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
Link To Document :
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