Deformation of a Beam with Partially Debonded Piezoelectric Actuators

A linear and a non-linear mathematical models for analyzing the deformation behavior of a beam with a pair of partially debonded piezoelectric actuators are developed on the basis of the Timoshenko beam theory. Effect of buckling is considered in the linear model, where the debonded actuator region is assumed to generate the Euler buckling load when the axial force in the region is larger than the load. The static behavior of the beam is investigated for extension and bending deformation. When the actuator debonds from its edge, the performance deteriorates; in contrast, the debonding in the middle of the actuator does not show any performance degradation until the debonded region buckles. The deformation behavior obtained from the linear model has been found to have good agreement with that from the non-linear model. The non-linear analysis shows that after the buckling the debonded actuator region maintains an axial force of the order of the Euler buckling load of a fix—fix column for the extending actuation, although for the bending actuation, it retains nearly 75% of the Euler buckling load. Further, the strain distribution in the debonded region shows that the buckling may occur before cracks begin in the actuator.

[1]  Daniel Guyomar,et al.  Semi-passive damping using continuous switching of a piezoelectric device , 1999, Smart Structures.

[2]  O. Zienkiewicz The Finite Element Method In Engineering Science , 1971 .

[3]  S. Timoshenko,et al.  Strength of materials : part I : elementary theory and problems / by S. Timoshenko , 1976 .

[4]  S. Timoshenko Theory of Elastic Stability , 1936 .

[5]  Satya N. Atluri,et al.  Sensing and actuating behaviours of piezoelectric layers with debonding in smart beams , 2001 .

[6]  Ephrahim Garcia,et al.  A Self-Sensing Piezoelectric Actuator for Collocated Control , 1992 .

[7]  Nagi G. Naganathan,et al.  Study of induced strain transfer in piezoceramic smart material systems , 1999 .

[8]  Liyong Tong,et al.  Control stability analysis of smart beams with debonded piezoelectric actuator layer , 2002 .

[9]  Izhak Sheinman,et al.  Post-buckling analysis of composite delaminated beams , 1991 .

[10]  Guoliang Huang,et al.  Modelling and analysis of piezoelectric actuators in anisotropic structures , 2002 .

[11]  Aditi Chattopadhyay,et al.  Modeling of smart composite laminates including debonding: A finite element approach , 1997 .

[12]  Robert L. Forward,et al.  Electronic Damping of Orthogonal Bending Modes in a Cylindrical Mast—Experiment , 1981 .

[13]  C. J. Swigert,et al.  Electronic Damping of Orthogonal Bending Modes in a Cylindrical Mast—Theory , 1981 .

[14]  Stephen P. Timoshenko,et al.  Elementary theory and problems , 1940 .

[15]  I. Sheinman,et al.  Delamination growth during pre- and post-buckling phases of delaminated composite laminates , 1998 .

[16]  George A. Kardomateas,et al.  Growth of internal delaminations under cyclic compression in composite plates , 1994 .

[17]  Aditi Chattopadhyay,et al.  Experimental investigation of composite beams with piezoelectric actuation and debonding , 1997, Adaptive Structures and Material Systems.

[18]  E. Crawley,et al.  Use of piezoelectric actuators as elements of intelligent structures , 1987 .

[19]  Francis C. Moon,et al.  Modal Sensors/Actuators , 1990 .

[20]  I. Sheinman,et al.  Energy release rate and stress intensity factors for delaminated composite laminates , 1997 .

[21]  R. Oppermann Strength of materials, part I, elementary theory and problems , 1941 .

[22]  C. K. Gim Plate finite element modeling of laminated plates , 1994 .

[23]  Nesbitt W. Hagood,et al.  Damping of structural vibrations with piezoelectric materials and passive electrical networks , 1991 .

[24]  M. Umeda,et al.  Analysis of the Transformation of Mechanical Impact Energy to Electric Energy Using Piezoelectric Vibrator , 1996 .