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Kinematic, Static and Dynamic Analyses of Flapping Wing Mechanism Based on ANSYS Workbench

Conference paper
Part of the Lecture Notes in Computer Science book series (LNCS, volume 10639)

Abstract

A method for kinematic, static and dynamic analyses of single degree of freedom flapping wing aircraft is shown in this paper. All the analyses are realized completely by using ANSYS Workbench. A 3D model built in SolidWorks is imported into ANSYS Workbench. Firstly, a rigid body dynamic analysis is implemented to judge the connections among joints and get the maximum joint forces to find potentially dangerous positions of the movement. Then, a static analysis is carried out to check deformation and stress of the mechanism. On the basis of above analyses, modal analysis and transient dynamic analysis are respectively achieved to determine the stress under dynamic loads, with the obtained results clearly demonstrating the rationality of the designed flapping wing mechanism.

Keywords

Flapping wing aircraft ANSYS Workbench Rigid body dynamic analysis Static analysis Transient dynamic analysis 

References

  1. 1.
    Mahjoubi, H., Byl, K.: Efficient flight control via mechanical impedance manipulation: energy analyses for hummingbird-inspired MAVs. J. Intell. Robot. Syst. 73(1), 487–512 (2014)CrossRefGoogle Scholar
  2. 2.
    Colmenares, D., Kania, R., Zhang, W., Sitti, M.: Compliant wing design for a flapping wing micro air vehicle. In: 2015 IEEE Conference on IROS, Hamburg, Germany, pp. 32–39 (2015)Google Scholar
  3. 3.
    Ryu, S., Kwon, U., Kim, H.J.: Autonomous flight and vision-based target tracking for a flapping-wing MAV. In: 2016 IEEE Conference on IROS, Daejeon, South Korea, pp. 5645–5650 (2016)Google Scholar
  4. 4.
    Hassanalian, M., Abdelkefi, A., Wei, M., Ziaei-Rad, S.: A novel methodology for wing sizing of bio-inspired flapping wing micro air vehicles: theory and prototype. J. Acta Mech. 228(3), 1097–1113 (2017)CrossRefGoogle Scholar
  5. 5.
    Ramezani, A., Chung, S.J., Hutchinson, S.: A biomimetic robotic platform to study flight specializations of bats. J. Sci. Robot. 2(3), 1–12 (2017)Google Scholar
  6. 6.
    Phan, H.V., Park, H.C.: Remotely controlled flight of an insect-like tailless flapping-wing micro air vehicle. In: 2015 IEEE Conference on URAI, Goyang, South Korea, pp. 315–317 (2015)Google Scholar
  7. 7.
    Sreetharan, P.S., Wood, R.J.: Passive torque regulation in an underactuated flapping wing robotic insect. Auton. Robots 31, 225 (2011)CrossRefGoogle Scholar
  8. 8.
    İşbitirici, A., Altuğ, E.: Design of a flapping-wing aerial vehicle based on four-bar mechanism. In: 2016 IEEE Conference on ICUAS, Arlington, USA, pp. 1240–1245 (2016)Google Scholar
  9. 9.
    İşbitirici, A., Altuğ, E.: Design and control of a mini aerial vehicle that has four flapping-wings: Theory and prototype. J. Intell. Robot. Syst. pp. 1–19 (2017)Google Scholar
  10. 10.
    Negrello, F., Silvestri, P., Lucifredi, A., Guerrero, J.E., Bottaro, A.: Preliminary design of a small-sized flapping UAV: II Kinematic and structural aspects. J. Meccanica 51(6), 1369–1385 (2016)CrossRefGoogle Scholar
  11. 11.
    Jitsukawa, T., Adachi, H., Abe, T., Yamakawa, H., Umezu, S.: Bio-inspired wing-folding mechanism of micro air vehicle (MAV). Artif. Life Robot. 22, 203–208 (2016)CrossRefGoogle Scholar
  12. 12.
    Jiang, H., Zhou, C., Xie, P.: Design and kinematic analysis of seagull inspired flapping wing robot. In: 2016 IEEE Conference on ICIA, pp. 1382–1386, Ningbo, China (2016)Google Scholar
  13. 13.
    Ma, N., He, G.P., Di, J.J.: Study of velocity fluctuation of bat-like flapping wing air vehicle. J. Mech. Trans. 38, 131–137 (2014)Google Scholar

Copyright information

© Springer International Publishing AG 2017

Authors and Affiliations

  • Youpeng Li
    • 1
  • Chen Qian
    • 1
  • Bingqi Zhu
    • 2
  • Yongchun Fang
    • 1
  1. 1.Nankai UniversityTianjinChina
  2. 2.Hohai University Changzhou CampusChangzhouChina

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