首页 > 专家库
李朝峰

领域:高端装备制造产业 学校:东北大学职称:副教授

(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。...

具体了解该专家信息,请致电:027-87555799 邮箱 haizhi@uipplus.com

教育背景

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。

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;

项目课题经历

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ᠦ୔

论文、成果、著作等

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, 等. 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,等. 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.

专利、著作版权等

授权及申请国家发明专利近10项,软件著作权10余项
声明:本站专家信息来源于各高校官网。