jinrui . Modeling and nonlinear vibration characteristics analysis of symmetrically 3-layer composite thin circular cylindrical shells with arbitrary boundary conditions. Thin-Walled Structures, 2019, 142: 311-321.

[3].Li Chaofeng *, Li Peiyong, Zhong Bingfu, Wen Bangchun. Geometrically nonlinear vibration of laminated composite cylindrical thin shells with non-continuous elastic boundary conditions. Nonlinear Dynamics, 2019,95(3): 1903–1921.

[4].Li Chaofeng*, She Houxin, Tang Qiansheng, Wen Bangchun. The coupling vibration characteristics of a flexible shaft-disk-blades system with mistuned features. Applied Mathematical Modelling, 2019, 67: 557-572.

[5].Tang Qiansheng, Li Chaofeng*, She Houxin, Wen Bangchun. Nonlinear response analysis of bolted joined cylindrical-cylindrical shell with general boundary condition. Journal of Sound and Vibration, 2019, 443(17):788-803.

[6].Li Chaofeng*, Zhang Zijian, Liu Xiaowen, Shen Zengchuang. An Improved Principle of Rapid Oscillation Suppression of a Pendulum by a Controllable Moving Mass: Theory and Simulation. Shock and Vibration, 2019, Article ID 5346463, 11 pages.

[7].Li Chaofeng*, Li Tao, Qiao Ruihuan, Wen Bangchun. Study on the Damping Mechanism of the Shrouded Blade Considering Contact Features. Shock and Vibration, 2019, Article ID 6594345, 11 pages.

[8].Peiyong Li, Chaofeng Li*, Ruihuan Qiao, Bangchun Wen. Sensitivity on the non-continuous supported laminated cylindrical shell to boundary conditions and lamination schemes. Archive of Applied Mechanics, 2019, 1-20.[online]

[9].She Houxin, Li Chaofeng *, Tang Qiansheng, Wen Bangchun. The investigation of the coupled vibration in a flexible-disk blades system considering the influence of shaft bending vibration. Mechanical Systems and Signal Processing, 2018, 111(2018): 545-569.

[10].Tang Qiansheng, LiChaofeng *, She Houxin, Wen Bangchun. Modeling and dynamic analysis of bolted joined cylindrical shell. Nonlinear Dynamics, 2018,93(4): 1953-1975.

[11].Tang Qiansheng, LiChaofeng *, She HouXin, Wen Bangchun.Vibration analysis of bolted joined cylindrical-cylindrical shell structure under general connection condition. Applied Accoustics,2018, 140, 236-247

[12].Li Chaofeng *, Tang Qiansheng, She Houxin, Wen Bangchun. Natural characteristic of thin-wall pipe under uniformly distributed pressure. Chinese Journal of Mechanical Engineering, 2018, 31(1): 1-10.

[13].Li Chaofeng*, Shen Zengchuang, Zhong Bingfu, Wen Bangchun. Study on the nonlinear characteristics of a rotating flexible blade with dovetail interface feature. Shock and Vibration, 2018, Article ID 4923898, 13 pages.

[14].Li Chaofeng*, Miao Boqing, Tang Qiansheng, Xi Chenyang, Wen Bangchun. Nonlinear vibrations analysis of rotating drum-disk coupling structure. Journal of Sound and Vibration.2018, 420(4): 35-60.

[15].Li Chaofeng*, She Houxin, Tang Qiansheng, Wen Bangchun. The effect of blade vibration on the nonlinear characteristics of rotor-bearing system supported by nonlinear suspension, Nonlinear Dynamics, 2017, 89(2), 987-1010.

[16].Li Chaofeng *, She Houxin, Liu Wen, Wen Bangchun. The influence of shaft’s bending on the coupling vibration of a flexible blade-rotor system. Mathematical Problems in Engineering, 2017, Article ID 7313956, 19 pages.

[17].Li Chaofeng *, Tang Qiansheng, Miao Boqing, Wen Bangchun. The sensibility on dynamic characteristics of pre-pressure thin-wall pipe under elastic boundary conditions. Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science, 2017, 231(6): 995-1009.

[18].Tang Qiansheng, LiChaofeng *, Wen Bangchun. Analysis on forced vibration of thin-wall cylindrical shell with nonlinear boundary condition. Shock and vibration, 2016, Article ID 8978932, 22 pages.

[19].Li Chaofeng*, Tang Qiansheng; Wen Bangchun. Nonlinear dynamic behavior analysis of pressure thin-wall pipe segment with supported clearance at both ends. Mathematical Problems in Engineering , 2016, Article ID 5432516, 22 pages.

[20].Li Chaofeng *, Zhou Shihou, Liu Jie, Wen Bangchun. Coupled lateral-torsional-axial vibrations of a helical gear-rotor-bearing system. Acta Mechanica Sinica, 2014, 30(5): 746-761.

[21].Li Chaofeng*, Zhou Shihua, Jiang Shijie, Yu Hexing, Wen Bangchun.Investigation on the stability of periodic motions of a flexible rotor-bearing system with two unbalanced disks. Journal of Mechanical Science and Technology, 2014, 28(7): 2561-2579.

[22].李朝峰*, 佘厚鑫, 李超, 闻邦椿. 弹支阀片双筒液压减振器的阻尼特性. 东北大学学报 (自然科学版), 2018, 39(10), 1480-1485.

[23].杨青玉, 李朝峰*, 杨树华, 孟继纲, 李凯华. 应用Labview开发非接触式压缩机叶片模态测试系统. 风机技术, 2018, 60(1): 53-60

[24].宁宝奇, 李朝峰*, 杨树华, . 轴流叶片非接触式模态特性测试系统的开发与研究. 航空发动机, 2017, 43(6):76-83.

[25].李朝峰*, 刘文, 佘厚鑫, 闻邦椿. 弹性叶片-轮盘-转轴系统的耦合振动特性. 振动工程学报, 2016,29(5):894-899.

[26].唐千升, 李朝峰*, 闻邦椿. 带有支承间隙的压力管道振动非线性动力学行为研究. 振动工程学报, 2016(6):1028-1033.

[27].李朝峰*, 胡永, 武斌,. 声致薄壁管道破坏抑制机理及实验研究. 风机技术, 2016(2):17-22.

[28].李朝峰*, 周世华, 任翔, 闻邦椿.含有失谐特征的叶片-转盘-转轴转子系统动态特性. 航空动力学报, 2015,30(1):67-75.

[29].李朝峰*,周世华, 杨树华, 刘广超. 含有碰摩故障的多盘双转子系统动态特性. 东北大学学报 (自然科学版), 2014, 35(5): 726-730.

[30].李朝峰*, 周世华, 刘文明, 任朝晖, 闻邦椿. 齿轮-转子-滚动轴承传动系统的弯扭耦合振动. 航空动力学报, 2014,29(7):1543-1555.

  

七、科研项目:

[1].国家自然科学基金面上基金,51575093,航空发动机叶片-轮盘-鼓筒装配部件的耦合动力学及其振动局部化控制研究、2016/01-2019/12,主持;

[2].教育部中央高校基本科研业务费项目,N160313001,航空发动机多界面耦连部装结构动力学特性研究,2017/01-2018/12,主持;

[3].辽宁省科技厅自然科学基金面上项目,2015020153,复杂载荷作用下旋转鼓筒振动特性及其控制研究、2015/07-2017/06,主持;

[4].国家自然科学基金青年基金,51105063,旋转叶片-机匣碰摩的精细化建模与振动局部化研究、2012/01-2014/12,主持;

[5].教育部中央高校基本科研业务费项目,N140304002,航空发动机叶片-轮盘-鼓筒耦合结构的振动局部化及其抑制研究,2015/01-2016/12,主持;

[6].教育部中央高校基本科研业务费项目,N120403004,复杂环境下叶片-转子-轴承系统的碰摩故障与振动特性研究,2013/01-2014/12,主持;

[7].国家重点基础研究发展计划(“973”计划)子课题,2009JX9730012010/01-2014/12,执行负责;

[8].教育部中央高校基本科研业务费项目,N100303001,含故障多跨转子系统的动态特性及稳定性研究,2011/01-2012/12,主持;

[9].中国博士后科学基金面上项目,20100480056,复杂转子系统由突变不平衡引起的碰摩故障动态特性及稳定性研究,2011/01-2012/12,主持;

[10].企业服务项目,轴流叶片时域共振法模态测试软件系统开发,2016/01/01-2018/12/31,主持;

[11].企业服务项目,充气式汽车减振器非线性动力学特性研究,2014/12/01-2017/06/31,执行负责。

  

八、联系方式:

Email: chfli@mail.neu.edu.cn; chaof.li@foxmail.com

通讯地址:辽宁省沈阳市和平区文化路三巷11号,东北大学319信箱。邮编:110819