Calculation and Improvement for Air Cooling Structure ofElectrical Aircraft Motor Controller
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(1. School of Electrical Engineering, Shenyang University of Technology, Shenyang 110870, China;2. Liaoning General Aviation Academy, Shenyang 110136, China;3. National Engineering Laboratory for Electric Vehicles, Beijing Institute of Technology,Beijing 100081, China)

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    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%.

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WANG Shuli, MA Shaohua, ZHANG Shuo. Calculation and Improvement for Air Cooling Structure ofElectrical Aircraft Motor Controller[J]. Electric Machines & Control Application,2019,46(6):84-90.

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  • Received:April 10,2019
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  • Online: December 02,2019
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