ABB IS215ACLEH1BB ACLE Application Control Layer Module,

IS215ACLEH1BB (ACLE‑H1‑BB) is 6U single‑slot VME‑bus application control layer processor board for GE Speedtronic Mark VI turbine‑generator control system and EX2100 excitation control systemABB DCS HE…. It is BB hardware revision of ACLE module, executing high‑level application control logic, algorithm calculation and multi‑protocol external communication functions. Supports simplex, dual and TMR triple‑modular‑redundant architecture. Responsible for turbine sequence control, excitation regulation logic and human‑machine interface data interaction. Hardware fault may result in application logic abort, communication loss or unit trip. Product status: Obsolete, spare‑part only supply available。

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Description

Hardware & Electrical Specifications

‑ Model:IS215ACLEH1BB ‑ Part Number:IS215ACLEH1BB ‑ Module Type:ACLE Application Control Layer Module ‑ Mounting:6U single‑slot VME rack installation ‑ Power supply:+5 VDC, ±12 VDC powered via VME backplane ‑ On‑board memory:Flash memory for firmware storage; SDRAM for runtime logic execution ‑ Processor:High‑performance embedded real‑time CPU for turbine application algorithm ‑ Communication interfaces:   • Dual 10/100 Mbps RJ45 Ethernet ports (Modbus TCP, SRTP, CIMPLICITY protocol)   • Two serial COM ports (RS‑232/RS‑485 configurable) for local diagnosis and third‑party device connection   • Internal VME bus interface for data exchange with other VME processor boards ‑ PCB treatment:BB‑revision conformal coated for dust‑moisture‑corrosion resistance ‑ On‑board protection:ESD protection, MOV surge suppression, watchdog self‑monitor circuit, firmware integrity check, communication link fault detection ‑ Compatibility note:Cannot run standalone; must match Mark VI VME rack and related processor boards; full logic‑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 / excitation cabinet ‑ EMC compliance:IEC 61000‑6‑2 ‑ Certifications:CE

Mechanical Data

‑ Weight:approx 0.48 kg ‑ Dimension:280 mm × 160 mm × 25 mm (6U VME standard form‑factor) ‑ Handling note:ESD‑sensitive PCB; real‑time control logic circuit, anti‑static wrist‑strap mandatory during handling ‑ Terminal tightening torque:0.6‑1.0 N·m

Main Functions

  1. Run turbine‑specific application control logic, perform sequence control, load‑setpoint calculation and auxiliary interlock logic processing for Mark VI / EX2100 system.
  2. Provide multi‑protocol external communication interface, realize data interaction with HMI workstation, DCS system and third‑party field devices.
  3. Exchange real‑time process data with VSVO, VTUR, VVIB and other VME I/O processor boards through VME backplane bus.
  4. Store trend data, event log and alarm records; support local serial port debugging and firmware download.
  5. On‑board self‑diagnosis: detect watchdog timeout, firmware check‑sum error, VME‑bus communication abnormality, Ethernet and serial‑port link failure; upload fault alarm to turbine main controller.
  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, check communication link status, perform application logic verification test before commissioning.
  6. Replacement note: For TMR triple‑redundant system application, hardware consistency and firmware version matching of related redundant boards shall be verified; full logic‑loop simulation test mandatory before unit put‑into‑service.

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