基本信息
赵奔  男  博导  中国科学院工程热物理研究所
email: zhaoben@iet.cn
address: 北京市海淀区北四环西路11号
postalCode:

招生信息

   
招生专业
080703-动力机械及工程
招生方向
叶轮机械,热力循环,气动噪音

工作经历

   
工作简历
2018-07~2019-10,University of Michigan, 博士后
2016-09~2018-07,Michigan State University, 博士后

专利与奖励

   
专利成果
( 1 ) Noise mitigating compressor, 2018, 第 2 作者, 专利号: US20200109721A1
( 2 ) System and methods for a variable geometry turbine nozzle actuation, 2017, 第 3 作者, 专利号: US2019015 3889A1
( 3 ) Variable geometry turbine vane, 2016, 第 3 作者, 专利号: US9267427
( 4 ) Systems and methods for a variable geometry turbine nozzle, 2016, 第 2 作者, 专利号: US2016014 6100A1

出版信息

   
发表论文
(1) Investigation on effects of shock wave on vortical wake flow in a turbine nozzle cascade, Aerospace science and technology, 2020, 第 1 作者
(2) Investigation of variable orifice plate design for centrifugal compressor low-end performance improvement, aerospace science and technology, 2020, 第 1 作者
(3) Effects of grooved vanes on shock wave and forced response in a turbocharger turbine, International journal of engine research, 2019, 第 1 作者
(4) A Comprehensive analysis on the structure of groove-induced shock waves in a linear turbine, aerospace science and technology, 2019, 第 1 作者
(5) Experimental and Numerical Investigation on the Shock Wave Structure Alterations and Available Energy Loss Variations With a Grooved Nozzle Vane, ASME Journal of turbomachinery, 2018, 第 1 作者
(6) Investigation of using multi-shockwave system instead of single normal shock for improving radial inflow turbine reliability, International Journal of Heat and Fluid Flow, 2018, 第 1 作者
(7) A physics-based zero-dimensional model for the mass flow rate of a turbocharger compressor with uniform/distorted inlet condition, International Journal of Engine Research, 2018, 第 2 作者
(8) Numerical analysis for impacts of nozzle end-clearances on aerodynamic performance and forced response in a VNT turbine, Chinese Journal of Aeronautics, 2018, 第 1 作者
(9) Variable nozzle turbocharger turbine performance improvement and shock wave alternation by distributing nozzle endwall clearances, Proceedings of the Institution of Mechanical Engineers Part D Journal of automotive, 2018, 第 1 作者
(10) Impact of Inlet Distortion on Turbocharger Compressor Stage Performance, Applied Thermal Engineering, 2017, 第 1 作者
(11) A novel clocking effect between inlet bend and volute in an automotive turbocharging system, Journal of Mechanical Science and Technology, 2016, 第 1 作者

科研活动

   
科研项目
( 1 ) 中国科学院****青年项目, 主持, 部委级, 2019-11--2022-11
( 2 ) 离心压气机..................., 主持, 国家级, 2021-01--2023-12