SC4809C Datasheet

SC4809A/B/C
High Performance Current Mode
PWM Controller
POWER MANAGEMENT
Description
Features
The SC4809A/B/C is a 10 pin BICMOS primary side
current mode controller for use in Isolated DC-DC and
off-line switching power supplies. It is a highly integrated
solution, requiring few external components. It features
a high frequency of operation, accurately programmable
maximum duty cycle, current mode control, line voltage
monitoring, supply UVLO, low start-up current, and
programmable soft start with user accessible reference.
It operates in a fixed frequency, highly desirable for
Telecom applications. Features a separate sync pin which
simplifies synchronization to an external clock. Feeding
the oscillator of one device to the sync of another forces
biphase operation which reduces input ripple and filter
size.
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‹
‹
‹
‹
‹
‹
Operation to 1MHz
Accurate programmable maximum duty cycle
Line voltage monitoring
External frequency synchronization
Bi-phase mode of operation for low ripple
Under 100µA start-up current
Accessible reference voltage
VDD undervoltage lockout
-40°C to 105°C operating temperature
10 lead MSOP package. Lead free package available.
Fully WEEE and RoHS compliant
Applications
‹ Telecom equipment and power supplies
‹ Networking power supplies
‹ Power over LAN applications
‹ Industrial power supplies
‹ Isolated power supplies
The SC4809A/B/C have different threshold and VREF
to accommodate a wide variety of applications.
These devices are available in the MSOP–10 lead free
package.
Typical Application Circuit
T1
+48V
C1
R2
R1
D1
D2
U1
SC4809
R3
SYNC
C7
VDD
2
LUVLO
OUT
9
1
IN
3
SYNC
GND
8
2
GND
VREF
10
4
RCT
FB
7
5
DMAX
SS
6
Vout
C8
U2
SC1301
1
3
EN
5
OUT
4
Q2
R13
R12
VCC
U3
R9
C9
R4
R6
R5
-- 48V
R10
R7
C3
R8
R11
U4
SC4431
R14
Q1
C2
C4
C5
C6
DISABLE
Revision: September 21, 2005
1
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SC4809A/B/C
POWER MANAGEMENT
Absolute Maximum Ratings
Exceeding the specifications below may result in permanent damage to the device, or device malfunction. Operation outside of the parameters specified
in the Electrical Characteristics section is not implied.
Parameter
Symbol
Maximum
Units
Supply Voltage
V DD
19
V
Supply Current
IDD
25
mA
-0.3V to VREF + 0.3V
V
IREF
15
mA
Current LUVLO
ILUVLO
-1
mA
Storage Temperature Range
TSTG
-65 to +150
°C
Junction Temperature
TJ
-40 to +150
°C
Thermal Resistance
θJ A
113
°C/W
Lead Temperature (Soldering) 10 Sec.
TLEAD
+300
°C
ESD Rating (Human body model)
ESD
2
kV
SS, UVLO, DMAX, RCT
Current VREF
Electrical Characteristics
Unless specified: VDD = 12V, CSS =1nF, FOSC = 500kHz, RT = 10K, CT = 100pF, DMAX = 2V, TA = TJ = -40ºC to +105ºC.
Parameter
Test Conditions
Min
Typ
Max
Unit
16
17.5
19
V
1.5
2.5
mA
110
µA
4.5
V
0.3
V
12
V
4
V
6.95
V
0.75
V
Supply Section
VDD Clamp
IDD
B version
IDD Starting
UVLO Section (A version)
Start Threshold
4.35
Hysteresis
UVLO Section (B version)
Start Threshold
11
Hysteresis
UVLO Section (C version)
Start Threshold
6.55
Hysteresis
VREF Section
VREF (A version)
0 - 5mA
-3%
4
+3%
V
VREF (B, C version)
0 - 5mA
-3%
5
+3%
V
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SC4809A/B/C
POWER MANAGEMENT
Electrical Characteristics (Cont.)
Unless specified: VDD = 12V, CSS =1nF, FOSC = 500kHz, RT = 10K, CT = 100pF, DMAX = 2V, TA = TJ = -40ºC to +105ºC.
Parameter
Test Conditions
Min
Typ
Max
Unit
Start Threshold
RA = 61.9k, RB = 10k
-3%
3
-3%
V
Hysteresis
RA = 61.9k, RB = 10k
150
LUVLO = 3.2V
-100
Output Off
-100
Line Under Voltage Lockout
Input Bias Current
mV
-250
nA
Comparator Section
IFB
nA
Comparator Threshold (A, B version)
570
600
630
mV
Comparator Threshold (C version)
950
1000
1050
mV
75
100
ns
-8.0
µA
OUT Propagation Delay (No Load)
VFB = 0.8V to 1.2V at TR = 10ns
Soft Start Section
ISS
VSS = 0V; -40 °C <Ta +105°C
-2
Shutdown Threshold (A, B version)
300
340
mV
Shutdown Threshold (C version)
440
500
mV
Oscillator Section
Frequency range
50
1100
kHz
RCT Peak Voltage
3.00
V
RCT Valley Voltage
0.05
V
50
ns
90
%
2.1
V
Minimum Duty Cycle Pulse Width
V FB = 2V
Maximum Duty Cycle
Sync/CLOCK
Clock SYNC Threshold
Minimum Sync Input Pulse Width
Positive Edge Triggered
FSYNC > Fosc
50
ns
Output VSAT Low
IOUT = 1mA
500
mV
Output VSAT High
IOUT = 1mA
Output Section
VREF - 0.5
V
Rise Time
COUT = 20pF
10
25
ns
Fall Time
COUT = 20pF
10
25
ns
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SC4809A/B/C
POWER MANAGEMENT
Pin Configuration
Ordering Information
Part Number
Top View
Package(1)
Temp. Range (TJ)
MSOP-10
-40°C to +150°C
SC4809AIMSTR
SC4809AIMSTRT(2)
SC4809BIMSTR
SC4809BIMSTRT(2)
SC4809CIMSTR
SC4809CIMSTRT(2)
Notes:
(1) Only available in tape and reel packaging. A reel
contains 2500 devices.
(2) Lead free product. This product is fully WEEE and
RoHS compliant.
MSOP-10
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SC4809A/B/C
POWER MANAGEMENT
Pin Descriptions
FB: This pin is the summing node for current sense feedback, voltage sense feedback (by optocoupler) and slope
compensation. Slope compensation is derived from the
rising voltage at the time capacitor and can be buffered
with an external small signal NPN transistor. External
high frequency filter capacitance applied from this node
to GND is discharged by an internal 250Ω on-resistance
NMOS FET during PWM off -time and offers effective leading edge blanking set by the RC time constant of the
feedback resistance from the current sense resistor to
the FB input and the high frequency filter capacitor capacitance at this node to GND.
DMAX: Duty cycle up to 98% can be programmed via R4
and R5 (the resistor divider from Vref in the Application
Circuit). When DMAX pin is taken above 3V, 100% duty
cycle is achieved.
SS: This pin serves two functions. The soft start timing
capacitor connects to SS and is charged by an internal
8µA current source. Under normal soft start SS is discharged to less than 1V and then ramps positive to 1V
during which time the output driver is held low. As SS
charges from 1V to 2V, soft start is implemented by an
increasing output duty cycle. If SS is taken below shutdown threshold, the output driver is inhibited and held
low. The user accessible voltage reference also goes
low and IDD < 100µA.
GND: Reference ground and power ground for all functions.
OUT: This pin is the logic level drive output to the external MOSFET driver circuit (similar to SC1301).
VDD: The power input connection for this device. This pin
is shunt regulated at 17.5V which is sufficiently below the
voltage rating of the DMOS output driver stage. VDD
should be bypassed with a 1µF ceramic capacitor.
VREF: The internal 4V (A) / 5V (B & C) reference output.
This reference is buffered and is available on the VREF
pin. VREF should be bypassed with a 0.47 - 1.0µF ceramic capacitor.
LUVLO: Line undervoltage lock out pin. An external resistive divider will program the undervoltage lock out level.
During the LUVLO, the Driver outputs are disabled and
the softstart is reset.
RCT: The oscillator frequency is configured by connecting resistor RT from VREF to RCT and capacitor CT from
RCT to ground. Using the equation below values for RT
and CT can be selected to provide the desired OUT frequency.
F=
SYNC: SYNC is a positive edge triggered input with a
threshold set to 2.1V. In the Bi-Phase operation mode
the SYNC pin should be connected to the CT
(Timing Capacitor) of the second controller. This will force
a out of phase operation. In a single controller operation, SYNC could be grounded or connected to an external synchronization clock with a frequency higher than
the on-board oscillator frequency. The external OSC frequency should be 30% greater for guaranteed SYNC
operation.
1


V
− RT • CT • ln 1 − P −K
VREF





where VP-K = RCT peak voltage
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SC4809A/B/C
POWER MANAGEMENT
Block Diagram
Marking Information
Top Mark
AF0A
yyww
Bottom Mark
xxxx
xxxx
Top Mark
AF0B
yyww
Bottom Mark
xxxx
xxxx
Top Mark
AF0C
yyww
Bottom Mark
xxxx
xxxx
Part Number (Example: 1456)
yyww = Datecode (Example: 0012)
xxxxx = Semtech Lot # (Example: E901
xxxxx =
01-1)
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90 - 300VDC
C1
1/450V
 2005 Semtech Corp.
C2
2.2n
L1
(Opt.)
C3
2.2n
Q2
FMMT718
C4
47/400V
7
C8
0.1
R7
7.5k
C5
0.1
R8
4.3k
R6
10k
Z1
BZX84C12
D1
SD103C
R9
5.6k
5
4
3
2
1
R5
510
SS
FB
GND
OUT
VREF
Fsw = 500kHz
DMAX
RCT
SYNC
LUVLO
VDD
U1
SC4809
C9
33n
C11
0.33
C12
0.1
3
2
1
VCC
GND
IN
OUT
EN
U2
SC1301A
T1
----------------------------------------Core: EFD15, 3C85
Magnetizing L = 230uH
Np1 = 24 ts
Np2 = 5 ts
Ns1 = 2 ts
Approximate Gap = 0.038mm
AL value = 397 nH/N²
C10
1n
6
7
8
9
10
4
5
R14
100
R13
300
R12
2.2
D2
US1G
Z3
SMBJ85
R15
1.5
Q3
IRFR420
Np1
T1
D3
US1B
2
1
R16
150
U3
MOC207
7
D4
B240
C15
0.1
Vcc
R17
1k
C13
4.7/20V/1.8 Ohm
R18
3k
U4
SC4431
C17
1n
C16
2.7n
R19
10k
C18
330/6.3V/0.04 Ohm
L2
10uH
U2: SC1301AISKTR, SOT-23-5, SEMTECH
U4: SC4431CSK, SOT-23-5, SEMTECH
Q3: IRFR420, Dpak, Inter.Rect.
B240, SMB, Vishay
C17: 6TPB330M, "7343", Sanyo
L2: TOKO, A920CY-100M or similar
U1: SC4809AIMSTR, MSOP-10, SEMTECH
CRITICAL COMPONENTS:
5
6
C14
220pF
Ns1
Np2
11
C19
10uF/6.3V
C21
2.2n
C20
0.1
R21
102
R20
316
+
_
5V@1A
POWER MANAGEMENT
Applications Information
R11
3k
C6
100p
Z2
CMZ5929
R10
1k
C7
100p
R4
100k
R3
820k
R2
2M
R1
750k
Q1
FZT458
SC4809A/B/C
Flyback, 90V - 300V to 5V @ 1A typ.
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SC4809A/B/C
POWER MANAGEMENT
Application Information
The flyback power stage is very popular in 48V input
telecom applications for output power levels up to
approximately 50 watts. The exact power rating of the
flyback power stage, of course, is dependent on the input
voltage/output voltage combination, its operating
environment and many other factors. Additional output
voltages can be generated easily by simply adding another
winding to the coupled inductor along with an output
diode and output capacitor. Obtaining multiple output
voltages from a single power stage is another advantage
of the flyback power stage.
A simplified schematic of the flyback power stage with a
drive circuit block included is shown in Figure 1. In the
schematic shown, the secondary winding of the coupled
inductor is connected to produce output voltage. The
power switch, Q1, is an N-channel MOSFET. The
secondary inductance, LSEC and capacitor C, make up the
output filter, The resistor R, represents the load seen by
the power supply output.
Figure 2: Discontinuous Mode Flyback Waveforms
The simplified voltage conversion relationship for the
flyback power stage operating in CCM is given by:
Figure 1: Flyback Power Converter
VO = VI •
The important waveforms of the flyback power stage
operating in DCM are shown in Figure 2.
NS
D
•
NP 1 − D
The simplified voltage conversion relationship for the
flyback power stage operating in DCM is given by:
VO = VI •
NS
D
•
NP
K
Where K is defined as:
K=
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2 • L SEC
R • TS
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SC4809A/B/C
POWER MANAGEMENT
Application Information (Cont.)
The DC transfer function of a CCM flyback converter is:
Control-to-Output transfer function for the flyback power
stage operating in CCM is given by:

S  
S
1 +
 • 1 −
ωz1   ωz 2
dVO
N
VI
=
• S •
2
dD (1 − D)
NP
S
S2
+
1+
ωO • Q ωO 2
VO + VD
1  Dmax
= • 
VIN(min) − VRds( on ) N  1 − Dmax



where VO = output voltage,
VD = forward voltage drop across rectifier D1,
where:
N = turns ratio, equal to NP/NS,
1
ωz1 =
RC • C
ωz 2 ≈
ωO ≈
Q≈




D = duty cycle.
(1 − D) • R
D • L SEC
2
Transformer Design
1− D
The transformer in a flyback converter is actually a coupled
inductor with multiple windings. Transformers provide
coupling and isolation whereas inductors provide energy
storage. The energy stored in the air gap of the inductor
is equal to:
L SEC • C
(1 − D) x R
L SEC
C
L P • (IPEAK )
2
2
E=
Control-to Output transfer function for the flyback power
stage operating in DCM is given by:
N
R • TS
dVO
•
= VI • S •
NP
2 • L SEC
dD
where E is in Joules, LP is the primary inductance in
Henries, and IPEAK is the primary peak current in Amperes.
When the switch is on, D1 is reverse biased due to the
dot configuration of the transformer. No current flows in
the secondary windings and the current in the primary
winding ramps up at a rate of:
1
1+
S
ωP
where:
ωP =
2
R•C
∆IL VIN(min) − VRds( on )
=
∆t
LP
Peak current mode control requires simpler
compensation, has pulse-by-pulse current limiting, and
has better load current regulation. Primary and secondary
RMS currents can be up to two times higher for
discontinuous mode than for CCM. Discontinuous
conduction mode would require using a transistor with a
higher current rating. Because the output ripple current
is less than it would be continuous mode were used, the
output capacitors are smaller. Continuous conduction
mode (CCM) was therefore chosen.
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The output capacitor, COUT, supplies all of the load current
at this time. Because the converter is operating in the
continuous conduction mode, ∆IL is the change in the
inductor current which appears as a positive slope ramp
on a step. The step is present because there is still
current left in the secondary windings when the primary
turns on. When the switch turns off, current flows through
the secondary winding and D1 as a negative ramp on a
step, replenishing COUT and supplying current directly to
the load.
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SC4809A/B/C
POWER MANAGEMENT
Application Information (Cont.)
MOSFET Selection
The primary inductance can be calculated given an
acceptable current ripple, ∆IL. ∆IL was set to equal onehalf the peak primary current. For a CCM flyback design,
the peak primary current is calculated:
 IOUT (max)
IPEAK = 
 N
 
1
•
  1− D
max
 
The switching element in a flyback converter must have
a voltage rating high enough to handle the maximum input
voltage and the reflected secondary voltage, not to
mention any leakage inductance induced spike that is
inevitably present. Approximate the required voltage
rating of the MOSFET using.
 ∆IL
+
 2


N
Vds = (VIN(max) + VL ) +  P

 NS
Because the converter is operating in the continuous
mode, the maximum peak flux density BMAX, is limited by
the saturation flux density, B SAT. Taking all this into
consideration, the maximum core size is determined by.
 L •I
•I
• 10 4
AP =  P PEAK RMS
420 • k • BMAX

where Vds = the required drain to source voltage rating of
the MOSFET,
1.31




VL = the voltage spike due to the leakage inductance of
the transformer, estimated to be thirty percent of VIN(MAX),
and the additions 1.3 factor includes an overall thirty
percent margin.
where AP = the core area product in cm4,
k = winding factor,
BMAX ≈ BSAT,
This FET will experience both switching and conduction
losses. The conduction losses will be equal to the I2R
losses, as shown by:
The result is compared to the product of the winding area,
Aw (cm2), and effective core area, Ae (cm2), listed in the
core manufacturer’s data sheet.
PCOND = (IRMS ) • R DS( ON)
2
Switching losses are the result of overlapping drain
current and drain to source voltage at turn on and turn
off.
The minimum number of primary turns is determined by:
NP =
L P • IPEAK • 10 4
B MAX • Ae
The total switching losses are estimated based on
equation:
Based upon this result and the predetermined turns ratio,
the number of secondary turns is established.
PSW =
The energy stored in the flyback transformer is actually
stored in an air gap in the core. This is because the high
permeability of the ferrite material can’t store much
energy without saturating first. By adding an air gap, the
hysteresis curve of the magnetic material is actually tilted,
requiring a much higher field strength to saturate the
core. The length of the air gap is calculated by:
lg =
 2005 Semtech Corp.


 • (VO + VD ) • 1.3



C OSS • ( VDS )2 • fSW
+ VDS • IPEAK • t ch • fsw
2
where tch:
t CH =
Q gd • R g
VDD − Vgs( th )
Diode Selection
Schottky rectifiers have a lower forward voltage drop than
typical PN devices, making it the rectifier of choice when
considering reducing converter losses and improving
overall efficiency. Selecting the appropriate Schottky for
a specific application depends mainly on the working
peak reverse voltage rating and peak repetitive forward
current.
µ o • µ r • (NP )2 • Ae • 10 −2
LP
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Application Information (Cont.)
Input and Output Capacitors
Slope Compensation
The input capacitors are chosen based upon their ripple
current rating and their rated voltage. The actual capacitor
value is not that critical as long as the minimum
capacitance gives an acceptable ripple voltage
determined by the following equation:
Sensing peak inductor current instead of average
inductor current results in a loop response that is Less
than ideal. Adding slope compensation to the current
signal cancels this error by maintaining a constant average
current independent of duty cycle. Slope compensation
is required for open loop stability in a current mode system
with 50% or greater duty cycles, but will benefit any
current mode application at the cost of a few small parts.
CMIN =
IRMS
8 • fSW • ∆V
The output capacitors are also chosen based upon their
low equivalent series resistance (ESR), ripple current and
voltage ratings. The ripple current that the output
capacitor experiences is a result of supplying the load
current during the FET conduction time and its charging
current during the FET off-time.
Loop Compensation
The continuous current mode flyback will contain a righthalf-plane (RHP) zero in its transfer function. Any increase
in load current will require the primary peak inductor
current to increase. The duty cycle must increase to
accomplish this. In a flyback converter, the inductor
current flows to the output only when the FET is off and
the diode is conducting. Increasing the duty cycle
increases the FET condition time but decreases the diode
conduction time. The result of this is the average diode
current, the current that supplies the load, actually
decreases. This is a temporary situation; as the inductor
current rises, the diode current eventually reaches its
proper value. The condition where the average diode
current must actually decrease before it can increase is
referred to as a right-half-plane zero. To complicate
matters, this zero contributes a phase lag, not a phase
lead as a normal zero would. This zero moves in frequency
as a function of load and input voltage, making it
impossible to cancel out by the insertion of a pole.
Voltage Feedback
The FB pin of the SC4809 sums the voltage feedback
signal to the current sense signal and any added slope
compensation. The voltage feedback signal is from an
optocoupler, which is driven from an error amplifier on
the secondary side of the converter. The signal from the
optocoupler is designed to trip the FB threshold of the
SC4809 internal comparator when the output voltage
exceeds its specified limit.
Current Limit
Selection of the current sense resistor is accomplished
by dividing the FB threshold value by the peak primary
current at the desired current limit point. This groundreferenced RSENSE must be a low inductance type and have
a rated power level to meet the (I RMS ) 2• R SENSE
requirement.
2
fRHPZERO =
The easiest way to deal with a right-half-plane zero is to
roll off the loop gain at a relatively low frequency using
simple dominant pole compensation. Unfortunately, the
result of this is poor dynamic response.
Current spikes caused by the leakage inductance of the
flyback transformer and the reverse recovery of the diode
could trip the current sense latch and prematurely shut
off the output. This unwanted spike can be suppressed
by adding a small RC filter for effective leading edge
blanking.
 2005 Semtech Corp.
2 • π • R OUT
N • VIN
• L P • ( VIN + N • VOUT )
The primary goal of the compensation network is to
provide good line and load regulation and dynamic
response. These objectives are best met by providing
high gain at low frequencies for good DC regulation and
high bandwidth for good transient response. Optimum
closed loop performance can only be achieved by first
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Application Information (Cont.)
knowing what the transfer characteristic of the PWM and
switching circuit looks like. Constructing a Bode plot of
the known poles and zeros in the power stage does this.
Bode plots give a visual interpretation of the gain versus
frequency and phase versus frequency characteristics
of a system. In the gain plot, the gain shown at each
frequency represents the amount by which the feedback
loop will reduce a disturbance at that frequency.
The scheme shown below will handle most compensation
requirements. There is a pole at the origin which
contributes a -1 slope in the gain plot, a low frequency
zero, fEAZERO flattens out the slope so the mid-range gain
is equal to Rf/Ri. A high frequency pole, fEAPOLE helps
suppress any high frequency noise from propagating
through the system. Rd forms a voltage divider with Ri
and provides a DC offset.
Besides the RHP zero, the output capacitor and the load
contribute a pole and the output capacitor alone will
contribute a zero based upon its ESR.
fEAZERO =
1
2 • π • R f • Cf
fEAPOLE =
1
2 • π • R f • Cp
fpole =
1+ D
2 • π • R OUT • C OUT
f zero =
1
2π • ESR • C OUT
The control to output gain is calculated by:


ISC • R OUT • VIN
GAIN = 20 • log• 

 VC • (1 − D) • (2 • N • VO + VIN ) 
Once the frequency response of the uncompensated
system is determined, the next step is to determine what
compensation is needed around the error amplifier for
optimum performance. As stated earlier, optimum
performance requires a high gain at low frequencies for
good DC regulation and high bandwidth for good transient
response. The crossover frequency, fc, is the frequency
at which the gain magnitude equals 0dB. High bandwidth
is achieved by having the highest possible fc. Because of
the RHP zero, the highest possible crossover frequency
is limited to fRHPZERO/π. The phase margin, or the amount
the phase lag measures at fc less 180°, should be at
least 45° for good transient response with little
overshoot. The magnitude of the gain at the frequency
where the phase plot measures - 180° is referred to as
the gain margin. If the slope of the gain plot is -2, or
-40dB/decade, at low frequencies, it much transition to
a -20dB/decade slope, also known as a -1 slope, one
decade before crossing the 0dB point. If the slope
remains at the -2 slope the resultant gain margin would
be too small causing sever underdamped oscillations at
fc.
 2005 Semtech Corp.
By combining the Bode plots of the PWM and power stage
with the error amplifier compensation, a plot of the entire
system is realized.
12
www.semtech.com
Za
ZMM5242B
Ra
300 1W
Qa
TIP30C
 2005 Semtech Corp.
C1
1.0/100V
13
R5
7.5k
R4
2.7k
R3
1k
C1
1.0/100V
R5
7.5k
R4
2.7k
R3
1k
C2
100p
R6
10k
R2
20k
C2
150p
R6
10k
R2
20k
R7
1k
5
4
3
2
1
R7
1k
5
4
3
2
1
U1
SC4809
R8
3.9k
SS
FB
GND
OUT
VREF
DISABLE
Q1
MMBT2907A
C3
0.47
DMAX
RCT
SYNC
LUVLO
VDD
R8
3.9k
SS
FB
GND
OUT
VREF
DISABLE
Q1
MMBT2907A
C3
0.47
DMAX
RCT
SYNC
LUVLO
VDD
U1
SC4809
C4
0.1
6
7
8
9
10
C4
0.1
6
7
8
9
10
C5
C6
0.47 200p
C7
0.1
C5
C6
0.47 200p
C7
0.1
R11
7.5k
VCC
R11
7.5k
OUT
EN
U2
SC1301
R9
100
GND
IN
R10
47k
VCC
OUT
EN
U2
SC1301
GND
IN
R10
47k
3
2
1
Z1
ZMM5242B
3
2
1
Z1
ZMM5242B
R9
100
R12
1k
4
5
R12
1k
4
5
Q2
IRF640N
Q2
IRF640N
R14
0.2 1/2W
R13
10
C8
1.0
L1
10uH
R14
0.2 1/2W
R13
10
C8
1.0
L1
10uH
R15
22k
C9
1n
D1
MURD620CT
R17
1k
R15
22k
C9
1n
D1
MURD620CT
R17
1k
R16
47k
Q3
BSS64ZXCT
R16
47k
Z2
ZMM5242B
C10
150/16V
Q3
BSS64ZXCT
Z2
ZMM5242B
C10
150/16V
C11
1.0
C11
1.0
R18
200 1W
R18
200 1W
+12V
GND
+12V
GND
POWER MANAGEMENT
Applications Information (Cont.)
-- 48V
"MASTER"
"SLAVE"
+48V
R1
1k
Rb
300 1W
SC4809A/B/C
Out of Phase, Synchronized, Dual Converter
www.semtech.com
 2005 Semtech Corp.
14
10k
10k
8.2k
A
B
C
R10
Q1
MMBT2222A
SYNC
100
62
62
604
604
1k
R7
5
4
3
2
1
R8
1.5k
0.22
0.15
0.15
R18
C3
0.1/25V
10k
R17
R6 2k
C4
*
Q2
MMBT2907A
R16
R5
10k
R4
10k
C2
0.01
R3
100k
2x10k| |
3x12k| |
2x12k| |
R12
R10
*
R9
7.5k
C5
0.01
300p
300p
200p
6
7
8
9
10
C7
0.47
390p
680p
680p
C8
C6
0.033
Z1
ZMM5245B
C4
SS
FB
GND
OUT
VREF
Fsw=330kHz
DMAX
RCT
SYNC
LUVLO
VDD
U1
SC4809_A_B_C
R11
100
C8
*
C9
1/25V
R12
*
3
2
1
VCC
GND
IN
4
5
R17
*
R16
*
R15
3.3
SMA
D2
ES1D
R18
*
4
2
3
1
6
5
7
C12
220pF
Q3
IRF640NS
U3
MOC207
R19
20 1/4W
10,11,12
7,8,9
C14-16: 6TPB470M, PosCap, Sanyo
C18
0.022
1
2
C13
1nF/50V
L1: ETQP6F2R5SFA, Panasonic
T1: PA0273, Pulse Eng.
OUT
EN
U2
SC1301A
C11
0.01/100V
6
R14
3.3k 1W
5
R20
1k
C19
0.01
U4
SC4431
R24
1.21k
C21
0.01
R23
62k
C17
10.0
C20
430pF
C14-16
470/6.3V
R22
39.2k
R21
1k
Vcc
D3
MBRB1530CT
L1
2.5uH@10A
R26
0
R25
3.83k
POWER MANAGEMENT
Evaluation Board Schematic
R2
1k
R1
5.1k
C1
1.0/100V
C10
1.0/16V
SC4809A/B/C
50W Forward Converter
www.semtech.com
SC4809A/B/C
POWER MANAGEMENT
Evaluation Board Layout
50W Forward Converter
Layout
Top
Bottom
 2005 Semtech Corp.
15
www.semtech.com
SC4809A/B/C
POWER MANAGEMENT
Outline Drawing - MSOP-10
DIMENSIONS
INCHES
MILLIMETERS
MIN NOM MAX MIN NOM MAX
e
A
DIM
D
2X E/2
ccc C
2X N/2 TIPS
E
E1
PIN 1
INDICATOR
.043
.000
.006
.030
.037
.007
.011
.003
.009
.114 .118 .122
.114 .118 .122
.193 BSC
.020 BSC
.016 .024 .032
(.037)
10
8°
0°
.004
.003
.010
A
A1
A2
b
c
D
E1
E
e
L
L1
N
01
aaa
bbb
ccc
N
12
B
1.10
0.00
0.15
0.75
0.95
0.17
0.27
0.08
0.23
2.90 3.00 3.10
2.90 3.00 3.10
4.90 BSC
0.50 BSC
0.40 0.60 0.80
(.95)
10
0°
8°
0.10
0.08
0.25
D
aaa C
SEATING
PLANE
A2
H
A
bxN
bbb
c
GAGE
PLANE
A1
C
C A-B D
0.25
L
(L1)
DETAIL
SEE DETAIL
SIDE VIEW
01
A
A
NOTES:
1. CONTROLLING DIMENSIONS ARE IN MILLIMETERS (ANGLES IN DEGREES).
2. DATUMS -A- AND -B- TO BE DETERMINED AT DATUM PLANE -H3. DIMENSIONS "E1" AND "D" DO NOT INCLUDE MOLD FLASH, PROTRUSIONS
OR GATE BURRS.
4. REFERENCE JEDEC STD MO-187, VARIATION BA.
Land Pattern - MSOP-10
X
DIM
(C)
G
C
G
P
X
Y
Z
Z
Y
DIMENSIONS
INCHES
MILLIMETERS
(.161)
.098
.020
.011
.063
.224
(4.10)
2.50
0.50
0.30
1.60
5.70
P
NOTES:
1.
THIS LAND PATTERN IS FOR REFERENCE PURPOSES ONLY.
CONSULT YOUR MANUFACTURING GROUP TO ENSURE YOUR
COMPANY'S MANUFACTURING GUIDELINES ARE MET.
Contact Information
Semtech Corporation
Power Management Products Division
200 Flynn Road, Camarillo, CA 93012
Phone: (805)498-2111 FAX (805)498-3804
 2005 Semtech Corp.
16
www.semtech.com