Advanced Search
Volume 38 Issue 9
Sep.  2012
Turn off MathJax
Article Contents
Journal of Beijing University of Aeronautics and Astronautics  > 2012  >  (9): 1139-1143,1153.
Nie Zi, Chen Ming. Calculation and analysis of electric-powered helicopter flight performance[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, (9): 1139-1143,1153. (in Chinese)
Citation: Nie Zi, Chen Ming. Calculation and analysis of electric-powered helicopter flight performance[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, (9): 1139-1143,1153. (in Chinese)
shu

Calculation and analysis of electric-powered helicopter flight performance

  • School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 16 Aug 2011
  • Publish Date: 30 Sep 2012
    Abstract
  • Based on the traditional method, a calculation method of electric-powered helicopter flight performance was proposed, which combined with the features of electric-power system and the characteristics of helicopter preliminary design. The influence of different variables and parameters on flight performance was analyzed. By taking a small-scale helicopter as an example, the flight performance before and after was calculated and compared. The calculated results and analysis show that electric-powered helicopter with short endurance due to battery technology limitation has higher ceiling. Compared with light and medium helicopter, micro and small-scale helicopter have a lot of advantage and latent capacity. This method is applicable to electric-powered helicopter preliminary design and parameter selection, which is also significant for helicopter.

     

    • FullText(HTML)
  • loading
    • References(14)
  • [1]
    许震宇,周华,杨志刚.电动力轻型飞机的研制[J].航空科学技术,2007 (6):26-30
    Xu Zhenyu, Zhou Hua, Yang Zhigang.Design of an electric powered light aircraft[J].Aviation Science and Technology,2007 (6):26-30 (in Chinese).
    [2]
    Moore M D.NASA Puffin electric tailsitter VTOL concept [R].AIAA 2010-9345,2010.
    [3]
    Lawrence D A,Mohseni K.Efficiency analysis for long-duration electric MAVs[R].AIAA 2005-7090,2005.
    [4]
    Stepaniak M J,van Graas F,de Haag M U.Design of an electric propulsion system for a quadrotor unmanned aerial vehicle [J].Journal of Aircraft,2009,46 (3):1050-1058.
    [5]
    Guinea D M,Roura M,Garcia-Alegra M C,et al.Specific weight:a challenge for a fuel-cell-powered electric helicopter [J].Journal of Aircraft,2007,44 (6):2073-2076.
    [6]
    刘斌,马晓平,王和平,等.小型电动无人机总体参数设计方法研究[J].西北工业大学学报,2005,23 (3):396-400
    Liu Bin,Ma Xiaoping,Wang Heping,et al.Design analysis methodology for electric-powered mini-UAV[J].Transactions of Northwestern Polytechnical University,2005,23 (3):396-400 (in Chinese).
    [7]
    刘伏虎,马晓平.小型电动无人机续航性能提升方法研究[J].飞行力学,2010,28 (5):13-15
    Liu Fuhu,Ma Xiaoping.Research for improving the endurance performance of minitype electric-powered UAV[J].Fight Dynamics,2010,28 (5):13-15 (in Chinese).
    [8]
    张呈林,郭才根.直升机总体设计[M].北京:国防工业出版社,2006:40-49
    Zhang Chenglin, Guo Caigen.Helicopter preliminary design[M].Beijing:Defense Industry Press,2006:40-49 (in Chinese).
    [9]
    蒋新桐.飞机设计手册第19册:直升机设计[M].北京,航空工业出版社,2005:166-170
    Jiang Xintong.Aircraft design handbook No19:helicopter design[M].Beijing:Aviation Industry Press,2005:133-170 (in Chinese).
    [10]
    王适存.直升机空气动力学[M].北京:航空专业教材编审组,1985:18-29
    Wang Shicun.Helicopter aerodynamics[M].Beijing:Aviation Professional Material Editing Group,1985:18-29 (in Chinese).
    [11]
    Ohad Gur,Aviv Rosen.Optimizing electric propulsion systems for unmanned aerial vehicles [J].Journal of Aircraft,2009,46 (4): 1340-1352.
    [12]
    Thipyopas C,Poutrique S,Barenes R,et al.Aerodynamic analysis of a multi-mission short-shrouded coaxial UAV:part Ⅱ—translation flight[R].AIAA 2010-1427,2010.
    [13]
    陈军,杨树兴,张国庆,等.炮射电动无人机总体概念设计方法研究[J].北京理工大学学报,2009, 29 (9):767-770
    Chen Jun,Yang Shuxing,Zhang Guoqing,et al.Conceptual design of electric-powered gun launched UAV[J].Transactions of Beijing Institute of Technology,2009, 29 (9):767-770 (in Chinese).
    [14]
    昌敏,周洲,张健,等.某型手掷电动无人机总体设计与飞行试验研究[J].飞行力学,2010,28 (2):82-84
    Chang Min,Zhou Zhou,Zhang Jian,et al.Design and flight test resarch for hand-launched electric-powered UAV [J].Fight Dynamics,2010,28 (2):82-84 (in Chinese).
    • Relative Articles
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF
    XML

    Article Metrics

    Article views(2769) PDF downloads(1483) Cited by()
    Proportional views
    Related

    Copyright © Journal of Beijing University of Aeronautics and Astronautics

    Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn

    Supported by: Beijing Renhe Information Technology Co., Ltd.    

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return