High-frequency performance for a spiral-shaped piezoelectric bimorph

2018 ◽  
Vol 32 (10) ◽  
pp. 1850111 ◽  
Author(s):  
Fang Sheng Huang ◽  
Zhi Hua Feng ◽  
Yu Ting Ma ◽  
Qiao Sheng Pan ◽  
Lian Sheng Zhang ◽  
...  

Piezoelectric cantilever is suitable as an actuator for micro-flapping-wing aircraft. Higher resonant frequency brings about stronger flight energy, and the flight amplitude can be compensated by displacement–amplification mechanism, such as lever. To obtain a higher resonant frequency, straight piezoelectric bimorph was rolled into spiral-shaped piezoelectric bimorph with identical effective length in this study, which is verified in COMSOL simulations. Simulation results show that compared with the straight piezoelectric bimorph, the spiral-shaped piezoelectric bimorph with two turns has higher inherent frequencies (from 204.79 Hz to 504.84 Hz in terms of axial oscillation mode, and from 319.77 Hz to 704.48 Hz in terms of tangential torsional mode). The spiral-shaped piezoelectric bimorph is fabricated by a precise laser cutting process and consists of two turns with effective length of 60 mm, width of 2.5 mm, and thickness of 1.6 mm, respectively. With the excitation voltage of 100 Vpp applying an electric field across the thickness of the bimorph, the tip displacement of the actuator in the axial oscillation and tangential torsional modes are 85 [Formula: see text]m and 15 [Formula: see text]m, respectively.

2018 ◽  
Vol 32 (17) ◽  
pp. 1850187
Author(s):  
Fang Sheng Huang ◽  
Zhi Hua Feng ◽  
Yu Ting Ma ◽  
Qiao Sheng Pan

Trapezoidal structure has been proposed for construction of piezoelectric cantilever to increase inherent frequency. To further break through the limitation on frequency value, trapezoidal piezoelectric cantilever is rolled into spiral-shaped piezoelectric cantilever with identical effective length in this study, which is verified in COMSOL simulations and experiments. A prototype shows that after rolling the straight shape into a spiral shape for the trapezoidal piezoelectric cantilever, the first inherent frequency promotes 4.5 times from 98100 Hz to 441,900 Hz, which is consistent with theoretic analysis. The spiral-shaped trapezoidal piezoelectric cantilever is suitable for working as an actuator in micro flapping-wing aircraft.


2003 ◽  
Vol 39 (1) ◽  
pp. 149 ◽  
Author(s):  
M. Enciso-Aguilar ◽  
F. Aniel ◽  
P. Crozat ◽  
R. Adde ◽  
H.-J. Herzog ◽  
...  

Sensors ◽  
2020 ◽  
Vol 20 (4) ◽  
pp. 1206 ◽  
Author(s):  
Wei-Jiun Su ◽  
Jia-Han Lin ◽  
Wei-Chang Li

This paper investigates a piezoelectric energy harvester that consists of a piezoelectric cantilever and a tip mass for horizontal rotational motion. Rotational motion results in centrifugal force, which causes the axial load on the beam and alters the resonant frequency of the system. The piezoelectric energy harvester is installed on a rotational hub in three orientations—inward, outward, and tilted configurations—to examine their influence on the performance of the harvester. The theoretical model of the piezoelectric energy harvester is developed to explain the dynamics of the system and experiments are conducted to validate the model. Theoretical and experimental studies are presented with various tilt angles and distances between the harvester and the rotating center. The results show that the installation distance and the tilt angle can be used to adjust the resonant frequency of the system to match the excitation frequency.


1993 ◽  
Vol 5 (6) ◽  
pp. 672-674 ◽  
Author(s):  
L.E. Tarof ◽  
J. Yu ◽  
R. Bruce ◽  
D.G. Knight ◽  
T. Baird ◽  
...  

2014 ◽  
Vol 23 (4) ◽  
pp. 315-319
Author(s):  
Wei Wang ◽  
Xiao Yang ◽  
Na Li ◽  
Lu Zhang ◽  
Gongshu Yue ◽  
...  

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