Piezoelectrics & Acoustooptics, Volume. 42, Issue 3, 326(2020)

Investigation of Sub-palm-scale Double Piezoelectric Driving Flapping Wing Micro-aircraft Based on Smart Composite Microstructures

WEI Mingchen... ZHANG Weiping*, WANG Chenyang, ZHAO Jiaxin and MENG Ran |Show fewer author(s)
Author Affiliations
  • [in Chinese]
  • show less

    In this paper, a flapping wing micro-aircraft with double-drive was designed, fabricated and investigated. This aircraft was mainly fabricated by smart composite microstructures(SCM). The total quality of the prototype was 244 mg, and the wingspan was 61 mm. The performance of the prototype piezoelectric driver was tested. The results showed that the no-load resonance frequency of the piezoelectric actuator was 1 100 Hz and the load resonance frequency was 28 Hz. The lift test of the prototype was carried out, and the lift of the prototype was 0.689 mN.

    Tools

    Get Citation

    Copy Citation Text

    WEI Mingchen, ZHANG Weiping, WANG Chenyang, ZHAO Jiaxin, MENG Ran. Investigation of Sub-palm-scale Double Piezoelectric Driving Flapping Wing Micro-aircraft Based on Smart Composite Microstructures[J]. Piezoelectrics & Acoustooptics, 2020, 42(3): 326

    Download Citation

    EndNote(RIS)BibTexPlain Text
    Save article for my favorites
    Paper Information

    Received: Nov. 21, 2019

    Accepted: --

    Published Online: Apr. 21, 2022

    The Author Email: Weiping ZHANG (zwp37@163.com)

    DOI:10.11977/j.issn.1004-2474.2020.03.010

    Topics