Self-sensing piezoelectric bistable laminates for morphing structures

被引:34
作者
Chillara, V. S. C. [1 ]
Ramanathan, A. K. [1 ]
Dapino, M. J. [1 ]
机构
[1] Ohio State Univ, Dept Mech & Aerosp Engn, NSF IUCRC Smart Vehicle Concepts, Columbus, OH 43210 USA
基金
美国国家科学基金会;
关键词
bistable; morphing; analytical model; sensing; piezoelectric PVDF; FIBER COMPOSITES; PVDF SENSOR; ACTUATION;
D O I
10.1088/1361-665X/ab9060
中图分类号
TH7 [仪器、仪表];
学科分类号
0804 ; 080401 ; 081102 ;
摘要
Bistable laminates offer opportunities for shape morphing, energy harvesting, and flow control devices. Smart materials such as piezoelectric macrofiber composites and shape memory alloys have been embedded in bistable laminates to actuate or harvest energy. However, sensor systems capable of measuring bistable shapes and snap-through events are lacking. In this paper, we present curved bistable laminates layered with piezoelectric PVDF films that can sense smooth shape changes as well as abrupt snap-through transitions. Near-static measurement is facilitated by a drift compensated charge amplifier with a large time constant that converts the sensor's charge output into a measurable voltage with minimal drift error. The sensing function is demonstrated on mechanically-prestressed bistable laminates. The laminated composites include two sensor layers such that one measures the changes in curvature and the other measures snap-through events. An analytical model is presented in which strains and curvatures calculated using a laminated-plate model are fed into a linear piezoelectric model to calculate voltage. Shapes measured by the sensors correlate well with shapes measured using a 3D motion capture system. A model-based analysis is performed to understand the laminates' design space.
引用
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页数:11
相关论文
共 36 条
[1]   Design and testing of a passively adaptive inlet [J].
Arena, G. ;
Groh, R. M. J. ;
Theunissen, R. ;
Weaver, P. M. ;
Pirrera, A. .
SMART MATERIALS AND STRUCTURES, 2018, 27 (08)
[2]   Piezoelectric Fiber Composites as Sensor Elements for Structural Health Monitoring and Adaptive Material Systems [J].
Brunner, Andreas J. ;
Birchmeier, Marcel ;
Melnykowycz, Mark M. ;
Barbezat, Michel .
JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES, 2009, 20 (09) :1045-1055
[3]   Stability considerations and actuation requirements in bistable laminated composites [J].
Chillara, V. S. C. ;
Dapino, M. J. .
COMPOSITE STRUCTURES, 2018, 184 :1062-1070
[4]   Mechanically-prestressed bistable composite laminates with weakly coupled equilibrium shapes [J].
Chillara, V. S. C. ;
Dapino, M. J. .
COMPOSITES PART B-ENGINEERING, 2017, 111 :251-260
[5]   Recent progress in flexible and stretchable piezoelectric devices for mechanical energy harvesting, sensing and actuation [J].
Dagdeviren, Canan ;
Joe, Pauline ;
Tuzman, Ozlem L. ;
Park, Kwi-Il ;
Lee, Keon Jae ;
Shi, Yan ;
Huang, Yonggang ;
Rogers, John A. .
EXTREME MECHANICS LETTERS, 2016, 9 :269-281
[6]   A Morphing Composite Air Inlet with Multiple Stable Shapes [J].
Daynes, S. ;
Weaver, P. M. ;
Trevarthen, J. A. .
JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES, 2011, 22 (09) :961-973
[7]   Multi-mode morphing using initially curved composite plates [J].
Eckstein, E. ;
Pirrera, A. ;
Weaver, P. M. .
COMPOSITE STRUCTURES, 2014, 109 :240-245
[8]   A Review on Bistable Composite Laminates for Morphing and Energy Harvesting [J].
Emam, Samir A. ;
Inman, Daniel J. .
APPLIED MECHANICS REVIEWS, 2015, 67 (06)
[9]  
Emamian Sepehr, 2015, 2015 IEEE Sensors. Proceedings, P1, DOI 10.1109/ICSENS.2015.7370651
[10]   Experimental Investigation of Bistable Winglets to Enhance Wing Lift Takeoff Capability [J].
Gatto, A. ;
Mattioni, F. ;
Friswell, M. I. .
JOURNAL OF AIRCRAFT, 2009, 46 (02) :647-655