2. Theoretical Background
This section imparts the general understanding of the electromagnetic behavior of the electrical machine and, subsequently, to the electromagnetic force excitation, which causes noise emissions. Assuming the radial electromagnetic force excitation
, mainly depending on the radial component of the magnetic flux density
, over a given surface area
and the vacuum permeability
, defined in (
1). The magnetic flux density
including the stator and rotor mmfs,
and
, as well as the magnetic permeance
is calculated as shown in (
2) [
1,
2,
4].
Considering the slotting of the stator and rotor, as well as the saturation in the magnetic permeance
, both the mmfs of stator and rotor,
and
, and their spatial position are the main focused parts for changing the operating points and subsequently the noise emissions. In
Figure 2b,c the magneto motive forces are calculated for three different d-q-axis currents for 60 Nm of torque, as shown in the d-q-diagram in
Figure 1. It is shown that the position and the amplitude of the magneto motive forces (mmfs) depend on the slip of the induction machine.
The schematic for the fundamental electromagnetic are shown in
Figure 3a–c, where
Decreasing the stator d-axis current, decreases the flux and the magnetic flux density, similar to the field weakening area of the machine operating range. Due to this behavior, the induction machine slip frequency is increased in order to hold the desired electromagnetic torque. Increasing the slip, increases the induced voltage into the rotor bars and, with it, the rotor bar currents. As the rotor bar currents produce the rotor mmf in order to act against its origin, a field is built from the rotor side in order to damp the stator field. Increasing the induction decreases the spatial position difference between stator and rotor mmfs in comparison to the referenced system in
Figure 3a. This reduces the summed mmf, as well as the resultant magnetic flux density, shown in
Figure 3b. Decreasing the slip decreases the induction into the rotor bars. This decreases the occurring rotor bar currents and the rotor mmf decreases. This implicates the less opposing field from the rotor side. Due to this behavior, the rotor mmf damps the system less than the reference operating in
Figure 3a and the summed mmf, as well as the magnetic flux density in
Figure 3c increases. The angle between stator and rotor mmf
is related to the stator and rotor currents
and
and are defined as,
The harmonics content of each operating set at 60 Nm of torque is shown for simulated speed run-ups in the Campbell diagrams in
Figure 4a–c. These Figures show the temporal frequency decomposition of the radial forces over the mechanical machine rotor speed. Since the voltage is produced by a pulse width modulation (PWM) inverter, thus the voltage supply is non-sinusoidal and same given to each operating system. It is shown, that the d-q-axis operating point and subsequently the magneto-motive force, as well as the saturation of the magnetic permeance have a huge influence on the electromagnetic force excitation, as explained in the following.
Keeping
Figure 4a as reference, the operation in the minimum d-axis stator current in
Figure 4b shows less harmonics coming from the non-sinusoidal voltage excitation. Due to the small spatial angle difference of the stator and rotor mmfs, the rotor is able to damp more harmonics than in the reference system. This small angle and the increased rotor current reduces the fundamental amplitude of 2. Order and the saturation harmonics, 6. and 12. Order. The mechanical harmonics, like the rotor slotting harmonics of ∼18. and ∼36. Order, due to 36 rotor bars and machine pole pair number 2, are more prominent. Harmonics, like ∼24. and ∼30. Order, caused by the interaction of saturation and slotting are reduced, due to the less saturation [
3,
4,
7].
Comparing the reference operation from
Figure 4a with the operating points from
Figure 4c, the PWM-beat is more prominent due to the less damping from the cage rotor. This causes higher flux and increases the saturation harmonics, 6., 8. and 12. Order, but reduces mechanical harmonics from the rotor slotting, ∼18. and ∼26. Order, because the tooth saturation decreases the electromagnetic slotting effect. The interaction harmonics from the saturation and slotting is partly increased, like ∼24. Order, and partly decreased, like the ∼30. Order, depending on the spatial position of the saturation to the slotting harmonics [
3,
4,
7].
The simulation of the radial force decomposition can also be viewed as the force levels in
Figure 5, calculated as the summed magnitudes over all frequencies for each rotor speed. It is shown, that the radial force level in the minimum d-axis current and subsequently in the minimum flux is always lower than the radial force levels of the reference and maximum flux operating, caused by the reduced amplitudes of saturation, PWM harmonics as well as the reduction of the fundamental flux. The calculation of the level of the radial force neglects the damping of the structural dynamics system of the stator and a A-weighting in order to validate the noise perception of the humans hearing. However, the force decomposition in minimum flux operation gives a strong indication for noise reduction.
The structural dynamic of the stator is also important in order to reduce noise emissions. The structural dynamics systems damps the forces depending on its temporal frequency decomposition. Thus, the noise emissions are depending on the ratio of force excitation and the damping of the structure. Relating to the temporal harmonics of the spatial radial force order, the damping on the system can be defined for the stator structure with a transfer function
for each spatial force mode, as shown in
Figure 6.
Here, temporal frequencies in the 0th spatial force mode are mostly damped, but frequencies which are in the range of 7–11 kHz, are much less damped than others. This effect is very important to reduce noises. In general, the procedure introduced in this paper relates to reduce force excitation. Reducing high amplitudes of force harmonics, which occur in the range of natural frequencies of the structural dynamic, have the highest potential to reduce the noise emissions of induction machine [
5,
6,
8].
Finally, the radial velocity
on the surface of the induction machine is defined, with the radial force
in the spatial and temporal frequency domain
u and
f, as well as the structural transfer function
, as
Since the sound pressure level is mainly explained in the spatial and temporal time domain
and
t, the radial surface velocity
is transformed back with an 2-dimensional Fast Fourier transform (FFT) [
3,
5,
6].
3. Acoustic Measurements
In order to validate the simulation results obtained from
Section 2, measurements were performed. To receive accurate results, the surface velocity of the induction machine is recorded, using an acceleration sensor on the surface of the induction machine. In general, the radial surface velocity
shows a direct impact on the sound pressure level with the sound power
P [
6,
8], where
with the mean-square surface radial velocity
for an infinite axial length defined as,
The Velocity levels, in the following, are rated with A weighting curve in order to get a ratio of the sound pressure level and the perception of human hearing.
The measured surface velocity levels are shown in Figure 8a for speed run-ups at 20 Nm of torque. The reference, minimum and maximum flux operating shows huge differences. As described in
Section 2, the minimum flux operation has mainly the lowest velocity level, but there are also operating points, where the operation in reference flux is beneath the minimum flux curve. These points can be explained with the Campbell diagrams in
Figure 7a–c. The saturation in this operating point is less, increasing the d-current, increases the flux and the saturation, as well as the PWM-harmonics. This causes the high level of surface velocity for the maximum flux operating. Due to the operating in minimum flux, the PWM-harmonics, as well as the saturation harmonics are minimized, but the slotting harmonics are increased. If the slotting harmonics in this operating come up with the natural frequencies of the system, the slotting harmonics become prominent and increase the velocity level over the reference level.
The measured surface velocity levels for speed run-ups of 60 Nm and 100 Nm of torque are shown in
Figure 8b,c. The reference, minimum and maximum flux operating differences are not as big as in the measurements for 20 Nm of torque. The theses from
Section 2 are also approved for these operating points. Relating to the slotting, saturation and PWM-harmonics, the measurements picture same behavior, as shown for the 20 Nm of torque measurements, shown in the Campbell diagrams for 60 Nm of torque in
Figure 9a–c and 100 Nm of torque in
Figure 10a–c. Due to the stator current limitation, the operating range for higher torques gets more and more limited, which reduces the difference between the choosable flux range and shrinks the differences between the measurements.
The potential velocity differences on the induction machine surface are shown for 20 Nm of torque in
Figure 11a, for 60 Nm of torque in
Figure 11b and for 100 Nm of torque in
Figure 11c. The measurements are performed for different stator d-axis currents, including a bigger range of d-axis operating currents, as shown in the comparison above. This potential analysis shows the maximum reducibility of the surface velocity for each rotor speed. Especially at partial load, the operating area has the biggest influence and subsequently the highest potential for noise reduction. Due to the current limitation, the operating range for higher torque is limited as well. Nevertheless it shows especially for the beginning field weakening area at 3500 rpm a possibility for reducing noise emissions.
At higher torques, the system temperature increases much faster in comparison to lower torques, influencing the acoustic measurements. This fact blurs the measurement and the potential at higher torques. Shown in
Figure 11c, the potential has to be rated lower, than shown especially for speed above 4000 rpm.