A Design of Innovative Experiment Platform Based on the Research of Flapping-Wing Aircraft

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According to the fact that it need several tests to determine the size and motion parameters of the flapping-wing aircraft in the development processes, the paper proposed a design scheme of flapping wing system experimental platform. Separately from the scheme, the system platform, driving mechanism design, motion parameters change, described in detail the design and implementation of this innovation experiment platform. Users can simulate and debug the platform system to determine the performance of the flapping-wing mechanism.

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587-592

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September 2014

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© 2014 Trans Tech Publications Ltd. All Rights Reserved

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[1] Jin Xiaoyi: Bionic flapping-wing flight mechanism and wings flying robot-driven approach [D]: PhD thesis Jiangsu: Southeast University(2007).

Google Scholar

[2] Emily Chu: Study bionic flapping-wing ornithopter flight mechanisms and institutions [D]: Jiangsu Master Thesis: Nanjing University of Aeronautics and Astronautics. (2010).

Google Scholar

[3] Jin Xiaoyi, Yan Jingping, Zhou Jianhua: Bionic flapping-wing flying robot experimental study and theoretical explanation of flexible wing [J] Chinese Mechanical Engineering, 18 (9): 1028 - 1032. (2007).

Google Scholar

[4] Hou Yu, Fang Zongde, Jian-Yi Kong: Public law status of bionic flapping-wing flight micro robotics research and key technologies [J] mechanical design, 25 (7): 1-4, (2008).

Google Scholar

[5] Seiichi Sudo, Koji Tsuyuki, Toshiaki Ikohagi et al: A study on the wing structure and f-lapping behavior of a dragonfly [J]. JSME International Journal. Series C, 42 (3) : 721-729. (1999).

DOI: 10.1299/jsmec.42.721

Google Scholar

[6] John Wood, Daniel Jensen, Peter Leetsma et al: Development of next-generation ornithopter prototypes [C]. / / AUVSI Unmanned Systems North America Conference 2009. Volume 1 of 2(2009): 478-491.

Google Scholar

[7] Miao Ruiping: Flapping wing aircraft designed device drivers [J] Shenyang Institute of Aeronautical Engineering, 24 (1): 25-27. (2007).

Google Scholar

[8] Xin Zhang, Jianwu Zhang, Qingliang Zeng et al: Optimization design of four-bar linkage of hydraulic support based on ADAMS [C]. / / 2009 Second International Conference on Information and Computing Science (ICIC 2009). [V. 4] : 1513-1516.

DOI: 10.1109/icic.2009.396

Google Scholar

[9] Chen Yuan, Zhang Weiping: Miniature bionic flapping-wing aircraft [M] Shanghai: Shanghai Jiaotong University Press. (2010).

Google Scholar

[10] Duan Xia : Dynamic characteristics and the drive mechanism bionic flapping-wing flying robot research [D]: master's degree thesis, Yangzhou University. (2008).

Google Scholar

[11] Tao Ye, Zhou Ji equality: Bionic flapping-wing aircraft designed flapping wing drive mechanism to explore [J]. Machine Design and Research, 22 (2): 29. 32(2006).

Google Scholar

[12] Zhou Kai, Fang Zongde so on: Optimized single-crank and double rocker flapping wi-ng drive mechanism design [J]. Aerospace. (2008).

Google Scholar

[13] Yan Sijiang , Li Fan: Variable rod length parameterization of the kinematics simulation of four-bar mechanism [J]. Mechanical transmission. (2011), 35 (12): 46-48 DOI:. 10. 3969/j. issn. 1004-2539. 2011. 12. 012.

Google Scholar