AUTOMATIC TURBINE RUN UP SYSTEM.ppt

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    AUTOMATIC TURBINE RUNUP SYSTEM(ATRS)

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    Presentation outline

    Overview of Plant Controls

    Functions of ATRS

    Structure of ATRSProgram Structure of ATRS and

    Turbine protection

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    MAN-MACHINE-INTERFACE

    OPERATOR

    INSTRUMENTATION & CONTROL

    PLANT

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    POWER PLANTCONTROLUNIT CONTROL

    BOILER TURBINE GENERATOR

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    MEASUREMENT

    CLOSE-LOOP

    CONTROL

    OPEN-LOOP

    CONTROL

    PROTECTION

    MONITORING

    INSTRUMENTATION

    ANDCONTROL

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    ADVANTAGES OF AUTOMATION OPERATING PERSONNEL FREED FROM ROUTINE TASKS.

    INCORRECT INTERVENTIONS IN THE PROCESS AVOIDED.

    STRESS ON EQUIPMENT REDUCED.

    PLANT OPERATIONS GEARED FOR MAXIMUM

    EFFICIENCY.

    INCIPIENT FAULTS RECOGNISED QUICKLY.

    ON FAULT OCCURRENCE, IMMEDIATE AND LOGICAL

    INTERVENTION POSSIBLE.

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    A. CONTROL SYSTEM:

    ANALOG(CLOSE LOOP)

    - ELECTROHYDRAULIC CONTROLLER (EHC)

    - TURBINE STRESS EVALUATOR (TSE)

    - LOW PRESSURE BYPASS CONTROLLER (LPBPC)

    - GLAND STEAM PRESSURE CONTROLLER (GSPC)

    BINARY(OPEN LOOP)

    - AUTOMATIC TURBINE RUN UP SYSTEM (ATRS)

    - AUTOMATIC TURBINE TESTER (ATT)

    B. MONITORING & MEASUREMENT SYSTEM

    - TURBINE SUPERVISORY INSTRUMENTATION (TSI)

    - MEASURMENT OF PARAMETERS LIKE, TEMP.,PRESS.,LEVEL etc.

    C. PROTECTION SYSTEM

    TURBINE C&I PACKAGE CONSISTS OF THE FOLLOWING SYSTEMS:

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    HIERARCHY OF CONTROL

    UNIT

    CONTROL

    GROUP CONTROL(WHEN, HOW MANY,WHICH)

    SUB-GROUP CONTRL-1 SUB-GROUP CONTRL-2

    CONTROL INTERFACE

    SWITCH GEAR (MCC)

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    CONCEPT OF C I IN THERMAL POWERSTATION

    UNIT CONTROL

    CLOSEDLOOP

    CONTROL

    FUNCTIONALGROUP

    CONTROL

    PROT-IVE

    LOGICS

    DATA PROCESS-ING, ALARM

    ANNUNCIATION

    SIGNAL

    CONDITIONING

    ALALOG, BINARY

    CONTROL INTERFACE

    MOTOR CONTROL CENTRE

    SWITCH GEAR

    M M DRIVESSIGNAL TRANSMITTER

    ANALOG AND

    BINARY

    SIGNALS

    CRT /MMI DISPLAY UNIT IN

    OWS

    LOGSCONTROL

    ROOM

    AUTOMATION

    EQUIPMENT

    PLANT INTERFACE

    EQUIPMENT

    PLANT (FIELD)

    OPERATOR

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    AUTOMATIC TURBINE RUN-UP SYSTEMTASKS PERFORMED:

    SWIFT,ACCURATE AND OPTIMUM STARTUP ( INCLUDING

    SYNCHRONISATION AND LOADINING) OF TURBINE

    MAINTAINING OIL SUPPLY

    BUILDING UP AND MAINTENANCE OF VACUUM

    FEATURES : BASED ON FUNCTIONAL GROUP CONTROL PHILOSOPHY

    EACH FUNCTIONAL GROUP ORGANISED AND ARRANGED IN SUB-GROUP

    CONTROL, SUB-LOOP CONTROL, AND CONTROL INTERFACE

    OPERATING MODES AVAILABLE:

    - MANUAL MODE ( OPERATOR GUIDE)- AUTOMATIC MODE

    - STEP BY STEP MODE

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    ATRS

    STRUCTUREOIL SYSTEM, VACUUM SYSTEM, TURBINE etc.

    GC

    SGC SGC

    SLC SLCSLC

    CI

    SGC

    CI

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    GROUP CONTROL: Decides WHEN, HOW MANY & WHICH

    SGC shall be operating and stopped.

    SUB GROUP CONTROL: Contains the sequential logics for

    switching drives ON and OFF. Perform sequence in STEPS, issue

    commands and get Checkbacks.

    SUB LOOP CONTROL: can be switched ON & OFF manually.Receive commands from GC, SGC and also Manual

    CONTROL INTERFACE: Standard Interface between the command

    transmitters and receivers in the plant, undertakes all necessary signal

    processing and monitoring.

    SYSTEM OPERATION MODES:

    AUTOMATIC,SEMI AUTOMATIC,OPERATOR GUIDE

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    ADVANTAGES OF ATRS

    ELIMINATES HUMAN ERROR PROVIDES MAXIMUM PROTECTION AGAINST MALFUNCTIONS

    OPERATORS TASK LESS ARDUOUS

    ENABLES SAFE, SMOOTH, STRESS CONSISTANT AND OPTIMUM

    WARM-UP, ROLLING AND SYNCHRONISATION OF TURBINE IN

    LEAST POSSIBLE TIME

    INCREASES PLANT AVAILABILITY

    REDUCES STARTING TIME WITHOUT IMPAIRING LIFE

    MEETS EMERGENCIES AUTOMATICALLY

    ALL PLANT OPERATING CONDITIONS CATERED TO BY

    CRITERIA DEPENDANT PROGRAMMING

    INCREASED OPERATING FLEXIBILITY, SAFETY AND

    RELIABILITY

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    ATRSAUTOMATIC TURBINE RUN UPSYSTEM

    Start up and Shutdown sequence performed inreliable way

    Protect drives and related auxiliaries

    Uniform and sequential information to operator aboutthe process

    Distinct information about the nature and location offaults

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    STEP 01

    STEP 02

    &

    START DRIVE A

    DRIVE A ON

    MONITOR &

    BLOCKING TIME

    MONITOR &BLOCKING TIME

    OPEN DMPR A

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    AUTOMATIC TURBINE RUN-UP SYSTEMSUB GROUP CONTROL ( SGC):

    SGC executes commands to bring the equipment upto a particular

    defined status.

    The commands are executed in a predefined sequence in the form of

    steps.

    Desired number of criteria act as preconditions before the SGC can

    take off or execute its defined sequence. The functional group continues to function automatically all the time

    demanding enabling criteria based on the process requirements and

    from other FGs, if required.

    In case the desired criteria is not available, the system would

    automatically act in such a manner as to ensure the safety of the mainequipment.

    The sequence is programmed in the processor. The process signals

    are acquired through the input modules and are available on the bus.

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    AUTOMATIC TURBINE RUN-UP SYSTEM

    WAITING AND MONITORING TIME FOR STEPS:

    Waiting Time :

    It implies that the subsequent step will not be executed unless the

    specified time elapses. If no waiting time is specified, the next step

    gets executed as soon as the enabling criteria are fulfilled.

    Monitoring Time :

    It is the time required for executing the command of any step as well

    as the time required for appearance of criteria for the next step.

    Under healthy conditions it should happen within the specified time,

    otherwise an alarm is initiated. Whenever there is uncertainty

    regarding the time required for completing a particular task, such

    as warming-up, pulling vacuum etc., the monitoring time is blocked.

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    PROGRAM STEP OF A SUBGROUPCONTROL

    02

    FROM STEP 1STEP CRITERIA FOR STEP -2

    BYPASS CRITERION

    PROGRAM LOOP

    WAIT

    50s

    MO TIME

    20sCOMMAND

    1

    2

    &

    &

    1

    &

    STEP 2 ( START UP PROGRAM) WITH 2 STEP CRITERIA, 2 COMMAND

    OUTPUTS AND A MONITORING & WAITING TIME .

    WITH ADDITIONAL PROGRAM LOOP CONTROL AND A BYPASS

    CRITERIA FOR STEP 1

    WAITING OR MO TIME CAN BE PROGRAMMED FOR 0.1 SEC TO 999

    MIN.

    NOS. 1-49 USED FOR START-UP, 51 TO 99 FOR SHUTDOWN PROGRAM.

    EXAMPLE

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    AUTOMATIC TURBINE RUN-UP SYSTEM

    WAITING AND MONITORING TIME FOR STEPS:

    ATRS can be switched on at any stage after

    completing certain tasks manually, if so desired. In

    such cases, the SGC program quickly scansthrough the steps and starts executing from the

    stage upto which the tasks have been completed

    manually. This is achieved by incorporating

    suitable overflow /bypass conditions in the logic.

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    AUTOMATIC TURBINE RUN-UP SYSTEM

    ATRS CONTROLS:1. ATRS is organised in the following four Sub-Groups:

    Oil supply

    Evacuation

    Turbine

    HP CONTROLFLUID

    2. SGC issues commands either to the SLC or directly to

    the drive through the Control Interface.

    3. Each of these SGCs has its subordinate SLCs and CI

    modules. These SGCs in conjunction with the turbinegoverning system , TSE and the auto-synchroniseraccomplish the function of start-up of the TG set.

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    AUTOMATIC TURBINE RUN-UP SYSTEM

    SUB-LOOP CONTROL (SLC) :

    A SLC, when switched on, actuates the equipment and brings it to thedesired status as demanded by the process and there is no sequence logic

    involved in it.

    SLC is like a watch-dog performing an assigned duty.

    All mechanical equipment which need to be switched on/off based on

    process consideration are hooked-up in various SLCs. Standby equipment

    is also interlocked in SLCs.

    SLC can be switched on either manually or through SGC and issues

    commands to the drive control level.

    SLC logic is also realised in the processor module.

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    AUTOMATIC TURBINE RUN-UP SYSTEM

    CONTROL INTERFACE (CI) :

    Each remote controlled drive has a dedicated CI module which acts as

    a standard interface between the transmitters and receivers in the plant

    and undertakes all necessary signal processing and monitoring.

    The CI module receives manual commands from the process

    keyboard/inserts, active protection signals and enabling signals from

    the protective logic, as well as automatic control commands from the

    SGC/SLC. It interlocks the input commands according to their priority and

    validity and then passes actuation signals to the interposing relays in

    the switch-gear.

    The status checkbacks received from the switchgear or actuators are

    monitored, processed and transmitted to VDU/desk tiles, the protective

    logic and the SGC.

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    AUTOMATIC TURBINE RUN-UP SYSTEM

    CONTROL INTERFACE (CI) : (Continue--)

    These modules have the firmware which defines the standard

    function of the module and its signalisation mode as well as the

    programmable logic for the drive protection and the permissive

    interlocks. The drive level automation tasks related to the respective

    drive is realised through the programmable logic.

    The module has hardwired inputs and outputs for connection of

    feedback signals and commands to the switchgear together with local

    bus interface for signal exchange via the system bus.

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    AUTOMATIC TURBINE RUN-UP SYSTEM

    ATRS STRUCTURAL SYSTEM:

    ATRS IS ORGANISED IN THREE SGCs :

    1. SGC-TURBINE :

    SGC Turbine acts directly on the following systems :

    Sub-loop Control (SLC) Drains.

    Warm up Controller.

    Starting Device of turbine governing system.

    Speed & Load Setpoint devices of turbinegoverning

    system.

    Auto-synchroniser.

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    AUTOMATIC TURBINE RUN-UP SYSTEM

    ATRS STRUCTURAL SYSTEM:

    2. SGC-OIL SUPPLY :

    SGC oil supply directly acts on the following system :

    Sub-loop control (SLC) turning gear.

    SLC auxiliary oil pump 1.

    SLC auxiliary oil pump 2.

    SLC emergency oil pump.

    SLC jacking oil pump.

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    AUTOMATIC TURBINE RUN-UP SYSTEM

    ATRS STRUCTURAL SYSTEM:

    3. SGC-CONDENSATE & EVACUATION :

    SGC- Condensate & Evacuation directly acts on the following systems :

    Sub-loop Control (SLC) condensate extraction

    pumps.

    Starting ejector, if provided.

    Main ejectors / vacuum pumps (as applicable). Vacuum breaker.

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    AUTOMATIC TURBINE RUN-UP SYSTEM

    ATRS STRUCTURAL SYSTEM:

    3. SGC-HPCF :

    SGC- HPCF acts on the foll :

    Sub-loop Control (SLC) HPCF

    SLC HPCF pumps

    HPCF pumps

    HPCF re-circulation pumps

    LPCF temp control valve

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    AUTOMATIC TURBINE RUN-UP SYSTEM

    3. SGC-HPCF :

    Both CF PUMPS GET SWITCHED ONTHRU SLC. IN CASE

    RUNNING PUMP DOES NOT DEVELOP THE REQUIREDPRESS, THE STANDBY PUMP GETS SWITCHED ON

    AFTER GETTING THE REQUIRED CF PRESS SLC

    HEATING IS PUT ON & CF CIRCULATION PUMP WHICH

    FEEDS THE REGENERATION CKT IS ALSO PUT ON.

    TEMP CONTOL VLV IS PUT IN AUTO MODE TOREGULATE THE TEMP.

    CF TEMP IN THE TANK IS MAINTAINED BETWEEN 55 TO

    57 C BY SWITCHING ON/OFF THE CF HEATER THRU

    THE SLC. IN CASE CF TEMP IN HTR EXCEEDS > 65 C

    THE HEATER IS SWITCHED OFF IN SHUTDOWN PROG ALL THE PUMPS ARE SWITCHED

    OFF AND SLC IS PUT OFF. SLC HEATING IS KEPT ON TO

    MAINTAIN THE TEMP REQUIRED FOR THE NEXTSTARTUP.

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    TURBINE START-UP / SHUT-DOWN CONTROL,

    OVERVIEW

    SUB-GROUP ( TURBINE START-UP / SHUT-DOWN)

    SUBLOOP

    DRAIN

    VALVE

    SUBLOOP

    LP-WATER

    INJECTION

    MECHANICAL

    HYDRAULIC

    CONTROL(MHC)

    ELECTRO-

    HYDRAULIC

    CONTROL(EHC)

    SEAL

    STEAM

    CONTROL(SSC)

    TURBINE

    TRIP

    SYSTEM(TTS)

    TURBINE

    STRESS

    EVALUATOR

    LP WATER

    INJECTION

    AUTOMATIC

    SYNCHRONIZER

    DRAIN

    VALVES

    GENERATOR

    MAIN CKT.

    BREAKER

    THYRISTOR

    VOLTAGE

    REGULATOR(TVR)

    CRITERIA

    CRITERIA

    AUTO-ON/OFF

    AUTO

    ON/OFF

    AUTOON/OFF

    MANUAL

    ON/OFF

    MANUALON/OFF

    MANUALOPEN/CLOSE

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    SGC-DISPLAY4 6 8 7 5

    1

    3

    2

    1. PUSHBUTTON SHUTDOWN

    2.PUSHBUTTON STARTUP OR OPERATION

    3.PUSHBUTTON AUTOMATIC ON/OFF

    4.LAMP SHUTDOWN PROGRAM5.LAMP STARTUP OR OPERATION PROGRAM

    6.LAMP AUTOMATIC OFF

    7.LAMP AUTOMATIC ON

    8.LAMP FAULT

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    SLC-DISPLAY2 3 4

    1. PUSHBUTTON MANUAL ON/OFF

    2.LAMP SLC OFF

    3.LAMP FAULT

    4.LAMP SLC ON

    1

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    DRIVE INTERFACE-DISPLAY3 4 5

    1. PUSHBUTTON OFF (CLOSE)

    2. PUSHBUTTON ON (OPEN)

    3. LAMP OFF (CLOSE)

    4. LAMP FAULT

    5. LAMP ON (OPEN)

    1 2

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    PROTECTION SYSTEMFOR

    STEAM TURBINE

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    TURBINE PROTECTION SYSTEM

    TASK PERFORMED:

    PROTECTS TURBOSET FROM INADMISSIBLE OPERATING

    CONDITIONS

    PREVENTS DAMAGE IN CASE OF PLANT FAILURE

    FAILURE OCCURRENCE REDUCED TO MINIMUM

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    TURBINE PROTECTION SYSTEM

    ADVANTAGES:

    DETECTION OF UNIT IRREGULARITIES

    PREVENTION OF UNIT OVERSTRESSING DUE TO TRIPS

    RELIEF OF OPERATING PERSONNEL FROM QUICK AND

    CORRECT DECISION TAKING

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    TURBINE PROTECTION SYSTEM

    HYDRAULIC

    TRIP SYSTEMELECTRICAL

    TRIP SYSTEMEXTENDED

    TURBINE PROT.PROT. CRITERIA

    FROM OTHER AREA

    - OVER SPEED

    TRIP DEVICE1/2

    - VACUUM TRIPDEVICE

    - HAND TRIPLEVER(LOCAL)1/2

    - MANUAL

    REMOTE TRIP( UCB)

    - LOW VACUUM

    TRIP

    - LOW LUBE OIL

    - FIRE PROT.

    TRIP-BRG METAL

    TEMP

    -AXIAL SHIFT

    -HP/IP TOP/BOT

    DIFF TEMP HI

    - LP EXH. STM.

    TEMP. > MAX

    -GENERATOR

    PROTECTION

    - MASTER FUEL

    TRIP RELAY

    ENERGISED

    - BOILERPROTECTION

    OPTD.

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    TURBINE PROTECTION SYSTEMGENERAL :

    The electrical trip system comprises of two identical and independent

    relay based trip channels viz. electrical trip channels 1 & 2.

    Both channels are connected to different (two) trip solenoid valves.

    All command signals for turbine trip are hooked up with both the

    channels.

    Actuation of any of the channels energises the respective trip solenoid

    which in turn trips the turbine.

    Each channel is realized in a local bus. Both the local buses are

    completely independent of each other and input modules, processor

    module and output modules reside on each.

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    TURBINE PROTECTION SYSTEMGENERAL :

    Trip signals from the sensors / field instruments are conditioned anddistributed to both the channels (local buses) via hardwired modules.

    Realisation of 2 out of 3 trip logic is carried out in the local bus. On

    detection of a fault in any one of the input signals to a channel, the

    configuration for that channel changes from 2 out of 3 to 1 out of 2 and is

    annunciated. Further failure in a channel changes the configuration to 1out of 1.

    Trip signal from each of the local buses acts on 3 relays in 2 out of 3

    combination.

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    TURBINE PROTECTION SYSTEMCYCLIC TEST:

    Both the channels are tested periodically, even while the turbine isrunning.

    Cyclic testing is done automatically at preset intervals and can be

    blocked from the protection cabinet, if desired.

    This testing can also be initiated manually from the cabinet.

    Only one channel can be tested at a time. Online testing is done by

    simulating the trip signals and it determines faults in the input modules,

    processor modules, output modules or the trip relays.

    These faults can be acknowledged from the cabinet. Next cycle test can

    only be carried out after acknowledging the fault.

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    TURBINE PROTECTION SYSTEM

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    TURBINE PROTECTION SYSTEMTRIPPING CRITERIA:

    1. CONDENSER VACUUM VERY LOW :

    This is a back up protection to the hydraulic low vacuum trip

    device.

    The protection acts if absolute pressure in the condenser rises

    above 0.3 Kg/cm2 (abs).

    2. LUBE OIL PRESSURE LOW :

    The protection acts if the lube oil pressure before thrust bearing

    decreases to 1.2Kg/cm2 .

    The trip signal is initiated by three pressure transmitters in 2-out-of-3-

    logic.

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    TURBINE PROTECTION SYSTEMTRIPPING CRITERIA:

    3. FIRE PROTECTION :

    The protection acts in the event of any of the following

    conditions :

    i) Fire protection switch, either in unit control

    room or in

    machine hall, operated.

    ii) Level in main oil tank falls to a very low value,

    indicating

    substantial leakage of oil from the system.

    The command signal under condition (ii) is initiated from

    three level transmitters in 2-out-of-3 logic cofiguration.

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    TURBINE PROTECTION SYSTEMTRIPPING CRITERIA:

    4. HP EXHAUST STEAM TEMPERATURE HIGH :

    The HP exhaust steam temperature protection circuit causes the exhaust

    sections of the turbine, the blading and the extraction points against

    overheating.

    Under extreme operating conditions the HP turbine can be run at low flow rate

    and simultaneous relatively high back pressure. This prevents the steam from

    expanding, which causes the exhaust steam temperature to rise ( > 5000C).

    The temperature is measured by means of three thermocouples and protection

    criteria is derived in 2 out of 3 logic.

    TURBINE PROTECTION SYSTEM

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    TURBINE PROTECTION SYSTEMTRIPPING CRITERIA:

    5. TURBINE TRIP SWITCH OPERATED :

    The protection acts when the turbine trip switch in unit control room

    is operated manually.

    6. TRIP COMMAND INITIATED FROM ATRS :

    The protection acts when the trip command signal is initiated from

    the Automatic Turbine Run-up System .

    TURBINE PROTECTION SYSTEM

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    TURBINE PROTECTION SYSTEMTRIPPING CRITERIA:

    7. GEN. PROTECTION OR MFT- RELAY ENERGISED :

    In the event of generator faults under Class-B trip both the turbine trip

    channels are actuated to trip the turbine. In such a case the generator

    protection acts through Reverse Power Relays.

    In the event of generator faults under Class-A trip or in the event of boiler

    "Master fuel trip relay" energised, command signal for turbine trip shall

    act simultaneously and independent of other equipment trip out sequence.

    8. OPERATION OF REVERSE POWER RELAY :

    The command signal is initiated with a time delay of 10 seconds after any of

    the two reverse power relays have operated.

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    THANK YOU