The Allen-Bradley 1771-P6R/C, also cataloged as the 1771-P6R Redundant Power Supply Module, operates as a dedicated hardware component for converting AC input into regulated 5 VDC backplane power within 1771 PLC-5 I/O System platforms.
| Parameter | Specification |
|---|---|
| Model | 1771-P6R/C |
| Brand | Allen-Bradley |
| Origin | United States |
| Module Type | Redundant Power Supply Module |
| Nominal Input Voltage | 220 VAC |
| Input Voltage Range | 194-264 Volts AC |
| Input Frequency | 47-63 Hz |
| Input Current | 0.5 A |
| Output Voltage | +5 VDC regulated |
| Backplane Output Current | 8 A (single unit) |
| Max Real Input Power | 59 W |
| Max Apparent Input Power | 92 VA |
| Max Transformer Load | 148 VA |
| Power Dissipation | 16 W maximum |
| Thermal Dissipation | 47.8 BTU/hr maximum |
| Isolation Voltage | 1000 V for 60 seconds |
| Fuse Protection | 1.5 A, 250 V, slow-blow |
| Wire Size | 14 AWG stranded copper, rated 85 deg C or greater |
| Location | 1771 Chassis, 1 Slot |
| Operating Temp | 0 to 60 deg C |
| Power Consumption | 59 W |
| Dimensions | 165 x 51 x 89 mm |
| Weight | 0.9 kg (1.98 lbs) |
The 1771-P6R/C supplies an 8 A current threshold to the 5 VDC backplane to secure data integrity across network architectures that utilize Profinet or EtherNet/IP deterministic networks. During periods of maximum I/O density scaling, the demand on the backplane bus communication velocity increases significantly. This module maintains strict voltage regulation under changing system loads, ensuring that the necessary firmware flash compatibility profiles across adjacent communication and processor modules remain stable without inducing power-related logic failures.
Q: How do the current capacities scale when combining multiple 1771-P6R/C modules in a redundant architecture?
A: In configured multi-unit setups, a 2-unit system delivers 8 A at 60 deg C, a 3-unit system scales up to 14 A, and a 4-unit system supports up to 20 A of backplane current capacity.
Q: Is hot-swapping permitted for a faulty 1771-P6R/C module inside an active redundant system?
A: No. The backplane architecture requires the local rack or the specific slot power supply source to be isolated and de-energized prior to structural extraction. Removing the unit while under active load hazards introducing transient backplane communication errors.
Q: What cabling is necessary to link the units for true redundant power balancing?
A: Redundant configurations require the dedicated redundancy cable interface (Allen-Bradley Part No. 941201-02) to verify cross-unit electrical balance and fault detection.
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