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

本期目录 | 过刊浏览 | 高级检索

前一篇 | 后一篇

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.

参考文献

[1] 黄俊, 杨凤田. 新能源电动飞机发展与挑战[J]. 航空学报, 2016, 37(1):57-68. HUANG J, YANG F T. Development and challenges of electric aircraft with new energies[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(1):57-68(in Chinese).
[2] 范振伟, 杨凤田, 项松,等. 我国电动飞机发展现状及建议[J]. 航空科学技术, 2019, 30(11):18-21. FAN Z W, YANG F T, XIANG S, et al. Present situation and advice of electric aircraft development in China[J]. Aeronautical Science & Technology, 2019, 30(11):18-21(in Chinese).
[3] 刘星. 混合动力及全电动飞机渐成新趋势[J]. 电气技术, 2019, 7(1):57-68. LIU X. Hybrid and all-electric aircraft are becoming a new trend[J]. Electric Technology, 2019, 7(1):57-68(in Chinese).
[4] 项松, 刘远强, 佟刚, 等. 某型电动飞机螺旋桨的设计与试验[J]. 西北工业大学学报, 2016, 34(3):460-465. XIANG S, LIU Y Q, TONG G, et al. Design and test of an electric pouered aircraft propeller[J]. Journal of Northwestern Polytechnical University, 2016, 34(3):460-466(in Chinese).
[5] 刘福佳, 杨凤田, 刘孟诏, 等. 电动轻型飞机起飞总质量估算方法[J]. 科学技术与工程, 2018, 18(5):118-123. LIU F J, YANG F T, LIU M Z, et al. Estimated meth-od of the take-off mass of the electric light aircraft[J]. Science Technology and Engineering, 2018, 18(5):118-123(in Chinese).
[6] 王书礼, 马少华. 电动飞机电机控制器风冷散热结构的计算与改进水[J]. 电机与控制应用, 2019, 46(6):86-90. WANG S L, MA S H. Calculation and lmprovement for air cooling structure of electrical aircraft moyor controller[J]. Electric Machines & Control Application, 2019, 46(6):86-90(in Chinese).
[7] 顾超, 黄俊, 杨凤田. 电动通用飞机复合材料结构设计及验证技术[J]. 航空制造技术, 2017, 13:93-98. GU C, HUANG J, YANG F T. Structure design and test technologyof electric general aircraft with composite materials[J]. Aeronautical Manufacturing Technology, 2017, 13:93-98(in Chinese).
[8] 康桂文, 胡雨. 超轻型电动飞机电动力系统的参数匹配[J]. 航空动力学报, 2013, 28(12):2641-2647. KANG G W, HU Y. Parameters matching of ultralight electric aircraft propulsion system[J]. Journal of Aerospace Power, 2013, 28(12):2641-2647(in Chinese).
[9] 李玉峰, 宁昭义. 电动飞机电推进系统可靠性建模与仿真[J]. 计算机仿真, 2019, 36(1):51-56. LI Y F, NING Z Y. Reliability modeling and simulation of electric aircraft electric propulsion system[J]. Computer Simulation, 2019, 36(1):51-56(in Chinese).
[10] 赵为平, 项松. 电动飞机系统可靠性分配方法研究[C]//2019年(第四届)中国航空科学技术大会论文集,2019. ZHAO W P, XIANG S. Reliability modeling and simula-tion of electric aircraft electric propulsion system[C]//Proceedings of the 2019(Fourth) China Aviation Science and Technology Conference, 2019(in Chinese).
[11] XIANG S, LIU Y Q, TONG G, et al. An improved propeller design method for the electric aircraft[J]. Aerospace Science and Technology, 2018, 78:488-493.
[12] 项松, 刘远强, 赵为平. 电动飞机螺旋桨气动性能计算与试验[C]//2019年(第四届)中国航空科学技术大会论文集,2019:1131-1135. XIANG S, LIU Y Q, ZHAO W P. Calculation and test of aerodynamic performance of electric aircraft propellers[C]//Proceedings of the 2019(Fourth) China Aviation Science and Technology Conference, 2019:1131-1135(in Chinese).
[13] ROMEO G, CESTINO E, PACINO M, et al. Design and testing of a propeller for a two-seater aircraft powered by fuel cells[J]. Proceedings of the Institution of Mechanical Engineers, Part G:Journal of Aerospace Engineering, 2012, 226(7):804-816.
[14] ROMEO G, FRULLA G. HELIPLAT®:High altitude very-long endurance solar powered UAV for telecommunication and Earth observation applications[J]. The Aeronautical Journal, 2004, 108(1084):277-293.
[15] ROMEO G, BORELLO F. Design and realisation of a two-seater aircraft powered by fuel cell electric propulsion[J]. The Aeronautical Journal, 2010, 114(1155):281-297.
[16] CHEN P W, CHEN K J. A crashworthiness simulation for a light aircraft constructed of composite materials[J]. Transactions of the Canadian Society for Mechanical Engineering, 2015, 39(4):829-843.
[17] AZADEH S S, BIERLAIRE M, MAKNOON M Y. A two-stage route optimization algorithm for light aircraft transport systems[J]. Transportation Research, 2019, 100:259-273.
[18] FROSINA E, CAPUTO C, MARINARO G, et al. Modelling of a hybrid-electric light aircraft[J]. Energy Procedia, 2017, 126:1155-1162.
[19] CARLO R, FEDERICO G, LORENZO T. Preliminary weight sizing of light pure-electric and hybrid-electric aircraft[J]. Transportation Research Procedia, 2018, 29:376-389.
[20] LEE S J, SHIM Y H, KIM D H, et al. RGPS-Based automatic landing system for light and commuter aircraft[J]. IFAC Proceedings Volumes, 1998, 31(21):413-418.
[21] 李亚东, 张子军, 杨凤田,等. 某型电动飞机起飞爬升性能分析及飞行试验[J]. 科学技术与工程, 2019, 19(35):364-369. LI Y D, ZHANG Z J, YANG F T, et al. Take-off and climb performance analysis and flight test of an electric aircraft[J]. Science Technology and Engineering, 2019, 19(35):364-369(in Chinese).
[22] 周明, 周洲. 某电动飞翼无人机横航向稳定性飞行试验研究[J]. 飞行力学, 2009, 27(4):70-73. ZHOU M, ZHOU Z. Flight test of lateral heading stability of an electric flying wing UAV[J]. Flight Mechanics, 2009, 27(4):70-73(in Chinese).
[23] 刘福佳, 杨凤田, 刘远强,等. 电动轻型飞机电推进系统选型与参数匹配[J]. 南京航空航天大学学报, 2019, 51(3):350-356. LIU F J, YANG F T, LIU Y Q, et al. Selection and parameter matching of electric propulsion system for electric light aircraft[J]. Journal of Nanjing University of Aeronautics and Astronautics, 2019, 51(3):350-356(in Chinese).

E-mail：hkxb@buaa.edu.cn

关于我们

期刊社服务

专业学科

封面文章

友情链接

主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

某型双座电动飞机设计与试验

Design and test of two-seater electric aircraft

RichHTML

PDF (PC)

可视化

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 15

编辑推荐

Metrics

本文评价

[1]	宋亚辉, 樊高宇, 瞿丽霞, 张跃林, 徐悦, 韩硕. 航空器声爆飞行试验测量技术研究进展[J]. 航空学报, 2023, 44(2): 626186-626186.
[2]	周伟, 马培洋, 郭正, 王道平, 周睿孙. 基于翼尖链翼的组合固定翼无人机研究[J]. 航空学报, 2022, 43(9): 325946-325946.
[3]	伍强, 徐浩军, 魏扬, 裴彬彬, 薛源. 结冰条件下飞机气动/运动耦合特性[J]. 航空学报, 2022, 43(8): 125566-125566.
[4]	岑飞, 刘志涛, 蒋永, 郭天豪, 张磊, 孔轶男. 民机极限飞行状态非定常气动力建模[J]. 航空学报, 2022, 43(8): 125582-125582.
[5]	赵鲲, 梁俊彪, Ivan BELYAEV, Victor KOPIEV, Gareth BENNETT. 民用飞机起落架噪声及其控制技术研究进展[J]. 航空学报, 2022, 43(8): 26996-026996.
[6]	周宜涛, 杨阳, 吴志刚, 杨超. 大展弦比无人机平台的阵风减缓飞行试验[J]. 航空学报, 2022, 43(6): 526126-526126.
[7]	陈广强, 豆国辉, 魏昊功, 邹昕, 李齐, 刘周, 周伟江. 火星探测器大气数据测量方法[J]. 航空学报, 2022, 43(3): 626619-626619.
[8]	徐欣, 贾贺, 陈雅倩, 荣伟, 蒋伟, 薛晓鹏. 织物透气性对火星用降落伞气动特性影响机理[J]. 航空学报, 2022, 43(12): 126289-126289.
[9]	陈艺夫, 王一雯, 邓一菊, 王波, 白俊强, 卢磊. 自然层流机翼的翼套试验及数值方法[J]. 航空学报, 2022, 43(11): 526793-526793.
[10]	王猛, 李玉军, 赵荣奂, 衷洪杰. 基于在线加热涂层的宽速域转捩探测技术[J]. 航空学报, 2022, 43(11): 526820-526820.
[11]	周桢尧, 吕飞, 周斌, 杨钊. 自然层流减阻验证方法及验证翼段布局设计[J]. 航空学报, 2022, 43(11): 526751-526751.
[12]	王浩, 钟敏, 华俊, 钟海, 杨体浩, 王猛, 雷国东. 自然层流飞行测试翼套的仿真和试验[J]. 航空学报, 2022, 43(11): 526785-526785.
[13]	杨超, 邱祈生, 周宜涛, 吴志刚. 飞机阵风响应减缓技术综述[J]. 航空学报, 2022, 43(10): 527350-527350.
[14]	付军泉, 史志伟, 耿玺, 朱佳晨, 王力爽, 吴大卫, 潘立军. 基于试验分岔分析的翼身融合飞行器纵向稳定性[J]. 航空学报, 2022, 43(1): 124931-124931.
[15]	饶崇, 张铁军, 魏闯, 刘影. 一种分布式电动飞机螺旋桨滑流影响机理[J]. 航空学报, 2021, 42(S1): 726387-726387.