某型双座电动飞机设计与试验

doi:10.7527/S1000-6893.2020.23972

电动飞机专栏

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某型双座电动飞机设计与试验

范振伟^1,2, 杨凤田^1,2, 李亚东^1,2, 项松^1,2, 赵为平¹

1. 沈阳航空航天大学通用航空重点实验室, 沈阳 110136;
2. 辽宁通用航空研究院, 沈阳 110136

收稿日期:2020-03-14 修回日期:2020-04-02 发布日期:2020-07-27
通讯作者: 赵为平 E-mail:3370477370@qq.com
基金资助:
辽宁省教育厅重点攻关和服务地方项目（JYT19004，JYT19022，JYT2020161，JYT2020162）

Design and test of two-seater electric aircraft

FAN Zhenwei^1,2, YANG Fengtian^1,2, LI Yadong^1,2, XIANG Song^1,2, ZHAO Weiping¹

1. Key Laboratory of General Aviation, Shenyang Aerospace University, Shenyang 110136, China;
2. Liaoning General Aviation Research Institute, Shenyang 110136, China

Received:2020-03-14 Revised:2020-04-02 Published:2020-07-27
Supported by:
Projects of Education Department of Liaoning Province (JYT19004, JYT19022, JYT2020161, JYT2020162)

摘要/Abstract

摘要： 沈阳航空航天大学一直致力于新能源电动飞机的研制，某型双座轻型电动飞机于2012年6月立项研制，该型电动飞机采用一台40 kW稀土永磁同步直流电机作为动力装置，全复合材料机体和板簧起落架结构。巡航升阻比24.1，起飞总重500 kg，最大飞行速度160 km/h，巡航速度110 km/h。该型电动飞机具有零排放、低噪声、运行成本低、使用维护方便等特点。参照中国民航CCAR-21部和美国ASTM标准，完成了电动飞机型号设计批准书TDA和生产许可PC取证。

关键词: 电动飞机, 双座, 锂电池, 气动特性, 飞行试验

Abstract: 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.

Key words: electric aircraft, two-seater, lithium battery, aerodynamics, flight test

中图分类号:

V221

范振伟, 杨凤田, 李亚东, 项松, 赵为平. 某型双座电动飞机设计与试验[J]. 航空学报, 2021, 42(3): 623972-623972.

FAN Zhenwei, YANG Fengtian, LI Yadong, XIANG Song, ZHAO Weiping. Design and test of two-seater electric aircraft[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(3): 623972-623972.

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E-mail：hkxb@buaa.edu.cn

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某型双座电动飞机设计与试验

Design and test of two-seater electric aircraft

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