GE DS200UCPBG6AFB Mark V Turbine Control I/O Engine CPU Board
GE DS200UCPBG6AFB Mark V Turbine Control I/O Engine CPU Board
GE DS200UCPBG6AFB Mark V Turbine Control I/O Engine CPU Board
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GE DS200UCPBG6AFB Mark V Turbine Control I/O Engine CPU Board

  • Manufacturer: GE Fanuc

  • Part Number: DS200UCPBG6AFB

  • Condition:New with Original Package

  • Product Type: CPU Processors

  • Country of Origin: USA

  • Payment:T/T, Western Union

  • Shipping port: Xiamen

  • Warranty: 12 months

GE DS200UCPBG6AFB Mark V Turbine Control Board

The GE DS200UCPBG6AFB serves as the primary DS200UCPB I/O Engine CPU Board utilized to execute real-time data processing across Mark V Turbine Control Systems platforms. The hardware processes discrete and analog operational parameters through a 32-bit RISC core, maintaining synchronized turbine velocity and fuel loop regulation. It uses an integrated multi-protocol interface network to convert raw sensor inputs into actionable control register words without modifying host backplane scan timing.

Hardware Specifications

Parameter Specification
Model DS200UCPBG6AFB
Brand GE
Origin USA
Weight 2.0 kg
Dimensions 309 mm x 211 mm x 41 mm
Operating Temp -40 to +70 deg C
Storage Temp -40 to +85 deg C
Power Consumption +5 VDC Logic Supply, 24 VDC Input Voltage
Processor Type 32-bit RISC Core
Memory Subsystem Onboard PROM with DIMM Expansion Support
Local Interfaces RS-232 Serial Port, Ethernet Port
Network Protocols ARCNET Integration, TCP/IP
Relative Humidity 5-95% Non-condensing

Deterministic Network Routing and Firmware Flash Synchronization

The board manages local I/O density scaling through separate internal pipelines assigned to Ethernet, RS-232, and legacy ARCNET structures. It features a built-in firmware flash compatibility layer that protects the core PROM sequence during remote update operations, avoiding data corruption risks. The dedicated 32-bit hardware processor guarantees stable backplane bus communication velocity regardless of network loading variables. This processing independence prevents memory synchronization delays and isolates local diagnostic scanning routines from primary execution loops during hot-standby system turnovers.

Frequently Asked Questions

Q: How does the memory subsystem handle validation checks during a hot-standby system transition?

A: The board performs continuous synchronization verification across the network interface. The 32-bit RISC processor runs background hardware parity checks on the onboard PROM and DIMM memory expansion boards, enabling a transition latency below standard limits if a primary processor failure occurs.

Q: What are the backplane current draw restrictions on the +5 VDC and 24 VDC rails?

A: The card isolates logic and field distribution circuits to maintain signal integrity. The logic sub-circuit draws current exclusively from the stabilized +5 VDC backplane rail, while secondary communication line drivers and external interfaces use the 24 VDC input feed to prevent internal power interruptions during network cable faults.

Field Installation Guidelines

  • Anti-Static Seating Procedures: Use a grounded ESD wrist strap before handling the circuit assembly. Insert the plug-in module firmly into the designated rack slot to ensure that all backplane multi-pin connections seat completely and uniformly.
  • Conduit and Shield Separation Requirements: Route the Ethernet and ARCNET network cables through separate dedicated metal conduits. Keep a minimum space of 300 mm from high-voltage turbine ignition or generator excitation cables to prevent noise from corrupting data.
  • DIMM Memory Installation Inspection: Verify that any extra memory boards seat properly in their DIMM sockets and that the side mechanical retention clips click into place. Loose memory cards can trigger diagnostic errors during high-vibration turbine startup phases.
  • Passive Heat Dissipation Management: Check that adjacent card slots do not impede natural airflow through the rack assembly. The board depends on unrestricted vertical convection currents to stabilize internal component temperatures within the -40 to +70 deg C operating range.
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