HCPL-4100#500 Avago Technologies US Inc., HCPL-4100#500 Datasheet - Page 7

• Manufacturer Part Number: HCPL-4100#500
• Description: OPTOCOUPLER 20MA LOOP 8-SMD
• Manufacturer: Avago Technologies US Inc.
• Type: Transmitterr

Specifications of HCPL-4100#500

• Package / Case: 8-SMD Gull Wing
• Voltage - Isolation: 3750Vrms
• Input Type: DC
• Voltage - Supply: 4.5 V ~ 20 V
• Operating Temperature: 0°C ~ 70°C
• Mounting Type: Surface Mount
• Logic Gate Type: Inverter
• Maximum Baud Rate: 20 KBps
• Configuration: 1 Channel
• Isolation Voltage: 3750 Vrms
• Output Type: Open Collector
• Maximum Propagation Delay Time: 1.6 us
• Maximum Continuous Output Current: 30 mA
• Maximum Power Dissipation: 360 mW
• Maximum Operating Temperature: + 70 C
• Minimum Operating Temperature: 0 C
• Number Of Elements: 1
• Baud Rate: 20Kbps
• Output Current: 30mA
• Package Type: PDIP SMD
• Operating Temp Range: 0C to 70C
• Power Dissipation: 360mW
• Propagation Delay Time: 1600ns
• Pin Count: 8
• Mounting: Surface Mount
• Operating Temperature Classification: Commercial
• Lead Free Status / RoHS Status: Contains lead / RoHS non-compliant
• Lead Free Status / RoHS Status: Lead free / RoHS Compliant, Contains lead / RoHS non-compliant

Notes:
10. Common mode transient immunity in the logic high level is the maximum (positive) dV
11. Common mode transient immunity in the logic low level is the maximum (positive) dV
12. Use of a 0.1 μF bypass capacitor connected between pins 5 and 8 is recommended.
13. In accordance with UL 1577, each optocoupler is momentary withstand proof tested by applying an insulation test voltage ≥ 4500 V rms for 1
Figure 3. Typical Mark State Output Voltage vs.
Temperature.
7
1. Derate linearly above 55°C free air temperature at a rate of 3.8 mW/ °C. Proper application of the derating factors will prevent IC junction
2. Derate linearly above a free-air temperature of 70°C at a rate of 2.3 mW/ °C. A significant amount of power may be dissipated in the HCPL-4100
3. Derate linearly above 55°C free-air temperature at a rate of 5.1 mW/ °C.
4. The maximum current that will flow into the output in the mark state (I
5. The device is considered a two terminal device, pins 1, 2, 3, and 4 are connected together, and pins 5, 6, 7, and 8 are connected together.
6. The t
7. The t
8. The rise time, t
9. The fall time, t
temperatures from exceeding 125°C for ambient temperatures up to 85°C.
output circuit during the transition from the SPACE state to the MARK state when driving a data line or capacitive load (C
dissipation during the transition can be estimated from the following equation which assumes a linear discharge of a capacitive load: P = I
+ V
applications driving twisted pair data lines with NRZ data as shown in Figure 12, the transition time will be less than 10% of one bit time.
short circuit shall not exceed 10 ms.
the output pulse.
the output pulse.
V
V
second (leakage detection current limit, I
3.0
2.8
2.6
2.4
2.2
2.0
1.8
1.6
1.4
1.2
CM
CM
, that can be sustained with the output in a Space (“L”) state (i.e., I
MO
, that can be sustained with the output in a Mark (“H”) state (i.e., I
PLH
PHL
-40
)/2, where V
propagation delay is measured from the 1.3 volt level on the leading edge of the input pulse to the 10 mA level on the leading edge of
propagation delay is measured from the 1.3 volt level on the trailing edge of the input pulse to the 10 mA level on the trailing edge of
20 mA
12 mA
2 mA
-20
I
O
T
A
f
– TEMPERATURE – °C
, is measured from the 90% to the 10% level on the falling edge of the output current pulse.
r
, is measured from the 10% to the 90% level on the rising edge of the output current pulse.
0
SO
is the output voltage in the SPACE state. The duration of this transition can be estimated as t = C
20
40
V
60
V
CC
I
= 2 V
= 5 V
80
100
i-o
≤ 5 μA).
Figure 4. Typical Output Voltage vs. Loop Cur-
rent.
3.5
3.0
2.5
2.0
1.5
1.0
0.5
0
0
5
I
O
– OUTPUT CURRENT – mA
10
O
O
> 12 mA).
< 3 mA).
SC
15
) is internally limited to protect the device. The duration of the output
V
V
T
A
CC
I
= 2 V
= 25 °C
20
= 5 V
25
CM
CM
/dt on the leading edge of the common mode pulse,
30
/dt on the leading edge of the common mode pulse,
Figure 5. Typical Space State Output Current vs.
Temperature.
1.0
1.3
1.2
1.1
0.9
0.8
0.7
0.6
-40
27 V
20 V
V
-20
O
T
A
– TEMPERATURE – °C
OUT
0
(V
OUT
20
SO
). The average power
- V
MO
40
)/I
V
V
SC
60
CC
I
. For typical
= 0.8 V
= 5 V
80
SC
(V
100
SO