2. Fundamental Design and Modelling of the Cantilever Beam
The proposed CB is illustrated in
Figure 1. Its bimorph-configured design mainly consists of two identical piezoelectric layers made of PZT-5A and a flexible, charge conductor layer made of copper. A tungsten proof mass is mounted at the tip of the upper PZT-5A layer for improved vibration sensitivity. Both PZT-5A layers are series-connected with opposite polarisation directions in order to sustain large displacements and high reliability whenever the CB’s operational threshold exceeds its coercive electric field. The piezoelectric constant
d31 is selected for the CB as its primary operating mode, therefore enabling maximisation of its power generation potential with respect to low matching impedance.
Hence, if both PZT-5A layers of the CB are physically deformed by applied mechanical stress such as vibration or pressure, electric charges will be generated to form an electric field. This process of converting mechanical energy into electrical energy is known as the forward piezoelectric effect, which can be defined by its constitutive equations [
7]:
where
S1 and
T1 are the mechanical strain and stress in length direction of the PZT-5A layers.
E3 is the electric field.
D3 is the electric displacement, or electric charge density.
s11 is the elastic compliance in a constant electric field.
d31 is the piezoelectric constant.
ε33 is the permittivity constant of the PZT-5A layers under constant stress.
Since the PZT-5A layers are assumed to be identical, the voltage across the electrodes of each layer is
vp(t)/2 when connected in series. Due to opposite polarisation directions in
d31 mode, the instantaneous electric fields of the PZT-5A layers are in the same direction, and can be defined as:
where
hp is the thickness of each PZT-5A layer. Based on the Euler-Bernoulli beam theory [
11], the CB is modelled as a uniform composite beam. As such, when the CB vibrates, the effects of rotary inertia and shear deformation are neglected, while its plane sections are assumed to remain plane. This is a reasonable assumption since commercially available CBs are typically manufactured using relatively thin piezoelectric layers.
To maximise the output power of the CB, it has to be operated at a resonant frequency that matches the vibration frequency of its intended application. Hence, it is crucial to attenuate the resonant frequency, where its angular form
ωr and regular form
fr can be defined as [
34,
35]:
where
k is the coupling coefficient,
meff is the effective mass of the CB,
Yp Ip is the flexural rigidity of the CB,
lp is the length of each PZT-5A layer,
m is the mass per unit length, and
mt the proof mass. The numeric constant 0.24 denotes that 24% of the CB’s mass is participative in vertical displacements. From (4), it is deduced that the CB’s resonant frequency can be attenuated by changing either the coupling coefficient or the aforementioned geometric parameters.
For oscillating devices such as the CB, it is mandatory to implement damping measures that mitigate excessive vibrations and protect the system which incorporates it. Thus, unnecessary power losses can be avoided while the CB operates at an optimal resonant frequency. In this case, the mechanical damping ratio
ζ is used to gauge the CB’s oscillatory behaviour based on (4). It can be expressed using the following equation [
36]:
where
c is the damping coefficient of PZT-5A. Succeedingly, the DC output voltage of the CB under vibration-induced vertical displacements can be analytically determined as follows [
36]:
in which:
where
ω is the ambient vibration frequency (in rad/s),
Yp is the Young’s modulus of PZT-5A,
Sz is the strain relative to the vertical displacement of the CB,
Ain is the input acceleration,
Rp is the load resistance,
Cp is the internal capacitance of the CB,
z is the vertical displacement,
bp is the width of the PZT-5A layers, and
le is the electrode length relative to the length of the PZT-5A layers.
Assuming that the CB’s resonant frequency
ωr matches the ambient vibration frequency
ω, Equation (7) can be simplified to:
hence maximising output power in conjunction with impedance matching, where the CB’s source resistance is equivalent to the load resistance. The output power
P can be computed as a function of the output voltage
Vp and the load resistance
Rp [
37,
38,
39]:
Through analyses of Equations (7)–(11), it is deduced that the key parameters which dictate the CB’s electrical output performance are its resonant frequency and load resistance, as both require concise formulation with respect to the CB’s geometric parameters (i.e., length, width, thickness and mass).
To perform design optimisation of the CB in COMSOL Multiphysics, its fundamental design is defined as input parameters for the software’s simulation model interface. These parameters [
40,
41] are shown in
Table 1,
Table 2 and
Table 3. The selected materials’ relatively high Young’s modulus and Poisson’s ratio indicate that the CB is capable of exhibiting high bending strength while supporting the weight of its proof mass if exposed to large, vibration-based excitation forces. Notably, PZT-5A was selected for its highly flexible yet robust nature, and for its renowned ability to detect low-level vibrations.
3. Optimisation of the Cantilever Beam
As part of the optimisation process of the CB in COMSOL Multiphysics, the finite element method (FEM) is used to evaluate it for stress distribution within a real-time environment based on structural vibrations from common ambient vibration sources. Through FEM, the CB is initially developed using the proposed input parameters (i.e.,
Table 1,
Table 2 and
Table 3) and triangular mapped meshing to facilitate discretisation. Eigenfrequency analysis is conducted to identify the range of resonant frequencies that the CB is able to operate in, while verifying against Equations (4) and (5). Thus, a range of 20–220 Hz has been identified, which is relatively similar to the vibration frequency range of common ambient vibration sources. Extensive optimisation of the CB is performed through frequency domain analysis, where simulated output power responses are acquired with respect to varying input parameters. These parameters are resonant frequency, load resistance, the length-width ratio of PZT-5A layers, the width of proof mass and thickness of PZT-5A layers.
Figure 2,
Figure 3,
Figure 4 and
Figure 5 present the respective simulation-based optimisation results.
From the results, it is observed that the CB’s output power tend to increase steadily before decreasing at a relatively proportional rate once it reaches its peak value, which indicates that the CB has a performance threshold for each input parameter. Hence, its design is modified according to the parameters that allowed it to achieve maximum output power.
Figure 2 has indicated peak performance of the CB at 120 Hz resonant frequency with an ideal operating load condition of 4 kΩ. Using results from
Figure 2 as the basis for subsequent optimisations, the length-width ratio of the PZT-5A layers is varied from 2 to 20, as shown in
Figure 3. It is discovered that as the length increases, vertical displacements of the CB will increase, therefore sharply increasing its output power. Contrastingly, as the width increases, vertical displacements will decrease, thus reducing the output power. The maximum output power of 7.4 mW is obtained at an optimum length-width ratio of 12.
To explore the proof mass’ effect on power generation, its width is varied from 5 mm to 32 mm, as shown in
Figure 4. The range of the experimental widths is identified based on (4), given that the CB needs to conform to a resonant frequency of 20-220 Hz in order to generate a substantial voltage. The width correlates with the weight of the proof mass,
mt, in (4), such that any change in the width affects the volume of the proof mass, thus fine-tuning
mt. Consequently, the CB’s resonant frequency is reduced to enhance its vertical displacements based on the inertia effect of the proof mass. Results indicate that the output power increases linearly with respect to increasing width of the proof mass (up to 17 mm), before decreasing moderately. The maximum output power of 15.4 mW is obtained when the width of the proof mass is 17 mm. Finally, the thickness of the PZT-5A layers is varied from 0.2 mm to 2 mm. The range of the experimental thickness is identified based on the viable thickness of PZT-5A layers [
40] used in the manufacturing of commercially available CBs.
Figure 5 illustrates the output power responses at the corresponding thickness, in which minor deviations are observed. The maximum output power of 16.15 mW is obtained when using PZT-5A layers that are 1.2 mm thick. Thus, by re-arranging (11) into
Vp =
, a corresponding output voltage of 11.37 V DC is computed. Based on the aforementioned results, it can be concluded that the dominant factor which affects the CB’s output is the weight of its proof mass.
The colour contour of simulated stress distribution across the optimised CB, notably known as von Mises stress, is illustrated in
Figure 6. Hence, both the location and magnitude of the stress can be examined. Starting near the CB’s clamped end, the stress distribution is found to be decreasing along its beam length, towards its free end. From Equation (2), the charge density is determined to be proportional to the distributed stress, therefore maximum charge density can be found near the clamped end. Minimum stress is indicated at the tip of the free end with a magnitude of 16.2 N/m
2, whereas maximum stress is indicated near the clamped end, with a magnitude of 1.98 × 10
7 N/m
2. As such, both magnitudes depict a positive response towards dynamic loading.
Table 4 presents the optimised parameters that have been acquired from the CB’s simulation-based optimisation. They will be utilised as reference data for setting the input conditions of the proposed SPDS in PSCAD/EMTDC.
5. Simulation Results and Analyses
Using PSCAD/EMTDC as a testbed to model the proposed SPDS, simulation evaluations are presented to observe corresponding transient responses and load-following performances where Vin fluctuates in conjuncture with arbitrary wind speed directed at the CB during vibration-based operation. The aforementioned proceedings constitute wind-enhanced vibration effects that emulate the SPDS’s deployment at the above-ground MRT train station in Khatib, Singapore, where its daily recorded ambient data depicts an arbitrary wind speed of 6–8 m/s and a structural vibration frequency of 119.58 Hz during non-peak operating hours. In order to demonstrate the dynamic responsiveness of the SPDS, it is modelled at a simulation run-time of 5 s.
Figure 13 depicts the transient response of the three-phase inverter’s output voltage (
Vq) and adjusted voltage (
Vq,adj) when matching the reference voltage (
Vq,ref) during feedback control. It is apparent that the adaptive proportional and integral gains (
Kp = 0.03,
Ki = 90.91 × 10
−6) of the PI-based BC have piloted fast settling-time response with negligible steady-state error, defining respective scalar gain at different time-step to quickly secure 49 V AC for
Vq,adj. Notably,
Vq,adj is strategically attenuated to anticipate accumulated losses (i.e., conduction loss and switching loss), hence attributing the desired 40.28 V AC for
Vq after incurring these losses. Conjointly, maximum peak overshoot is decreased due to low
Kp, while residual errors are mitigated using
Ki to complement
Kp.
Figure 14 depicts the fundamental operation of the qZSI-based PVEH when the CB is controlled to wind-enhanced vibrations. It is observed that the boost factor (
B) consistently attenuates to step-up the input voltage (
Vin) which randomly deviates from 11.37 V DC to 20.31 V DC due to variegated wind components of the arbitrary wind speed. As evidenced in
Figure 14b,
B manages to conform to its respective limits in (12) with respect to the DC-link voltage (
Vboost) attained from
Vq,adj conversion in the PI-based BC’s boost control unit. Such attenuation involving
B aims to secure a constant
Vboost of 56.85 V DC despite
Vin fluctuation during uncertain output performances of the CB.
Figure 15 validates this analogy to a large extent since minor clipping (i.e., 2.4%) is found in
Vboost when observing its voltage transient. Moreover, minimisation of clipping is attributed by low inductor and capacitor ratings in the qZS network; which were determined based on the permissible maximum shoot-through period (
TZ,max), since
TZ,max prevents
Vboost from being forcibly constrained.
Figure 16 depicts the transient response of the inductors (
L1,
L2) and capacitors (
C1,
C2) in the qZS network, specifically their ripple characteristics. It is evident that the determined ratings for these components have rendered consistency in the inductor currents (
IL1,
IL2) and capacitor voltages (
VC1,
VC2), strictly conforming to the selected 10% peak-to-peak inductor current ripple and 0.9% capacitor voltage ripple respectively. Furthermore, it is observed in
Figure 16a that the measured average inductor current (
IL) and maximum inductor current (
IL,max) correlates with their theoretical formulations in Equations (16) and (17). The strategic acquisition of both currents synchronises optimised charging and discharging sequences between the capacitors and inductors as depicted. Therefore,
Vboost stability is enforced throughout the shoot-through and non-shoot-through periods initiated by the aforementioned sequences.
Figure 17 presents the measured output voltage (
Vout) and load power (
Pload) of the SPDS. Both measurements proved that successful integration of the PI-based BC in the SPDS has established viable load-following synchronisation across all sub-systems to secure 54.4 V DC for
Vout, which constitutes
Pload measured value of 14.8 mW. Given that the SPDS’s input power is equivalent to
Pload rated value of 16.15 mW, its computed efficiency
ƞ is 91.64% based on:
ƞ = [
Pload (measured)/
Pload (rated)] × 100%. It is also apparent that there is almost no distortion of
Vout and
Pload, thus further validating the PI-based BC’s excellent control functionality.
Figure 18 illustrates the efficiency characteristics of the CB and SPDS when experimented against different DC load sizes. It is observed that the respective efficiencies are proportional to each other due to synchronised operations from the CB to the entirety of the SPDS, peaking at the rated load power of 16.15 mW before deteriorating. This is attributed by the limited
B, which impairs the SPDS’s output power since
Vout is required to be increased at larger loads. Furthermore, the SPDS tend to have lower efficiency in comparison to the CB as a result of cumulative losses across its circuitry.