Design and test of two-seater electric aircraft

被引：0
|
作者：
Fan Z. [1 ,2 ]
Yang F. [1 ,2 ]
Li Y. [1 ,2 ]
Xiang S. [1 ,2 ]
Zhao W. [1 ]
机构：
[1] Key Laboratory of General Aviation, Shenyang Aerospace University, Shenyang
[2] Liaoning General Aviation Research Institute, Shenyang
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2021年 / 42卷 / 03期
关键词：
Aerodynamics; Electric aircraft; Flight test; Lithium battery; Two-seater;
D O I：
10.7527/S1000-6893.2020.23972
中图分类号：
学科分类号：
摘要：
Shenyang Aerospace University has been committed to the development of new energy electric aircraft. The development project of a type of two-seater light electric aircraft was approved and started in June 2012, using a 40 kW rare earth permanent magnet synchronous DC motor as the power source. With all-composite body and leaf spring landing gear structure, a cruise lift to drag ratio of 24.1, take-off weight of 500 kg, a maximum flight velocity of 160 km/h, a cruise velocity of 110 km/h, the electric aircraft has the characteristics of zero emission, low noise, low operation cost and easy operation and maintenance. According to the CAAC CCAR-21 and the American ASTM standard, the electric aircraft type design approval TDA and the production certification PC are completed. © 2021, Beihang University Aerospace Knowledge Press. All right reserved.
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