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
Link To Document