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By Andrew Levido
Power
Electronics
Part 3: Isolated DC-DC Converters
Isolated DC-DC converters offer both improved safety and flexibility compared to the
non-isolated kind. To design an isolated converter, first we need to understand how
transformers work, plus their potential roles in DC/DC and AC/DC converters. This
article will start with transformer/inductor fundamentals, then move on to using them.
T
Fig.1: this shows the relationships
between the key magnetic quantities: field intensity, flux and flux linkage.
Together, these allow us to determine the inductance of the coil.
The left side of Fig.1 shows a winding of several turns of wire around a
magnetically permeable core (we’ll
consider what that means soon). The
N-turn winding carries a current i,
which induces some kind of magnetic flux (or field in some textbooks)
denoted by the Greek capital phi (Ø),
shown in red. The core itself has a
cross sectional area A and an average
length l.
By convention, the direction of the
flux follows the ‘right-hand rule’ illustrated at the bottom left of the figure.
If you curl the fingers of your right
hand in the direction of current flow,
the resulting flux points in the direction of your thumb.
Gauss’ law for magnetism tells us
that the net flux entering and leaving
any closed region is zero, which means
that flux lines have no beginning or
end – they must always be closed
loops. For us, this just means that all
of the flux leaving the coil at the top
enters it again at the bottom. For now,
we will assume that all of the flux is
confined to the core.
You can think of this arrangement
in two ways at the same time; as loops
of current enclosing a flux, or as loops
of flux enclosing a current.
Flux is driven around the core by a
‘driving force’ known as the magnetomotive force (mmf) that describes
the amount of current linking with
the flux. This mmf is N times the current i, since the current passes through
the flux loop once for each turn of the
winding.
We can also describe this magnetising force as a magnetic field intensity, which we denote with the letter
H. This is defined by Ampère’s law to
be equal to Ni ÷ l, or the mmf per unit
length of core.
The right-hand side of the figure
shows a section of the core with the
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he DC-DC converters we have looked
at so far have been non-isolated types.
That means there is a direct electrical connection between the input
and output. In many cases, we want
the output to be isolated from the
input; for safety reasons, if the input
is connected to the mains, or because
we need the output to be referenced
to a different potential than the input.
Isolation is usually achieved using
a transformer. Adding a transformer
to a switching converter can provide
a host of other benefits – for example,
it can reduce the range of duty cycle
(and consequent component stress)
required to achieve high step-up or
step-down ratios. It can also allow us
to get multiple outputs from a single
converter.
As we have seen in this series so far,
we cannot get very far in the field of
power electronics before coming up
against magnetic components such
as inductors and transformers. Like
everything else, it is the second-order
non-ideal behaviour of these components that will catch us out if we are
not careful.
Transformers, in particular, are
highly specific to the application, so
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sooner or later we will have to roll our
own. This means that a solid understanding of magnetics theory is necessary before we get to isolated DC-DC
converters, so let’s dive in.
Back to basics
One of the reasons magnetics can
be confusing is the number of terms
that sound similar but have different
meanings. This comes about because
magnetics was one of the earliest areas
of electrical engineering to be studied
by the likes of Gauss, Ampère and Faraday, who each invented their own
terms, which we live with to this day.
With terms like magnetic field intensity, magnetic flux, magnetic flux density, magnetic flux linkage, magnetic
permeability and magnetic permeance, it is no wonder many of us get
confused. Don’t even get me started
on Maxwell’s equations! (We covered
those in the November 2024 issue –
siliconchip.au/Article/17029).
I promise that it is not as hard to wrap
your head around as you might think.
As usual, I will not cover this topic in a
rigorous academic fashion, but from the
perspective of a working engineer. We
will employ just a little basic algebra.
flux lines passing through it. As we
have seen, the magnetic field intensity H drives a total flux Ø through
the core, equal to µHA. This results
in a flux density, B, which is simply
the amount of flux divided by the
cross-sectional area of the core.
B is also related to H by the magnetic permeability, or µ, of the core
according to the relationship B = µH.
Permeability is a measure of how ‘easily’ a given field intensity can create a
flux density in the core. Materials with
a higher permeability will develop a
higher flux density for a given field
intensity.
The permeability of a material is
usually expressed as the permeability
of free space, µ0 (which is equal to 4π
× 10-7H/m) multiplied by a unitless
relative permeability, µr.
The permeability of free space is
the basic measure of how much flux
a given current will produce in a vacuum or in air. The relative permeability is a measure of how many times
more permeable a material is than this
baseline. Thus, you often see permeability expressed as µ0 × µr.
Relative permeabilities for magnetic
materials range from a few hundred for
mild steel, to 5000-10,000 for transformer steel, up to 40,000 or more for
some ferrites.
In addition to the flux and the flux
density, we need to introduce the concept of flux linkage, which describes
how a flux links with a winding. From
Fig.1, you should be able to see that the
red flux lines pass through each turn
of the winding, giving it a flux linkage
λ = NØ (λ is the Greek letter lambda).
So, to sum up, the current flowing
in a winding produces a magnetic field
intensity, which drives a flux around
the core. This produces a flux density
in the core that is related to the field
intensity by the permeability, and to
the total flux by the cross-sectional
area of the core. The resulting flux
passes through the winding, resulting
in a flux linkage, λ.
Fig.2: reducing magnetic
geometries to equivalent circuits
makes analysis much easier, since
you can use all the usual circuit
theory tricks.
magnetic field. In our example, the
magnetic flux will change proportionally to changes in the current, so it follows that a voltage is produced across
the terminals of our winding as the
current through the winding changes.
The changing coil current effectively induces a voltage in itself. This
is known formally as self-inductance,
but we usually just refer to it by the
shorter name “inductance”. Inductance kind of wraps up all of the N,
H, B, Ø, and µ malarky into a relationship between the current and the flux
linkage. In fact inductance, is defined
as the flux linkage per unit of current,
L = λ ÷ i.
For the mathematically inclined,
you can see how this works by working
out an expression for the inductance
of the arrangement in Fig.1. Combining the equations for field intensity
(H = Ni ÷ l) and flux density (B = µ0 µr
H) we get B = µ0 µr Ni ÷ l. Multiplying
by the area gives us the total flux Ø =
µ0 µr NiA ÷ l.
We can then use the formula for flux
linkage (λ = NØ) to get λ = µ0 µr N2iA ÷
l, and finally use the formula for inductance to arrive at L = N2 × µ0 µr A ÷ l.
The inductance is therefore the product of the square of the number of turns
multiplied by a term related to permeability of the core and its dimensions.
This latter term is referred to as the
permeance of the core (not to be confused with the permeability). If you
know the permeance of a core, you can
easily calculate the number of turns
required to obtain a given inductance.
Manufacturers of cores usually provide the permeance in their data sheets
as an “Al” value, in units of nanohenries per turn squared or similar.
Electric circuit model
The inverse of permeance is reluctance, which is an extremely useful
quantity we can use to build a model
of magnetic systems that is analogous
to electric circuits. In these circuits,
reluctance (denoted R) is equivalent to
resistance and the mmf (F), equal to Ni,
is equivalent to voltage. The resulting
flux (Ø) is analogous to current.
Fig.2 shows the electrical circuit
equivalent of the magnetic circuit in
Fig.1. The circuit obeys the magnetic
version of Ohm’s law, so F = ØR.
We can use all of our usual circuit
analysis techniques, so this is really
helpful to calculate inductances and
the like when faced with more complex core geometries such as that in
Fig.3. At the top, we have a classic
E-I core with a winding on the centre
leg that is wider than the outer legs.
Fig.3: analysis of an E-I core and a gapped core using the magnetic
equivalent circuit shows how easy it can be to calculate the inductance of
complex geometries.
Inductors
You might have noticed that this is a
bit circular – the current in the winding produces a flux that links with
the winding. By introducing the third
member of the magnetic holy trinity,
Mr Faraday, we can use this to understand how inductors work.
Faraday’s law states that a voltage is
induced in a winding by a changing
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The magnetic equivalent circuit is
shown to the right. It is easy to calculate the reluctance of the centre leg,
R1, and that of the two outer legs, R2,
based on the dimensions of the core
and its permeability. You can then
use what you know about resistors
in series and parallel to calculate an
equivalent reluctance and therefore
the inductance as shown in the figure.
Fig.3 also shows another common
configuration, where a very narrow air
gap is included in the magnetic circuit.
This is done to increase the stability
of the inductance and the amount of
energy that can be stored in the core.
The reluctance of the air gap is much
higher than that of the core, because
the relative permeability of air is one,
compared to many thousands for the
core. This means the inductance is
dictated by the air gap, and is largely
independent of the core material.
This can be a good thing for the stability of the inductance, since the relative permeability of most core materials changes with temperature and flux
density, as we will see below.
I won’t cover the maths, but for the
same reason, for a given flux density,
the amount of energy that can be stored
per unit volume is much higher in the
air gap than in the core.
In fact, it is common to assume that
all of the energy is stored in the gap,
and it’s not unusual to start the design
process for inductors by selecting a
core with sufficient gap volume (the
area of the core times the gap length) to
store the required energy each switching cycle.
Leakage
As usual, I have made a few simplifications in the above discussion,
and some other factors come into
play when we get into the nitty-gritty
of magnetics design. One of these is
leakage flux. In the above examples,
we assumed that all of the flux was
constrained to the core.
Fig.4 shows that this may not be
the case – some flux may leak away
from the core and pass through the
air where there is a lower reluctance
path; however, it will always return,
due to Gauss’ law.
The effect of this on the magnetic
circuit is shown in the right-hand side
of the figure. The leakage paths form
a leakage (generally high) reluctance,
which appears in parallel with the
core reluctance. You can see from the
formula that this leakage will result in
a slightly increased inductance over
the ideal case.
It will be useful later to think of the
leakage producing an extra ‘leakage
inductance’ in series with the main
core inductance, as shown in the lower
equation.
Saturation, hysteresis and
residual flux
We have also assumed up until now
that the relationship between field
intensity and flux density is linear,
described by a simple proportional relationship of permeability. The reality (as
always) is a little more complex. A typical magnetic material has a B-H characteristic like that in Fig.5, although it
is shown a bit exaggerated for clarity.
Remember that H is the magnetising
‘drive’, proportional to the winding
current, and B is the resulting flux density. There are three important things
to note. First, the path that B follows
when H is increasing is not the same
as it does when H is decreasing; there
is hysteresis.
Second, neither path passes through
the origin. When H is zero, there will
be some residual flux density Bres
(either positive or negative) present
in the material when it is not excited.
Thirdly, the slope of the characteristic (the permeability) saturates at some
flux density, Bsat – it deviates from the
ideal value of µ shown in red as the
field intensity increases.
We normally want to avoid saturation (although there are some notable exceptions where this characteristic is used to advantage), so we take
some care to ensure the maximum
flux density stays well below the saturation level.
Losses
We have also so far assumed inductors are lossless, but of course, we
know this cannot be the case. Losses
in magnetic components fall into two
categories: copper losses (sometimes
called winding losses) and core losses.
Copper losses include the familiar
ohmic loss determined by the resistivity of the winding material, its cross
sectional area and its length.
Be aware that the resistivity of copper, the most common winding material, is temperature-dependent and
increases by approximately 40% for
every 100°C temperature rise. Make
sure to calculate losses using the resistivity at the highest operating temperature you will see in the winding.
Resistive losses are exacerbated by
a phenomenon known as ‘skin effect’.
As the frequency of a current passing
through a conductor increases, eddy
currents create magnetic fields inside
the conductor that force the current
outward, so it flows only in the outside ‘skin’ of the conductor. The higher
the frequency, the more the current is
forced to the outside of the conductor.
The ‘skin depth’ is a measure of
how much of the conductor is effectively useful.
For copper, the skin depth is about
9.2mm at 50Hz, which explains why
high-current AC busbars tend to be
broad but are rarely more than 10mm
thick. At 100kHz, the skin depth is
about 0.2mm, and at 1MHz, it is just
Fig.4: flux leakage in an inductor produces an extra leakage reluctance in
parallel with the core’s reluctance, and increases the total inductance slightly.
Fig.5: magnetic materials have a less-than-ideal B-H characteristic that includes
hysteresis, saturation and residual flux density.
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65µm. There is no point in using a
cylindrical conductor with a diameter greater than twice the skin depth,
since there will be no corresponding
reduction in resistance.
At 100kHz, for example, any conductor with a diameter larger than
0.4mm will be a waste of copper.
For this reason, the magnetics in
high-power switching converters use
multiple thin conductors in parallel,
or are wound with copper foil (or even
multiple parallel layers of copper foil).
You can also use Litz wire, which is an
intricate arrangement of fine insulated
wires twisted together into bundles,
which are themselves twisted together.
It is lovely stuff, but expensive.
Core losses also come from two
sources: eddy currents and hysteresis.
Eddy current losses are resistive losses
caused by currents circulating within
the core material. In conductive core
materials like steel, these losses are
mitigated by making the core from thin
laminations that are insulated from
each other by an oxide layer.
You will have seen these laminations in the cores of E-I type mains
transformers. Toroidal mains transformer cores are wound from a long
thin strip of steel (like a roll of sticky
tape) to achieve the same end. At
higher frequencies, we tend to use
cores made of materials that have poor
electrical conductivity, such as ferrite
or sintered metal oxides, to avoid eddy
current losses.
Hysteresis loss is caused by the
shape of the B-H curve. When the
material is magnetised in one direction, it takes some magnetic force in
the other direction to overcome the
residual flux and bring the flux density
back to zero. This takes energy, which
becomes heat in the core.
The amount of loss is proportional
to the area within the hysteresis loop,
so choosing a material with a narrower
Fig.7: a realistic
transformer has
leakage inductances
due to imperfect
coupling of the flux,
and a magnetising
inductance due to the
finite permeability of
the core.
hysteresis curve will help minimise
these losses, as will limiting the maximum flux density excursions.
Manufacturers usually provide a
measure of core losses for their materials in kW per cubic metre for a (usually pretty small) range of frequencies
and flux densities in the data sheets.
You have to multiply these by the core
volume to get an estimate of core loss
in your application.
Transformers
Adding a second winding to our
inductor, as shown in Fig.6, produces
a transformer. If the flux is perfectly
linked by both windings, as shown
here, the transformer is said to be
perfectly coupled. While we are at it,
let us also assume that the core is so
permeable that the reluctance is zero.
This is, after all, an ideal transformer.
Since the flux linked by each turn
on both windings is identical, so is
the voltage produced across each turn.
Each winding voltage is therefore proportional to the number of turns in that
winding. The ratio of voltages v1 : v2 is
equal to the turns ratio, N1:N2.
Due to the sense of the windings in
the diagram and the right-hand rule,
the total mmf is the sum of the Ni values of each winding. If current flows
into the dotted ends of either winding,
it produces a clockwise flux as shown.
I have indicated the direction of flux
for a current into the dotted terminal
by a red arrow on the electrical equivalent circuit on the right.
Fig.6: adding a second winding to a core produces a transformer. The currents
in the windings oppose each other, reducing the flux to almost zero.
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The magnetic circuit shows that
even though the two mmfs are pushing flux around the core in the same
direction, when one is excited, the
other will see an mmf of the opposite
polarity. The mmf seen at F2 due to a
positive F1 will be negative and vice
versa. This means that a current entering the dotted terminal of one winding
will force a current out of the dotted
terminal on the other winding.
If the reluctance is zero, the mmfs
will be equal in magnitude as well as
opposite in sign. In other words, the
ratio of transformer currents i1 : i2 is
equal to -N2:N1. Don’t get too worried about the negative sign here; it
is just there because convention says
positive current flows into the dotted
terminal.
In an ideal transformer, then, perfect flux linkage means the voltages
are related by the turns ratio (v1 : v2 =
N1:N2), and zero reluctance means the
currents are related by the inverse of
the turns ratio (i1 : i2 = N2:N1). The net
flux in the core must be zero since the
input and output mmfs cancel out as
they are identical but opposite in sign.
The impedance looking into one
winding with the other open will be
infinite (it will look like an open circuit), and when the other is short-
circuited, it will be zero.
A transformer model
While ideal transformers are handy
for circuit analysis, they are not realistic. We can summarise these non-
idealities in the equivalent circuit of
Fig.7. There is an ideal transformer in
the centre of the diagram. The inductances in series with each side are leakage inductances caused by incomplete
coupling of the flux, as we saw in Fig.4.
I have shown a leakage inductance
on either side of the transformer, but
it is also sometimes handy to have it
all ‘lumped’ onto one side or the other.
For example, if we wanted to show
Ll 2 on the same side as Ll 1, we would
shift it over but multiply its value by
(N1÷N2)2. We could equally move Ll 1
January 2026 29
to the same side as Ll 2 by multiplying
its value by (N2÷N1)2.
Since any real transformer core has
a finite reluctance, the opposing mmfs
of each winding will not completely
cancel out, and there will be some
level of residual flux in the core. This
is represented by the parallel inductance known as the magnetising inductance. This is responsible for the small
current that will flow in a transformer’s
primary winding when its secondary
is open circuit.
There are also copper losses and
core losses in transformers, driven by
the same mechanisms as discussed
above for inductors. The copper losses
can be represented by appropriate
resistances in series with the leakage
inductances, and the core losses by a
resistor in parallel with the magnetising inductor. I have not bothered to
show them here to keep things simple.
The forward converter
Knowing what we do about magnetics, we can begin to understand isolated DC-DC converters. In the upperleft corner of Fig.8 is a non-isolated
buck converter that we are by now very
familiar with. To its right is an isolated
version of the same topology, known
as a single-ended forward converter.
An ideal (for now) transformer with
a turns ratio of N:1 has been inserted
pretty much in the middle of the buck
converter’s switch Q1, which now consists of a Mosfet (Q1) on the primary
side and diode (D2) on the secondary side.
When Q1 is on, current flows into
the dotted primary terminal of the
transformer. A current, scaled by a
factor of N, emerges from the dotted secondary terminal and passes
through D2, forming the second half
of the switch feeding the filter inductor. When Q1 and D2 are off, the filter inductor current flows via diode
D1, just as it does in the non-isolated
converter.
The transfer function of the forward
converter is the same as the buck converter, but scaled by the transformer
turns ratio, N. I have drawn the forward converter with the Mosfet in the
positive input line to match the buck
converter, but in reality, it is typically
moved to the ‘ground’ side of the transformer primary to make its gate drive
simpler, as shown in the circuit at
lower left in Fig.8.
In this circuit, I have also added the
magnetising inductance to the transformer, and a clamp circuit consisting
of diode D3 and zener diode ZD1. You
can probably already see why these
are necessary. We don’t need to worry
about the leakage inductances, as they
are in series with the ideal transformer,
so there is always a path for their current to flow.
They will affect voltage regulation a
bit, but we won’t worry about that now.
This is a ‘single-ended’ converter
because power flows through the
transformer only during the part of
the cycle when Q1 is conducting. This
means that when the Mosfet switches
off, the magnetising current needs a
path to flow or else the Mosfet’s drain
terminal voltage will spike and it will
be toast.
The clamp circuit limits the Mosfet
drain voltage to the sum of Vin plus the
zener voltage. The energy stored in the
magnetising inductance is dissipated
in the clamp every cycle.
The price we pay for the convenience of the transformer is the additional complexity and power dissipation of a clamping circuit, and
the additional voltage stress on the
switch. There are several other ways
to implement the clamping circuit,
two of which are shown at lower right
in Fig.8.
The first, a resistor-capacitor-diode
(RCD) clamp, relies on a capacitor to
absorb the energy, which is then dissipated in the parallel resistor. This is
probably the cheapest option and is
often seen in low-cost designs.
A more efficient option is to add
an extra winding to the transformer
and a diode, as shown in the energy
recovery clamp partial circuit. When
the Mosfet switches off, the magnetising current causes the transformer terminal voltage to rise until the clamp
diode conducts.
If the clamp winding had the same
number of turns as the primary,
the Mosfet drain voltage would be
Fig.8: the single-ended forward converter is essentially a buck converter with Q1 replaced by a Mosfet, transformer and
diode. The transformer’s magnetising inductance requires the addition of a clamp circuit, as shown along the bottom of
the figure.
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clamped to twice Vin. You can choose
the number of turns on the clamp
winding to limit the drain voltage
even further if necessary. As the name
implies, the advantage here is that the
magnetising energy is returned to the
supply.
Another similar variant of the
single-
ended forward converter, the
isolated hybrid bridge converter, is
shown in Fig.9. It is still a single-ended
converter, because the Mosfets can
only drive flux through the transformer
in one direction, but it solves the magnetisation current problem by clamping both ends of the windings to the
supply rails when the Mosfets are off.
The Mosfets are never subject to
more voltage stress than the supply
rails, but the gate drive for the upper
Mosfet is more complex in this configuration.
Double-ended forward
converters
An obvious(?) next step would be
to replace the diodes in the hybrid
bridge converter with Mosfets to produce a full-bridge converter. This has
the huge advantage of driving flux in
both directions in the transformer and
allowing us to use a full-bridge rectifier on the secondary side.
The single-ended converter can only
drive the magnetising flux around
the transformer core in one direction
(remember, the magnetising flux is
what’s left in the core after most of the
Fig.9: the isolated hybrid bridge converter solves the problem of magnetising
inductance at the cost of circuit complexity.
flux is cancelled out).
In a double-ended converter such as
this one, the magnetising current can
change sign. We can therefore utilise
the full range of flux density in the core
material, making for a more efficient
and smaller transformer.
Being able to use a full-bridge rectifier means we can use a smaller filter inductor, since the frequency at
the output of the rectifier is twice the
switching frequency. This type of converter does require that we take care
to limit the duty cycle of each phase
to less than 50%, or we run the risk
of switching on the upper and lower
Mosfets at the same time, with catastrophic results.
The price to pay for such advantages
is complexity. There are now two highside and two low-side Mosfets to drive,
and four output diodes. Moreover, the
arrangement means that two of these
Mosfets and two diodes are in series
each cycle, so the efficiency is less than
ideal. If only we could get the advantages of the double-ended converter
without these disadvantages!
Well, you can, by using a more complex transformer, as shown at the bottom of Fig.10.
This is the transformer-coupled
half-bridge or push-pull topology,
and it has all the advantages of the
full bridge, but is considerably simpler. There are only two switches, and
both are ground-referenced. Only two
diodes are required, and the output
current only ever passes through one
of them. Nice.
The flyback converter
Next, I want to cover the flyback
topology, which is an isolated topology derived from the boost converter
(Fig.11). This time, we split the circuit
in the middle of the inductor, creating
two coupled sections. It looks a lot like
a transformer, but strictly speaking,
does not behave that way.
Fig.10: double-ended converters can drive flux through the transformer core in both directions, increasing the efficiency of
the magnetics.
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Fig.11: the flyback converter is derived from the
boost topology. The ‘transformer’ is actually two
coupled inductors – the windings never conduct at
the same time.
When Q1 is on, current flows into
the dotted primary terminal of the
‘transformer’. True transformer action
would require it to emerge from the
secondary’s dotted terminal, but it cannot, because it is blocked by the diode
(D1). The secondary winding is effectively open circuit, so the ‘transformer’
acts like an inductor, building up flux
and storing up energy in the core.
When the Mosfet switches off, the
primary winding is open-circuited and
the magnetic field begins to collapse,
reversing the voltage on both windings
and allowing D1 to conduct.
Now that the primary winding is
open-circuit, the flyback transformer
secondary acts like an inductor and the
current ramps down, just as it does in
the boost converter. The only difference is that the turns ratio means the
secondary current is scaled by a factor
N. The voltage transfer function for the
flyback converter is therefore the same
as for the boost converter, but scaled
by the turns ratio.
While the flyback circuit looks a lot
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like the forward converter, the crucial difference is in the operation of
the transformer. A forward converter
has a true transformer in that the net
flux largely cancels (except for the
magnetising flux), and no appreciable energy is stored. The output filter
inductor remains the primary energy
storage element.
In flyback converters, the ‘transformer’ is also the energy storage element. Since the two windings never
conduct simultaneously, the flux
increases significantly. Flyback transformers are really two-winding inductors and usually have gapped cores. If
you are ever unsure about what topology you have, take a look at the dots
on the transformer, and work out if
both windings can conduct at the same
time or not.
The fact that flyback converters combine the energy storage element and
the isolation element into one piece
of magnetics (and because they use
The Mornsun LM25-23B12 25W 12V
isolated power supply.
one less diode) is one of the reasons
why they are the most common topology for small mains converters. That
includes many phone chargers, plugpacks and other low-power DC-DC
converter modules below about 50W.
Flyback converter transformers do
not have the magnetising inductance
concern that single-ended forward
converters do (because they are not
really a transformer), but they do have
a problem with leakage inductance, as
shown at the bottom of Fig.11.
When the Mosfet switches off, the
energy stored in the core is delivered
to the secondary, but any that is stored
in the primary side leakage inductance
has no place to go since it is, by definition, not linked by the secondary
winding. So weirdly, it turns out that
a practical flyback converter needs a
similar type of clamp as a single-ended
forward converter, but for a different
reason altogether.
A professional design
To add a practical twist, I want to
take a close look at the design of a commercial flyback converter, because you
can learn a lot by looking at designs
by experts. The converter I chose is
a Mornsun LM25-23B12, an offline
isolated 25W switcher with a 12V DC
output. It can accept input voltages in
the range of 100V to 277V AC and can
deliver 2.1A at 50°C.
You might think this is an AC-DC
converter and not a DC-DC converter,
and by some definitions, you would
be right. Still, I will argue that, like
many mains-powered supplies, it is
an AC-DC converter followed by a
DC-DC converter.
The AC-DC side of this converter
is a simple bridge rectifier, so all the
interesting stuff is happening in the
DC-DC part. These converters are built
to a price, but they do claim to meet a
bunch of international specifications
for safety & EMC (electromagnetic emissions compliance). Looking at the construction & component choice, I don’t
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Fig.12: the reverse-engineered circuit of a commercial 25W switching converter (the Mornsun LM2523B12). The text describes some of the interesting design features.
doubt that this is a well-designed unit.
The accompanying photos show the
power supply and both sides of the
PCB. It is a single-sided board with
through-hole components on the top
side and SMT parts on the bottom.
The slots milled into the board are to
provide creepage isolation between
primary and secondary and between
high voltages.
The circuit, as best as I could reverse
engineer it, is shown in Fig.12. Starting
on the left is the mains input, with a
fuse and an inrush-limiting NTC resistor. An X2 capacitor and common-
mode inductor provide some filtering
to minimise the amount of EMI (electromagnetic interference) conducted
back onto the mains.
This filter is followed by a full-wave
bridge rectifier and three 15µF 400V
DC capacitors in parallel, to smooth
the input to the flyback converter.
The negative side of the high-voltage
DC supply is tied to mains Earth via a
2.2nF X1 capacitor, and to the output
negative rail by two 1nF X1 capacitors
in series. These capacitors provide a
path to shunt high-frequency noise to
Earth without compromising the safety
or isolation.
The power circuit looks like any flyback circuit, with one side of the transformer primary connected to the positive supply and the other to the drain
of the Mosfet switch, which is incorporated into the SDH8666Q control IC.
The Mosfet’s source is connected
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to the current sense (CS) pin, which
is connected to the negative supply
via a 0.5W shunt resistor (three parallel 1.5W resistors). This chip uses
current-mode control, and this is the
current-sense resistor.
An RCD clamp with a 120kW resistor
(two parallel 240kW resistors) and an
unmarked capacitor protects the Mosfet
from spikes caused by the transformer
leakage inductance I described above.
On the secondary side, the rectifier
consists of two SK3150AS schottky
diodes connected in parallel. These are
150V 3A diodes, and I guess two are
used in parallel since the peak current
could easily be twice the maximum
output current of 2.1A.
The diodes are followed by two parallel 470µF electrolytic filter caps. I
am a bit surprised not to see a ceramic
cap in parallel with these, given the
switching frequency is in the 65kHz
range. These caps must be working
hard from a ripple current perspective
(but presumably within their specifications).
A secondary filter comprising a
small inductor and a 47µF capacitor
helps eliminate a lot of the switching
noise on the output.
Isolated voltage feedback and control loop compensation is provided
via the circuit at lower right. This
uses a TL431 shunt reference and
opto-coupler in a clever (but common)
arrangement.
I think this circuit is worth a bit of
Australia's electronics magazine
a closer look, so I have redrawn it in
Fig.13. The converter’s output voltage is divided down and compared
to the 2.5V reference internal to the
TL431. The resulting error voltage
at the TL431’s anode is converted
to a current by Rb to drive the opto-
coupler’s LED.
A current proportional to this will
flow into the coupler phototransistor’s
collector and be converted back to an
error voltage by the pullup resistor
internal to the control chip.
Fig.13: the Mornsun voltage feedback,
error amplifier, isolation and loop
compensation circuit uses a TL431,
and opto-coupler and a handful of
passives. The compensator is a Type
II circuit, suitable for current-mode
controllers, as described last month.
January 2026 33
I calculated the circuit’s small-signal
transfer function using the complex
impedance method we covered last
month. As we would expect with a
current-mode controller, the result is
characteristic of a Type II compensator. I will spare you the maths.
The constant terms at the front
of the transfer function relate to the
opto-coupler’s current transfer ratio
(CTR), and the resistors on each side
that convert voltage to current to voltage. The interesting part is inside the
brackets.
There is a pole at the origin and
another formed by the capacitor Cb
and the pullup resistor Rpu inside the
controller. There is also a zero formed
by Ra and Ca. This zero cancels the
output capacitance/load resistance
zero, and the Cb/Rpu pole cancels the
zero formed by the output capacitor
and its ESR.
The purpose of the capacitor
directly under the opto-coupler in
Fig.12 is a bit of a mystery, but as it
measures about 22pF and is connected
at the output of the TL431’s internal
op amp, I suspect it is there for stability and plays no meaningful part in
the control loop.
The next interesting part of the flyback converter is the power supply for
the control chip. This is derived from
an auxiliary winding on the flyback
transformer via a diode and a couple
of capacitors to supply the Vcc pin of
the controller.
You may ask yourself how this circuit can possibly start, given that the
chip is powered by its own output. The
chip has a clever trick up its sleeve in
that there is an internal high-voltage
depletion-mode (normally on) Mosfet
connected to the DRAIN pin (pin 6)
that initially provides a small trickle
current to charge the 22µF capacitor
on the Vcc pin.
To keep the power dissipation in
the depletion Mosfet to a minimum,
this current is very small – nowhere
near enough to power the chip – so
the chip is not enabled until the Vcc
voltage reaches some fairly high predetermined level. At this point, the chip
switches on and uses the charge stored
in the 22µF cap to run for long enough
for the external supply to take over.
Once everything is up and running,
the depletion-mode Mosfet is switched
off to save energy.
This leaves only the DEM pin,
which is fed from the auxiliary secondary winding prior to the rectifier
diode. This pin is used to (roughly)
sense the output voltage to provide
output overvoltage protection, and
something called “valley lockout”,
which appears to be a mechanism to
prevent the chip restarting too quickly
due to small dips in the input voltage.
The DEM pin can indirectly sense
the converter’s output voltage because
the voltage on the auxiliary winding
is proportional to the output voltage
(less one diode drop) according to the
turns ratio.
I suspect that the valley lockout
works by ignoring short dips in the
input voltage (sensed at the DRAIN pin)
if the output voltage (sensed at the DEM
pin) does not also drop. This would prevent the start-up sequence described
above from happening unnecessarily
for very short mains interruptions that
don’t impact the output.
That’s it for this month. Next month,
we will have a look at AC-to-DC converters, and we will go through the
design process for a simple DC power
source in detail. We will build and test
the circuit to see how well the theory
SC
and practice align.
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Silicon Chip
Australia's electronics magazine
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