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电动飞机电机控制器风冷散热结构的计算与改进
引用本文:王书礼,马少华,张硕.电动飞机电机控制器风冷散热结构的计算与改进[J].航空动力学报,2019,46(6):84-90.
作者姓名:王书礼  马少华  张硕
作者单位:沈阳工业大学 电气工程学院,辽宁 沈阳110870;辽宁通用航空研究院,辽宁 沈阳110136,沈阳工业大学 电气工程学院,辽宁 沈阳110870,北京理工大学 电动车辆国家工程实验室,北京100081
基金项目:辽宁省教育厅科学技术研究项目(LZGD2017041)
摘    要:根据电动飞机的飞行剖面,建立了电机控制器的系统损耗及IGBT模块的热阻网络模型,对电机控制器IGBT模块的温度进行计算。以轻量小型化为目标,对电机控制器的散热结构进行了改进。MATLAB/Simulink系统仿真试验和地面台架样机试验结果表明:改进的风冷散热器能够满足电动飞机电机控制器的散热需求,且重量降低5%。

关 键 词:电机控制器    电动飞机    IGBT模块    风冷散热器    系统仿真
收稿时间:2019/4/10 0:00:00

Calculation and Improvement for Air Cooling Structure ofElectrical Aircraft Motor Controller
WANG Shuli,MA Shaohua and ZHANG Shuo.Calculation and Improvement for Air Cooling Structure ofElectrical Aircraft Motor Controller[J].Journal of Aerospace Power,2019,46(6):84-90.
Authors:WANG Shuli  MA Shaohua and ZHANG Shuo
Institution:School of Electrical Engineering, Shenyang University of Technology, Shenyang 110870, China;Liaoning General Aviation Academy, Shenyang 110136, China,School of Electrical Engineering, Shenyang University of Technology, Shenyang 110870, China and National Engineering Laboratory for Electric Vehicles, Beijing Institute of Technology,Beijing 100081, China
Abstract:According to the flight profile of the electric aircraft, the system loss of the motor controller was studied, the thermal resistance network model of the IGBT module was established, and the temperature of the IGBT module of the motor controller was calculated. On the premise of meeting the allowable temperature of motor controller, the cooling structure of IGBT module was improved. The results of MATLAB/Simulink simulation and ground bench test showed that the improved aircooled radiator could meet the cooling requirements of electric aircraft motor controller, and the weight of the aircooled radiator was reduced by 5%.
Keywords:motor controller  electric aircraft  IGBT module  air cooling radiator  system simulation
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