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STEAM TURBINE
CONTROL
&
INSTRUMENTATION
STEAM TURBINE TYPE
Conventional Cycle
• 210MW
• 250MW
• 300/350MW
• 500/600MW
Combined Cycle
• MN Series (Dual Pressure)
• HMN Series (Triple Pressure)
Nuclear Turbine
• 500MW
High Pressure Turbine
• 250/270MW
• 660/800 MW (Super Critical)
AIMS OF AUTOMATION
• Improvement in quality of control
• Increase in plant availability
• Increase in plant safety
• Increase in Plant efficiency
• Faster start-up and load change
• Easy handling of the plant
• Avoidance of maloperation
MEASUREMENT
CLOSE-LOOP
CONTROL
OPEN-LOOP
CONTROL
PROTECTION
MONITORING
INSTRUMENTATION
AND
CONTROL
Thermal Cycle in a Power Plant
ST SUBSYSTEMS
A. CONTROL SYSTEM:
ANALOG (CLOSED LOOP)
- ELECTROHYDRAULIC CONTROLLER (EHC)
- LOW PRESSURE BYPASS CONTROLLER (LPBPC)
- GLAND STEAM PRESSURE CONTROLLER (GSPC)
- LUBE OIL/ WARM-UP TEMPERATURE
CONTROLLERS
BINARY (OPEN LOOP)
- AUTOMATIC TURBINE RUN UP SYSTEM (ATRS)
- AUTOMATIC TURBINE TESTER (ATT)
ST - SUBSYSTEMS
B. MONITORING & MEASUREMENT SYSTEM
- TURBINE SUPERVISORY INSTRUMENTATION (TSI)
- TURBINE STRESS EVALUATOR/CONTROLLER (TSE/TSC)
- MEASURMENT OF PARAMETERS LIKE, TEMPERATURE,
PRESSURE , LEVEL etc.
C. PROTECTION SYSTEM
- TURBINE PROTECTION SYSTEM
- BYPASS PROTECTION SYSTEM
A T R S
AUTOMATIC TURBINE RUNUP SYSTEM
AUTOMATIC TURBINE RUN-UP SYSTEM
INTRODUCTION:
• The task of the automatic startup control "SGC Turbine” is to
implement transition of the steam turbine-generator from turning
gear operation to power operation.
• A successful start-up of the TG-set normally requires acquisition,
analysis and collation of a wide variety of information pertaining
to various parameters like Press, Temp., Vacuum., Speed etc.
• Difficult task for the operator to handle and collate so many bits
of information swiftly & correctly along with status of auxiliary
equipments
• A Microprocessor based ATRS performs this task accurately and
at an appropriate time
AUTOMATIC TURBINE RUN-UP SYSTEM
CONCEPT:
• A programmable Automatic Turbine Run-up
System (ATRS) is based on the “Functional
Group Control” philosophy
• The control area is divided into clearly defined
functional areas called “Functional Groups”
• Each Functional Group is organised & arranged
in SGC, SLC and Drive Interface Function
CONCEPT OF C&I IN THERMAL POWER STATION
UNIT CONTROL
CLOSED
LOOP
CONTROL
FUNCTIONAL
GROUP
CONTROL
PROT-
IVE
LOGICS
DATA PROCESS-
ING, ALARM
ANNUNCIATION
SIGNAL
CONDITIONING
ALALOG, BINARY
CONTROL INTERFACE
MOTOR CONTROL CENTRE
SWITCH GEAR
M M DRIVES
SIGNAL TRANSMITTER
ANALOG AND
BINARY
SIGNALS
DISPLAY UNIT
LOGS
CONTROL
ROOM
PLANT (FIELD)
OPERATOR
AUTOMATIC TURBINE RUN-UP SYSTEM
TASKS 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 ‘SUB-GROUP CONTROL’, ‘SUB-LOOP
CONTROL’, AND ‘CONTROL INTERFACE’ OPERATION
ALONG WITH STATUS DISPLAYS IN OWS
• OPERATING MODES AVAILABLE:
- MANUAL MODE ( OPERATOR GUIDE)
- AUTOMATIC MODE
- STEP BY STEP MODE
HIERARCHY OF CONTROL
UNIT
CONTROL
GROUP CONTROL
(WHEN, HOW MANY,WHICH)
SUB-GROUP CONTRL-1 SUB-GROUP CONTRL-2
CONTROL INTERFACE
SWITCH GEAR (MCC)
SLC ( SUB LOOP CONTROL)
ADVANTAGES OF ATRS
• ELIMINATES HUMAN ERROR
• PROVIDES MAXIMUM PROTECTION AGAINST
MALFUNCTIONS
• LESS DIFFICULT OPERATOR TASK
• 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
AUTOMATIC TURBINE RUN-UP SYSTEM
SUB 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 main
equipment.
• The sequence is programmed in the processor. The process signals
are acquired through the input modules and are available on the bus.
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.
AUTOMATIC TURBINE RUN-UP SYSTEM
• ATRS can be switched on at any stage after completing
certain tasks manually, if so desired.
• In such cases, the SGC program quickly scans through
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.
PROGRAM STEP OF A SUBGROUP CONTROL
02
FROM STEP 1
STEP CRITERIA FOR STEP -2
BYPASS CRITERION
PROGRAM LOOP
WAIT
50s
MO TIME
20s
COMMAND
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
EXPLANATION OF KWU IDENTIFICATION SYSTEM (KKS)
0 1 2 3
A NAAANN AANNN AANN
A 1MAV22 AP001 XB01
ORDINAL SECTION
GENERAL
EXAMPLE
SIGNAL IDENTIFICATION
CONSECUTIVE NO. OF EQUIPMENT
TYPE OF EQUIPMENT
NO. OF SUBGROUP
PLANT GROUP (FUNCTIONAL GROUP)
NO. OF UNIT
AUTOMATIC TURBINE RUN-UP SYSTEM
• ATRS CONTROLS:
1. ATRS is organized in the following three Sub-Groups :
• Oil supply system
• Evacuation system
• Turbine system
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
Drive Control Macros. These SGCs in conjunction with
the turbine governing system , TSE and the auto-
synchronizer accomplish the function of start-up of the
TG set.
AUTOMATIC TURBINE RUN-UP SYSTEM
SUB-LOOP CONTROL (SLC) :
• A SLC, when switched on, actuates the equipment and brings
it to the desired 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.
AUTOMATIC TURBINE RUN-UP SYSTEM
( DRIVE CONTROL INTERFACE )
DRIVE CONTROL MACROs : ( Software realization)
Basically three types of Drive Control Macros:-
1 a) LTUDPB (for Unidirectional LT drives with Pushbutton
Interface)
b) LTUD (for Unidirectional LT drives without Pushbutton
Interface)
2 a) BDPB (for Bidirectional drives with Pushbutton Interface)
b) BD (for Bidirectional drives without Pushbutton Interface)
3 a) SOVPB (for solenoid drives with Pushbutton Interface)
b) SOV (for solenoid drives without Pushbutton Interface
AUTOMATIC TURBINE RUN-UP SYSTEM
( DRIVE CONTROL INTERFACE )
DRIVE CONTROL MACROs : (Software realization)
The drive control macro functions (‘custom blocks’ in maxDNA terminology)
LTUDPB & LTUD are used to control unidirectional drives such as pumps,
fans, motors etc., Bi-directional drives (BDPB/BD) such as Valves, Dampers
etc& Solenoid valves.
The Pushbutton commands & LED indications exclusively for LTUDPB /
BDPB/SOVPB are for interfacing with control desk and not available in
respective functional blocks without PBs.
Drive commands can be issued from:
- Pushbutton panel in the control desk
(only for LTUDPB/BDPB/SOVPB)
- HMI operator station
- Automatic higher level system
- Protection signals.
AUTOMATIC TURBINE RUN-UP SYSTEM
( DRIVE CONTROL INTERFACE )
DRIVE CONTROL MACROs : (Software realization)
• Pushbutton commands ON/OFF (OPEN/CLOSE) are effective
only when pressed alongwith “Pushbutton” release.
• “Pushbutton” commands and auto commands are processed
alongwith the respective release logic input signals.
• Protection command inputs do not need any release input.
• No separate manual release required for HMI commands.
AUTOMATIC TURBINE RUN-UP SYSTEM
( DRIVE CONTROL INTERFACE )
DRIVE CONTROL MACROs : (Software realization)
( For SOV / unidirectional / bi-directional drives)
AUTOMATIC TURBINE RUN-UP SYSTEM
DRIVE ICON :
( For Bi-directional drives)
DRIVE ICON :
( For Uni-directional drives)
INDICATION ON HMI
DRIVE ICON :
( For Solenoid Valves)
AUTOMATIC TURBINE RUN-UP SYSTEM
ATRS STRUCTURAL SYSTEM:
1. SGC-TURBINE SYSTEM :
SGC Turbine acts directly on the following systems :
• Sub-loop Control (SLC) Drains.
• Warm up Controller.
• Turbine controller.
• Turbine startup & lift limiter
AUTOMATIC TURBINE RUN-UP SYSTEM
2. SGC-OIL SUPPLY SYSTEM :
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 pumps.
• SLC exhausters.
AUTOMATIC TURBINE RUN-UP SYSTEM
3. SGC EVACUATION SYSTEM :
SGC Evacuation directly acts on the following systems :
• SLC Vacuum pumps
• Drive of Vacuum pumps
SGC-DISPLAY
4 6 8 7 5
1
3
2
1. CONTROL BUTTON “SHUTDOWN”
2. CONTROL BUTTON “STARTUP” OR “OPERATION”
3. CONTROL BUTTON “AUTOMATIC ON/OFF”
4. LAMP “SHUTDOWN PROGRAM”
5. LAMP “STARTUP” OR “OPERATION” PROGRAM
6. LAMP “AUTOMATIC OFF”
7. LAMP “ AUTOMATIC ON”
8. LAMP “FAULT”
SLC-DISPLAY
2 3 4
1. CONTROL BUTTON “MANUAL ON/OFF”
2 .LAMP “SLC OFF”
3. LAMP “ FAULT”
4. LAMP “SLC ON”
1
DRIVE INTERFACE-DISPLAY
3 4 5
1. CONTROL BUTTON “OFF” (CLOSE)
2. CONTROL BUTTON “ON” (OPEN)
3. LAMP “ OFF” (CLOSE)
4. LAMP “FAULT”
5. LAMP “ON” (OPEN)
1 2
PROTECTION SYSTEM
FOR
STEAM TURBINE
TURBINE PROTECTION SYSTEM
TASK PERFORMED :
PROTECTS TURBOSET FROM INADMISSIBLE
OPERATING CONDITIONS
PREVENTS DAMAGE IN CASE OF PLANT FAILURE
FAILURE OCCURRENCE REDUCED TO MINIMUM
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
TURBINE PROTECTION SYSTEM
GENERAL :
• 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.
TURBINE PROTECTION SYSTEM
• Trip signals from the sensors / field instruments are conditioned
and distributed 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 1 out of 1.
• Trip signal from each of the local buses acts on 3 relays in 2 out
of 3 combination.
TURBINE PROTECTION SYSTEM
TRIPPING 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 switches in 2-out-of-3-
logic.
TURBINE PROTECTION SYSTEM
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.
TURBINE PROTECTION SYSTEM
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
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
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.
AUTOMATIC TURBINE RUNUP SYSTEM

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AUTOMATIC TURBINE RUNUP SYSTEM

  • 2. STEAM TURBINE TYPE Conventional Cycle • 210MW • 250MW • 300/350MW • 500/600MW Combined Cycle • MN Series (Dual Pressure) • HMN Series (Triple Pressure) Nuclear Turbine • 500MW High Pressure Turbine • 250/270MW • 660/800 MW (Super Critical)
  • 3. AIMS OF AUTOMATION • Improvement in quality of control • Increase in plant availability • Increase in plant safety • Increase in Plant efficiency • Faster start-up and load change • Easy handling of the plant • Avoidance of maloperation
  • 5. Thermal Cycle in a Power Plant
  • 6. ST SUBSYSTEMS A. CONTROL SYSTEM: ANALOG (CLOSED LOOP) - ELECTROHYDRAULIC CONTROLLER (EHC) - LOW PRESSURE BYPASS CONTROLLER (LPBPC) - GLAND STEAM PRESSURE CONTROLLER (GSPC) - LUBE OIL/ WARM-UP TEMPERATURE CONTROLLERS BINARY (OPEN LOOP) - AUTOMATIC TURBINE RUN UP SYSTEM (ATRS) - AUTOMATIC TURBINE TESTER (ATT)
  • 7. ST - SUBSYSTEMS B. MONITORING & MEASUREMENT SYSTEM - TURBINE SUPERVISORY INSTRUMENTATION (TSI) - TURBINE STRESS EVALUATOR/CONTROLLER (TSE/TSC) - MEASURMENT OF PARAMETERS LIKE, TEMPERATURE, PRESSURE , LEVEL etc. C. PROTECTION SYSTEM - TURBINE PROTECTION SYSTEM - BYPASS PROTECTION SYSTEM
  • 8. A T R S AUTOMATIC TURBINE RUNUP SYSTEM
  • 9. AUTOMATIC TURBINE RUN-UP SYSTEM INTRODUCTION: • The task of the automatic startup control "SGC Turbine” is to implement transition of the steam turbine-generator from turning gear operation to power operation. • A successful start-up of the TG-set normally requires acquisition, analysis and collation of a wide variety of information pertaining to various parameters like Press, Temp., Vacuum., Speed etc. • Difficult task for the operator to handle and collate so many bits of information swiftly & correctly along with status of auxiliary equipments • A Microprocessor based ATRS performs this task accurately and at an appropriate time
  • 10. AUTOMATIC TURBINE RUN-UP SYSTEM CONCEPT: • A programmable Automatic Turbine Run-up System (ATRS) is based on the “Functional Group Control” philosophy • The control area is divided into clearly defined functional areas called “Functional Groups” • Each Functional Group is organised & arranged in SGC, SLC and Drive Interface Function
  • 11. CONCEPT OF C&I IN THERMAL POWER STATION UNIT CONTROL CLOSED LOOP CONTROL FUNCTIONAL GROUP CONTROL PROT- IVE LOGICS DATA PROCESS- ING, ALARM ANNUNCIATION SIGNAL CONDITIONING ALALOG, BINARY CONTROL INTERFACE MOTOR CONTROL CENTRE SWITCH GEAR M M DRIVES SIGNAL TRANSMITTER ANALOG AND BINARY SIGNALS DISPLAY UNIT LOGS CONTROL ROOM PLANT (FIELD) OPERATOR
  • 12. AUTOMATIC TURBINE RUN-UP SYSTEM TASKS 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 ‘SUB-GROUP CONTROL’, ‘SUB-LOOP CONTROL’, AND ‘CONTROL INTERFACE’ OPERATION ALONG WITH STATUS DISPLAYS IN OWS • OPERATING MODES AVAILABLE: - MANUAL MODE ( OPERATOR GUIDE) - AUTOMATIC MODE - STEP BY STEP MODE
  • 13. HIERARCHY OF CONTROL UNIT CONTROL GROUP CONTROL (WHEN, HOW MANY,WHICH) SUB-GROUP CONTRL-1 SUB-GROUP CONTRL-2 CONTROL INTERFACE SWITCH GEAR (MCC) SLC ( SUB LOOP CONTROL)
  • 14. ADVANTAGES OF ATRS • ELIMINATES HUMAN ERROR • PROVIDES MAXIMUM PROTECTION AGAINST MALFUNCTIONS • LESS DIFFICULT OPERATOR TASK • 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
  • 15. AUTOMATIC TURBINE RUN-UP SYSTEM SUB 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 main equipment. • The sequence is programmed in the processor. The process signals are acquired through the input modules and are available on the bus.
  • 16. 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.
  • 17. AUTOMATIC TURBINE RUN-UP SYSTEM • ATRS can be switched on at any stage after completing certain tasks manually, if so desired. • In such cases, the SGC program quickly scans through 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.
  • 18. PROGRAM STEP OF A SUBGROUP CONTROL 02 FROM STEP 1 STEP CRITERIA FOR STEP -2 BYPASS CRITERION PROGRAM LOOP WAIT 50s MO TIME 20s COMMAND 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
  • 19. EXPLANATION OF KWU IDENTIFICATION SYSTEM (KKS) 0 1 2 3 A NAAANN AANNN AANN A 1MAV22 AP001 XB01 ORDINAL SECTION GENERAL EXAMPLE SIGNAL IDENTIFICATION CONSECUTIVE NO. OF EQUIPMENT TYPE OF EQUIPMENT NO. OF SUBGROUP PLANT GROUP (FUNCTIONAL GROUP) NO. OF UNIT
  • 20. AUTOMATIC TURBINE RUN-UP SYSTEM • ATRS CONTROLS: 1. ATRS is organized in the following three Sub-Groups : • Oil supply system • Evacuation system • Turbine system 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 Drive Control Macros. These SGCs in conjunction with the turbine governing system , TSE and the auto- synchronizer accomplish the function of start-up of the TG set.
  • 21. AUTOMATIC TURBINE RUN-UP SYSTEM SUB-LOOP CONTROL (SLC) : • A SLC, when switched on, actuates the equipment and brings it to the desired 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.
  • 22. AUTOMATIC TURBINE RUN-UP SYSTEM ( DRIVE CONTROL INTERFACE ) DRIVE CONTROL MACROs : ( Software realization) Basically three types of Drive Control Macros:- 1 a) LTUDPB (for Unidirectional LT drives with Pushbutton Interface) b) LTUD (for Unidirectional LT drives without Pushbutton Interface) 2 a) BDPB (for Bidirectional drives with Pushbutton Interface) b) BD (for Bidirectional drives without Pushbutton Interface) 3 a) SOVPB (for solenoid drives with Pushbutton Interface) b) SOV (for solenoid drives without Pushbutton Interface
  • 23. AUTOMATIC TURBINE RUN-UP SYSTEM ( DRIVE CONTROL INTERFACE ) DRIVE CONTROL MACROs : (Software realization) The drive control macro functions (‘custom blocks’ in maxDNA terminology) LTUDPB & LTUD are used to control unidirectional drives such as pumps, fans, motors etc., Bi-directional drives (BDPB/BD) such as Valves, Dampers etc& Solenoid valves. The Pushbutton commands & LED indications exclusively for LTUDPB / BDPB/SOVPB are for interfacing with control desk and not available in respective functional blocks without PBs. Drive commands can be issued from: - Pushbutton panel in the control desk (only for LTUDPB/BDPB/SOVPB) - HMI operator station - Automatic higher level system - Protection signals.
  • 24. AUTOMATIC TURBINE RUN-UP SYSTEM ( DRIVE CONTROL INTERFACE ) DRIVE CONTROL MACROs : (Software realization) • Pushbutton commands ON/OFF (OPEN/CLOSE) are effective only when pressed alongwith “Pushbutton” release. • “Pushbutton” commands and auto commands are processed alongwith the respective release logic input signals. • Protection command inputs do not need any release input. • No separate manual release required for HMI commands.
  • 25. AUTOMATIC TURBINE RUN-UP SYSTEM ( DRIVE CONTROL INTERFACE ) DRIVE CONTROL MACROs : (Software realization) ( For SOV / unidirectional / bi-directional drives)
  • 26. AUTOMATIC TURBINE RUN-UP SYSTEM DRIVE ICON : ( For Bi-directional drives) DRIVE ICON : ( For Uni-directional drives) INDICATION ON HMI DRIVE ICON : ( For Solenoid Valves)
  • 27. AUTOMATIC TURBINE RUN-UP SYSTEM ATRS STRUCTURAL SYSTEM: 1. SGC-TURBINE SYSTEM : SGC Turbine acts directly on the following systems : • Sub-loop Control (SLC) Drains. • Warm up Controller. • Turbine controller. • Turbine startup & lift limiter
  • 28. AUTOMATIC TURBINE RUN-UP SYSTEM 2. SGC-OIL SUPPLY SYSTEM : 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 pumps. • SLC exhausters.
  • 29. AUTOMATIC TURBINE RUN-UP SYSTEM 3. SGC EVACUATION SYSTEM : SGC Evacuation directly acts on the following systems : • SLC Vacuum pumps • Drive of Vacuum pumps
  • 30. SGC-DISPLAY 4 6 8 7 5 1 3 2 1. CONTROL BUTTON “SHUTDOWN” 2. CONTROL BUTTON “STARTUP” OR “OPERATION” 3. CONTROL BUTTON “AUTOMATIC ON/OFF” 4. LAMP “SHUTDOWN PROGRAM” 5. LAMP “STARTUP” OR “OPERATION” PROGRAM 6. LAMP “AUTOMATIC OFF” 7. LAMP “ AUTOMATIC ON” 8. LAMP “FAULT”
  • 31. SLC-DISPLAY 2 3 4 1. CONTROL BUTTON “MANUAL ON/OFF” 2 .LAMP “SLC OFF” 3. LAMP “ FAULT” 4. LAMP “SLC ON” 1
  • 32. DRIVE INTERFACE-DISPLAY 3 4 5 1. CONTROL BUTTON “OFF” (CLOSE) 2. CONTROL BUTTON “ON” (OPEN) 3. LAMP “ OFF” (CLOSE) 4. LAMP “FAULT” 5. LAMP “ON” (OPEN) 1 2
  • 34. TURBINE PROTECTION SYSTEM TASK PERFORMED : PROTECTS TURBOSET FROM INADMISSIBLE OPERATING CONDITIONS PREVENTS DAMAGE IN CASE OF PLANT FAILURE FAILURE OCCURRENCE REDUCED TO MINIMUM
  • 35. 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
  • 36. TURBINE PROTECTION SYSTEM GENERAL : • 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.
  • 37. TURBINE PROTECTION SYSTEM • Trip signals from the sensors / field instruments are conditioned and distributed 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 1 out of 1. • Trip signal from each of the local buses acts on 3 relays in 2 out of 3 combination.
  • 38. TURBINE PROTECTION SYSTEM TRIPPING 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 switches in 2-out-of-3- logic.
  • 39. TURBINE PROTECTION SYSTEM 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.
  • 40. TURBINE PROTECTION SYSTEM 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.
  • 41. TURBINE PROTECTION SYSTEM 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 .
  • 42. TURBINE PROTECTION SYSTEM 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.