Honeywell TC-PRR021 51309288-225 C200 Redundant Relay Module
Honeywell TC-PRR021 51309288-225 C200 Redundant Relay Module
Honeywell TC-PRR021 51309288-225 C200 Redundant Relay Module
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Honeywell TC-PRR021 51309288-225 C200 Redundant Relay Module

  • Manufacturer: HONEYWELL

  • Part Number: TC-PRR021 51309288-225

  • Condition:New with Original Package

  • Product Type: Redundancy Modules

  • Country of Origin: Sweden

  • Payment:T/T, Western Union

  • Shipping port: Xiamen

  • Warranty: 12 months

Honeywell TC-PRR021 C200 Redundancy Module

The Honeywell TC-PRR021, also cataloged as the Honeywell 51309288-225 Redundancy Module, operates as a dedicated hardware component for processor redundancy within Honeywell C200 control system platforms. The hardware monitors the active status of the primary controller execution path and coordinates automatic switchover parameters during an internal fault event. Internal bus transceivers transfer state synchronization parameters across the chassis frame to eliminate interruption of loop signals.

Hardware Specifications

Parameter Specification
Model TC-PRR021
Part Number 51309288-225
Brand Honeywell
Origin USA
Type Redundancy Module / Digital Output Relay Module
Number of Channels 16 relay output channels
Output Type Relay contacts (NO/NC)
Rated Voltage 24 VDC / 120 VAC
Output Current Up to 2 A per channel
Dimensions 267 x 178 x 51 mm
Weight 0.6 kg
Operating Temp -20 to +55 deg C
Power Consumption Powered via Series-A chassis backplane

Process Control and DCS Interface Architecture

The interface circuitry utilizes channel-to-channel and channel-to-system galvanic isolation barriers to prevent loop noise induction between adjacent terminals and the controller backplane. The module hosts 16 independent relay output channels rated at 2 A each, executing digital field control interlocks while running localized diagnostics. Synchronized hardware logic continuously reconciles diagnostic signatures with the central DCS nodes, providing sub-millisecond status updates and driving dedicated LED arrays for instant visual verification of hardware switchover paths.

Frequently Asked Questions

Q: What specific hardware mechanism triggers the changeover from the primary controller to the secondary back-up unit?

A: The module executes real-time system health checks across the C200 backplane. If the primary processor misses a heartbeat interval or flags an internal fault code, the redundant hardware executes an automated switchover to lock the secondary processor into control loop execution.

Q: Can maintenance technicians swap this redundancy module out while the rest of the chassis remains energized?

A: Yes, the unit accommodates standard hot-swap procedures inside the Series-A chassis line. Technicians can extract the faulty module and insert a replacement assembly without dropping power to the surrounding backplane logic blocks.

Q: Does the 2 A current capacity rating on the relay outputs apply across both direct current and alternating current topologies?

A: The relay contact paths tolerate loads up to 2 A per channel at either 24 VDC or 120 VAC operating limits. System engineers must incorporate external interposing relays if the inductive field startup spikes surpass these boundary thresholds.

Field Installation Guidelines

  • Chassis Attachment Actions: Align the plastic alignment ribs with the target slots on the Series-A backplane carrier framework. Push the module forward until the interface pins lock securely into the carrier sockets, then engage the upper and lower mechanical clips.
  • Shield Grounding Methods: Gather all incoming drain wires from shielded command loop cables and clamp them down to the copper grounding bus within the lower marshaling frame. Maintain separation between shield ground lines and safety ground structures.
  • Low-Voltage Cable Partitioning: Route the 24 VDC/120 VAC relay signal bundles through dedicated wire paths separate from analog input loops or communication cables to minimize cross-talk risks.
  • Screw Terminal Connections: Strip back field connection conductors by 7 mm and screw them into the terminal block assembly. Apply a standard verification torque to ensure the contact remains consistent under vibrational strain.
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