By Steven M.
Sandler, Charles E. Hymowitz, and Harold
Eicher
This page includes detailes relating to the
above entitled article published in Power Technology Magazine not
included in the article.
Please note that the MPP core and many other models are
part of the AEi
Systems Power IC Model Library for PSpice.

The design approach for an isolated flyback transformer for
PFC is almost exactly similar to doing a design for a DCM flyback. The
variation that comes into play is that for PFC Isolated flyback (hereafter “PFCIF”)
the Vdc Input and Ipk current are going to vary over ½ cycle of the AC input
waveform. To optimize the transformer therefore means to make an accurate
computation of the winding and core losses. The method used herein is to
compute the Fourier components of the voltage waveform (across the Primary) and
then compute core loss for each harmonic of the waveform. This sets up nicely
since the core loss curves or equations supplied by most core manufacturers are
for sine wave excitation. Similarly, the Fourier components of the current
waveforms for the Primary and Secondary are derived and the winding losses for
each harmonic are then computed. This sets up nicely because a formulaic
approach using skin and proximity effects can be used to accurately predict the
loss. Suffice it to say that most traditional methods for DCM do not go into
this level of detail as a 1st order approach is often satisfactory.
So…… Where to begin? Well, the power to be processed is
similar to DCM flyback. An engineer may have experience from a previous design
or can use a suitable software design package. This will produce a result that
is approximate. In the end, design equations must be written and the results
there from compared to empirical data on efficiency and temperature rise. Our
design is [1] phase of a [2] phase PFCIF – so, 100W Pout at 100 Khz ---our transformer design starts with the following
given design parameters from the topology simulation:
Our 1st goal is low cost. Another essential
goal for the design is to minimize the leakage inductance since it is DCM. This
is our 2nd goal. Our 3rd goal is<1”
height restriction. A 4th goal is smallest volume. These led to a 4th chosen
goal—that is, to compare the results with a planar device vs
a conventional wound device. Our two choices decided upon were the PQ2620 size
ferrite and a std planar ferrite size. Mechanical
details are (MM):
|
Core
|
Width
|
Length
|
Height
|
Core Area
|
Volume
|
|
PQ2620
|
19
|
27.3
|
20.2
|
1.09
|
5.47
|
|
PL58
|
20
|
25
|
11
|
0.75
|
3.2
|
The
next comparison to be made is cost (US$):
|
Core
|
1K
|
10K
|
50K
|
100K
|
1M+
|
|
PQ2620
|
2.20
|
1.35
|
.675
|
.655
|
.62
|
|
PL58
|
3.80
|
3.20
|
2.50
|
1.80
|
1.50
|
The obvious conclusion from the chart above is that
there is a premium to be paid for low profile height and smallest volume. The
other factor that is not obvious is that the PQ core finds worldwide usage
currently in existing “off-line” AC-DC power supplies. Any manufacturer in the
Asian market place active in this arena has 1 or more OEM customers they are
currently supplying in the 10M+ quantity. The planar cost is directly related
to the number of boards or layers (lead frame or pcb) required to stack to achieve the design.
Applications more amenable to planar designs usually occupy niches in telecom,
“bricks”, servers, and high current/power.
The particulars of the PQ2620 design are as follows:
20
Turn Primary
Ferrite Core Gap is ~ .072cm
Checking for <Bsat:
Flux at Peak Current:
Actual Gap is ~ .079cm ( .031”)
when accounting for fringing flux.
If specifying for core manufacturer:

RMS Flux (Gauss)
Brms = 1533 Gauss
Using Core Loss Equation for Ferroxcube
"3C96" mat'l at 40 degrees C temp rise:
Core Loss 1.18W --but this is only over 1 switching interval
at Peak Vin
Accuracy requires averaging over ½ Cycle Interval or performing
Fourier Analysis
SPICE Simulation yields Peak Primary & Secondary
Currents at 1st four Harmonics:
PEAK CURRENT of first four harmonics
Corresponding RMS Flux Value:
Now use Core Loss Equation above for each Harmonic and RMS Flux amplitude:
Total Core Loss is .44W
Now we must assess the mechanical aspects of the design and
iterate magnet wire choices with “fit” in the available bobbin window.
The winding length of the bobbin is .354 inches so fitting
the 20 turns in a single layer
Which is diameter for #26 wire
Due to practical limitations in fitting the wire and the
space taken up for the start & finish--
the part was wound with #28AWG
magnet wire.
...and the bobbin area in square inches is:

..... so that the maximum build
height is
..and the #28 AWG primary layer has
a max dia of .0127 inches. Interleaving two layers
(one under the secondary and one over the secondary consumes
.026 inch build allowing .115" for the secondary.
Choose 20x#30 Litz for the
secondary. Wind 5 Turns
Calculating the DCR and Cu Losses as follows:
Mean turn Length (inches) is:

Recorded actual
value 116
milli-
W
Recorded
actual value 4
milli-
W
..and the copper loss is
Total Loss is 1.52W
Now on to figure temperature rise
...and the approximate core surface area is (sq cm): 
.. and the temperature rise is
estimated to be

36C Temp Rise Convection Only
Nomographs from popular authors:
Tartar
36C Temp Rise
McClyman
40C Temp Rise
_____________________________________________________________________________
We now apply the same analysis to the planar design PL58
size core (in shortened format).
Center Post gap
calculated is ~ .10cm (.036”)
RMS Flux (Gauss)
Brms is 1738 Gauss
Now use Core Loss Equation for each Harmonic and RMS Flux
amplitude:
Total Core Loss is .327W
_____________________________________________________________________________
Now, moving on to calculate copper losses in the windings:
Primary DCR calculated &
recorded = 150
milli-W
Primary Copper Loss is
0.415W
_____________________________________________________________________________
Secondary Turns
Secondary DCR calculated
& recorded = 11.5
milli-Watt
Secondary Copper Loss is 0.48W
Total Loss is 1.22W
As stated
at the outset, we need to perform a Fourier analysis of the winding loss to
verify that we chose the correct wire size for the PQ2620 core. We performed a
“conventional” loss calculation for the PQ2620 and we performed a fourier loss for the planar but
only for the 1st four harmonics. In brief, we need to see the
results of choosing #28AWG wire for the PQ2620 and 4oz copper for the planar
design and see if there is relative agreement with winding loss.
The 1st step is to
compute penetration depth (cm) ---- given 100 Khz fundamental.
Dp(nn) = Penetration Depth -- in cm

A stipulated Design Goal was to
minimize leakage inductance. A corollary to that goal was to minimize AC
Resistance. We do that by what’s termed “sandwiching” Secondary -- i.e. Primary will occupy 1
layer "under" -- 1 layer "over" the Secondary.
Pri #28AWG = .00635 inches radius,
... .0127 dia
inches thk, but assume penetration [1] side of wire, i.e proximity due to no "countervailing current
flow", i.e. Flyback Inductor current flows in primary only during storage
cycle and current flows in secondary only during load dump cycle.
Therefore, conductor thickness = 0.32MM, .032 CM - .000322 meters thk
Conductor Thickness = .032 CM | Conductor Thickness = .013 inches
(rounded off)
AC Resistance Formula:
"Effective" # Layers
AC Resistance Ratio

Conductor AC Resistance Multiplier.
Now we need to generate RMS amplitudes at all the relevant
harmonics of the Primary Current Waveform and multiply each by the AC
Resistance.
(DCR multiplied by each of the AC Resistance factors in the
column above).
Compute fourier
coefficients:
Form a partial sum of coefficients and plot at t intervals
to view convergence:
Recalling the DCR value for the Primary from the above
computations for PQ2620 design:
Baseline
Pri
DCR = 120
milli-W
Primary AC Resistance for each of 1st 15 Harmonics
Pri AC Loss @
each Harmonic
Calculated Primary Cu Loss (including DC) is:
Summary Results:
|
Core
|
Conventional Cu
Loss
|
Core Loss
|
Total Loss
|
AC Loss
|
Total Loss
|
|
PQ2620
|
1.08
|
0.44
|
1.52
|
1.136
|
1.58
|
|
Planar PL58
|
-
|
0.33
|
-
|
.90
|
1.23
|