The heat generated by the coil is one of the major design aspects of a DC linear actuator. In addition to significantly shortening the life expectancy of its mechanical components, the temperature changes can affect the actuator’s efficiency and repeatability. Hence, in this application note, an electrothermal simulation is performed versus multiple variables such as the coil thickness and input currents to study the heat distribution and variation at different conditions and design scenarios. Temperature-dependent material properties will be used at the end of this work to estimate the temperature variation of the actuator versus time while the electrical resistivity of the coil material changes.
Figure 1 shows the original DC linear actuator. Figure 2 contains the simulated 3D CAD model. Some non-magnetic parts were removed because they do not have any impact on the magnetic results like magnetic fields and force. However, they can affect thermal results but this effect will be neglected in this analysis. Moreover, the effect of a spring can be included in the motion study when the magnetic study is coupled to motion study.
Figure 2 illustrates the different components of the simulated DC actuator. The moving plunger and the actuator core are made of 12L14 carbon steel while the coil bobbin is made of an insulator material (FEP).
In magnetic static simulation, the heat is only produced by Joule Effect inside a conductor supplied with current. It is the only component where ohmic losses are generated.
The Ohmic loss or winding loss is expressed by the following relation: Where is the electrical resistivity of the coil material and is the current density of the coil.
Therefore, both the Ohmic loss and consequently the coil temperature are directly proportional to the coil material and the current density. Since the material of the coil is maintained the same, the current density will be varied. In this section, the input current is constant, and the coil dimensions will be changed to affect the current density results.
The coil current density depends mainly on the cross-section surface of the coil. Thus, the parametrized variable is the coil thickness as shown in Figure 3.
Figures 4a) and 4b) illustrate, respectively, full, and cross section views of the magnetic field distribution when the coil thickness is 2.2mm. It is the maximum thickness allowed by the free space of the designed actuator. The magnetic field is around 0.55T in the actuator core while it reached 2T in the moving plunger.
Figures 5a) and 5b) contain, respectively, full, and cross section views of the magnetic field distribution when the coil thickness is 1.1mm. The magnetic field results are the same as the previous scenario because input current is constant. A vector plot of the magnetic flux is shown in Figure 6.
Figure below contains the coil resistance variation versus its thickness. The resistance increases linearly from 0.094Ohm at 1.1mm to 0.106Ohm at 2.2mm.
Figures 10a) and 10b) demonstrate the steady state temperature distribution of the actuator, at the thickness of 1.1mm and 2.2mm, respectively. The computed temperature when the coil thickness is 1.1mm is 132 C while it is around 80 C in case of 2.2mm thickness. The maximum temperature is obtained in the source of heat in the actuator which is the coil and it has lower values in the other components which are in contact with the coil. Moreover, when the coil thickness becomes larger, more heat is propagated to the whole model as illustrated in Figure 10b). Figure 11 contains the temperature variation results versus different thicknesses of the coil. It follows the same behaviour as the current density variation.
In this section, the coil thickness is maintained constant at 2.2mm and the input current is varied. Values from 1A to 5A with step of 0.35A were used for the simulation.
Results of the magnetic flux density at current of 1A are given in Figures 13a) and 13b). The maximum reached magnetic field is around 1.29T in the moving plunger. At an input current of 5A, the magnetic field goes to peak value of 2.15T as shown in Figures 14a) and 14b).
The current density results calculated versus different input current rates is demonstrated in Figure 15. It represents a linear shape regarding the input current. Ohmic losses versus the coil currents are plotted in Figure 16.
The cross-section plots in Figures 17a) and 17b), illustrate steady state temperature results, respectively, at 1A and 5A for the applied current. The predicted temperature of the actuator ranges from 30 C to 32 C at 1A while it varies from 110 C up to 174 C at 5A. The highest actuator temperature is evaluated in the coil in both cases. It propagates from the coil to the whole actuator bodies until it achieves the thermal equilibrium.
Figure 18 shows the maximum temperature in the actuator versus the different applied current rates. The temperature rises with the increase of the input current as explained above.
In this final section, the copper coil is defined with temperature-depend electrical resistivity. The electrical conductivity of the copper versus temperature data is shown in Figure 19. This figure shows that the electrical conductivity of the copper decreases with the temperature i.e the electrical resistivity increases. Hence, when the temperature rises from its ambient value, the electrical resistivity of the copper winding will augment and consequently the Ohmic loss will increase also. Figure 20 illustrates the evolution of the coil Ohmic losses versus both temperature and time. Both curves confirm the previous statement. The coil copper loss increases linearly versus time to reach 2.33W after half of hour. After that, the loss becomes almost constant which indicates that the steady state is reached.
Since the coil material changes with temperature, thus its resistance will be affected. Figure 21 gives a plot of the coil DC resistance versus both time and temperature. It shows that the DC resistance increases with temperature. It measures a value of 0.1035Ohm at the ambient temperature and achieves its steady state value of 0.1295Ohm after a half of hour.
Figure 22 contains the temperature variation of the coil. It mimics the Ohmic loss evolution. The temperature increases from 25 C at t=0 to the steady state temperature of 90.03 C at t=1800 s. The actuator steady state temperature distribution is plotted in Figure 23.
In this application, EMS was used to study a linear DC actuator. The temperature results were under different operating conditions like using different coil thicknesses and input currents. The coil material was varied to make the simulation more realistic by using temperature depend electrical resistivity. The goal behind these simulation is to help users to reduce the heat generated by a coil in a DC actuator which can improve its reliability and efficiency.