• DocumentCode
    267916
  • Title

    Nanostructured silicon flapping wing with higher strength and low reflectivity for solar powered MEMS aircraft

  • Author

    Kashyap, Kunal ; Kumar, Ajit ; Chi-Nan Chen ; Hou, Max T. ; Yeh, J. Andrew

  • Author_Institution
    Inst. of Nanoengineering & Microsyst., Nat. Tsing-Hua Univ., Hsinchu, Taiwan
  • fYear
    2014
  • fDate
    26-30 Jan. 2014
  • Firstpage
    648
  • Lastpage
    651
  • Abstract
    This work presents silicon flapping wings design with higher bending strength and low reflectivity for MEMS aircraft. The design was bio-inspired by the cicada wings which are having numerous nanostructures upon it. The nanostructure on silicon increases the bending strength by ~6 times. The higher strength silicon samples can successfully demonstrate the 100 μm thick bendable silicon by nanostructure surface texturing used for flapping wings. Moreover, same nanostructures act as antireflective layer due to improved light trapping for solar cell. The reflectivity of the nanotextured surface reduces to ~2%.
  • Keywords
    aerospace components; aircraft; biomimetics; micromechanical devices; nanostructured materials; silicon; solar cells; solar powered vehicles; Si; bioinspired wings; cicada wings; high bending strength wing; light trapping; low reflectivity for MEMS aircraft; nanostructured silicon flapping wing; size 100 mum; solar cell; solar powered MEMS aircraft; Aircraft; Micromechanical devices; Nanostructures; Photovoltaic cells; Reflectivity; Silicon; Surface morphology;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Micro Electro Mechanical Systems (MEMS), 2014 IEEE 27th International Conference on
  • Conference_Location
    San Francisco, CA
  • Type

    conf

  • DOI
    10.1109/MEMSYS.2014.6765724
  • Filename
    6765724