Chapter 3

Off-Line Converter Design and Magnetics

First, the transformer-based flyback topology is introduced and it is shown how it can be mapped into equivalent inductor-based Buck-Boost models for easy analysis and design. Flyback zener clamp design is discussed here, and the importance of reducing both Primary-side and secondary-side leakage inductances is highlighted. Concepts like skin depth are introduced, and a quick-lookup chart is provided for designing the flyback transformer’s windings, keeping in mind the target current density (in cmil/A or A/m2). Temperature rise of commonly used cores is also discussed. Next, the Forward converter is introduced and the designs of both its output choke and transformer are discussed in detail. This includes estimation of proximity loss based on Dowell’s equations. Quick-lookup charts are presented for lowering the AC resistance (FR) by optimizing the number of layers per portion and selecting the best wire/foil thickness. Window utilization is explained, and all necessary design equations are provided. Detailed worked examples are presented throughout this chapter.

Off-line converters are derivatives of standard DC–DC converter topologies. For example, the flyback topology, popular for low-power applications (typically <100 W), is really a Buck-Boost, with its usual single-winding inductor replaced by an inductor with multiple windings. Similarly, the Forward converter, popular for medium-to-high powers, is a Buck-derived topology, with the usual inductor (“choke”) supplemented by a transformer. The flyback inductor actually behaves both as an inductor and as a transformer. It stores magnetic energy as any inductor would, but it also provides “mains isolation” (mandated for safety reasons), just like any transformer would. In the Forward converter, the energy-storage function is fulfilled by the choke, whereas its transformer provides the necessary mains isolation.

Because of the similarities between DC–DC converters and off-line converters, most of the spadework for this chapter is in fact contained in Chapter 2. The basic magnetic definitions have also been presented therein. Therefore, the reader should read that chapter before attempting this one. More information is available in Chapter 5 too.

Note that in both the flyback and the Forward converters, the transformer, besides providing the necessary mains isolation, also provides another very important function — that of a fixed-ratio down-conversion step, determined by the “turns ratio” of the transformer. The turns ratio is the number of turns of the input (“Primary”) winding, divided by the number of turns of the output (“Secondary”) winding. The question arises — why do we even feel the need for a transformer-based step-down-conversion stage, when in principle, a switching converter should by itself have been able to up-convert or down-convert at will? The reason will become obvious if we carry out a sample calculation — we will then find that without any additional “help,” the converter would require impractically low values of duty cycle — to down-convert from such a high-input voltage to such a low-output voltage. Note that the worst-case AC mains input can be as high as 270 V in certain countries. So, when this AC voltage is rectified by a conventional bridge-rectifier stage, it becomes a DC rail of almost image , which is fed to the input of the switching converter stage that follows. But the corresponding output voltage can be very low (5 V, 3.3 V, 1.8 V, and so on), so the required DC transfer ratio (conversion ratio) is extremely hard to meet, given the minimum on-time limitations of any typical converter, especially when switching at high frequencies. Therefore, in both the flyback and Forward converters, we can intuitively think of the transformer as performing a rather coarse fixed-ratio step-down of the input to a more amenable (lower) value, from which point onward the converter does the rest (including the regulation function).

Flyback Converter Magnetics

Polarity of Windings in a Transformer

In Figure 3.1, the turns ratio is n=NP/NS, where NP is the number of turns of the Primary winding, and NS is the number of turns of the Secondary winding.

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Figure 3.1: Voltage and currents in a flyback.

We have also placed a dot on one end of each of the windings. All dotted ends of a transformer are considered to be mutually “equivalent.” All non-dotted ends are also obviously mutually equivalent. This means that when the voltage on a given dotted end goes “high” (to whatever value), so does the voltage on the dotted ends of all other windings. That happens because all windings share the same magnetic core, despite the fact that they are not physically (galvanically) connected to each other. Similarly, all the dotted ends also go “low” at the same time. Clearly, the dots are only an indication of relative polarity. Therefore, in any given schematic, we can always swap all the dotted and non-dotted ends of the transformer simultaneously, without changing the schematic in any way.

In a flyback, the relative polarity of the windings is deliberately arranged such that when the Primary winding conducts, the Secondary winding is not allowed to do so. So, when the switch conducts, the dotted end at the Drain of the MOSFET in Figure 3.1 goes low. And therefore, the anode of the output diode also goes low, thereby reverse-biasing the diode. We should recall that the basic purpose of a Buck-Boost (which this in fact also is) is to allow incoming energy from the source during the switch on-time to build up in the inductor (only), and then later, during the off-time, to “collect” all this energy (and no more) at the output. Note that this is the unique property that distinguishes the Buck-Boost (and the flyback) from the Buck and the Boost. For example, in a Buck, energy from the input source gets delivered to the inductor and the output (during the on-time). Whereas, in a Boost, stored energy from the inductor and the input source gets delivered to the output (during the off-time). Only in a Buck-Boost do we have complete separation between the energy-storage and the collection process, during the on-time and the off-time. So, now we start to understand why the flyback is considered to be just a Buck-Boost derivative. More on this in Chapter 5.

We know that every DC–DC topology has a so-called “switching node.” This node represents the point of diversion of the inductor current — from its main path (i.e., by which the inductor receives energy from the input) to its freewheeling path (i.e., by which the inductor provides stored energy to the output). So, clearly, the switching node is necessarily the node common to the switch, the inductor, and the diode. We thus find that the voltage at this node is always “swinging” — because that is what is required to get the diode to alternately forward and reverse-bias, as the switch toggles. But looking at Figure 3.1, we see that with a transformer replacing the traditional DC–DC inductor, there are now, in effect, two “switching nodes” — one on each side of the transformer, as indicated by the “X” markings in Figure 3.1 — one “X” is at the Drain of the MOSFET, and the other “X” is at the anode of the output diode. These two nodes are clearly “equivalent” because of the dots, as explained above. And since at both these nodes, the voltage is swinging, both are considered to be “switching nodes” (of the transformer-based topology). Note that if we had, say, three windings (e.g., an additional output winding), we would have had three switching nodes.

Transformer Action in a Flyback and Its Duty Cycle

Classic “transformer action” implies that the voltages across the windings of the transformer, and the currents through each of them, scale according to the turns ratio, as described in Figure 3.1. But it is perhaps not immediately apparent why the flyback inductor exhibits transformer action since the windings do not conduct at the same time.

When the switch turns ON, a voltage VIN (the rectified AC input) gets impressed across the Primary winding of the transformer. And at the same time, a voltage equal to VINR=VIN/n (“R” stands for reflected) gets impressed across the Secondary winding (in a direction that causes the output diode to get reverse-biased). Therefore, there is no current in the Secondary winding when the Primary winding is conducting.

Let us calculate what VINR is. The voltage translation across the isolation boundary follows from the induced voltage equation applied to each winding:

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Note that both windings enclose the same magnetic core, so the flux ϕ is the same for both, and so is the rate of change of flux dϕ/dt for each winding. Therefore,

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or

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Also,

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This above equation represents classic “transformer action” with respect to the voltages involved. But we also learn from the preceding equation that the Volts/turn for any winding (at any given instant) is the same for all the windings present on a given magnetic core — and this is what eventually leads to the observed voltage scaling.

Note also that voltage scaling in any transformer occurs irrespective of whether a given winding is passing current or not. That is because, whether a given winding is contributing to the net flux ϕ present in the core or not, each winding encloses this entire flux, and so the basic equation V=−N×dϕ/dt applies to all windings, and so does voltage scaling.

We know that energy is built up in the transformer during the on-time. When the switch turns OFF, this stored energy (and its associated current) needs to flyback/freewheel. We also know that the voltages will automatically try to adjust themselves in any possible way, so as to make that happen. So, we can safely assume the diode will somehow conduct during the switch off-time. Now, assuming we have reached a “steady state,” the voltage on the output capacitor has stabilized at some fixed value VO. Therefore, the voltage at the Secondary-side switching node gets clamped at VO (ignoring the diode drop). Further, since one end of the Secondary winding is tied to ground, the voltage across this winding is now equal to VO. By transformer action, this reflects a voltage across the Primary winding, equal to VOR=VO×n. But the switch is OFF during this time. Therefore, under normal circumstances, the voltage at the Primary-side switching node would have settled at VIN. However, now this reflected output voltage VOR, coming through the transformer, adds to that. Therefore, the voltage at the Primary-side switching node eventually goes up to VIN+VOR (for now, we are ignoring the leakage spike encircled in Figure 3.1).

Note: During the on-time, the Primary side is the one determining the voltages across all the windings. And during the off-time, it is the Secondary winding that gets to “call the shots”!

We can calculate duty cycle from the most basic equation (from voltseconds law):

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We have the option of performing this calculation, either on the Primary winding, or on the Secondary winding. Either way, we get the same result, as shown in Table 3.1.

Table 3.1. Derivation of DC Transfer Function of Flyback.

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We should be always very clear that transformer action applies only to the voltages across windings. And “voltage across” is not necessarily “voltage at”! To describe the voltage at a given point, we have to consider what the reference level (i.e., “ground” by definition) is, with respect to which its voltage needs to be measured, or stated. In fact, the reference level (i.e., by definition, “ground”) is called the “Primary ground” on the Primary side and the “Secondary ground” on the Secondary side. Note that these are indicated by different ground symbols in Figure 3.1.

To find out the (absolute) voltage at the swinging end of any winding, we can use the following level-shifting rule:

To get the value of the voltage at the swinging end of any winding, we must add the voltage across the winding to the DC voltage present at its “nonswinging” end.

So, for example, to get the voltage at the Drain of the MOSFET (swinging end of Primary winding), we need to add VIN (voltage at other end of winding) to the voltage waveform that represents the voltage across the Primary winding. That is how we got the voltage waveforms shown in Figure 3.1.

Coming to the question of how currents actually reflect from one side of the transformer to the other, it must be pointed out that even though the final current-scaling equations of a flyback transformer are exactly the same as in the case of an actual transformer, this is not strictly “classic transformer action.” The difference from a conventional transformer is that in the flyback, the Primary and Secondary windings do not conduct at the same time. So, in fact, it seems a mystery why their currents are related to each other at all!

The current scaling that occurs in a flyback actually follows from energy considerations. The energy in a core is in general written as

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We know the windings of our flyback conduct at different times, so the energy associated with each of them must be equal to the energy in the core and must therefore be equal to each other (we are ignoring the ramp portion of the current here for simplicity). Therefore,

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where Lp is the inductance measured across the Primary winding with the Secondary winding floating (no current), and LS the inductance measured across the Secondary winding with the Primary winding floating. But we know that

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where AL is the inductance index, defined previously. Therefore, in our case we get

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Substituting in the energy equation, we get the well-known current-scaling equations:

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or

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We see that analogous to the Volts/turns rule, the Ampere-turns also need to be preserved at all times. In fact, the core itself doesn’t really “care” which particular winding is passing current at any given moment, so long as there is no sudden change in the net Ampere-turns of the transformer. This becomes the “transformer-version” of the basic rule we learned in Chapter 1 — that the current through an inductor cannot change discontinuously. Now we see that the net Ampere-turns of a transformer cannot change discontinuously.

Summarizing, transformer action works as follows — when reflecting a voltage from Primary side to Secondary side, we need to divide by the turns ratio. When going from the Secondary side to the Primary side, we need to multiply by the turns ratio. The rule reverses for currents — so we multiply by the turns ratio when going from Primary to Secondary and divide in the opposite direction.

The Equivalent Buck-Boost Models

Because of the many similarities, and also because of the way voltages scale in the transformer, it becomes very convenient (most of the time) to study the flyback as an equivalent DC–DC (inductor-based) Buck-Boost. In other words, we separate out the coarse fixed-ratio step-down ratio and incorporate it into equivalent (reflected) voltages and currents. We thereby manage to reduce the flyback transformer into a simple energy-storage medium, just like any conventional DC–DC Buck-Boost inductor. In other words, for most practical purposes, the transformer goes “out of the picture.” The advantage is that almost all the equations and design procedures we can write for a conventional Buck-Boost now apply to this equivalent Buck-Boost model. One exception to this is the leakage inductance issue (and everything related to it — the clamp, the loss in efficiency due to it, the turn-off voltage spike on the switch, and so on). We will discuss this exception later. But other than that, all other parameters — such as the capacitor, diode, and switch currents — can be more readily visualized and calculated if we use this DC–DC model approach.

The equivalent DCDC model is created essentially by reflecting the voltages and currents across the isolation boundary of the transformer to one side. But again, as in the case of the duty cycle calculation (see Table 3.1), we have two options here — we can reflect everything either to the Primary side or to the Secondary side. We thus get the two equivalent Buck-Boost models as shown in Figure 3.2. We can use the Primary-side equivalent model to calculate all the voltages and currents on the Primary side of the original flyback and the Secondary-side equivalent model for calculating all the currents and voltages on the Secondary side of the original flyback.

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Figure 3.2: The equivalent Buck-Boost models of the flyback.

We know that voltages and currents reflect across the boundary by getting either multiplied or divided by the turns ratio. In fact, the “reflected output voltage” VOR is one of the most important parameters of a flyback. As the name indicates, VOR is effectively the output voltage as seen by the Primary side. In fact, if we compare the switch waveform of the flyback in Figure 3.1 with that of a Buck-Boost, we will realize that to the switch, it seems as if the output voltage is really VOR. See Figure 3.2.

As an example, suppose we have a 50-W converter with an output of 5 V at 10 A and a turns ratio of 20. The VOR is therefore 5×20=100 V. Now, if we change the set output to say 10 V and reduce the turns ratio to 10, the VOR is still 100 V. We will find that none of the Primary-side voltage waveforms change in the process (assuming efficiency doesn’t change). Further, if we have also kept the output power constant in the process, that is, by changing the load to 5 A for an output at 10 V, all the currents on the Primary side will also be unaffected. Therefore, the switch will neverknow the difference”. In other words, the switch virtually “thinks” that it is a simple DC–DC Buck-Boost — delivering an output voltage of VOR with a load current of IOR.

As mentioned, the only difference between a transformer-based flyback that “thinks” it is providing an output of VOR with IOR and an inductor-based version that really is providing an output of VOR with IOR is the “leakage inductance” of the flyback transformer. This is that part of the Primary side inductance that is not coupled to the Secondary side and therefore cannot partake in the transfer of useful energy from the input to the output. We can confirm from Figure 3.1 that the only portion of the Primary-side (switch) voltage waveform that “doesn’t make it” to the Secondary side is the spike occurring just after the turn-off transition. This spike comes from the uncoupled leakage inductance, as we will soon see.

Note that in the equivalent Buck-Boost models, the reactive component values also get reflected — though as the square of the turns ratio. We can understand this fact easily from energy considerations. For example, the output capacitor CO in the original flyback was charged up to a value of VO. So, its stored energy was image . In the Primary-side Buck-Boost model, the output of the converter is VOR, that is, VO×n. Therefore, to keep the energy stored in this capacitor invariant (in the DC–DC model, as in the flyback), the output capacitance must get reflected to the Primary side according to CO/n2. Notice also from Figure 3.2 how the inductance reflects. This is consistent with the fact that LΝ2.

The Current Ripple Ratio for the Flyback

Looking at the equivalent Buck-Boost models in Figure 3.2, the center of the ramp on the Secondary side (average inductor current, “IL” or IDC) must be equal to IO/(1–D), as for a Buck-Boost (because the average diode current must equal the load current). This Secondary-side “inductor” current gets reflected to the Primary side, and so the center of the Primary-side inductor current ramp is “ILR,” where ILR=IL/n. Equivalently, it is equal to IOR/(1–D), where IOR is the reflected load current, that is, IOR=IO/n. Similarly, the current swings on the Primary and Secondary sides are also related via scaling (turns ratio n). Therefore, we see that the ratio of the swing to the center of the ramp is identical on both sides (Primary- and Secondary-side DC–DC models). We are thus in a position to define a current ripple ratio r for the flyback topology too — just as we did for a DC–DC converter. We just need to visualize r in a slightly different manner this time — in terms of the center of the ramp (switch or diode) rather than the DC inductor level (because there is no inductor present really). And as for DC–DC converters, we should try to set it to around 0.4 in most cases.

The value of r for a flyback is the same for both the Primary and the Secondary DC–DC equivalent models.

The Leakage Inductance

The leakage inductance can be thought of as a parasitic inductance in series with the Primary-side inductance of the transformer. So, just at the moment the switch turns OFF, the current flowing through both these inductances is “IPKP,” that is, the peak current on the Primary side. However, when the switch turns OFF, the energy in the Primary inductance has an available freewheeling path (through the output diode), but the leakage inductance energy has nowhere to go. So, it expectedly “complains” in the form of a huge voltage spike (see Figure 3.1). This spike (or a scaled version of it) is not seen on the Secondary side, simply because this is not a coupled inductance, like the Primary inductance.

If we don’t make any effort to collect this leakage energy, the spike can be very large, causing switch destruction. Since we certainly can’t get this energy to transfer to the Secondary side, we have just two options — either we can try to recover it and cycle it back into the input capacitor, or we burn it (dissipation). The latter approach is usually preferred for the sake of simplicity. It is commonly accomplished by means of a straightforward “zener diode clamp,” as shown in Figure 3.1. Of course, the zener voltage must be chosen according to the maximum voltage the switch can tolerate. Note that for several reasons, in particular efficiency, it is preferable to connect this zener across the Primary winding, as shown (via a blocking diode in series with it). An alternative method is to connect it from the switching node to Primary ground.

We can ask — where does the leakage inductance reside? Most of it is inside the Primary winding of the transformer, though some of it lies in the printed circuit board (PCB) trace sections and transformer terminations, especially with those associated with the Secondary winding, as we will see further.

Zener Clamp Dissipation

If we intend to burn the energy in the leakage, it is important to know how this affects the efficiency. It is sometimes intuitively felt the energy dissipated every cycle is image , where IPK is the peak switch current and LLKP is the Primary-side leakage. That certainly is the energy residing in the leakage inductance (at the moment the switch turns OFF), but it is not the entire energy that gets dissipated in the zener clamp on account of the leakage.

The Primary winding is in series with the leakage, so during the small interval that the leakage inductance is trying, in effect, to attain reset by freewheeling into the zener, the Primary winding is forced to follow suit and continues to provide this in-series current. Though the Primary winding is certainly trying (and managing partially) to freewheel into the Secondary side, a part of its energy also gets diverted into the zener clamp — continuing till the leakage inductance achieves full reset (zero clamp current). In other words, some energy from the Primary inductance gets virtually plucked out by the series leakage inductance, and this energy also finds its way into the zener, along with the energy residing in the leakage itself. A detailed calculation (see Figure 7.10) reveals that the zener dissipation actually is

image

So, the energy in the leakage image gets multiplied by the term Vz/(VzVOR) (this additional term is from the Primary inductance).

Note that if the zener voltage is too close to the chosen VOR, the dissipation in the clamp goes up steeply. VOR therefore always needs to be picked with great care. That simply means that the turns ratio has to be chosen carefully!

Secondary-Side Leakages also Affect the Primary Side

Why did we use the symbol “LLK” in the dissipation equation above? Why didn’t we identify it as the Primary-side leakage (“LLKP”)? The reason is that LLK represents the overall leakage inductance as seen by the switch. So, it is partly LLKP — but it also is influenced by the Secondary-side leakage inductance. This is a little hard to visualize, since by definition, the Secondary-side leakage inductance is not supposed to be coupled to the Primary side (and vice versa). So, how could it be affecting anything on the Primary side?

The reason is that just as the Primary-side leakage prevents the Primary-side current from freewheeling into the output immediately following the turn-off transition (thereby causes an increase in the zener dissipation), any Secondary-side inductance also prevents the freewheeling path from becoming available immediately. Basically, the Secondary-side inductance insists that we (“politely” and) slowly build up the current through it — respecting the fact that it is an inductance after all! However, until the current in the bona fide freewheeling path can build up to the required level, the Primary-side current still needs to freewheel somewhere! The path the inductor current therefore seeks out is the one containing the zener clamp (that being the only path available). The zener can therefore see significant dissipation, even assuming zero Primary-side leakage.

In brief, the Secondary-side leakage has created much the same effect as a Primary-side leakage.

When both Primary- and Secondary-side leakages are present, we can calculate the effective Primary-side leakage (as seen by the switch and zener clamp) as

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So, like any other reactive element, the Secondary-side leakage also reflects onto the Primary side according to the square of the turns ratio, where it adds up in series with any Primary-side leakage present (see Figure 3.2).

For a given VOR, if the output voltage is “low” (e.g., 5 V or 3.3 V), the turns ratio is much greater. Therefore, if the chosen VOR is very high, the reflected Secondary-side leakage can become even greater than any Primary-side leakage. This can become quite devastating from the efficiency standpoint.

Measuring the Effective Primary-side Leakage Inductance

The best way to know what LLK really is, is by measuring it! Commonly, a leakage inductance measurement is done by shorting the Secondary winding pins and then measuring the inductance across the ends of the (open) Primary winding. By shorting, we virtually cancel out all coupled inductance. And so what we measure is just the Primary-side leakage inductance in this case.

However, the best method to measure leakage is actually an in-circuit measurement so that we include the Secondary-side PCB traces in the measurement. The recommended procedure is as follows.

On the given application board, a thick piece of copper foil (or a thick section of braided copper strands), with as short a length as possible, is placed directly across the diode solder pads on the PCB. A similar piece of conductor is placed across the output capacitor solder pads. Then, if we measure the inductance across the (open) Primary winding pins, we will measure the effective leakage inductance LLK (not just LLKP).

We will find that the contribution from the Secondary-side traces can in fact make LLK several times larger than LLKP. LLKP can of course be measured, if desired, by placing a thick conductor across the Secondary pins of the transformer.

The PCB used in the above-described procedure can be just a bare board with no components mounted on it other than the transformer. Or it can even be a fully assembled board (though sometimes, we may need to cut the trace connecting the Drain of the MOSFET to the transformer).

If we want to mathematically estimate the inductance of the Secondary-side traces, the rule of thumb we can use is 20 nH per inch. But here, we need to include the full electrical path of the high-frequency output current — starting from one end of the Secondary winding, returning to its other end, through the diode and output capacitor(s). We will be surprised to calculate or measure that even an inch or two of trace length can dramatically decrease the efficiency by 5–10% in low-output voltage applications.

Worked Example (7) — Designing the Flyback Transformer

A 74-W Universal Input (90–270 VAC) flyback is to be designed for an output of 5 V at 10 A and 12 V at 2 A. Design a suitable transformer for it, assuming a switching frequency of 150 kHz. Also, try to use a cost-effective 600-V-rated MOSFET.

Fixing the VOR and Vz

At maximum input voltage, the rectified DC to the converter is

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With a 600-V MOSFET, we must leave at least 30-V safety margin when at VINMAX· So, in our case, we do not want to exceed 570 V on the Drain. But from Figure 3.1, the voltage on the Drain is VIN+VZ. Therefore,

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We pick a standard 180-V zener.

Note that if we plot the zener dissipation equation presented earlier, as a function of VZ/VOR, we will discover that in all cases, we get a “knee” in the dissipation curve at around VZ/VOR=1.4. So, here too, we pick this value as an optimum ratio that we would like to target. Therefore,

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Turns Ratio

Assuming the 5-V output diode has a forward drop of 0.6 V, the turns ratio is

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Note that the 12-V output may sometimes be regulated by a linear post-regulator. In that case, we may have to make the transformer provide an output 3–5 V higher (than the final expected 12 V) — to provide the necessary “headroom” for the linear regulator to operate properly. This additional headroom not only caters to the dropout limits of the linear regulator, but in general also helps achieve a regulated 12 V under all load conditions. However, there are also some clever cross-regulation techniques available that allow us to omit the 12-V linear regulator, particularly if the regulation requirements of the 12-V rail are not too “tight,” and also if there is some minimum load assured on the outputs. In our example, we are assuming there is no 12-V post-regulator present. Therefore, the required turns ratio for the 12-V output is 128/(12+1)=9.85, where we have assumed the diode drop is 1 V in this case.

Maximum Duty Cycle (theoretical)

Having verified the selection of VZ and VOR at highest input, now we need to get back to the lowest input voltage because we know from the previous discussions about the Buck-Boost (see the “general inductor design procedure” in Chapter 2) that VINMIN is the worst-case point we need to consider for a Buck-Boost inductor/transformer design.

The minimum-rectified DC voltage to the converter is

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We are ignoring the voltage ripple on the input terminals of the converter, and therefore we will take this as the DC input to the converter stage. So, the duty cycle at minimum input voltage is

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This is clearly a “theoretical” estimate — implying 100% efficiency. We will in fact ignore this value ultimately, as we will be estimating D more accurately by another trick.

Note, however, that this is the operating DMAX. When we “power down” our converter for example, the duty cycle will actually increase further in an effort to maintain regulation (unless current limit and/or duty cycle limit is encountered along the way). Then depending upon the number of missing AC cycles for which we may need to ensure regulation (the “holdup time” specification), we will need to select a suitable input capacitance and also the maximum duty cycle limit, DLIM of our controller. Typically, DLIM is set around 70%, and the capacitance is selected on the basis of the 3 µF/W rule of thumb. For example, for our 74-W supply with an estimated 70% efficiency at low line, we will draw an input power of 74/0.7=106 W. Therefore, we should use a 106×3=318 μF (standard value 330 µF) input capacitor. However, note that the ripple current rating of this capacitor (and its life expectancy) must be verified as described in Chapter 6.

Effective Load Current on Primary and Secondary Sides

Let us lump all the 74-W output power into an equivalent single output of 5 V. So, the load current for a 5-V output is

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On the Primary side, the switch “thinks” its output is VOR and the load current is IOR, where

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Duty Cycle

The actual duty cycle is important because a slight increase in it (from the theoretical ideal efficiency value) may lead to a significant increase in the operating peak current and the corresponding magnetic fields.

The input power is

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The average input current is therefore

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The average input current tells us what the actual duty cycle “D” is, because IIN/D is also the center of the Primary-side current ramp and must equal ILR, that is,

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solving,

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We thus have a more accurate estimate of duty cycle.

Actual Center of Primary and Secondary Current Ramps

The center of the Secondary-side current ramp (lumped) is

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The center of the Primary-side current ramp is

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Peak Switch Current

Knowing ILR, we know the peak current for our selected current ripple ratio:

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We may need to set the current limit of the controller, for example, based on this estimate.

Voltseconds

We have at VINMIN

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The on-time is

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So, the voltsμseconds is

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Primary-Side Inductance

Note that when we come to designing off-line transformers, for various reasons like reducing high-frequency copper loss, reducing size of transformer, and so on, it is more common to set r at around 0.5. So, the Primary-side inductance must then be (from the “L×I” rule)

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Selecting the Core

Unlike made-to-order or off-the-shelf inductors, when designing our own magnetic components, we should not forget that adding an air gap dramatically improves the energy-storage capability of a core. Without the air gap, the core could saturate even with very little stored energy. See Chapter 5 for a deeper understanding of air gaps.

Of course, we still need to maintain the desired L, corresponding to the desired r! So, if we add too much of a gap, we will also need to add many more turns — thus increasing the copper loss in the windings. At one point, we will also run out of window space to accommodate these windings. So, a practical compromise must be made here, one that the following equation actually takes into account (applicable to ferrites in general, for any topology):

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where f is in kHz.

In our case, we get

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We start looking for a core of this volume (or higher). We find a candidate in the EI-30. Its effective length and area are given in its datasheet as

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So, its volume is

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which is a little larger than we need, but close enough.

Number of Turns

The voltage-dependent equation

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connects B to L. However we also know that a statement about r is equivalent to a statement about L — for a given frequency (the “L×I equation”). So, combining these equations, and also connecting the swing in the B-field to its peak (through r), we get a very useful form of the voltage-dependent equation, in terms of r (expressed in MKS units):

image

So, even with no information about the permeability of the material, air gap, and so on, we already know the number of turns required on a core with area Ae that will produce a certain B-field. We also know that with or without an air gap, the B-field should not exceed 0.3 T for most ferrites. So, solving the equation for N (N is NP here, the number of Primary turns),

image

We will have to verify that this can be accommodated in the window of the core — along with the bobbin, tape insulation, margin tape, Secondary windings, sleeving, and so on. Usually, that is no problem for a flyback.

Note that if we want to reduce N, the possible ways are — choose a larger r, or decrease the duty cycle (i.e., pick a lower VOR), or allow a higher B (select new material!), or increase the area of the core — the latter, hopefully, without increasing the volume.

The number of Secondary turns (5-V output) is

image

But we want an integral number of turns. Further, approximating this to just one turn is not a good idea since there will be more leakage. We therefore prefer to set

image

So, with the same turns ratio (i.e., VOR unchanged)

image

The number of turns for the 12-V output is obtained by the scaling rule

image

where we have assumed the 5-V diode has a drop of 0.6 V and the 12-V diode has a drop of 1 V.

Actual B-Field

So, now we can use the voltage-dependent equation to solve for B:

image

But in fact we don’t have to use this equation anymore! We realize that ΒPK is inversely proportional to the number of turns. So, if, with a calculated 35.5 turns, we had a peak field of 0.3 T, then with 46 turns we will have (keeping L and r unchanged!)

image

The swing is related to the peak by (see section titled “Field Ripple Ratio” in Chapter 2)

image

Note that in CGS units, the peak is now 2,315 G, and the AC component is half the swing, that is, 463 G (since r=0.5).

Note: If we start with a B-field target of 0.3 T, we are likely to reach a lesser B-field after rounding up the Secondary turns to the nearest higher integer, as we did above. That of course is not only expected, but also acceptable. However, note that on power-up or power-down, for example, the B-field will increase further, as the converter tries to continue regulating. That is why we need to set the maximum duty cycle limit and/or current limit accurately, or the switch can be destroyed due to inductor/transformer saturation. Cost-effective flyback designs with fast-acting current limit and fast switches (especially those with an integrated MOSFET) generally allow for a peak B-field of up to 0.42 T, so long as the operating field is 0.3 T or less. But see Chapter 5 too.

Air Gap

Finally, we need to consider the permeability of the material. L is related to permeability by the equation:

image

Here z is the “gap factor”:

image

Note that z can range from 1 (no gap) to virtually any value. A z of 10, for example, increases the energy-handling capability of an ungapped core set by a factor of 10 (its AL value falls by the same factor, and so does its effective permeabilityμe=μμ0/z). So, large gaps certainly help, but since we are still interested in maintaining L to a certain value based on our choice of r, we will have to increase the number of turns substantially. As mentioned, at some point, we just may not be able to accommodate these windings in the available window, and further, the copper loss will also increase greatly. So, z in the range of 10–20 is a good compromise for gapped transformers made out of ferrite material. Let us see what it comes out to be, based on our existing requirements and choices

image

So,

image

This is an acceptable value too. Finally, solving for the length of air gap,

image

Note: In general, if we use a center-gapped transformer, the total gap in the center must be equal to the above-calculated value, whether each center limb has been ground or not. But if spacers are being inserted on both side limbs (say on an EE or EI type of core), the thickness of the spacer on each outer limb must be half of the above-calculated value because the total air gap is then as desired. See Figure 5.17.

Selecting the Wire Gauge and Foil Thickness

In an inductor, the current undulates relatively smoothly. However, in a flyback transformer, the current in one winding stops completely to let the other winding take over. Yes, the core doesn’t care (and doesn’t even know) which of its windings is passing current at a given moment, as long as the Ampere-turns is maintained — because only the net Ampere-turns determine the field (and energy) inside the core. But as far as the windings themselves are concerned, the current is now pulsed — with sharp edges and therefore with significant high-frequency content. Because of this, “skin depth” considerations are necessary for choosing the appropriate wire thickness of the windings of a flyback transformer.

Note: We had ignored this for DC–DC inductors, but in high-frequency DC–DC designs too (or with high r), we may need to apply skin depth considerations.

At high frequencies, the electric fields between the electrons become strong enough to cause them to repel each other rather decisively and thereby cause the current to crowd on the exterior (surface) of the conductor (see exponential curve in Figure 3.3). This crowding worsens with frequency as per image . There is thus the possibility that though we may be using thick wire in an effort to reduce copper loss, a good part of the cross-section of the wire (its “innards”) just may not be available to the current. The resistance presented to the current flow is inversely proportional to the area through which the current is flowing or is able to flow. So, this current crowding causes an increase in the effective resistance of the copper (as compared to its DC value). The resistance now presented to the current is called the “AC resistance” (see lower half of Figure 3.3). This is a function of frequency because so is the skin depth. Therefore, instead of wasting precious space inside the transformer and losing efficiency, we must try to use more optimum diameters of wire — in which the cross-sectional area is better utilized. Thereafter, if we need to pass more current than the chosen cross-sectional area can handle, we need to parallel several such strands.

image

Figure 3.3: Skin depth and AC resistance explained.

So, how much current can a given wire strand handle? That depends purely on the heat buildup and the need to keep the overall transformer at an acceptable temperature rise. For this, a good guideline/rule of thumb for the current density of flyback transformers is 400 circular mils (“cmils”) per Ampere, and that is our goal too in the analysis that follows.

Note: Expressing “current density” in the North American way of cmils/A needs a little getting used to. It is actually area per unit Ampere, not Ampere per unit area (as we would normally expect a “current density” to be)! So, a higher cmils/A value actually is a lower current density (and vice versa) — and will produce a lower temperature rise.

We define the skin depthδ” as the distance from the surface of a conductor at which the current density falls to 1/e times the value at the surface. Note that the current density at the surface is the same as the value it would have had all through the copper, were there no high-frequency effects. As a good approximation to the exponential curve, we can also imagine the current density remaining unchanged from the value at the surface, until the skin depth is reached, falling abruptly to zero thereafter. This follows from an interesting property of the exponential curve that the area under it from 0 to ∞ is equal to the area of a rectangle passing through its 1/e point (see Figure 3.3 and also Figures 5.21 and 5.22).

Therefore, when using round wires, if we choose the diameter as twice the skin depth, no point inside the conductor will be more than one skin depth away from the surface. So, no part of the conductor is unutilized. In that case, we can consider this wire as having an AC resistance equal to its DC resistance — there is no need to continue to account for high-frequency effects so long as the wire thickness is chosen in this manner.

If we use copper foil, its thickness too needs to be about twice the skin depth.

In Figure 3.4, we have a simple nomogram for selecting the wire gauge and thickness. The upper half of this is based on the current-carrying capability as per the usual requirement of 400 cmil/A. But the readings can obviously be linearly scaled for any other desired current density. The vertical grid on the nomogram represents wire gauges. An example based on a switching frequency of 70 kHz is presented in the figure. In a similar manner, for our previous worked example, we see that for 150-kHz operation, we should use AWG 27. But its current-carrying capacity is only 0.5 A at 400 cmils/A (and only 0.25 A at a lower current density of 800 cmils/A!). Therefore, since the center of the Primary current ramp was iterated and estimated to be 1.488 A, we need three strands of AWG 27 (twisted together) to give a combined current-carrying capability of 1.5 A (which is slightly better than what we need).

image

Figure 3.4: Nomogram for selecting wires and foil thicknesses, based on skin depth considerations.

Coming to the Secondary side of the worked example, we remember we had lumped all the current as a 5-V equivalent load of 15 A. But in reality it is only 10 A, two-thirds of that. So, the center of its current ramp, which we had calculated was about 34 A, is actually (2/3)×34=22.7 A. The balance of this, that is, 34–22.7=11.3 A, reflects as (5.6/13)×11.3=4.87 A into the 12-V winding. So, the center of the 12-V output’s current ramp is 4.87 A. We can choose the 12-V winding arrangement using the same arguments we present below for the 5-V winding.

For the 5-V winding, we can consider using copper foil, since we have only two turns and we need a high current-carrying capability. The center of the 5-V Secondary-side current ramp is about 23 A. The appropriate thickness (2δ) at this frequency is found by projecting downward along the AWG 27 vertical line. We get about 14-mil thickness. But we still don’t know if the current through it will follow our guideline of 400 cmil/A, since it is a foil. We need to check this out further.

One “cmil” is equal to 0.7854 square mils (sq.mils). Therefore, 400 cmils is 400×0.7854=314 sq.mils (note π/4=0.7854). So, for 23 A, we need 23×314=7,222 sq.mils. But the thickness of the foil is 14 mils. Therefore, we need the copper foil to be 7,222/14=515 mils wide, that is, about half an inch. Looking at a bobbin for the EI-30 in Figure 3.5, we see it can accommodate a foil 530 mils wide. So, this is just about acceptable. Note that if the available width is insufficient, we would need to look for another core altogether — one with a “longer” (stretched-out) profile. Cores like that are available as American “EER” cores (these are EE cores with the “R” indicating a round centerpost). Or we can again consider using several paralleled strands of round wire. The problem is that a bunch of 46 twisted strands (of AWG 27) is going to be bulky, difficult to wind, and will also increase the leakage inductance. So, we may like to use say 11 or 12 strands of AWG 27 twisted together into one bunch, and then take four of these bunches (all electrically in parallel), laid out side by side to form one layer of the transformer. For a two-turns Secondary, therefore, we would wind two layers of this.

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Figure 3.5: Checking to see if a 23-A foil can be accommodated on an EI-30 bobbin.

Forward Converter Magnetics

The procedure presented in this section applies explicitly to the single-switch Forward converter. However, the general procedure remains unchanged for the two-switch Forward converter as well.

Duty Cycle

The duty cycle of a Forward converter is

image

Comparing this with the duty cycle of a Buck, we see that the only difference is the term NS/NP. As mentioned, this is the coarse fixed-ratio step-down function available due to transformer action. We can therefore visualize that the input voltage VIN gets reflected to the Secondary side. This reflected voltage (VINR=VIN/n where n=NP/NS) gets impressed at the Secondary-side switching node. From there on, we have in effect a simple DC DC Buck stage, with an input voltage of VINR and an output voltage of VO (see Figure 3.6). Therefore, the design of the Forward converter’s choke is not going to be covered here, as it is designed using the same procedure as that of any Buck inductor. However, the Forward converter’s transformer is another story altogether!

image

Figure 3.6: The single-ended Forward converter.

Note: Regarding choke design, we should keep in mind that for high-current inductors, as would be found in a typical Forward converter, the calculated wire gauge may be too thick (and stiff) for winding easily over the core/bobbin. In that case, several thinner wire gauges may be twisted together to make the winding more flexible and easier to handle in production. Further, since choke and inductor design has usually little to do with high-frequency skin depth considerations, we can choose strands of almost any practical diameter, so long as we have enough net copper cross-sectional area to keep the temperature rise to within about 40–50°C.

Unlike a flyback transformer, the Forward converter’s Secondary winding conducts at the same time as the Primary winding. This leads to an almost complete flux cancellation inside the core. But there is one component of the Primary current waveform which remains the same, irrespective of the load. This is the magnetization current component — shown in gray on the left side of Figure 3.6. At zero load, this is the entire current through the Primary winding and switch (assuming duty cycle remains fixed). As soon as we try to draw some load current, the Secondary-winding current increases, and so does the Primary-winding current. Each current increases proportionally to the load current, and so their increments too are mutually proportional — the proportionality constant being the turns ratio. But more significantly, they are of opposite sign — that is, looking at Figure 3.6, we see that the current enters the dotted end of the transformer on the Primary side, and on the Secondary side, it leaves by the dotted end at the same time. Therefore, the net flux in the core of the transformer remains unchanged from the zero load condition (assuming D is fixed) because the core just never “sees” any change in the net Ampere-turns flowing through its windings. All conditions inside the core, that is, the flux, the magnetic fields, the energy stored, and even the core loss, are dependent only on the magnetization current. Of course, the windings themselves have a different story to relate — they bear the entire brunt, not only of the actual load current, but also of the sharp edges and consequent high-frequency content of the pulsed current waveforms.

The magnetization current component is not coupled by transformer action to the Secondary current. In that sense, it is like a “parallel leakage inductance.” We need to subtract this component from the total switch current, and only then will we find that the Primary and Secondary currents scale according to the turns ratio. In other words, the magnetization current does not scale — it stays confined to the Primary side.

But in fact, the magnetization current is the only current component that is storing any energy in the transformer. So, in that sense, it is like the flyback transformer! But, if we are to achieve a steady state, even a transformer needs to be “reset” every cycle (along with the output choke). But unfortunately, the magnetization energy is effectively “uncoupled,” because of the output diode direction, and so we can’t transfer it over to the Secondary side. If we don’t do anything about this energy, it will certainly destroy the switch by a spike similar to the leakage in a flyback. We don’t want to burn it either, for efficiency reasons. Therefore, the usual solution is to use a “tertiary winding” (or “energy-recovery winding”), connected as shown in Figure 3.6. Note that this winding is in flyback configuration with respect to the Primary winding. It conducts only when the switch turns OFF, and thereby it freewheels the magnetization energy back into the input capacitor. There is some loss associated with this “circulating” energy term because of the diode drop and resistance of the tertiary winding. Note, however, that any bona fide leakage inductance energy also gets recycled back into the input by the tertiary winding. So, we don’t need an additional clamp for it in a traditional Forward converter.

For various subtle reasons, like being able to ensure the transformer resets predictably under all conditions, and also for various production-related reasons, the number of turns of the tertiary winding is usually kept exactly the same as the Primary winding. Therefore by transformer action, the voltage at the Primary-side switching node (Drain of the MOSFET) must rise to 2×VIN when the switch turns OFF. Therefore, in a Universal Input off-line single-ended (i.e., single-switch) Forward converter, we need a switch rated for at least 800 V.

As soon as the transformer is reset (i.e., the current in the tertiary winding returns to zero), the Drain voltage suddenly drops to VIN — that is, no voltage is then present across the Primary winding — and therefore there is no voltage across the Secondary winding either. The catch diode of the output stage (i.e., the diode connected to the Secondary ground in Figure 3.6) then freewheels the energy contained in the choke. Note that there is actually some ringing at the Drain of the MOSFET for a while, around an average level of VIN, just after transformer reset occurs. This is attributable to various undocumented parasitics. The ringing contributes significantly to the radiated electromagnetic interference (EMI).

Note that even prior to transformer reset occurring, the Secondary winding has not been conducting for a while — simply because the output diode (i.e., the one connected to the swinging end of the Secondary winding) has been reverse-biased during the time the tertiary winding was conducting.

Note also that the duty cycle of such a Forward converter can under no circumstances ever be allowed to exceed 50%. The reason for that is we have to unconditionally ensure that transformer reset will always occur, every cycle. Since we have no direct control on the transformer current waveforms, we have to just leave enough time for the current in the tertiary winding to ramp down to zero on its own. In other words, we have to allow voltseconds balance to occur naturally in the transformer. However, because the number of turns in the tertiary winding is equal to the Primary turns, the voltage across the tertiary winding is equal to VIN when the switch is ON and is also equal to VIN (opposite direction) when the switch is OFF. Reset will therefore occur when tOFF becomes equal to tON. So, if the duty cycle exceeds 50%, tON would certainly always exceed tOFF, and therefore transformer reset would never be able to occur. That would eventually destroy the switch. Therefore, just to allow tOFF to be large enough, the duty cycle must always be kept to less than 50%.

We realize that the Forward converter transformer is always in discontinuous mode (DCM) (its choke, i.e. inductor L, is usually in continuous conduction mode (CCM), with an r of 0.4). Further, since the flux in the transformer remains unchanged for all loads, we can logically deduce that no part of the energy flowing through it into the output must be being stored in the transformer. So, the question really is — what does the power-handling capability of a Forward converter transformer depend on? We intuitively realize that we can’t use any size transformer for any output wattage! So, what governs the size? We will soon see that it is determined simply by how much copper we can squeeze into the available “window area” of the core (and more importantly, how well we can utilize this available area) without getting the transformer too hot.

Worst-Case Input Voltage End

The most basic question in design invariably is — what input voltage represents the worst-case point at which we need to start the design of the magnetics (from the viewpoint of core saturation)? For the Forward converter choke, this should be obvious — as for any Buck converter, we need to set its current ripple ratio at around 0.4 at VINMAX. But coming to the transformer, we need some analysis before we can make a proper conclusion.

Note that the transformer of a Forward converter is in DCM, but the duty cycle is determined by the choke, which is in CCM. Therefore, the duty cycle of the transformer also gets “slaved” at the CCM duty cycle of D=VO/VINR, despite the fact that it is in DCM. This rather coincidental CCM+DCM interplay leads to an interesting observation — the voltseconds across the Forward converter transformer is a constant irrespective of the input voltage. The following calculation makes that clear, by the fact that VIN cancels out completely:

image

So, in fact, the swing of the transformer current (or its field) is the same at high input or at low input, or in fact at any input (as long as the choke remains in CCM). Since the transformer is in DCM, its peak is equal to its swing, and so the peak too does not depend on VIN. Of course, the peak switch current ISW_PK is the sum of the peak of the magnetization current IM_PK, and the peak of the Secondary-side current waveform reflected onto the Primary side, that is,

image

So, although the current limit of the switch must be set high enough to accommodate ISW_PK at VINMAX (since that is where the maximum peak of the reflected output current component occurs), as far as the transformer core is concerned, the peak current (and corresponding field) is just IM_PK, which does not depend on VIN! This is, indeed, an interesting situation. Note also that as far as the choke is concerned, the peak inductor current is no longer equal to the (reflected) peak switch current (as in a DC–DC Buck topology), though the peak (free wheeling) diode current still is. Yes, if we subtract the magnetization current from the switch current, and then scale (reflect) it to the Secondary side according to the turns ratio, then the peak of that waveform will be equal to the peak inductor current.

So, effectively IM has the property of input voltage rejection. We can understand this in the following way — as the input increases, the slope of the transformer current increases, and ΔI therefore tends to increase. However, the output choke, sensing a higher VINR, decreases its duty cycle and therefore also the on-time of the transformer, and that tends to reduce its current swing. Coincidentally, these two opposing forces counterbalance each other perfectly, and so there is no net change in the current swing of the transformer.

As a corollary, the core loss in the transformer is independent of the input voltage too. The copper loss, on the other hand, is always worse at low inputs (except for the DC–DC Buck) — simply because the average input current has to increase so as to continue to satisfy the basic power requirement PIN=VIN×IIN=PO.

Though we can pick any specific input voltage point for assuring ourselves that the core does not saturate anywhere within its input range, since the copper loss is at its worst at VINMIN, we conclude that the worst case for a Forward converter transformer is at VINMIN. For the choke, it is still VINMAX.

Window Utilization

Looking at a typical winding arrangement on an “ETD-34” core and bobbin in Figure 3.7, we see that the plastic bobbin occupies a certain part of the space provided by the core — thus reducing the available window “Wa” from 171 mm2 to 127.5 mm2 — that is, by 74.5%. Further, if we include the 4-mm “margin tape” that needs to be typically provided on either side (to satisfy international safety norms regarding clearance (separation through air) and “creepage” (separation over surface of insulator) requirements between Primary and Secondary sides), we are left with an available window of only 78.7 mm2 — that is a total reduction of 78.7/171=46%. In addition to this, looking at the left side of Figure 3.8, we see that for any given wire, only 78.5% of the square area it “physically occupies” (or will occupy in the transformer) is actually conducting (copper). So, in all, this leads to a total reduction of the available window space by 0.46×0.785=36%. See also Figure 5.21.

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Figure 3.7: An ETD-34 bobbin analyzed.

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Figure 3.8: The area physically occupied by a round wire and a “square wire” of the same conducting cross-sectional area as a round wire.

We realize some more space will be lost to interlayer insulation (and any EMI screens if present), and so on. Therefore, finally, we estimate that perhaps only 30–35% of the available core window area will actually be occupied by copper. That is the reason why we need to introduce a “window utilization factor” K (later we will set it to an estimated value of 0.3). So,

image

and

image

Here ACU is the cross-sectional area of one copper wire and Wa is the entire window area of the core (note that for EE, EI types of cores this is only the area of one of its two windows!).

Relating Core Size to Its Power Throughput

We remember that the original form of the voltage-dependent equation is

image

Substituting for N, the number of Primary turns, we get

image

Performing some manipulations,

image

where image is the current density in A/m2 and “AP” is called the “area product” (AP=Ae×Wa). Let us now convert into CGS units for greater convenience. We get

image

where AP is also in cm2 now. Finally, converting the current density into cmils/A by using

image

we get

image

Solving for the area us do some substitutions here. Assuming a typical current density of 600 cmil/A, utilization factor K of 0.3, and ΔΒ equal to 1,500 G, we get the following fundamental core-selection criterion:

image

Note: In a typical Forward converter, it is customary to set the swing in the B-field of the transformer at Δ≈ 0.15 T. This helps reduce core loss and usually also leaves enough safety margin for avoiding hitting Bsat under say power-up condition at high line. Note that in a flyback, the core loss tends to be much less because ΔΙ is a fraction of the total current (40% typically). But since the transformer of a Forward converter is always in DCM, the swing in B is now more significant — equal to its peak value, that is, BPKΒ. So, if we set the peak field at 3,000 G, ΔΒ would be 3,000 G too, roughly twice that of a flyback set to the same peak. That is why we must reduce the peak field in a Forward converter to about 1,500 G.

Worked Example (8) — Designing the Forward Transformer

We are building a 200-kHz Forward converter for an AC input range of 90–270 V. The output is 5 Vat 50 A, and the estimated efficiency is 83%. Design its transformer.

Input Power

We have

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Selection of Core

We use the criterion calculated previously:

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The area product of the ETD-34 shown in Figure 3.7 is

image

This is, in theory, probably a little larger than required. But it is the closest standard size in this range. Later we will see it is in fact just about adequate.

Skin Depth

The skin depth is

image

where f is in Hz and T is the temperature of the windings in °C. Therefore, assuming a final temperature of T=80°C (40 °C rise over a maximum ambient temperature of 40°C), we get at 200 kHz

image

Thermal Resistance

An empirical formula for EE-EI-ETD-EC types of cores is

image

where Ve is in cm3. Therefore, since Ve=7.64 cm3, for the ETD-34

image

Maximum B-Field

For a 40 °C estimated rise in temperature, the maximum allowed dissipation is

image

Let’s divide this loss equally into copper and core losses (typical first-cut assumption). So,

image

Therefore, the allowed core loss per unit volume is

image

Using “System B” of Table 2.5, we get

image

where B is in Gauss and f in Hz. Therefore, solving for B,

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If we are using the ferrite grade “3C85” (from Ferroxcube), we see from Table 2.6 that p=2.2, d=1.8, and C=2.2×10–14. Therefore,

image

We note that the “B” referred to here is actually, by convention, BAC. So, we get the total allowed swing as

image

Voltµseconds

Earlier, we had presented the following form of the voltage-dependent equation:

image

where A is the effective area in cm2. The duty cycle of a typical Forward converter is set to about 0.35 at low line so as to meet the typical 20 ms holdup time requirement without requiring an inordinately sized input capacitor. The rectified input at low line is 90×2=127 V. The applied voltseconds is therefore (at any line voltage)

image

Number of Turns

Since ΔΒ=1,440 G, we solve the following equation for N:

image

Note that this says nothing about the required inductance. We need this number of turns irrespective of the (Primary) inductance. Yes, changing the inductance will affect the peak magnetization and the switch current because it changes the proportionality constant connecting B and I. However, B still remains fixed independent of the inductance!

Assuming a 0.6-V forward drop across the diode, the required turns ratio is

image

Therefore, the number of Secondary turns is

image

Note that this could have turned out to be significantly different from an integer. In that case, we would round it off to the nearest (higher) integer, and then recalculate the Primary turns, the new flux density swing, and the core loss — similar to what we did for the flyback. But at the moment, we can simply use

image

Secondary Foil Thickness and Losses

The concept of skin depth presented earlier actually represents a single wire standing freely in space. For simplicity, we just ignored the fact that the field from the nearby windings may be affecting the current distribution significantly. In reality, even the annular area we were hoping would be fully available for the high-frequency current, is not. Every winding has an associated field, and when this impinges on nearby windings, the charge distribution changes, and eddy currents are created (with their own fields). This is called the “proximity effect.” It can greatly increase the AC resistance and thus the copper losses in the transformer.

The first thing we need to do to improve the situation is have opposing flux lines cancel each other. In a Forward converter, that is in fact something that tends to happen automatically because the Secondary windings pass current at the same time as the Primary, and in the opposite direction. However, even that can prove totally inadequate, especially at the higher power levels that a Forward converter is more commonly associated with. So, a further reduction in these proximity losses is achieved by interleaving as shown in Figure 3.9.

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Figure 3.9: How proximity losses are reduced by interleaving.

Basically, by splitting the sections and trying to get Primary and Secondary layers adjacent to each other as much as possible, we can increase cancellation of local adjoining fields. In effect, we are trying to prevent the Ampere-turns from cumulating as we go from one layer to the next. Note that the Ampere-turns are proportional to the local fields that are causing the proximity losses. However, it is impractical to interleave too much — because we will need several more layers of Primary-to-Secondary insulation, more terminations, and also more EMI screens at every interface (if required) — all of which will add up to higher cost and eventually lead to possibly higher, rather than lower, leakage. Therefore, most medium-power off-line supplies just split the Primary into two sections, one on either side of a single-section Secondary.

The other way to reduce losses is to decrease the thickness of the conductor. But there are several ways we can do this. If, for example, we take a winding made up of single-strand wire, and split the wire into several paralleled finer strands in such a way that the overall DC resistance does not change in the process, we will find that the AC resistance goes up first before it reduces. On the other hand, if we take a foil winding, and decrease its thickness, the AC resistance falls before it rises again.

In Figure 3.9, we have also defined “p,” the layers per portion. Note how p changes when we interleave.

But how do we go about actually estimating the losses? Dowell reduced a very complex multidimensional problem into a simpler, one-dimensional one. Based on his analysis, we can show that there is an optimum thickness for each layer. Expectedly, this turns out to be much less than 2×δ, where δ is the skin depth defined earlier.

Note: In the flyback, we had ignored the proximity effect for the sake of simplicity. But in any case, since the Primary and Secondary windings do not conduct at the same time, interleaving won’t help. But interleaving is still carried out in the flyback in a manner similar to the Forward converter. However, the purpose then is to increase coupling between Primary and Secondary, and thereby reduce the leakage inductance. However, this also increases the capacitive coupling — unless grounded screens are placed at the Primary–Secondary interface. Screens are in general helpful in reducing high-frequency noise from coupling into the output and suppressing common-mode-conducted EMI. But they also increase the leakage inductance, which is of great concern particularly in the flyback. Note also that screens must be very thin, or they will develop very high eddy current losses of their own. Further, the ends of an internal screen should not be connected together, or they will constitute a shorted turn in the transformer.

In Figure 3.10, we have plotted out Dowell’s equations in a form applicable to a square current waveform (unidirectional) in a transformer with foil windings. Note that the original Dowell curves actually plot FR versus X. But we have plotted FR/X versus X, where

image

and

image

h being the thickness of the foil. The reason why we have not plotted FR versus X is that FR is only the ratio of the AC-to-DC resistance. It is not FR, but RAC that we are really interested in minimizing. So, the “optimum RAC” point need not necessarily be the point of the lowest FR.

image

Figure 3.10: Finding the lowest AC resistance, as the thickness of a foil is varied.

Let us try to understand this for a stand-alone foil (similar to what we did in Figure 3.3). If we slowly increase the thickness of the foil, once the foil thickness exceeds 2δ, the AC resistance won’t change any further, since the cross-sectional area available for the high-frequency current remains confined to δ on each side of the foil. But the DC resistance continues to decrease as per 1/h — and as a result FR will increase. So, the relationship between RAC and FR is not necessarily obvious. Therefore, since FR=RAC/RDC, with RDC∝1/h, we get RACFR/h. And this is what we really need to minimize (for a foil). Further, since we always like to write any frequency-dependent dimension with reference to the skin depth, we have plotted FR/X versus X in Figure 3.10.

Note that in Figure 3.10, the p=1 and p=0.5 curves do not really have an “optimum.” For these, the FR/X (AC resistance) can be made even smaller as we increase X (thickness). FR will in fact become much greater than 1. However, we see that for p=1, for example, no significant reduction in AC resistance occurs if X exceeds about 2, that is, thickness of foil equal to twice the skin depth. We can make it thicker if we want, but only for marginal improvement in the Secondary-winding losses. Further, in the process, we may also take away available area for the Primary windings (and any other Secondary windings), and that can lead to higher overall losses. Though we are also cautioned not to fill up all “available space” with copper, especially when we come to (round) wire windings. That can be shown, not only to increase FR, but RAC too.

Now let us apply what we have learned to our ongoing numerical example. We start by taking a copper foil wound twice on the ETD-34 bobbin — to form the 5-V Secondary winding. Since this is interleaved with respect to the Primary, only one turn “belongs” to each split section. So, the layers per portion for the Secondary is p=1. We will calculate the losses, and if acceptable, we will stay with the resulting arrangement.

We can start with a reasonable current density (about 400 cmils/A should suffice here). We use

image

where h is the foil thickness in mm, IO is the load current (50 A in our example), and “width” is the width available for the copper strip (20.9 mm for the ETD-34).

Alternatively, we can directly consult Figure 3.10 and pick an X of 2.5 for an estimated FR/X of 1.4. Thus,

image

The mean length per turn (“MLT”) of ETD-34 is 61.26 mm (see Figure 3.7), the (“hot”) resistivity of copper (“ρ”) is 2.3×10–5 Ω-mm, so we get the resistance of the Secondary winding in ohms as

image

Note that since FR/X is set to 1.4, the corresponding FR is

image

This is fairly high, but as explained, it is actually helpful here, because RAC goes down. Now, the current in the Secondary looks like a typical switch waveform, with its center equal to the load current (50 A), and a certain current ripple ratio set by the output choke. Its root mean square (RMS) value is

image

However, we do not yet know what the current ripple ratio of the choke r is at 90 VAC. The r has probably been set to 0.4 at VINMAX, not at VINMIN. Nevertheless, it is easy to work out the new r as follows. The duty cycle is inversely proportional to input voltage. Therefore, if D is 0.35 at 270 VAC, then at 90 VAC it is 0.35/3=0.117. Further, r varies as per (1−D) for a Buck stage. Therefore, the value of r at 90 VAC is

image

So, the RMS current in the Secondary winding is

image

The heat dissipated in the Secondary windings is finally

image

If the losses are not acceptable, we may need to look for a bobbin that will allow a wider width of foil. Or we can consider paralleling several thinner foils to increase p. For example, if we take four paralleled (thinner) foils in parallel (each insulated from the others), we will get four effective layers for the Secondary, and the layers per portion will then become two.

Primary Winding and Losses

For the Secondary, we have finally chosen copper foil of thickness 0.4625 mm (i.e., 0.4625×39.37=18 mil). Let us assume each foil is covered on both sides by a 2-mil thick Mylar® tape. Since 1 mil is 0.0254 mm, we have effectively added 4×0.0254 mm to the foil thickness. In addition, there will be three layers of 2-mil tape between each of the two Primary–Secondary boundaries (a total of 12 mil). So, in all, the thickness occupied by the Secondary and the insulation, hS, is

image

or

image

So, in our case,

image

The ETD-34 has an available height inside the bobbin of 6.1 mm. That now leaves 6.1−1.434=4.67 mm. Therefore, each section of the split Primary has an available winding height of 2.3 mm only. We should ultimately check that we can accommodate the Primary winding we decide on, within this space.

Note that for the Primary, the available width is only 12.9 mm (since there is 4-mm margin tape on each side — for the Secondary, since we have a foil with tape wrapped over it, we do not need margin tape). We need to find how best to accommodate eight turns into this available area with minimum losses.

Note: It is not mandatory to use a particular thickness of insulating tape, provided it is safety approved to withstand a specified voltage. We can, for example, use 1-mil approved tape or even ½-mil approved tape (if it suits our production, helps lower the cost, and/or improves performance in some way).

Let us now understand the basic concept behind winding wires. For a standalone wire, as in Figure 3.3, as we increase the diameter of the wire, the cross-sectional area available for the high-frequency current is (π×dδ. And since resistance is inversely proportional to cross-sectional area, we get RAC∝1/d. Similarly, RDC∝1/d2. So, FRd. Therefore, RAC∝1/FR. This actually means that a higher FR (bigger diameter) will decrease the AC resistance! That is not surprising because the annulus available for the high-frequency current does increase if the diameter increases. However, this is not the way to go when dealing with “non-standalone” wire. Because, by increasing the diameter, we will inevitably move to higher number of layers, and Dowell’s equation then tells us that the losses will increase significantly on account of that alone, not decrease.

On the top left side of Figure 3.11, we have Dowell’s original curves, which show how FR varies with respect to X (i.e., h/δ). The parameter for each curve is layers per portion (i.e., p). Note that Dowell’s curves talk in terms of equivalent foils (layers of current) only. They don’t care about the actual number of turns in the Primary or Secondary (i.e., from the electrical point of view), but only about the effective layers per portion (from the field point of view). So, when we consider a layer of round wires of diameter “d,” we need to convert this into an equivalent foil. Looking back at the right side of Figure 3.8, we see that this amounts to replacing a wire of diameter d with a foil slightly thinner (i.e., with the same amount of copper, but in a square shape). Alternatively, if we want to get a foil of X=4 for example, we need to start with a wire of diameter 1/0.886=1.13 times X. Finally, as indicated, all these copper squares then merge (from the field point of view) to give an equivalent layer of foil.

image

Figure 3.11: Understanding the process of “subdivision” — keeping the DC resistance unchanged and how the equivalent foil transformation process takes place.

In Figure 3.11, we are also conducting a certain strategy — as an alternative way of laying out wires optimally. Suppose we have several round wires laid out side by side with a diameter 1.13×4δ. Suppose also, that this constitutes one layer per portion in a certain winding arrangement. This is therefore equivalent to a single-layer foil of thickness 4δ, that is, X=4. Now using Dowell’s curves, the corresponding FR is about 4 (points marked “A” in Figure 3.11). Suppose we then divide each strand into four strands, where each strand has a diameter half the original. Therefore, the cross-sectional area occupied by copper remains the same because

image

However, the equivalent foil thickness is now half of what it was — 2δ (i.e., X=2). And we also now have two layers per portion from Dowell’s standpoint. Consulting Dowell’s curves, we get an FR of about 5 now (marked “B”). Since we are keeping RDC fixed this subdivision strategy, RACFR. Therefore now, decreasing FR is a sure way to go to decrease RAC. So an FR of 5 is decidedly worse than an FR of 4 (not so for an actual foil winding). We now go ahead and subdivide once more in a similar manner. So, we then get four layers per portion, each with X=1, and FR has gone down to about 2.6 (points marked “C”). We subdivide once more, and we get eight layers per portion, with X=0.5. This gives us an FR of about 1.5 (marked “D”). This is an acceptable value for FR.

Note that all these steps have been collected and plotted out in Figure 3.11 on the right side, with the horizontal axis being the number of successive subdivision steps (in each step we subdivided each wire into four of the same DC resistance). These steps are being called “sub” (for subdivision step), where sub goes from 0 (no subdivision) to 1 (one subdivision), 2 (two subdivisions), and so on. We then also realize that with each step, X and p change as per

image

For example, after four subdivision steps, the foil thickness will drop by a factor of 16, and the number of layers will increase by the same factor. We can then look at Dowell’s curves to find out the new FR.

However, there are a few problems with directly applying Dowell’s curves to switching power regulators. For one, the original curves only talked about the ratio of the thickness to the skin depth — and we know skin depth depends on frequency. So, implicitly, Dowell’s curves provide the FR for a sine wave. Further, Dowell’s curves do not assume the current has any DC value. So, engineers, who adapted Dowell’s curves to power conversion, would usually first break up the current waveform into its AC and DC components, apply the FR obtained from the curves to the AC component only, compute the DC loss separately (with FR=1), and then sum as follows:

image

However, in our case, we have preferred to follow the more recent approach of using the actual (unidirectional) current waveform, splitting it into Fourier components, and summing to get the effective FR. The losses are expressed in terms of the thickness of the foil as compared to the δ at the fundamental frequency (first harmonic). We also include the DC component in computing this effective FR. That is the reason when calculating the Secondary-winding losses, that we were able to use the simple equation:

image

In that case, the FR was actually the effective FR (computed for a square wave with DC level included), though not explicitly stated. However, note that the graphs in Figure 3.11 are still based on the original sine-wave approach, and the purpose there was only to demonstrate the subdivision technique through the original curves.

In Figure 3.12, we have modified Dowell’s original sine-wave curves. Fourier analysis has been carried out while constructing these curves, and so the designer can apply them directly to the typical (unidirectional) current waveforms of power conversion. We will shortly use these curves to do the calculations for the Primary winding of our ongoing numerical example.

image

Figure 3.12: Dowell’s curves modified for square current waveforms and the corresponding FR curves for the subdivision method.

But one question may be puzzling the reader — why are we not using the previous FR/X curves (see Figure 3.10) that we used for the Secondary? The reason is the situation is different now. The curves in Figure 3.10 were also Dowell’s curves interpreted for a square wave, except that on the vertical axis we used FR/X, not FR. That is useful only when we are varying h and seeing when we get the lowest RAC, as for a Secondary foil winding. But for the Primary (round wire) windings, we are going to fix the height of the windings in each step of the iterations that follow. We will be using the subdivision technique in each iteration, and therefore we keep the DC resistance constant. So, now the minimum RAC (for a given iteration step) will be achieved at the minimum FR, not at the minimum FR/X.

The subdivision method was presented in Figure 3.11, but now we will use the modified curves in Figure 3.12.

First Iteration

Let us plan to try to fit eight turns on one layer. Lesser number of layers will usually be better. We remember that we have 12.9 mm available width on the bobbin. So, if we stack eight turns side by side (no gap between them), we will require each of these eight round wires to have a diameter of

image

We can check that the available height of 2.3 mm is big enough to accommodate this diameter of wire. The penetration ratio X is (using the equivalent foil transformation)

image

The p is equal to 1. From either of the graphs in Figure 3.12, we can see that the FR will be about 10 in this case (marked “A”). Further, from the graph on the right side, we can see that we need to subdivide the “X=7.7” curve (imagine it close to the X=8 curve) seven times to get the FR below 2. That would give strands of diameter

image

The corresponding AWG can be calculated by rounding off

image

So, we get

image

But this is an extremely thin wire and may not even be available! Generally, from a production standpoint, we should not use anything thinner than 45 AWG (0.046 mm).

Second Iteration

The problem with the first iteration is that we started with a very thick wire, with a very high FR. So, this demanded several subdivisions to get the FR to fall below 2. But what if we start off with a wire of diameter lesser than 1.6125 mm? We would then need to introduce some wire-to-wire spacing so that we can spread the eight turns evenly across the bobbin. However, that would be wasteful! We should remember that if a layer is already assigned and present, we might as well use it to our full advantage to lower the DC resistance — the problem only starts when we indiscriminately increase the number of layers. Therefore, in our case, let us try paralleling two thinner wires to make up the Primary. We still want to keep to one layer (without spacing). That means we will now have 16 wires placed side by side in one layer. We now define a “bundle” as the number of wires paralleled to make the Primary winding (we will be subdividing each of these further). So, in our case,

image

The diameter we are starting off with is

image

The penetration ratio X is

image

The p is still equal to 1. From both the graphs in Figure 3.12, we can see that the FR will be about 5.3 in this case (marked “B”). Further, from the graph on the right side, we can see that we need to subdivide five times to get the FR below 2. That would give strands of diameter

image

This is still thinner than the practical AWG limit of 0.046 mm.

Third Iteration

So, we now parallel three wires to make up the Primary. That means we will have 24 wires side by side in one layer.

image

The diameter we are starting off with is

image

The penetration ratio X is

image

The p is still equal to 1. From both the graphs in Figure 3.12, we can see that the FR will be about 3.7 in this case (marked “C”). Further, from the graph on the right side, we can see that we need to subdivide four times to get the FR below 2. That would give strands of diameter

image

But this is still too thin!

Fourth Iteration

Let us now parallel four wires to start with. We will have 32 wires in one layer.

image

The diameter we are starting off with is

image

The penetration ratio X is

image

The p is still equal to 1. From both the graphs in Figure 3.12, we can see that the FR will be about 2.8 in this case (marked “D”). Further, from the graph on the right side, we can see that we need to subdivide three times to get the FR below 2. That would give strands of diameter

image

This corresponds to AWG 44 and would be of acceptable thickness.

Note that by the process of subdivision, the number of layers per portion goes up as

image

So, with three subdivisions, we will get

image

that is, eight layers. The penetration ratio has similarly now become

image

The FR is now about 1.8 as can also be confirmed from the graph on the left side of Figure 3.12 (for X=0.241, p=8). This is point “E” in the two graphs.

The number of strands each original “bundle” has been divided into is

image

So, finally, the Primary winding consists of four bundles in parallel, each bundle consisting of 64 strands, side by side in one layer, with an FR of about 1.8.

We can continue the process if we want to get a slightly lower FR. But at some point, we will find the FR will start to go up again. For our purpose, we will take an FR less than 2 as acceptable to proceed with the loss estimates.

Note that further tweaking will always be required since when we bunch wires together to form a bundle, they will “stack” in a certain manner that will affect the dimensions from what we have assumed. Further, the diameter of the wire we used was for bare wire and was slightly less than the coated diameter. Note that in general, if after winding several layers evenly, we are left with a few turns that seem to need another layer to complete, we are better off reducing the Primary number of turns and sticking to the existing completed layers, because even a few turns extra will count as a new layer from the field point of view and increase proximity losses.

We can now calculate the losses for the two Primary sections combined, since they can be considered to be identical and with the same FR. The AC resistance in ohms of the entire Primary winding is

image

So, the loss is

image

Had we gone further and divided the Primary into five bundles and then subdivided three times, we would get eight layers with 64 strands of 0.04-mm diameter wire per bundle and an FR of 1.65 — which seems better than the 1.8 we got in the last step. But since the wires are so thin to start with, the DC resistance now goes up, and the dissipation will rise to 1.26 W.

Total Transformer Losses

The total dissipation in the transformer is therefore

image

The estimated temperature rise

image

What we are seeing is a typical practical situation! The temperature rise is 15°C higher than we were expecting! However, 55°C is perhaps still acceptable (even from the standpoint of getting safety approvals without special transformer materials). Admittedly, there is room for more optimization. However, the next time we do the process, we must note that the core loss is only a third the total loss, not half, as we had initially assumed.

Note also that calculations in related literature may predict a smaller temperature rise. But the fact is that these are usually based on the sine-wave versions of Dowell’s equations, and we know that will typically underestimate the losses significantly.

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