A simultaneous approach for compliance minimization and piezoelectric actuator design considering the polarization profile

2019 ◽  
Vol 121 (2) ◽  
pp. 334-353
Author(s):  
Juliano Fagundes Gonçalves ◽  
Daniel Milbrath De Leon ◽  
Eduardo André Perondi
2009 ◽  
Vol 24 (2) ◽  
pp. 305-313 ◽  
Author(s):  
X. Ojeda ◽  
X. Mininger ◽  
H. Ben Ahmed ◽  
M. Gabsi ◽  
M. Lecrivain

2007 ◽  
Vol 20 (3-4) ◽  
pp. 187-192 ◽  
Author(s):  
C. Potthast ◽  
R. Eisseler ◽  
D. Klotz ◽  
J. Wallaschek ◽  
U. Heisel

2017 ◽  
Vol 199 ◽  
pp. 1665-1670 ◽  
Author(s):  
J.F. Gonçalves ◽  
D.M. De Leon ◽  
E.A. Perondi

1993 ◽  
Vol 16 (5) ◽  
pp. 859-864 ◽  
Author(s):  
Santosh Devasia ◽  
Tesfay Meressi ◽  
Brad Paden ◽  
Eduardo Bayo

2011 ◽  
Vol 7 (3) ◽  
pp. 353-360 ◽  
Author(s):  
Zion Tsz Ho Tse ◽  
Yum Ji Chan ◽  
Henning Janssen ◽  
Abbi Hamed ◽  
Ian Young ◽  
...  

2014 ◽  
Vol 998-999 ◽  
pp. 674-677 ◽  
Author(s):  
Xing Zhang ◽  
Wei Wang ◽  
Guang Hua Zong

This paper describes the design, construction, and analysis of a new piezoelectric actuator design for small aircrafts in the special requirements of the steering weight. It describes the working principle of piezo actuator, optimizes the piezo chip specification parameters by experimental measurements, put forward the finite element analysis simulation and the experimental testing of piezoelectric actuators’ drive performance. The simulation and experimental results show that the new design meets the design requirements of weight and space control.


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