电动飞机专栏

某型双座电动飞机设计与试验

  • 范振伟 ,
  • 杨凤田 ,
  • 李亚东 ,
  • 项松 ,
  • 赵为平
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  • 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

  网络出版日期: 2020-07-27

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 ,
  • YANG Fengtian ,
  • LI Yadong ,
  • XIANG Song ,
  • ZHAO Weiping
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  • 1. Key Laboratory of General Aviation, Shenyang Aerospace University, Shenyang 110136, China;
    2. Liaoning General Aviation Research Institute, Shenyang 110136, China

Received date: 2020-03-14

  Revised date: 2020-04-02

  Online published: 2020-07-27

Supported by

Projects of Education Department of Liaoning Province (JYT19004, JYT19022, JYT2020161, JYT2020162)

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。

本文引用格式

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 . DOI: 10.7527/S1000-6893.2020.23972

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.

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