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
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.
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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
Received: Nov. 21, 2019
Accepted: --
Published Online: Apr. 21, 2022
The Author Email: Weiping ZHANG (zwp37@163.com)