3.2. Frequency-domain analysis
Figure 10 shows the numerical results obtained with ANSYS AQUA 19.2 for the three floating bodies analysed.
Figure 10a corresponds to the variation of the added mass with respect to the analysed frequency of 0.05-0.5 Hz with a constant bathymetry of
ha=30 m. It can be observed that the value of the added mass of the three bodies for the
heave and
surge movements reach a maximum value and then decreases as period increases. For the heave motion, the maximum value of the semi-sphere is 5955 kg/m at
ω=0.107 Hz, followed by the cylinder 4476 kg/m with
ω=0.054 Hz and then the proposed geometry with a value of 4170 kg/m with
ω=0.057 Hz. The added mass physically represents an additional force that resists the movement; the intended outcome is that the value of this mass is as low as possible. In this sense, it can be observed that the proposed geometry provides less resistance to the movement. In addition,
Figure 10a shows that for the heave motion of three geometries, high values of the frequency may lead to better device performance.
Figure 10b represents the variation of the excitation force throughout the frequency; it is observed that as the frequency decreases, the
heave motion increases while the
surge decreases. In addition, the semi-sphere reaches values without significant changes from
ω=0.125 Hz, while the other two geometries show similar behaviour. It is important to point out that this force is related to the amplitude of the wave; for this reason, it has units of
N/m. It can be inferred that for high periods, the Froude-Krylov force is stronger, causing an increase in the vertical movement of the buoy and, as a result, in the angle within the
x-y plane. This causes the translation speed to be greater than or equal to the electrical power generated.
Figure 10c illustrates the behaviour of the hydrodynamic damping coefficient. It can be seen that the coefficients of the semi-sphere decrease as the period increases. As the period increases for the cylinder and proposed geometry, the
heave motion increases and eventually achieves a maximum value at
ω=0.164 Hz before decreasing again, whereas the
surge motion has almost the same behaviour in these two geometries. Therefore, this type of device would be recommended for long periods.
Finally,
Figure 10d shows the response amplitude operator (RAO) of the buoy through the
z-axis. It can be observed that the semi-sphere performs best at short wave periods, whilst the other two devices perform best at long periods. Point absorbers work best when the incident wave frequency matches their natural frequency, which for these geometries is around 0.056-0.061 Hz for the semi-sphere and 0.25-0.33 Hz for the other two.
3.3. Analysis in the time domain
In this subsection, the findings of the hydrodynamic response in the time domain obtained by ANSYS AQWA 19.2 are provided. In these simulations, a duration of 500 s is considered for the analysis and comparison between the three geometries. The wave conditions were set to
Hs = 2.2 m and
T=10.27 s and
β=0°. The first simulation enables the analysis of the system's behaviour under the influence of a second-order Stokes wave [
53], with
FPTO=0, a time step of
∆t=0.01 s,
LI=50 m and
LII=50 m. From the movement of the centre of mass, it is possible to determine the angular displacement in the rotation axis
D. Figure 11a depicts the temporal evolution of the angular motion transmitted to the PTO for the three geometries investigated during the whole simulation duration, whereas
Figure 11b depicts the first 50 seconds of simulation. It is observed that the angular displacement in the wave troughs and crests is larger for the semi-sphere geometry, while the cylinder has the opposite tendency, and the proposed geometry maintains an intermediate movement between these two. Furthermore, for the three figures it can be seen that when a crest occurs, it has more angular displacement than the trough since it does not have a damping effect from the water movement when ascending.
To determine the instantaneous power, equations (10) and (11) are used with the data in
Figure 11:
where
P is the power,
F the force of the body,
v the speed,
g the gravity and
a the instantaneous acceleration. The behaviour of the power absorbed over time is then obtained for the analysed bodies represented in
Figure 12 for the first 50 s. It can be seen that the absorbed power is variable over time, so it is necessary to determine a representative value. The average power achieved for the half sphere, cylinder, and proposed geometry was 14.98 kW, 15.8 kW, and 16.87 kW, respectively.
Figure 13 and
Figure 14 show the matrices of the average and maximum power, respectively, of the three analysed geometries. These figures show the periods from 5 to 15 s with different wave heights in the range of 0 to 4.5 m with
β=0°. For the three geometries it can be observed that for wave heights less than 0.5 m, the absorbed energy is less than 4.11 and 8.7 kW, for the mean and maximum average power, respectively. The greatest powers are found for periods of 5-7 s and wave heights greater than 3 m. For the average power, the one with the highest value is the cylinder with 90.68 kW, followed by the proposed geometry of 87.64 kW and finally the semi-spheres with 71.81 kW. The maximum power follows the same order but with the following values 437.7, 328 and 225.6 kW.
Table 4 compares the average power of each geometry analysed for different conditions. The first condition is for the significant wave height
Hs, the next one is for the average power matrix (
Figure 13) and the third one corresponds to more frequent wave conditions. It is seen that for the three cases the one that absorbs more power is the proposed geometry, followed by the cylinder and finally the semi-sphere. The average power for
Hs with the proposed geometry is 10.88% larger than that of the semi-sphere. In the average power matrix, the proposed geometry increases 2.16 kW with respect to the semi-sphere and finally, for the average of the most recurrent conditions, the proposed geometry gives 1% and 2.71% more power than the semi-sphere and the cylinder, respectively.
Table 5 shows the seasonally significant wave height, the associated wave period and the average power generated, in kWh, of each geometry analysed according to
Figure 13. It is observed that the most energetic sea condition occurs in winter, followed by autumn, spring and finally summer. However, the season of the year with the highest production in autumn, followed by winter, and finally spring and summer with the lowest generation. The percentage difference between autumn and spring is 15.02%, 14.33% and 14.39%, while for winter and spring is 4.65%, 2.78% and 2.32% for the three analysed geometries semi-sphere, cylinder and the proposed one, respectively. Furthermore, this table illustrates the energy output throughout the year, and that of the three geometries presented, the one that can collect the most energy is the one proposed, followed by the cylinder, and lastly the semi-sphere. The same occurs in the annual power, having an annual difference of 2.59 MW between the proposed geometry and the semi-sphere.
Once the dynamics at the PTO inputs are known (
Figure 6), the transmission designed for the three studied floats is evaluated by applying Equations (6)-(9), with a speed ratio
RV=10, α=-0.01 rad/s
2and the conditions of
Hs at 33.33%,
Table 1. The results are shown in
Figure 15 and only the first 50 s of the simulation are shown. The left column corresponds to positions and the second to angular velocities. These last two variables are compared to the input and three output cases; the first output is without UC and is coupled, the second with two UCs and is also coupled, and the third is with three UCs and is uncoupled. In general, it can be seen that in the first case, only the gearbox serves to increase the rotation speed, so that at the PTO output it has almost the same behaviour, but with RV amplified as much as the position and angular velocities oscillate. This could be a disadvantage for the generator that it will have to constantly change the direction of the magnetic fields.
One advantage of the second situation when ω≥0 is that ω will only be positive and the generator will always be moving in a single direction, causing the position to progressively grow. For the last case, a UC has a flywheel that absorbs movement in the form of kinetic energy, which is employed so that when the PTO speed begins to decrease, the flywheel may be uncoupled and the generator is continued going, and this does not exceed ω =0. As a result, the final proposal will be examined in greater depth in this study, as it is the most ideal for keeping the electric generator going, which translates into relatively constant electric energy, further information can be found at [
54].
Of the three geometries, the first to reach its steady-state was the semi-sphere at 20 s, then the proposed geometry at 110 s, and finally the cylinder. In the transient stage, the velocities fluctuate between 0.054-0.076, 0.053-0.084 and 0.05-0.084 rad/s, while in the steady-state they range between 0.056-0.076, 0.052-0.074 and 0.053-0.077 rad/s, for the studied semi-spheres, cylinder, and proposed geometry, respectively.
Figure 16 shows the matrix of the maximum angular displacement, in the range of
T= 5-15 s and
H ranging from 0-4.5 m and divided into intervals of 1 s and 0.5 m, respectively. The following trends are generally observed in the three study cases: for small wave heights less than 0.5 m, the displacement is minimal no matter the wave period, and as the height increases, the angle also increases. Furthermore, for
H>1 m it is observed that as the period increases, the movement is reduced, with the greatest displacement taking place when
H>3 m and
T=5-7 s. In this regard, the semi-spheres has the smallest displacement movement (0.017 rad) while the cylinder has the highest (2.556 rad). In
Figure 16a, which corresponds to the semi-spheres, its smallest values occur at
H<0.5 m when
T>7 s, while the highest occurs at
H>4 m between 6-7 s.
Figure 16b shows the maximum angular displacement matrix of the cylinder. Here, it is observed that the angles range between 0.038-2.56 rad and that the maximum angle significantly increases compared to the rest of the values, so it can be inferred that it is close to resonance at
T=6-7 s and
H=4-4.5 m.
Figure 16c shows the maximum angular displacement matrix for the proposed geometry. This figure shows that the values range between 0.026-2.18 rad, with the largest angle close to the resonance between
H=4-4.5 m and
T=5-6
s. Furthermore, by comparing the three geometries, the one with the greatest angular movement is the cylinder with 0.148 rad, followed by the proposed design with 4.7% less and finally the semi-spheres with a difference of 0.015 rad. Thus, the one with the greatest angular movement is the cylinder.
Finally,
Table 6 shows the maximum angular displacements in each season of the year for the analysed WECs obtained from
Figure 16, as well as the annual average of that movement. The one that presents the greatest movements in the four seasons of the year is the cylinder, followed by the proposed geometry and finally the semi-sphere. It is also observed autumn is where the maximum values are presented for the three geometries with values of 0.148, 0.143 and 0.133 rad. Regarding the annual average values, there is a difference between the cylinder and the semi-sphere and the proposed geometry of 12.84% and 8.21%, respectively. These displacement values aid in the right selection of the electric generator, specifically knowing at what revolutions it must function.