This section begins by describing the core design and working principle of the vibration energy harvesting device, followed by a theoretical and simulation-based analysis to verify the feasibility of the proposed design.
2.1. Structural Design and Working Principle
This paper presents a piezoelectric energy harvester designed for vibrational energy recovery in vehicle suspension systems. The core structure of the device comprises an array of eight cantilever beams aligned axially (x-direction) and sixteen permanent magnets, all encapsulated within a cylindrical housing rigidly connected to the vehicle body. The root of each cantilever beam is fixed to the inner wall of the housing, with its free end integrated with a permanent magnet mass. The permanent magnets adopted in this design are N40-grade NdFeB magnets (supplied by Ningbo Yunsheng Co., Ltd., Ningbo, China), with a diameter of 10 mm, height of 4 mm, residual magnetism (Br) of 1.28–1.32 T, coercive force (Hcb) ≥ 955 kA/m, and maximum energy product ((BH)max) of 293–318 kJ/m3. These performance parameters ensure a stable nonlinear magnetic coupling force to drive the deformation of the cantilever beam.
Correspondingly, an additional set of permanent magnets is symmetrically mounted on the vehicle suspension coil spring (adapted to the MacPherson independent suspension, supplied by Wanxiang Qianchao Co., Ltd., Hangzhou, China). The suspension coil spring has a wire diameter of 12 mm, a central diameter of 80 mm, an effective number of turns of 8, and a stiffness of 16,000 N/m, forming a nonlinear magnetic attractive coupling with the permanent magnet mass at the tip of each cantilever beam. As shown in
Figure 1, this design addresses critical issues faced by conventional nonlinear energy harvesters, including their limited adaptability to complex and variable vibrational environments due to a reliance on unidirectional excitation responses, as well as the low energy conversion efficiency of conventional cantilever structures. The latter issue stems from a natural frequency significantly higher than the ambient excitation frequency within the ultra-low-frequency spectrum typical of vehicle vibrations. By integrating a mass block at the free end of the cantilever beam, the overall equivalent mass and stiffness of the system are effectively reduced, thereby significantly lowering the natural frequency and promoting a shift of the resonance peak toward the lower frequency region. This tuning mechanism aligns with the vibrational frequency characteristics of vehicle suspension systems, as Sun [
28] et al. highlighted that the human body is highly sensitive to 4–8 Hz vertical vibrations (consistent with ISO 2361 From the ISO 2361 [
28], the human body is much sensitive to vibrations of 4–8 Hz in the vertical direction.) and that finite frequency-targeted optimization outperforms full-frequency-domain control in suppressing relevant vibrations, while Zhang et al. [
29]. revealed, via evolutionary power spectral density (EPSD) analysis, that suspension resonant frequencies form a dynamic frequency domain (DFD) that shifts toward lower ranges with increasing vehicle speed. This frequency-tuning mechanism enables highly efficient matching between the resonance frequency of the energy harvester and the actual vibrational spectrum of vehicles, thereby fundamentally enhancing the device’s energy capture performance in low-frequency vibrational environments.
Figure 2 illustrates the operating mechanism of the energy harvester, which functions through the collaborative interaction between the electrical and structural domains. The structural domain is centered on a cantilever beam, with an attached mass at its free end to modulate the natural frequency, while the electrical domain consists of a PZT-5H piezoelectric ceramic patch bonded to the upper surface of the beam. The core operational principle of the system lies in the electromechanical coupling effect. In the static state, the two permanent magnets are horizontally aligned to ensure that the initial magnetic coupling force is in a stable linear interval, avoid pre-bending deformation of the cantilever beam caused by excessive static magnetic attraction, and ensure that the nonlinear characteristics of the magnetic coupling force are controllable during dynamic excitation [
30]. When external excitation, such as suspension vibration generated during vehicle operation, induces vibration of the beam, the permanent magnet corresponding to the one at the free end of the cantilever moves following the suspension vibration. The magnetic force generated between the two permanent magnets causes repeated bending deformation of the beam. This mechanical deformation directly induces strain in the PZT-5H piezoelectric patch attached to the beam, which subsequently converts the mechanical strain into electrical charge output through the direct piezoelectric effect, thereby transforming mechanical energy into electrical energy.
In addition, the piezoelectric ceramic patch bonded to the cantilever beam surface is PZT-5H (supplied by Baoji Tianbo Electronic Materials Co., Ltd., Baoji, China), with dimensions of 60 mm × 20 mm × 0.2 mm, an electromechanical coupling coefficient (Kp) of 0.68, and a piezoelectric constant (d31) of 320 × 10−12 C/N, which ensures efficient conversion of mechanical strain into electrical energy.
2.2. Feasibility Analysis
In the designed vibrational energy harvesting system, the nonlinear magnetic coupling force between the cylindrical permanent magnet integrated at the end of the piezoelectric cantilever beam and the permanent magnet mounted on the suspension coil spring serves as the core excitation mechanism. The initial gap distance plays a critical role as a key design parameter of the mechanism. When the initial gap distance is excessively large, the coupling strength between the magnets attenuates significantly. As a result, under external excitation along the z-axis, the vibration amplitude of the cantilever beam is suppressed, thereby substantially reducing the electrical output power generated by the piezoelectric transduction layer. Conversely, if the initial gap distance is too small, the attractive force generated between the magnets will significantly exceed the elastic restoration force threshold of the cantilever beam. Such a mechanical imbalance would lead to a complete loss of functionality in the energy harvester.
To investigate the relationship between the interaction force of cylindrical permanent magnets and the gap distance, a finite element model was developed using the COMSOL Multiphysics 6.2 platform. The model adopts the Magnetic Fields, No Currents physics interface, which is dedicated to simulating static magnetic field distributions and magnetic force interactions between permanent magnets without external current excitation. The model comprises two cylindrical N40-grade NdFeB magnets of identical dimensions (diameter: 10 mm; height:4 mm), with their magnetization direction defined as the axial direction (
z-axis), consistent with the actual installation orientation of the magnets in the energy harvester. The initial gap distance defined as s. In this model, the left magnet is fixed as a constraint, while the right magnet is subjected to a displacement excitation along the
z-axis (for a specified gap distance s). The computational domain was set to include the magnet region and the surrounding air domain, with a far-field boundary condition applied to the outer surface of the air domain to simulate the infinite extension of the magnetic field and eliminate boundary reflection effects.
Figure 3a displays the meshed model of the magnet system, including the enclosing air domain, while
Figure 3b presents the computed contour plot of magnetic flux density, which is utilized to evaluate the interaction force between the magnets.
To validate the accuracy of the developed finite element model, this study selected representative methods for comparison based on a literature review. Akoun [
31] first proposed the complete analytical expression for the force between magnets, which was further applied to the design of magnetic devices. Furlani [
32] derived the expression for the axial force between magnetic disks by using the charge model. Under the condition of uniform magnetization, Vokoun [
33] et al. presented the expression for the axial force between two transversely moving cylindrical magnets. Avvari et al. [
30] expressed the axial and lateral forces between cylindrical magnets in the form of integrals, which were then used to investigate piezoelectric energy harvesters. Among various analytical approaches for calculating the interaction forces between permanent magnets, Avvari et al. [
30] derived expressions for both axial and lateral forces between cylindrical magnets through an integral formulation, which demonstrated high consistency with experimental measurements.
Figure 4 illustrates the geometric configuration of two cylindrical magnets under both axial and lateral relative displacements. The derived analytical formula for the lateral force between identical magnets is presented below:
In Equation (1), s denotes the axial distance between the magnets, J represents the Bessel function of the first kind and order 1, μ0 is the permeability of free space, ε takes a value of +1 for attraction and a value of −1 for repulsion, q is a dimensionless parameter reflecting the characteristic shape function of the cylindrical magnets and the properties of the magnetic vector potential in Fourier space, M denotes the magnetization, R is the radius, t is the thickness of the magnet, and r indicates the lateral spacing between the magnets.
The data obtained from the developed finite element model were compared with those from the model developed by Avvari et al. [
30]. As S0 (the initial horizontal distance between the two permanent magnets) increased progressively from 5 mm to 10 mm, both the theoretical model and the finite element model demonstrated a consistent variation trend. The two methods exhibited a highly consistent positively increasing pattern within the parameter range of S0 = 5 mm to S0 = 10 mm. Although minor discrepancies exist in the computational results of the finite element model (FEM), it maintains high overall accuracy. Analysis of the data at 8 mm, as shown in
Table 2, indicates that the error ranges approximately from 5% to 10%. The variation trends predicted by both models are highly consistent, with the FEM results being slightly lower than the theoretical values across all dimensional parameters. This reflects the higher sensitivity of the numerical method to the structural mechanical response. Nevertheless, the observed differences remain within an acceptable range and do not undermine the reliability of finite element analysis as an effective tool for evaluating structural performance, as shown in
Figure 5.
To investigate the mechanical response of the cantilever beam structure under external loading, with a specific focus on the quantitative relationship between the load applied at its free end and the resulting displacement, this study systematically modeled and analyzed the deflection behavior of a cantilever beam subjected to a concentrated load at the free end based on classical beam theory from mechanics of materials. The study focuses on a composite laminated cantilever beam structure consisting of a piezoelectric ceramic (PZT-5H) layer and an elastic steel substrate. Its equivalent bending stiffness is governed by the geometric dimensions and physical properties of the constituent materials.
In such laminated structures, the synergistic deformation between different material layers necessitates the introduction of an equivalent bending stiffness to characterize the overall flexural resistance. This equivalent stiffness expression comprehensively incorporates the contributions of both the PZT layer and the steel substrate, as given by the following formula:
According to the deflection solution of a cantilever beam subjected to a concentrated force (
F) at its free end, the relationship between the free-end deflection and the applied load can be expressed as follows:
Equivalently, the required applied force can be solved as follows:
where
Ieq is the equivalent bending stiffness,
A is the area of the PZT layer,
L is the length of the beam,
EPZT is the Young’s modulus of the PZT layer, and
Esteel is the Young’s modulus of the elastic steel substrate.
Based on the theoretical model described above, this study further calculated the concentrated load required to achieve a free-end deflection of the cantilever beam ranging from 1 to 8 mm. The calculation results are shown in
Figure 6. As the deflection increases, the required external load exhibits a significant non-linear growth trend, indicating that the structure may exhibit geometric nonlinear characteristics. To further evaluate the excitation feasibility of the cantilever beam system, a comparative analysis was conducted between the calculated elastic restoring force and the magnetic attractive force under various initial horizontal gaps. The results indicate that at a horizontal magnet gap of 8 mm, the magnetic attractive force significantly exceeds the elastic restoring force of the beam throughout the displacement range, except near the 8 mm deflection point. This demonstrates that the magnetic configuration can effectively overcome the structural stiffness, achieve the intended deformation of the cantilever beam, and induce a stable electromechanical coupling response. Simultaneously, this gap configuration both ensures excitation effectiveness and prevents excessive structural deformation or damage caused by an overpowering magnetic force, thereby balancing actuation performance and safety. In contrast, when the magnet gap increases to 9 mm, the magnetic attraction force attenuates significantly, becoming insufficient to overcome the beam’s elastic restoring force over most of the deflection range. This results in inadequate excitation and fails to drive the cantilever beam to produce an effective dynamic response.
Therefore, based on a comprehensive trade-off between excitation efficiency and structural integrity, a horizontal gap of 8 mm between the permanent magnet at the free end of the cantilever beam and the fixed magnet on the suspension coil spring is identified as the optimal design parameter. This configuration ensures sufficient excitation of the cantilever beam while effectively preventing structural failure or fatigue damage caused by excessive deformation, thereby significantly enhancing the operational stability and long-term reliability of the entire energy harvesting device.