INPUTS AND OUTPUTS OF COMPRESSOR CONTROL SYSTEM

INPUTS AND OUTPUTS OF COMPRESSOR CONTROL SYSTEM

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INPUTS AND OUTPUTS OF COMPRESSOR CONTROL SYSTEM

Speed Inputs

The CCS can accept one, two or three speed inputs. Each speed input is monitored by two module’s. With six possible speed signals from which to control with, the CCS can withstand multiple speed input failures with no loss of control functionality. Only one of the possible six inputs is required for speed control. The control can accept a ‘slow speed’ detect probe on channel 4 which can be unique or different from the other speed signals.
All speed inputs are connected to the control, via termination modules (FTMs). An inputs termination module is
used to terminate customer control wiring and distribute each input signal to the two module’s. After the control receives their input values, the Application Software Redundancy Manager then compares each module’s voted
result to select a value to be used within the application logic.
A speed input signal is determined to be faulty and is taken out of the input voting logic when it is below its “Speed Failure Level” setting. This failure level setting is common to all inputs and can be adjusted via de CCT program’s Service mode.
An input deviation alarm is also used to annunciate if any of the three possible speed input channels is sensing a value that is different than the voted-good value used by the application. If an input channel’s sensed value deviates from the voted-good signal value, by a greater margin than the speed control’s “Max Deviation” setting, an input channel alarm will be issued.
This type of annunciation can be used to indicate when an input channel, or magnetic pickup unit is intermittently failing high or low. Max Deviation input settings are tunable via the CCT program’s Service mode, and are defaulted to 1% (deviation range = 0.01 to 20%) of the “Overspeed Limit” setting. If a deviation alarm condition occurs, the alarmed input is not removed from the control’s voting logic and still can be used to control with, in case all other channels fail.

Analog Inputs

The control can accept one or two transducer inputs for all critical parameters (ext/adm, aux, casc inputs). Only one input signal is accepted for non-critical functions (remote setpoint inputs). Each analgo input can withstand one failure with no loss of control functionality. If any of an analog input’s two “legs” are failed, the control uses the second healthy leg’s sensed input signal from which to control with.
All analog inputs are connected to the control, via field termination modules (FTMs). An input’s termination module is used to terminate customer control wiring and distribute each input signal to all two modules. After the control’s modules double exchange their input values, and vote out any erroneous values, the Application Software Redundancy Manager then compares each module’s voted result to select a value to be used within the application logic.
Optionally, each leg of an input channel can be tested and its calibration verified through the CCT program’s Service mode, by individually removing the other input leg.
An analog input signal is determined to be faulty when it is below its “Fail Low Value” setting, or above its “Fail High Value” setting. These failure level settings can be adjusted via the CCT program’s Service mode and are defaulted to values in engineering units which correspond to 2mA and 22mA respectively. If an input is determined to be failed, that input is removed from the control’s voting logic.

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OVERVIEW AND CONTROL HARDWARE FOR COMPRESSOR CONTROL SYSTEM

OVERVIEW AND CONTROL HARDWARE FOR COMPRESSOR CONTROL SYSTEM


The integrated control system includes a compressor control system (CCS) incorporated on the MicroNet Plus.
SYSTEM OVERVIEW
The CCS includes the following functionalities:
• Controlled and Emergency shutdown
• Performance Control.
• Surge map
• Surge Prevention
• Surge detection
• Boost
• Surge Counter
• Surge Control
SYSTEM ARCHITECTURE
The full architecture of the CCS system can be found in the System Architecture Drawings. This overview displays the location of each PDW and CCS control systems and where they connect to.
The CCS control can be operated by hardwired signals, ModBus RS-485 communication, or through an HMI PDW. When
connected with ModBus to a DCS system the DCS can perform actions such as start, stop, reset, raise/lower setpoint and emergency shutdown.

Control hardware

The CCS consists of the following components:
System Cabinet
·        System chassis
·        Power Supply modules
·        CPU module
·        48/24 Discrete Combo Module
·        24/8 Analog module
·        Analog Combo module
·        Network Switch (Cisco IE3000)
·        Power Supply (24VDC)
·        Marshalling Cabinet
·        Discrete Field Termination module
·        Analog Combo Field Termination module
·        Analog High density Field Termination module
·        HART Multiplexer

Basic control system functions

The MicroNet Plus control is a 32-bit microprocessor-based digital controllers that is programmable for many
types of applications in the control of:
• Gas and Steam Turbines
• Gas and Diesel Engines
• Hydro Turbines
• Compressors
The MicroNet Controls family provides a flexible system to control any prime mover and its associated processes.
Dedicated inputs and outputs (I/O) are available onboard for key control signals while distributed I/O can be used for other less critical parameters.
Communications with the MicroNet platform are available to program and service the control as well as to interface with other systems (Plant DCS, HMI, etc.). Application code is generated by use of Woodward’s GAP program or Woodward’s Ladder Logic programming environment. A service interface allows the user to view and tune system variables. Several tools are available to provide this interface.
Communication protocols such as TCP/IP, OPC, Modbus, and other current designs are included so that the user can correctly interface the control to existing or new plant level systems.

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