GE IS215UCVEH2AB UCV Control VME Processor Board

IS215UCVEH2AB (UCVE‑H2‑AB) is 6U VME‑bus main control processor board for GE Speedtronic Mark VI turbine‑generator control system. It is the core single‑board computer running turbine real‑time application software under QNX real‑time multitasking operating system. It exchanges data with VME I/O boards via VME backplane bus, and provides external communication interfaces for HMI, DCS and engineering workstation. Supports simplex, duplex and TMR triple‑modular‑redundant configuration. Critical main controller; hardware fault will result in loss of turbine control, unit shutdown or trip. Product status: Obsolete, spare‑part only supply available。

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Description

Hardware & Electrical Specifications

  • Model:IS215UCVEH2AB
  • Part Number:IS215UCVEH2AB
  • Module Type:UCV Control VME Processor Board
  • Mounting:6U single‑slot VME rack installation
  • Power supply:+5 VDC, ±12 VDC powered via VME backplane
  • Operating System:QNX real‑time multi‑tasking OS
  • Memory:SDRAM for runtime execution; Flash memory for firmware and application program storage
  • Communication interfaces:   • Dual 10/100 Mbps Ethernet ports for HMI, SRTP, Modbus TCP communication   • Two serial COM ports (RS‑232 configurable) for local debug and third‑party device connection   • VME bus interface for internal high‑speed data exchange with other I/O processor boards
  • Processing performance:Up to 100 000 logic blocks execution per second
  • PCB treatment:AB‑revision conformal coated for dust‑moisture‑corrosion resistance
  • On‑board protection:ESD protection, MOV surge suppression, watchdog self‑monitor circuit, firmware check‑sum verification, communication link fault detection
  • Compatibility note:Cannot run standalone; must match Mark VI VME rack and related I/O boards; full control‑loop simulation test mandatory after replacement.

Environmental Specifications

  • Operating temperature:‑20 ℃ ~ +60 ℃
  • Storage temperature:‑40 ℃ ~ +85 ℃
  • Relative humidity:5%‑95% non‑condensing
  • Installation location:Indoor turbine control cabinet
  • EMC compliance:IEC 61000‑6‑2
  • Certifications:CE

Mechanical Data

  • Weight:approx 1.2 kg
  • Dimension:280 mm × 160 mm × 25 mm (6U VME standard form‑factor)
  • Handling note:ESD‑sensitive PCB; real‑time turbine control circuit, anti‑static wrist‑strap mandatory during handling
  • Terminal tightening torque:0.6‑1.0 N·m

Main Functions

  1. Execute core real‑time turbine control algorithms: speed control, load regulation, valve position closed‑loop calculation, protection logic and unit sequence control.
  2. Exchange real‑time process data with VSVO, VTUR, VVIB, VTCC and other VME I/O boards through VME backplane bus.
  3. Provide multi‑protocol external communication for data interaction with operator HMI, engineering workstation and plant DCS system.
  4. Store event log, alarm information and trend data; support local serial port for firmware download and on‑site maintenance debugging.
  5. On‑board self‑diagnosis: detect watchdog timeout, firmware integrity error, VME‑bus communication abnormality, Ethernet and serial‑port link failure; upload fault alarm status.
  6. LED status indication:   ‑ Green LED:Board power supply normal / RUN status   ‑ Yellow LED:Communication port activity indicator   ‑ Red LED:Module FAIL / fault alarm

Installation & Wiring Requirements

  1. Cut off rack power supply before replacement. Hot‑swap is forbidden. Strict anti‑static protection when handling PCB board.
  2. Insert board into designated VME slot, secure panel locking screws; ensure VME backplane contact is reliable.
  3. External Ethernet and serial‑port wiring strictly follow GE Speedtronic Mark VI wiring manual; communication cables adopt shielded twisted‑pair, strictly separated from high‑power cables; connect shielding to dedicated ground terminal.
  4. Complete protective grounding according to GE system specification.
  5. After replacement: verify VME rack power‑on status, download matching firmware and turbine application code, check communication link status, perform full control‑loop commissioning test.
  6. Replacement note: For TMR triple‑redundant system application, hardware consistency and firmware‑version matching of redundant controller boards shall be verified; full control‑loop simulation test mandatory before unit put‑into‑service.

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