2014
DOI: 10.1007/s00419-014-0910-6
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Modeling of torsion actuation of beams using inclined piezoelectric actuators

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Cited by 10 publications
(10 citation statements)
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“…(6), the displacement at the interface of the composite structure is continuous, and the neutral axis of the substrate is moved from the original position as shown in Fig. 3.…”
Section: Modified Pin Force Modelmentioning
confidence: 99%
See 1 more Smart Citation
“…(6), the displacement at the interface of the composite structure is continuous, and the neutral axis of the substrate is moved from the original position as shown in Fig. 3.…”
Section: Modified Pin Force Modelmentioning
confidence: 99%
“…Traditional actuator and motor became more and more difficult to meet these requirements. An effective approach to solve the problem is to integrate active materials into structure, such as shape memory alloys [3,4], piezoelectrics [5,6] and magnetostrictive materials [7]. The most common form of integration is bonding active materials to the surface of structure.…”
Section: Introductionmentioning
confidence: 99%
“…For the beam type laminates, the plane stress assumption is adapted and the width along y direction is assumed to be stress free. Therefore, Eq.6a is reduced to Eq.6b and only the transformed piezoelectric coefficient along x axis is considered [12]. are the transformed reduced stiffness matrix and transformed piezoelectric modules in the k th orthotropic layer, respectively.…”
Section: Mathematical Modellingmentioning
confidence: 99%
“…ωi k , i={1,2} shown in Eq.12 represents the linear interpolation function of the k th orthotropic layer in a smart piezo-composite laminate. ω ω (12) Pn, ta, and tp in Eq.12 are the number of inclined piezoelectric actuators, and actuator thickness, and host structure (composite laminate) thickness, respectively (See Fig.1). Governing partial differential equation relating the transverse bending and twisting moments to mid-plane displacements and electro-mechanical loads in a smart laminated piezo composite plate is stated in Eq.13 [38].…”
Section: Mathematical Modellingmentioning
confidence: 99%
“…Under various mechanical boundary conditions, Smits et al [11] derived the constituent equations for piezoelectric bimorphs. By adopting Euler–Bernoulli beam theory, Elshafei et al [12] made a static analysis for beams with piezoelectric actuators subjected to axial, transverse, and torsion loads, and derived the equation of motion of the structure system. Without specifying the function expressions of materials, Zhong and Yu [13,14] proposed the general elasticity solutions for FGPM beams subjected to various loads.…”
Section: Introductionmentioning
confidence: 99%