首页 | 本学科首页   官方微博 | 高级检索  
     检索      

某型双座电动飞机设计与试验
引用本文: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.
作者姓名:范振伟  杨凤田  李亚东  项松  赵为平
作者单位: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
基金项目:辽宁省教育厅重点攻关和服务地方项目(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。

关 键 词:电动飞机  双座  锂电池  气动特性  飞行试验  
收稿时间:2020-03-14
修稿时间:2020-04-02

Design and test of two-seater electric aircraft
FAN Zhenwei,YANG Fengtian,LI Yadong,XIANG Song,ZHAO Weiping.Design and test of two-seater electric aircraft[J].Acta Aeronautica et Astronautica Sinica,2021,42(3):623972-623972.
Authors:FAN Zhenwei  YANG Fengtian  LI Yadong  XIANG Song  ZHAO Weiping
Institution:1. Key Laboratory of General Aviation, Shenyang Aerospace University, Shenyang 110136, China;2. Liaoning General Aviation Research Institute, Shenyang 110136, China
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.
Keywords:electric aircraft  two-seater  lithium battery  aerodynamics  flight test  
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号