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 AN707
Vishay Siliconix
Designing Low-Power Off-Line Flyback Converters Using the Si9120 Switchmode Controller IC
Getting high efficiency from low-power off-line power supplies has always posed difficulties for the design engineer. Power hungry control circuits require either line frequency transformers for bias or bleeder circuits for start-up. The problem with the bleeder approach is that, to date, no provisions have been made in PWM ICs to turn off the bleeder; so several watts of power get consumed during normal operation -- serving no purpose but to heat the bleed resistor. While solutions are available, they all require additional parts, which increase costs and use precious circuit board real estate. The Si9120 from Siliconix was designed to address these problems. This current-mode control, pulse-width modulator IC is implemented with combined BiC/DMOS technology. All logic functions are implemented in CMOS to reduce the typical quiescent power requirements to 0.85 mA while driving a 500-pF load at 50 kHz. Included on chip is a 450-V DMOS, depletion-mode transistor configured as a linear voltage regulator to supply operating power to the chip directly from the rectified 115-V mains. The chip contains MOS capacitors for the clock circuit, so the only external timing component required is a resistor to set the operating frequency. Other features include a temperature-compensated buried Zener reference for less than 0.2 mV/_C drift; a latchable shutdown feature; and a dual current-limit comparator, which minimizes false tripping due to leading-edge current spikes. A major advantage of CMOS processing is speed--current-limit delays are typically under 100 ns while supply current is kept at less than 1 mA. This allows reliable operation up to 500 kHz. the device on, and an amplifier and voltage reference can be used to implement a linear regulator, as shown in Figure 2. The CMOS circuitry is thus protected from transients which appear on the input power bus. For some applications it is useful to turn off the pre-regulator after start-up. This is easily accomplished by using an auxiliary winding on the transformer to develop a bootstrap supply voltage. After the converter starts, its own output feeds 10 to 12 V to pin 7 (VCC), and the amplifier pulls the gate of the MOSFET to the -VIN rail. Thus, VGS = -VCC, and the device is turned off. For operation of +VIN > 250 V, a 10-kW, 1/4-W resistor should be placed in series with +VIN (Pin 1). For +VIN > 380 V, a 15-kW, 1/4-W resistor is recommended. (Reference Figure 10, R13, C22 are also required.) Oscillator A ring of inverters and internal MOS capacitors form the oscillator circuit, as shown in Figure 3. This circuit requires only a resistor (no external capacitor) to program the frequency. The internal capacitance is charged towards VCC through ROSC. When the capacitor voltage reaches VCC/2 (the CMOS logic threshold), inverter INV1 changes state (from high to low), and the INV2 output goes from a low to a high output. The capacitor, C2, provides positive feedback to ensure stable operation without frequency jitter. It also causes the "bump" at the end of the ramp until INV2 can turn on the discharge switch, Q1, to terminate the cycle. Oscillator synchronization is achieved by prematurely terminating each clock cycle using a positive going pulse capacitively coupled onto the oscillator ramp voltage. The pulse forces INV1 to change states, Q1 discharges C = C1 + C2, and the cycle repeats. An internal flip-flop blanks out the output during every other clock cycle, so the switch duty ratio is limited to a maximum of 50%. Therefore, the oscillator frequency and SYNC pulse repetition rate must be set at two times the switching frequency, fs.
FUNCTIONAL DESCRIPTION
Pre-regulator A BiC/DMOS power integrated circuit process is used to integrate a high-voltage (450-V rated) lateral DMOS transistor with the CMOS PWM controller. By using an ion implant to shift the gate threshold to a negative value, as shown in Figure 1, the transistor is made to operate as a depletion-mode device. This eliminates the need for a pull-up voltage above VCC to turn
ID
Depletion-Mode MOSFET Characteristics Enhancement-Mode MOSFET Characteristics
+VIN 10 to120 VDC Cbypass GND -VIN - +
VCC
To Internal Circuitry Cbypass
8.6 V
-VCC
Vth2
0
Vth1
VGS
FIGURE 1. Depletion-mode MOSFET Characteristics
Document Number: 70580 24-Mar-97
FIGURE 2. Pre-regulator/Start-up Circuit
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AN707
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Oscillator Waveforms Free-running VCC/2
ROSC
With External Sync VCC/2
C2 21.5 pF
To Internal Control Logic
Input Sync Pulse 3k C1 100 pF 8 Sync Pulse OSC IN INV1 21.5 pF Q1 5 9 Discharge INV2 INV3 2k 7 OSC OUT
FIGURE 3. Si9120 Oscillator Circuit Operation
Error Amplifier
VCC
Ibias
The bias resistor, connected from pin 16 (bias) to pin 6 (-VIN), programs the current sources in the analog portion of the current-mode controller -- including the error amplifier, the current-mode and current-limit comparators, and the voltage reference. The Si9120 data sheet guarantees the performance of these functions at one value of bias current--15 mA. It is possible to change the performance characteristics of these functions by changing the bias current. (See Siliconix Application Note AN703 for an explanation of how this is accomplished.)
b ' 130
100 240 Compensation (Pin 13) 10 x Ibias
-VIN
FIGURE 4. Error Amplifier Output Stage
The error amplifier circuit employs PMOS transistors in a differential input stage to achieve a high input impedance of 40 MW typically (2-MW minimum). This input impedance, combined with a 1-kW small-signal output impedance, enables the amplifier to be used with feedback compensation, unlike transconductance error amplifiers. The amplifier can source 2 mA and sink 0.140 mA, as can be seen from the output stage equivalent circuit in Figure 4. Yes, an NPN transistor is used here. Most of the PWM controller is CMOS, but the process allows the flexibility of using bipolar devices where they are advantageous.
The error amplifier is unity gain stable with a typical bandwidth of 1.4 MHz and 70_ phase margin. Bias current values from 5 mA to 50 mA have been tested, and the error amplifier does remain stable over this range. Actually, the bandwidth and phase margin increase somewhat as Ibias is increased above 15 mA. Higher bias currents may, therefore, be useful when compensating higher frequency converters (above 250 kHz).
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Document Number: 70580 24-Mar-97
AN707
Vishay Siliconix
Voltage Reference A buried Zener with merged temperature compensating diode (Patent no. 4766469) is used to achieve stability of 0.2 mV/_C. The Si9120 voltage reference is trimmed to 4 V plus or minus 2% with a bias current of 15 mA. Note that trimming is done with the error amplifier connected for unity gain, so the effect of the offset voltage is removed. The reference voltage varies by about 1% as Ibias is varied from 5 to 50 mA. If 2% reference accuracy must be guaranteed, Ibias should be set at 15 mA. Comparators The delay time of the current-limit and current-mode comparators can be modeled as a current source charging an internal nodal capacitance, as shown in Figure 5. The
current-mode comparator is intentionally made to be four times slower than the current-limit comparator. In many circuits, this permits the elimination of the RC filter in the current-sense circuit, which is used to prevent false trips by the leading edge current spike. After one of the comparator outputs goes high, there is an additional 20 ns of gate propagation delay before the output driver can begin switching. The total current-limit delay to output versus Ibias is shown in Figure 6 for VCC equal to 8.5 V. The delay time is 180 ns for Ibias = 5 mA, but decreases to 50 ns for Ibias = 30 mA. As operating frequency is increased, Ibias may be increased to speed up the current limiting and reduce the minimum MOSFET pulse width. As Ibias is increased, however, the current-limit trip voltage also increases. Figure 7 shows how the trip voltage is established and how it varies with Ibias. The current sense resistor and Ibias determine the peak value of switch current. Since this current limiting is very fast, the trip level of current is usually set to be well above the maximum normal operating current (by a factor of 1.5 to 2). This prevents false trips but still protects the MOSFET switch from exceeding its pulse current ratings.
VCC
200 180
4 x Ibias Output (To MOSFET Gate) 0.9 pF
V CC 2
160 140 t D (ns) 120 100 80 60 40 20 0 0 10 20 30 40 50 Ibias (mA)
t D ] 20 ns ) C node
(4xI bias)
+ 20 ns ) 0.9 pF 4.25 V (4xIbias) FIGURE 5. Current-limit Comparator Delay (Equivalent Circuit Model)
FIGURE 6. Current-limit Comparator Delay vs.Bias Current
2.5 VCC 2.0 Trip Voltage (V) Ibias 1.5 To Current Limit Comparator Vbe has negative temp coefficient. R has positive temp coefficient. R 36 k VCL = 0.7 V + Ibias x 36 k
1.0
0.5
0 0 10 20 Ibias (mA) 30 40 50
FIGURE 7. Current-Limit Trip Voltage vs. Programmed Bias Current
Document Number: 70580 24-Mar-97
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MOSFET Driver The driver circuit is a CMOS inverter whose typical characteristics are shown in Figure 8. The n-channel (turn-off) peak drive current is about 20% higher than that of the p-channel (turn-on) device. Although the on-resistance (rDS(on)) of the output drive is specified, usually the saturation current (where DID/DVDS is very small) determines the switching speed. This is due to the vertical load line of capacitive loads. In other words, the MOSFET gate capacitance appears as a short circuit across the driver's output. The CMOS driver is fast enough to effectively eliminate cross-conduction current during switching transitions, at least when VCC v10 V. Above this level, a small amount of cross conduction occurs. Therefore, the greatest gate drive efficiency (approaching 100%) is achieved by keeping VCC v10 V, and the gate drive power is given by
Pgate = Qg x fs x VCC
internal current-source pull-ups (equal to Ibias), so they can be left open when unused. As long as the SHUTDOWN input is held low, the output is OFF. If the RESET input is hard wired to -VIN (through a normally closed reset button if desired), any LOW input to SHUTDOWN will latch the output in the "off" state. It will remain off until power is recycled (or the reset button is pushed).
Undervoltage Lockout During start-up, the depletion transistor charges the capacitance connected to the VCC pin with a typical charging current of 15 to 20 mA. The output is disabled until VCC reaches the undervoltage (UV) lockout voltage (typically 8.1 V). The IC requires less than 0.5 mA of current during this time, since the largest component of supply current is usually for the gate drive. When VCC reaches 8.1 V, the output is enabled and the MOSFET begins switching. The supply current increases by Qg x fs, and VCC charges more slowly until it reaches the pre-regulator voltage (8.6 V).
where
Qg = MOSFET gate charge = switching frequency fs VCC = supply voltage
Shutdown Logic The shutdown logic employs an RS flip-flop to disable the output drive. Both the SHUTDOWN and RESET inputs have
If too much current is drawn from VCC (for instance, to supply other circuitry), it is possible that the converter will be prevented from starting. Or it may oscillate on and off as it starts up, loads down the VCC pin, shuts off, and then repeats this cycle. Consult the factory if a minimum pre-regulator current specification above 5 mA must be guaranteed.
ID 250 - 200 - 150 - 100 - Output -6 -5 -4 -3 -2 -1 50 - 1
N-channel (Turn-OFF Drive) VCC = 12 V 11 V 10 V 9V
VCC
2
3
4
5
6 VDS
- -50 VGS = 9 V 10 V 11 V 12 V P-channel (Turn-ON Drive) - -100 - -150 - -200
-VIN
FIGURE 8. Output Drive Characteristics
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Document Number: 70580 24-Mar-97
AN707
Vishay Siliconix
OSC IN 9 OSC OUT 8
FB 15 Error Amplifier
COMP 14
DISCHARGE 10
OSC VREF 11 - + 4V Ref Gen Clock (1/2 fOSC) 2V - + S + - 1.2 V BIAS 16 Current Sources To Internal Circuits C/L Comparator Current-mode Comparator R Q 5 OUTPUT To VCC
6
-VIN
4 VCC Undervoltage Comparator Q R 12 13
SENSE
VCC +VIN
7 1 8.1 V - + 8.6 V
- +
S
SHUTDOWN RESET
Pre-regulator/Startup
FIGURE 9.
Si9120 Block Diagram
Flyback Converter Example To illustrate the design procedure for a low-power off-line SMPS, a typical example should be presented. But what is a "typical" 5- to 10-W supply requirement? Should the output be a single +5 V or +12 V, or should a dual output, "5 V or "12 V, be used? How about +5 V and "12 V? There is no typical requirement, so a multiple-output design was chosen since cross regulation requirements make this the more difficult problem. The specifications for a 5-W supply with four outputs is given below.
Circuit Description The flyback converter circuit, shown in Figure 10, was designed for minimum cost and parts count. Since the regulation requirements are fairly loose, it is advantageous to eliminate feedback from primary to secondary. Output voltage is controlled indirectly by regulating a bootstrap auxiliary winding on the primary side. (Strictly speaking, the auxiliary winding is not required, as the chip will run directly from line power; but another feedback scheme would obviously be necessary.) All outputs are isolated from one another. Also, the primary-to-secondary isolation is designed to meet VDE safety requirements. The power switching transistor (Q1) is an IRF820 rated at 500 V and 2.5 A. On-resistance is specified at 3 W. While this device may appear to be overkill for a 5 W output, it is the smallest 500-V die available, and it allows operation without a heatsink. Ripple (mVp-p)
200 200 50 15
Specifications Input Voltage 90- to 130-V ac, 50 to 60 Hz
TABLE 1.
Output Voltage (v)
+30 +12 +5(Main) +5(Aux)
Min Load (mA)
1 80 25 20
Max Load (mA)
4 340 110 80
Regulation (%)
"5 "5 "5 "5
Efficiency >80% Minimum Switching Frequency 32 kHz Document Number: 70580 24-Mar-97
The flyback inductor (T1) is designed to operate in the discontinuous conduction mode. This makes loop compensation simple since there is no right half plane zero in DCM flyback converters. Also, since the power level is so low, the higher peak currents associated with this mode of operation pose no significant problems. The Si9120 provides all necessary control functions with only a handful of passive components.
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L1 AC
TI
CR3 + C8 1 mF 50 V C9 1 mF 50 V 30 V 4 mA -
AC IN
C1 0.1
C2 0.1
-
CR1
+
AC C19 0.0047
C3 + 33 mF 200 V
CR4 + C10 0.1 + C11 2200 mF 16 V 12 V 320 mA CR5 + Q1 IRF820 C12 0.1 + C13 2200 mF 6.3 V 5V 110 mA C18 75 pF R7 2.4 W CR6 L2 13 mH
RTN C20 0.0047 C22 R1 453 k R8 10 5 R6 1k 4 14 C4 0.0025 R4 10 k C5 0.1 R5 15 k R3 10 k C7 1 mF CR2 IN4148 R9 20 6 10 11 7 C6 120 pF C14 0.1 +C15 2200 mF 6.3 V C16 0.1 R13
0.01 1 16 8 9
R12 510
Si9120
15
CR7 IN4148
C21 220 pF R10 1k
R2 390 k
Q2 2N7000 R11 2k
+ C17 220 mF 6.3 V 5V 80 mA +
TO DC RTN
FIGURE 10. 5-W Offline Flyback Converter
Flyback Fundamentals
The flyback circuit works by storing energy in the flyback inductor during the switch's on-time and releasing this energy to the secondary circuits during the switch's off-period. The power transformer, in the case of a flyback converter, is not a transformer at all. Transformers work by coupling energy from primary to secondary, storing as little energy as possible. The flyback, however, stores all the energy for one cycle of operation in what is properly an inductor.
It is widely believed that current in an inductor cannot be changed instantaneously. This is not quite true. Ampere-turns are what cannot change instantaneously. If you could somehow change the turns, you could change the current on
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demand. This is what happens in the flyback inductor. During the switch-on time, some number of ampere-turns are developed in the primary winding. The power switch is then turned off in essentially zero time, forcing the ampere-turns to appear at the secondary windings. Thus, turns have changed, and amperes scale accordingly. Autotransformer action between the various windings forces the output voltages to track in proportion to the turn ratios of the windings. This forces the output capacitors to peak charge to the respective winding voltages and, thereby, provides regulation between windings. The better the coupling between windings, the better the cross regulation. Hence, all four outputs are wound closely together with no additional insulation between windings. By controlling the peak current through the primary winding during the on-time, the total energy per cycle, hence the total throughput power, can be controlled. By making this current a function of the output voltage error, voltage regulation is achieved.
Document Number: 70580 24-Mar-97
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AN707
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On initial application of power to the supply, the high-voltage DMOS transistor in the Si9120 begins to charge the VCC supply capacitor, C7. When approximately 8.1 V appears on the bias supply, the Si9120 undervoltage lockout enables the output driver. All internal bias voltages are stable at this point, and clean operation is assured. When VCC reaches 8.6 V, the DMOS linear regulator reduces the charging current to maintain this voltage. Within a few cycles of operation, the bootstrap winding raises VCC beyond the point at which the linear regulator tries to hold the bias supply. The DMOS transistor is forced to cut off. Now the VCC supply is totally independent of the power line and draws no current from it.
A major problem exists in any converter with a large input-to-output isolation voltage -- leakage inductance of the flyback inductor. A portion of the energy stored in this inductance will appear as a voltage spike on the feedback winding. The VCC supply tends to charge to the peak of the spike, forcing the control loop to regulate all of the output voltages substantially below the desired values. Spike suppression and proper operation of the regulator loop are provided by a blanking circuit (consisting of R9, R10, R11, C21, CR7, and Q2). At the instant Q1 turns off, a positive-going voltage appears at the anode of CR7. C21 forms a differentiator with R10 and R11 that produces a positive voltage on the gate of Q2. This turns on Q2 and clamps the anode of CR2 to ground, back-biasing CR2 and preventing the spike from passing through to the VCC supply. A substantial portion of the energy contained in the voltage spike is shunted to ground through CR7 and R9 (the circuit is behaving, to some degree, like an active snubber). When the spike energy has been dissipated, the voltage drops to the nominal level. R11 then pulls Q2's gate voltage back down, turning off Q2 and allowing the remainder of the pulse to pass through to the VCC supply. Figure 11 shows details of the blanking circuit in operation. Figures 12-15 show details of the power supply operation. The input voltage for all photos was 115 V RMS and all loads are at maximum. Table 1 gives the line and load regulation of the circuit along with output ripple and efficiency data. At 85% efficiency, absolutely no heatsinks are required.
A cycle is initiated by the Si9120 clock toggling the output driver on. The driver turns on power switch Q1, causing current to begin ramping up linearly in T1's primary winding. The current is sensed by R7 and filtered by R6 and C6. When the Si9120's current-sense comparator detects that the primary current has reached the control loop's programmed level, the power switch is shut off and energy stored in T1 begins to discharge into the secondary circuits.
To close the regulator loop, the voltage of the VCC supply winding on the primary side is sensed and compared to a reference. The difference is multiplied by a high-gain amplifier. These functions are all performed by the Si9120. R3 and R5 divide the bias voltage down to the 4 V reference level. R4 and C4 provide for loop compensation, and C7 filters VCC.
FIGURE 11. Top Trace - Anode of CR2 Center Trace - Gate of Q2 Bottom Trace - Anode of CR7 Note spike amplitude of 23.5 V.
FIGURE 12. Top Trace - Gate Drive Q1 Center Trace - Anode of CR2 Bottom Trace - Cathode of CR7
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FIGURE 13. Top Trace - Gate Drive Q1 Center Trace - Voltage Across R7 Bottom Trace - Drain Voltage of Q1 (100 V/div)
FIGURE 14. Top Trace - Gate Drive Q1 Center Trace - Anode of CR4 Bottom Trace - CR4 Current (500 mA/div)
FIGURE 15. Top Trace - 30-V Output Ripple Bottom Trace - 5-V, 80-mA Ripple
TABLE 2. 5 W OFF LINE FLYBACK TEST DATA
Full Load Outputs (V) AC Input (V RMS)
80 100 115 130
12 V
11.00 11.05 11.08 11.11
30 V
28.50 28.60 28.70 28.77
5(Main) V
5.019 5.046 5.060 5.072
5(Aux) V
5.058 5.080 5.095 5.111
Half Load Outputs (V)
80 100 115 130 11.26 11.32 11.33 11.34 29.10 29.16 29.19 29.92 5.170 5.180 5.186 5.190 5.214 5.223 5.230 5.234
Half Load Outputs (V)
80 100 115 130 11.26 11.32 11.33 11.34 29.10 29.16 29.19 29.92 5.170 5.180 5.186 5.190 5.214 5.223 5.230 5.234
Output Ripple (mV Pk-Pk)
90 125 23 12 Actual measured outputs tabulated at various line and load conditions (5(Main) = 5 V, 110 mA, 5(Aux) = 5 V, 80 mA) Full Load Drop Out Voltage = 64-V RMS Efficiency = (Pout/Pin) 100% = (4.98/5.86) 100 = 85% www.vishay.com S FaxBack 408-970-5600 Document Number: 70580 24-Mar-97
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CIRCUIT DESIGN DETAILS
Selecting the Input Capacitor
V off(max) + V in(max) ) 125 V + 130 2 ) 125 + 308 V
For a 90-V ac input, the bus voltage is Allowing approximately 100 V for the leakage inductance spike, VDS(max) v 408 V. A 500-V FET gives a good safety margin. The IRF820 is rated 500 V, 3 W. For TJ = 100_C, the rDS(on) scale factor = 1.6, so the worst case on-resistance is
= 3 W (1.6) = 4.8 W
90 2 + 127 V dc
If 20 V of ripple is allowed, the lowest input voltage is 107 V dc. For some margin, use 100 V dc. For a 5-W output with 80% efficiency, h = 0.8;
Pin = Pout/h = 5/0.8 = 6.25 W Iin = Pin/VIN = 6.25/100 = 62.5 mA
rDS(on)
Conduction loss is
(0.11 A)2 (4.8 W) = 0.058 W
Input ripple is assumed to be 20 Vp-p. The low frequency limit is 50 Hz; thus, the ripple frequency is 100 Hz.
C = I x DT/DV = (0.0625) (0.01)/20 = 31.25 mF
Assuming switching losses are equal to conduction losses, total dissipation in the FET equals 0.116 W. With no heatsink,
33 mF is a standard value. Finding the Peak Switch Current At 100 V dc in, the maximum duty factor D = 45%.
Ipk = 2 x Iavg/Dmax = 2 (0.0625)/0.45 = 0.28 A
DTJ
= (R QJA) (PDISS) = (80_C/W) (0.155 W) = 9.3_C
Primary Inductance Operating frequency was selected at approximately 32 kHz to permit synchronization to a television horizontal scan if needed. Period TS = 31.25 ms, so
ton(max)
The RMS switch current is
= (0.45) (31.25) = 14 ms
I RMS + Ipk
D + 0.28 3
0.45 3 + 0.11 A
Ipk was calculated at 0.28 A and is also invariant with line voltage. At low line,
VIN(min) = 100 V and
Switch Voltage Rating and Temperature Rise The transformer primary voltage during the off-time will be independent of input line voltage but must be equal to or greater than the dc input voltage at low line. The maximum switch off-voltage equals the dc input at high line plus the transformer off-voltage. If the transformer off-voltage is assumed to be 125 V (the peak of the rectified sine wave at low line), then
Document Number: 70580 24-Mar-97
LP + VDt + DI
100(14ms) + 5 mH 0.28
where
LP = Primary Inductance Dt = ton(max) DI = Ipk
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Flyback Inductor Design Using the area product method,
(25.32 LPIpkD 2) 108 B max
Solve for secondary turns, NS. Based on the feedback winding,
V O ) Vf (1 - D msc) Vin(min) D max
A cA e +
(REF-2)
NS + NP
[See REF. 2] (117) (10.0 ) 0.7) (1 - 0.45) + + 15.3 turns (100 V) (0.45)
where where
Vf = diode forward voltage VO = output voltage Dmax = maximum duty factor VIN(min) = dc bus voltage at low line Use 15 turns. This must be less than or equal to the calculated number of turns to ensure current resetting to zero during the off time. Scaling voltages for other outputs:
D Bmax Ac Ae AcAe
= wire diameter in inches = maximum flux swing in gauss = core cross sectional area in cm2 = effective window are in cm2 = core-window area product in cm4
Assuming 400 cir/mil/A and 0.11 A RMS, #32 AWG is adequate. Use #31 for cool operation; the diameter of #31 AWG is 0.0108 inches. Allow Bmax = 2000 gauss.
(25.32)(5 mH)(0.28 A)(0.0108) 2 (108) A cA e + 2000 = 0.207 cm4 where
10.7 V/15 turns = 0.7133 V/turn For all outputs: Vpk = VO + Vf
PQ 42020 size core has AcAe = 0.238 cm4, so it should handle the power.
Vpk is transformer secondary voltage. NS = Vpk/0.7133 V/turn After calculating all turn numbers and scaling slightly to optimize output voltage balances, the following turns resulted:
Find the air gap, lg, as:
1.26 LP I2 pk x 108 (1.26)(5.0 E-3)(0.28) 2(10) 8 (0.58) (2000) 2
+30 V +12 V +5 V 10 V bias
43 turns 17 turns 8 turns 15 turns
Ig +
A cB 2 max
+
= 0.213 cm = 8.4 mils
Choose Wire Sizes. Core window area Ae = 0.384 cm2. Allowing about a 50% fill factor results in a winding area of 0.5 (0.384) = 0.192 cm2
8 mils is a standard air gap.
#31 AWG was assumed for primary. The wire chart lists 1072 turns/cm2 for #31 AWG. 117/1072 = 0.1091 cm2 0.192 - 0.1091 = 0.083 cm2 left for secondaries Scaling for the percentage of power output and allotting window area accordingly, the following wire gauges result: 30 V, #40 AWG. (This is about the smallest wire gauge one would use for reliable design and ease of manufacture.) 12 V, #25 AWG 5 V, #31 AWG both outputs Feedback, #40 AWG for same reasons as +30 V output
Document Number: 70580 24-Mar-97
Calculate primary turns, NP. For the chosen core with an 8 mil air gap, the inductance factor, AL = 363 mH/1000 turns.
N P + 1000 LP AL 5.0 + 117 turns 363
N P + 1000
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Calculating Output Currents To determine the peak and RMS output currents, the following equations apply:
Ipk Iout 0 t1 Output Current Waveform t1 + 2 (I out) A L N 2 f(V OUT ) V f)(109)
1 2
peak-to-peak ripple will be approximately equal to (Ipk)(ESR). On the 5 V, 80 mA output, due to a very low ripple specification, a two stage filter to minimize capacitor size was easiest to use. The inductor is a small ferrite core with a few turns of wire. The 30-V output needs only a couple of microfarads of capacitance if ESR = 0. A 2-mF ceramic capacitor fills the bill.
The timing resistor was initially selected at 500 kW (from the graph on the Si9120 data sheet) and was optimized empirically at 453 kW . Be sure to measure operating frequency on pin 5, as the scope probe capacitance on pin 9 will substantially alter the operating frequency. Calculating the Primary Current Sense Resistor Value The minimum current limit threshold is specified at 1 V. The calculated peak primary current is 0.28 A. Allowing approximately 25% over current,
Ipk Rcs = (0.28) (1.25) = 0.35 A = Es/Ipk = 1.0/0.35 = 2.86 W
2(I ) I pk + out t 1f I RMS + t 1f 3
Where:
t1 = current decay time Iout = average load current AL = core inductance constant in mH/1000 turns Ipk = peak secondary current f = operating frequency N = number of turns
2.7 W is the nearest standard value. R6 and C6 set a 120 ns time constant on the current sense to filter noise spikes.
The blanking circuit differentiator time constant was selected at approximately 0.5 ms. R10 and R11 reduce the gate voltage amplitude to an acceptable level. R3 and R5 divide the feedback voltage down to 4.00 V. R5 was made adjustable for test purposes, and should be approximately 15 kW . Loop Compensation
Results are as follows:
TABLE 3.
Ipk (A)
12 V 30 V 5(Aux) V 5(Main) V 10 V bias 1.60 0.11 1.08 1.28 0.16
t1 (ms)
12.85 2.34 4.60 5.39 1.2
IRMS (A)
0.59 0.017 0.24 0.31 1.8
Selecting Output Diodes and Capacitors Armed with the above data, selection of diode current ratings is possible using the RMS currents calculated. Also, the output capacitors can be sized based on the peak currents. The
A frequently asked question is "How can I close the loop without a $40-K analyzer?" Well, a number of techniques exist -- some tedious, others not quite as bad. The most reliable approach is to apply a pulsed load to the output and empirically adjust the RC compensation for a well-damped exponential output-voltage recovery. With a little practice, this can be done expeditiously. It also has the advantage of showing any problems which may arise when one or more circuit elements are driven non-linear, as can occur during a large transient. This information is missing in a small-signal response plot. Be aware, however, that a load-pulse test lacks the quantitative information of a good Bode plot and fails to permit an accurate assessment of design margins. But with a little hands-on experience, it will be easy to get a good feel for when it's right.
Document Number: 70580 24-Mar-97
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AN707
Vishay Siliconix
VO Power Supply Under Test VCC VCC RTN Square Wave Gen fO ' 100 Hz SMP25N05 O-Scope RTN 2RL 2RL
Figure 16. This allows a load step to be applied to the highest power output. If a bootstrap winding is not used for feedback, apply the step load to the regulated output. The amplitude of the step should be 25% to 50% of the full load current. The repetition rate should be low, around 100 Hz. Monitor the voltage on the VCC pin of the Si9120, as this is controlled by the feedback loop, and watch the recovery characteristics. Gradually increase R4 and decrease C4 to obtain a good response.
FIGURE 16. Pulse Load Test Setup
Proceed as follows: Set C4 to approximately 0.1 mF. This sets the error amplifier to unity gain at approximately 100 Hz (Xc = R5 @ 100 Hz). Set R4 to zero. Set up the circuit shown in
Figure 17 shows the step response to several combinations of RC compensation. A small capacitor across R5 will also speed up the response, but may not be required. In addition, it may be desirable to add a small (100 to 1000 pF) capacitor directly across pins 14 and 15 of the Si9120 to roll off the error amplifier's high frequency gain. Be sure to repeat the above procedure for low and high input line voltages. When the response looks like line D in Figure 17, you're done.
Hi Load Gate Voltage Pulse - 5 V/Div Low Load C4 = 0.1 mF R4 = 0 50 mV/div C4 = 0.01 mF R4 = 0 50 mV/div C4 = 1000 pF R4 = 0 20 mV/div C4 = 2500 pF R4 = 10 K 20 mV/div Very Slow Overdamped
A
B C D
Better But Still Slow
Fast But Under damped Note Ringing Good Speed Near Critical Damping
FIGURE 17. Step Response to Combinations of RC Compensation
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Document Number: 70580 24-Mar-97
AN707
Vishay Siliconix
CONCLUSION
Using the Si9120, the design of low-power, high-efficiency, switching power supplies for off-line applications becomes straightforward. By running a DCM flyback topology under current-mode control, a reliable, easily compensated design is achieved. The leakage inductance spike-blanking circuit presented here makes for a well-regulated supply while allowing VDE voltage-isolation requirements to be met.
FLYBACK CONVERTER PARTS LIST
C1, C2 . . . . . . . . . . . . . . . . . . . . . 0.01 mF, 250 V ac, class X2, Vishay Roederstein F1773-310-2900 C3 . . . . . . . . . . . . . . . . . . . . . . . . 33 mF, 200 V United Chemicon SL200VB33RU16X31LL C4 . . . . . . . . . . . . . . . . . . . . . . . . 2500 pF, 50 V ceramic, Vishay Vitramon VJ1206Y252KXAAT C5, C10, C12, C14, C16 . . . . . 0.1 mF, 50 V ceramic, Vishay Vitramon VJ1206Y104KXAAT C6 . . . . . . . . . . . . . . . . . . . . . . . . 120 pF, 50 V ceramic, Vishay Vitramon CJ0402Y121KXAAT C7, C8, C9 . . . . . . . . . . . . . . . . . 1 mF, 50 V ceramic, Vishay Vitramon VJ1812Y105KXAAT C11 . . . . . . . . . . . . . . . . . . . . . . . . 2200 mF, 16 V United Chemicon SXC16VB222M18X35LL C13, C15 . . . . . . . . . . . . . . . . . . 2200 mF, 6.3 V United Chemicon SXC6.3VB222M16X25LL C17 . . . . . . . . . . . . . . . . . . . . . . . 220 mF 6.3 V United Chemicon SXC6.3VB221M10X12LL C18 . . . . . . . . . . . . . . . . . . . . . . . 75 pF, 500 V (mica or ceramic), Vishay Vitramon VJ12DCA750KXEAT C19, C20 . . . . . . . . . . . . . . . . . . . 0.0047 mF, 250 V ac, class Y, Vishay Roederstein F1710-247-1000 C21 . . . . . . . . . . . . . . . . . . . . . . . 220 pF, 50 V (ceramic), Vishay Vitramon VJ0402Y221KXAAT CR1 . . . . . . . . . . . . . . . . . . . . . . . Bridge rectifier 600 V, 1 A CR3 . . . . . . . . . . . . . . . . . . . . . . . MUR110 CR4 . . . . . . . . . . . . . . . . . . . . . . . 1N5822 CR5, CR6 . . . . . . . . . . . . . . . . . . 1N5819 IC1 . . . . . . . . . . . . . . . . . . . . . . . . Si9120DJ L1 . . . . . . . . . . . . . . . . . . . . . . . . . Common-mode choke 8 mH L2 . . . . . . . . . . . . . . . . . . . . . . . . . 13 mH: core: Magnetics Inc J40401TC with 6 turns # 26 AWG Q1 . . . . . . . . . . . . . . . . . . . . . . . . IRF820 Q2 . . . . . . . . . . . . . . . . . . . . . . . . 2N7000 R1 . . . . . . . . . . . . . . . . . . . . . . . . 453 kW . . . . . . . 1% . . . . . 1/4 W. Vishay Dale CRCW12064533FRT1 R2 . . . . . . . . . . . . . . . . . . . . . . . . 390 kW . . . . . . . 5% . . . . . 1/4 W. Vishay Dale CRCW12063903FRT1 R3 . . . . . . . . . . . . . . . . . . . . . . . . 10 kW . . . . . . . . . 1% . . . . . 1/4 W. Vishay Dale CRCW12061002FRT1 R4 . . . . . . . . . . . . . . . . . . . . . . . . 10 kW . . . . . . . . 5% . . . . . 1/4 W. Vishay Dale CRCW1206103JRT1 R5 . . . . . . . . . . . . . . . . . . . . . . . . 15 kW . . . . . . . . . 1% . . . . . 1/4 W. Vishay Dale CRCW12061502FRT1 R6, R10 . . . . . . . . . . . . . . . . . . . . 1 kW . . . . . . . . . . 5% . . . . . 1/4 W. Vishay Dale CRCW1206102JRT1 R7 . . . . . . . . . . . . . . . . . . . . . . . . 2.7 W . . . . . . . . 5% . . . . . 1/4 W. Vishay Dale CRCW12062R7JRT1 R8 . . . . . . . . . . . . . . . . . . . . . . . . 10 W . . . . . . . . . . 5% . . . . . 1/4 W. Vishay Dale CRCW120610RJRT1 R9 . . . . . . . . . . . . . . . . . . . . . . . . 20 W . . . . . . . . . . 5% . . . . . 1/4 W. Vishay Dale CRCW120620RJRT1 R11 . . . . . . . . . . . . . . . . . . . . . . . . 2 kW . . . . . . . . . . 5% . . . . . 1/4 W. Vishay Dale CRCW120602JRT1 R12 . . . . . . . . . . . . . . . . . . . . . . . 510 W . . . . . . . . 5% . . . . . 1/4 W. Vishay Dale CRCW1206511JRT1 R13 . . . . . . . . . . . . . . . . . . . . . . . 10 kW . . . . . . . . 5% . . . . . 1/4 W. Vishay Dale CRCW1206103JRT1 T1 . . . . . . . . . . . . . . . . . . . . . . . . . Schott Corp #6712244
REFERENCES
1) Liu, K.H., "Effects of Leakage Inductance on the Cross Regulation in a Discontinuous-Mode Flyback Converter," Proceedings, 1989 High Frequency Power Conference, Naples, Florida.
2) Chryssis, G., "High Frequency Switching Power Supplies," McGraw Hill 1984.
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