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Journal of Bionic Engineering

, Volume 16, Issue 5, pp 894–903 | Cite as

Dragonfly Inspired Nanocomposite Flapping Wing for Micro Air Vehicles

  • David KumarEmail author
  • Preetamkumar Marutrao Mohite
  • Sudhir Kamle
Article
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Abstract

The current research is aimed towards the development of dragonfly inspired nanocomposite flapping wing for micro air vehicles (MAVs). The wing is designed by taking inspiration from the hind wing of dragonfly (Anax Parthenope Julius). Carbon nanotubes (CNTs)/polypropylene nanocomposite and low-density polyethylene are used as the wing materials. The nanocomposites are developed with varying CNTs’ weight percentage (0% – 1%) and characterized for dynamic mechanical properties, which revealed that the 0.1 weight percentage case produces highest storage modulus values throughout the frequency range (1 Hz – 90 Hz). It is also observed that the storage modulus values are in the range of Young’s modulus of veins and membrane of natural insect wings. This is useful to achieve true biomimicking. Advanced manufacturing technique such as photolithography is used for wing fabrication. The length, weight and average thickness of the fabricated wing are ~44 mm, 26.22 mg and 187 μm, respectively. The structural dynamic properties of the fabricated wing are obtained experimentally and computationally using DIC and ANSYS, respectively. The developed dragonfly inspired wing showed a natural frequency of 29.4 Hz with a bending mode shape which is close to the characteristic frequency of its natural counterpart.

Keywords

flapping wings biomimicking nanocomposites MAVs 

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Notes

Acknowledgement

The authors thank 4i Lab from Department of Mechanical Engineering, IIT Kanpur and Lithography Lab from Department of Material Science and Engineering, IIT Kanpur for their help in the manufacturing of wing mold. Authors also thank ANSYS for providing the student version to carry out the computational finite element modal analysis study.

References

  1. [1]
    Combes S A, Daniel T L. Flexural stiffness in insect wings I. Scaling and the influence of wing venation. Journal of Experimental Biology, 2003, 206, 2979–2987.Google Scholar
  2. [2]
    Bos F M. Numerical Simulations of Flapping Foil and Wing Aerodynamics: Mesh Deformation Using Radial Basis Functions. Delft University of Technology, Delft, Netherlands, 2010.Google Scholar
  3. [3]
    Bolsman C T, Goosen J F L, van Keulen F. Design overview of a resonant wing actuation mechanism for application in flapping wing MAVs. International Journal of Micro Air Vehicles, 2009, 1, 263–272.CrossRefGoogle Scholar
  4. [4]
    Brown D. Deception Point. Random House, New York, USA, 2013.Google Scholar
  5. [5]
    Brodsky A K. The Evolution of Insect Flight, Oxford University Press, Oxford, UK, 1994.Google Scholar
  6. [6]
    Haas F, Gorb S, Blickhan R. The function of resilin in beetle wings. Proceedings of the Royal Society of London B: Biological Sciences, 2000, 267, 1375–1381.CrossRefGoogle Scholar
  7. [7]
    Hou D, Zhong Z, Yin Y, Pan Y, Zhao H. The role of soft vein joints in dragonfly fight. Journal of Bionic Engineering, 2017, 14, 738–745.CrossRefGoogle Scholar
  8. [8]
    Zhang S, Ochiai M, Sunami Y, Hashimoto H. Influence of microstructures on aerodynamic characteristics for dragonfly wing in gliding fight. Journal of Bionic Engineering, 2019, 16, 423–431.CrossRefGoogle Scholar
  9. [9]
    Raney D L, Slominski E C. Mechanization and control concepts for biologically inspired micro air vehicles. Journal of Aircraft, 2004, 41, 1257–1265.CrossRefGoogle Scholar
  10. [10]
    Wood R J. Design, fabrication, and analysis of a 3DOF, 3cm flapping-wing MAV. IEEE/RSJ International Conference on Intelligent Robots and Systems, San Diego, USA, 2007, 1576–1581.Google Scholar
  11. [11]
    Pornsin-sirirak T N, Lee S W, Nassef H, Grasmeyer J, Tai Y C, Ho C M, Keennon M. MEMS wing technology for a battery-powered ornithopter. IEEE The Thirteenth Annual International Conference on Micro Electro Mechanical Systems, Miyazaki, Japan, 2000, 799–804.Google Scholar
  12. [12]
    Shang J K, Combes S A, Finio B M, Wood R J. Artificial insect wings of diverse morphology for flapping-wing micro air vehicles. Bioinspiration & Biomimetics, 2009, 4, 036002.CrossRefGoogle Scholar
  13. [13]
    Richter C, Lipson H. Untethered hovering flapping fight of a 3D-printed mechanical insect. Artificial Life, 2011, 17, 73–86.CrossRefGoogle Scholar
  14. [14]
    Kumar D, Goyal T, Kumar V S, Mohite P M, Kamle S, Verma V. Development and modal analysis of bioinspired CNT/epoxy nanocomposite MAV flapping wings. Journal of Aerospace Sciences and Technologies, 2015, 67, 88–93.Google Scholar
  15. [15]
    Greenewalt C H. The wings of insects and birds as mechanical oscillators. Proceedings of the American Philosophical Society, 1960, 104, 605–611.Google Scholar
  16. [16]
    Jafferis N T, Graule M A, Wood R J. Non-linear resonance modeling and system design improvements for underactuated flapping-wing vehicles. IEEE International Conference on Robotics and Automation, Stockholm, Sweden, 2016, 3234–3241.Google Scholar
  17. [17]
    Zhang J, Deng X. Resonance principle for the design of flapping wing micro air vehicles. IEEE Transactions on Robotics, 2017, 33, 183–197.CrossRefGoogle Scholar
  18. [18]
    Chen J S, Chen J Y, Chou Y F. On the natural frequencies and mode shapes of dragonfly wings. Journal of Sound and Vibration, 2008, 313, 643–654.CrossRefGoogle Scholar
  19. [19]
    Combes S A, Daniel T L. Into thin air: Contributions of aerodynamic and inertial-elastic forces to wing bending in the hawkmoth Manduca sexta. Journal of Experimental Biology, 2003, 206, 2999–3006.CrossRefGoogle Scholar
  20. [20]
    Masoud H, Alexeev A. Resonance of flexible flapping wings at low Reynolds number. Physical Review E, 2010, 81, 056304.CrossRefGoogle Scholar
  21. [21]
    Tobing S, Young J, Lai J C S. Effects of wing flexibility on bumblebee propulsion. Journal of Fluids and Structures, 2017, 68, 141–157.CrossRefGoogle Scholar
  22. [22]
    Smith C W, Herbert R, Wootton R J, Evans K E. The hind wing of the desert locust (Schistocerca gregaria Forskal). II. Mechanical properties and functioning of the membrane. Journal of Experimental Biology, 2000, 203, 2933–2943.Google Scholar
  23. [23]
    Song F, Lee K L, Soh A K, Zhu F, Bai Y L. Experimental studies of the material properties of the forewing of cicada (Homoptera, Cicadidae). Journal of Experimental Biology, 2004, 207, 3035–3042.CrossRefGoogle Scholar
  24. [24]
    Wootton R J. Functional morphology of insect wings. Annual Review of Entomology, 1992, 37, 113–140.CrossRefGoogle Scholar
  25. [25]
    Kumar V S, Kumar D, Goyal T, Mohite P M, Kamle S. Development and application of PP-CNT composite for hummingbird inspired MAV flapping wings. International Micro Air Vehicle Conference and Competition, Delft, The Netherlands, 2014, 180–187.Google Scholar
  26. [26]
    ASTM. D1708: Standard Test Method for Tensile Properties of Plastics by Use of Microtensile Specimens. ASTM International, New York, USA, 2013.Google Scholar
  27. [27]
    Song F, Xiao K W, Bai K, Bai Y L. Microstructure and nanomechanical properties of the wing membrane of dragonfly. Materials Science and Engineering: A, 2007, 457, 254–260.CrossRefGoogle Scholar
  28. [28]
    Talucdher R, Shivakumar K. Tensile properties of veins of damselfly wing. Journal of Biomaterials and Nanobiotechnology, 2013, 4, 247–255.CrossRefGoogle Scholar
  29. [29]
    Kreuz P, Arnold W, Kesel A B. Acoustic microscopic analysis of the biological structure of insect wing membranes with emphasis on their waxy surface. Annals of Biomedical Engineering, 2001, 29, 1054–1058.CrossRefGoogle Scholar
  30. [30]
    ASTM. D882: Standard Test Method for Tensile Properties of Thin Plastic Sheeting. ASTM International, New York, USA, 2012.Google Scholar
  31. [31]
    Azuma A, Watanabe T. Flight performance of a dragonfly. Journal of Experimental Biology, 1988, 137, 221–252.Google Scholar
  32. [32]
    Tong J, Zhao Y, Sun J, Chen D. Nanomechanical properties of the stigma of dragonfly Anax parthenope julius Brauer. Journal of Materials Science, 2007, 42, 2894–2898.CrossRefGoogle Scholar
  33. [33]
    Kesel A B, Philippi U, Nachtigall W. Biomechanical aspects of the insect wing: An analysis using the finite element method. Computers in Biology and Medicine, 1998, 28, 423–437.CrossRefGoogle Scholar
  34. [34]
    Kumar D, Kamle S, Mohite P M, Kamath G M. A novel real-time DIC-FPGA-based measurement method for dynamic testing of light and flexible structures. Measurement Science and Technology, 2019, 30, 045903.CrossRefGoogle Scholar

Copyright information

© Jilin University 2019

Authors and Affiliations

  • David Kumar
    • 1
    Email author
  • Preetamkumar Marutrao Mohite
    • 1
  • Sudhir Kamle
    • 1
  1. 1.Department of Aerospace EngineeringIndian Institute of Technology KanpurKanpurIndia

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