• DocumentCode
    2336386
  • Title

    A new type of flapping-wing mechanism and the character measurement

  • Author

    Liu Yun ; Jiangang Lv ; Hongzhi Teng

  • Author_Institution
    Dept. of Artillery Eng., Mech. Eng. Coll., Shijiazhuang
  • fYear
    2009
  • fDate
    25-27 May 2009
  • Firstpage
    1724
  • Lastpage
    1726
  • Abstract
    The research background of bionic flapping-wing mechanism is introduced; the characteristics and the application prospect are analyzed. It is concluded that bionic flapping-wing flying has better lift fore generation efficiency, which is the development trend of aerial vehicles. By the scaling effect analysis on bionic flying mechanism, it is presented that bionic flying could be realized more easily when the sizes are decreased. In this article, the flying mechanism of inset and Aves was studied and the high lift force mechanism of flapping-winging was concluded. In order to make the flapping-flying easier, we design a new type flapping-flying mechanism. A set of flapping-wing move comparatively. It can provide lift force all the time. We test the lift force in the condition of different speed and different frequency. The lift effect is validated on a simple suspend flight device. An experimental platform to measure the aerodynamic force is devised and developed by ourselves. On this equipment, the aerodynamics force of the prototype is test. The result is that enhancing speed or frequency can improve lift force in evidence.
  • Keywords
    aerial equipment; aerospace components; aerospace simulation; biocybernetics; aerial vehicles; bionic flying mechanism; character measurement; flapping-wing mechanism; Aerodynamics; Aircraft; Animals; Birds; Force measurement; Frequency; Insects; Intelligent sensors; Intelligent systems; Testing; flapping-wing mechanism; measurement;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Industrial Electronics and Applications, 2009. ICIEA 2009. 4th IEEE Conference on
  • Conference_Location
    Xi´an
  • Print_ISBN
    978-1-4244-2799-4
  • Electronic_ISBN
    978-1-4244-2800-7
  • Type

    conf

  • DOI
    10.1109/ICIEA.2009.5138491
  • Filename
    5138491