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 1 HYDR A U L IC T U R NING G E A R 1. 0  Int r oduc t ion:  T he func t i on of hy dr aul i c tu r ni ng gear i s to rot ate the T ur bo -Gener ator s haft system at a sufficient speed during the period before start-up and the period after shut down. During cold or hot rolling of turbine, it is necessary to measure and monitor the eccentricity of the rotor even before the admission of steam into the turbine in order to ensure that no vibration is caused and no rubbing between the moving and the stationary parts takes place. The eccentricity of the rotor is caused when it bec ome s uns tr aight due to bending. Hydrauli c T ur ning gea r is us eful to rotate the Turbo generator shaft system at a sufficient speed during the period before start up and the period after shut down. Mechanical Barring gear is also ava ilab le a s a ba c k up. 2. 0  Neces s it y Of T ur nin g Gear : R otor is s aid to be r otating with ec centr icity when its ax is of r ota ti on do es not c oinc ide with i ts tr ue c enter li ne o f mass . E c c entr icit y of the rotor i s caus ed dur ing cold or hot rolling. Before cold rolling of turbine, a natural deflection of rotor is there due to the non-unifor m dis tr ibuti on of it s own we ight s ince the weight of the dif ferent s tag e dif fer. T his is an ini ti al conditi on of ec c entr icit y. Mo r e over uni form hea ti ng up of rotor is necessitated while admitting the steam for sealing at glands on raising vacuum. Due to the above reasons, slow rotation of turbine rotor is done with the help of turning gear for a sufficient duration of time prior to cold rolling. As the tur bine s pe ed is grad uall y in c r eas ed , the rotor s tart s to s tr aighten its elf a nd the eccentricity gets greatly reduced beyond the critical speed.  T he c ondit ions in hot r oll i ng are dif fer ent. When the tu r bine i s tr i pped, the r otor comes to rest fr om it s rated s peed. T he tur bine s tar ts cooli ng ve r y s lowly s ince it is well insulated. Due to the difference in the area exposed in different sections of the cylinder, viz. the cylinder top and bottom, the rate of cooling varies leading to uneven cooling. In such conditions if the rotor is allowed to be stationary, after it

SHAFT TURNING GEAR

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SHAFT TURNING GEAR

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    HYDRAULIC TURNING GEAR 1.0 Introduction:

    The function of hydraulic turning gear is to rotate the Turbo-Generator shaft

    system at a sufficient speed during the period before start-up and the period after

    shut down. During cold or hot rolling of turbine, it is necessary to measure and

    monitor the eccentricity of the rotor even before the admission of steam into the

    turbine in order to ensure that no vibration is caused and no rubbing between the

    moving and the stationary parts takes place. The eccentricity of the rotor is caused

    when it becomes unstraight due to bending. Hydraulic Turning gear is useful to

    rotate the Turbo generator shaft system at a sufficient speed during the period

    before start up and the period after shut down. Mechanical Barring gear is also

    available as a backup.

    2.0 Necessity Of Turning Gear:

    Rotor is said to be rotating with eccentricity when its axis of rotation does not

    coincide with its true centerline of mass. Eccentricity of the rotor is caused during

    cold or hot rolling.

    Before cold rolling of turbine, a natural deflection of rotor is there due to the

    non-uniform distribution of its own weight since the weight of the different stage

    differ. This is an initial condition of eccentricity. More over uniform heating up of

    rotor is necessitated while admitting the steam for sealing at glands on raising

    vacuum. Due to the above reasons, slow rotation of turbine rotor is done with the

    help of turning gear for a sufficient duration of time prior to cold rolling. As the

    turbine speed is gradually increased, the rotor starts to straighten itself and the

    eccentricity gets greatly reduced beyond the critical speed.

    The conditions in hot rolling are different. When the turbine is tripped, the

    rotor comes to rest from its rated speed. The turbine starts cooling very slowly since

    it is well insulated. Due to the difference in the area exposed in different sections of

    the cylinder, viz. the cylinder top and bottom, the rate of cooling varies leading to

    uneven cooling. In such conditions if the rotor is allowed to be stationary, after it

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    comes to rest, it would be exposed to uneven temperatures, resulting in thermal

    stresses, bending and eventually eccentricity in the rotor. This problem is also

    overcome by having a slow rotation of rotor by means of turning gear. The blade

    ventilation during turning operation provides good heat transfer at the inner wall of

    the casing, which is conducive for temperature equalization between the top and

    the bottom cylinder.

    3.0 Hydraulic Turning Gear:

    Hydraulic turning gear is located in the bearing pedestal between IP turbine

    and the HP turbine. Mechanical barring gear is available as a back up to this.

    During turning gear operation, the turbo-generator shaft system is rotated by

    a double row blade wheel, which is driven by oil. The oil is supplied by the auxiliary

    oil pump and it flows through a gate valve gearing and a nozzle box. Gate valve

    gearing is an electrically operated valve through which the high pressure oil is

    supplied to turning gear thro Nozzle box. Nozzles guide the jet of oil towards the

    moving blades. Nozzles increase the velocity of oil and guide the jet of oil towards

    the moving blades. This flow of high velocity jet of oil through the two rows of

    moving blades result in slow rotation of the Turbo generator rotor system. Speed of

    rotation of TG rotor during the turning gear operation is 120 rpm without condenser

    vacuum and 160 rpm with condenser vacuum.

    In order to reduce the gap losses at the moving blades, sealing strips are

    caulked into the nozzle boxes. After passing through the moving blades, the oil

    drains into the bearing pedestal and flows along with the bearing drain oil into the

    return flow piping.

    To overcome the initial breakaway torque on startup and to prevent dry

    friction, the bearings are relieved for a short time by jacking oil supplied below the

    shaft. The shafts are thus slightly.

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    4.0 Mechanical Barring Gear:

    The turbo generator is also equipped with a mechanical barring gear, which

    enables the combined shaft system to be rotated manually in the event of failure

    of the normal hydraulic turning gear.

    4.1 Construction: The mechanical barring gear consists of a gear machined on the rim of the

    turning gear wheel and a pawl. The pawl engages with the ring gear and turns the

    shaft system when operated by means of a bar attached to a lever. The pawl can

    be engaged or disengaged by using a lever. The lever is held in position by means

    of a latch.

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    Fig.No.1a HYDRAULIC TURNING GEAR & MANUAL BARRING GEAR

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    4.2 Operation of STG:

    The following steps of operation are to be made

    Remove the cover and unlatch, Attach a bar to the lever, Barring of lever will rotate the combined turbo-generator shaft system. After the barring has been completed return the lever and the pawl to

    disengaged position.

    Secure the lever by means of latch and replace the cover. The barring gear shall be operated only after the turbo-generator shaft

    system has been lifted with jacking oil. If it is hard to start turning by means of the

    mechanical barring gear, this may be due to incorrect adjustment of the jacking oil

    system or due to rubbing of the shaft. Corrective action must be taken before the

    steam is admitted into turbine. After shut down of turbine, turning gear should be in

    operation till the maximum metal temperature reaches 120 C.

    5.0 Hydraulic Lifting Device:

    When the turbine is started up or shut down, the hydraulic lifting device is

    used to maintain the oil film between rotor and bearings. The necessary torque for

    rotation is reduced in this way when the hydraulic device or manual turning device

    is in service.

    The turbo-generator bearings are supplied with high-pressure oil delivered by

    a jacking oil pump. The high pressure oil lifts the rotor when it is forced under the

    journal of the bearings. To avoid damage to the bearings, the jacking oil pump

    must be switched ON at turbine speed below 510 RPM. (approximately) during shut

    down and it should be switched OFF at turbine speed above 540 RPM.

    (approximately) during start-up.

    5.1 Need Of The Jacking Oil For Lifting: The way in which liquids lubricate can be explained by considering the

    example of a plain journal bearing as shown in fig no.4.

    As the shaft (journal) rotates in the bearing, lubricating oil is dragged into the

    loaded zone. Since the loaded zone will be the point at which the shaft and the

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    bearing surfaces are closet together, the entry into this zone is tapered, like a

    curved wedge. As the oil is forced to move into the narrower part of the wedge, its

    pressure increases, and it is this hydrodynamic pressure which supports the shaft

    load.

    Increasing load reduces the oil film thickness while increasing hydrodynamic

    pressure increases the oil film thickness. The hydro dynamic pressure, in turn, is

    determined by the viscosity of the oil and the speed at which it is squeezed into the

    wedge shaped entry zone. Thus the rise in hydrodynamic pressure and therefore

    the thickness of the film will depend on the shaft speed and the lubricant viscosity.

    The relationship between speed, viscosity, load, film thickness and friction

    can be understood by considering a graph shown in fig no.4. In this graph, the co-

    efficient of friction is plotted against expression V/P where, V/P = (Oil viscosity *

    Shaft speed)/ Bearing pressure.

    There are three different zones in the graph, separated by the points A & B.

    At B, the co-efficient friction is at its minimum, and this is the point at which

    the oil film is just thick enough to ensure that there is no contact between the shaft

    and the bearing surfaces. The zone 3, to the right of B, the oil film thickness is

    increasing and the co-efficient of friction also increases (as the film thickness

    increases). This increase in the oil film thickness is because of increasing viscosity or

    increasing shaft speed or reducing the bearing load. Zone 3 is the zone of

    hydrodynamic lubrication or Full film lubrication.

    As the conditions change from B towards A, the oil film thickness reduces

    and hence the shaft and the bearing rub against each other, the amount of

    rubbing, and the friction increases as the oil film thickness decreases, zone 2,

    between A & B, is known as the zone of mixed lubrication or partial lubrication. The

    shaft load was supported by a mixture of oil pressure and surface contacts,

    At A, the oil film thickness has been reduced to nil and the load between

    shaft and bearing is carried entirely on surface contact. In zone1, the co-efficient of

    friction is almost independent of load, viscosity and shaft speed. Zone1 is the zone

    of boundary lubrication.

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    The different lubrication zones also have an influence on wear, the amount

    of wear which takes place depends on the severity with which two surfaces rub

    against each other. In zone 3, there is no contact between the surfaces and

    therefore the wear is minimum. As the oil film thickness becomes thinner in zones 2

    and 1, there is a greater tendency to wear.

    When the turbine is on Turning Gear during start-up or shut down, the shaft

    speed is much less compared to its normal operating speed. Hence the shaft

    rotates in the region of boundary lubrication. Since the oil film thickness is minimum

    during low shaft speed, there is increasingly severe contact between the shaft and

    the bearing surface resulting in increased wear and reduction in life of the bearing.

    To avoid this, a jacking oil system also known as hydraulic lifting device is

    necessitated to supply high pressure oil called as jacking oil under the journal of the

    bearing thereby slightly lifting the journal. Slow rotation of turbine rotor during

    turning operation is thus done in slightly lifted condition so as to avoid damage to

    the bearings. Hence the shaft rotates now in the region of Hydrodynamic

    lubrication.

    5.2 Jacking Oil System: To supply the high-pressure oil for the lifting device, two jacking oil

    pumps of each 100% capacity are provided on the main oil tank. When one pump

    is intended to be in service, the other one is stand by.

    5.2.1 Jacking Oil Pump: The jacking oil pump is a self-priming screw spindle pump with three spindles

    and internal bearings. The screw spindle pump is connected vertically to the cover

    plate (2) of the Main oil tank via a support (5) and immerses with the suction casing

    (15) into the oil. The drive is an electric motor that is bolted to the cover plate. The

    oil flows into the suction branch of the suction casing from underneath and is

    supplied to the jacking oil system by the pump via the pressure pipe (3).

    The driving spindle (16) and the two moving spindles (20) run in the inner

    casing (13). Due to the special profile given by the sides of the threads, the three

    spindles form-sealed chambers, the contents of which are continuously being

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    moved axially from the suction side to the pressure side of the pump as the spindles

    rotate.

    There is a balancing piston in the form of a shrunk on sleeve in the main drive

    spindle just above the screwed portion of the main drive spindle and this runs inside

    the throttle bushing (11). Pressure oil of a small quantity flows in a very small gap

    between the throttle bushing (11) and the driving spindle (16) in an upward

    direction. This gap is known as throttling gap since the pressure of oil which is

    coming out of this gap is very much reduced. The oil that leaves the throttle gap

    flows via the grooved ball bearing (7) and lubricates it. This bearing serves as both

    support and thrust bearing. There after the oil flows through the support to the main

    oil tank itself via an opening in the support. The driving spindle is fixed by means of

    the grooved ball bearing in the bearing carrier (9) that is bolted to the pressure

    casing (12) of the pump. The drive main spindle is a solid one. The cumulative axial

    thrust generated by the main drive spindle screw is countered by the balancing

    piston in the form of the shrunk on sleeve. The p across the balance piston and the annular area of it are so designed to match with the cumulative axial thrust

    generated by the main drive spindle.

    There are two idler screw spindles, which are hollow and are driven by the

    main drive spindle whose continuous helical screw is in mesh with the continuous

    helical screws of them. Pressure oil in a very small quantity flows via gaps in the top

    of the screwed portion of the main drive spindle though the hollow spaces of the

    two idler screw spindles in a downward direction.

    The two idler screw spindles also exert a cumulative axial thrust in a

    downward direction, which are to be balanced, to perform this task, each idler

    screw spindle is having a balancing bushing (21) in its bottom. These are fixed to the

    support plate (18), which also supports the inner casing (13) by means of distance

    pipes (17) attached to it. The balancing bushing has a small piston with a guide pin

    in its bottom and can move only in a vertical direction in a small cylinder, which is

    open in its top. The piston is located just below the ending point of the continuous

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    Fig. No. 5 Jacking oil pump

    helical screw of the idler spindle. Pressure oil is supplied in the bottom of the piston

    via hollow space of the idler spindle through a small opening. The top of the piston

    is exposed to pressure less oil in the tank. The upward counter thrust provided by the

    balance piston in the balancing bushing encounters the cumulative axial thrust

    exerted by the continuous helical screw of each one of the idler spindle screws in

    the downward direction. There is provision for leakage oil to escape to the main oil

    tank from the balancing bushing on the pressure side.

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    5.2.2 Jacking Oil Supply: Ref fig no.6. The discharge pressure oil piping of both the jacking oil pumps is connected

    in parallel to supply high-pressure oil to the common jacking header. In each

    discharge line, a check valve is provided to prevent the jacking oil returning from

    the header to the oil tank, if the pump concerned is not in operation. A spring

    loaded safety relief valve is provided between the jacking oil pump and the check

    valve. This is to prevent any damage to the jacking oil pumps discharge piping in

    case that the concerned jacking oil pump is in operation and the check valve

    continues to remain in closed position.

    The pressure in the common jacking oil header is maintained at a constant

    value (approximately 120 bar) by means of a pressure-limiting valve. The pressure-

    limiting valve can be relieved by a bypass valve. The superfluous flow from the

    pump is conducted into the main oil tank.

    The jacking oil required for each bearing is supplied from the common

    header as detailed below.

    Bearing No of lines

    Hp front One

    Hp Rear journal cum thrust One

    IP Rear Two

    LP Rear Two

    Generator Front Two

    Generator Rear One

    In each supply line, a fine control valve and a check valve are provided. The

    necessary jacking oil pressure sufficient to lift the shaft varies with respect to bearing

    load. The lift will be of 0.03 to 0.05 mm. The required jacking oil pressure is set for

    each bearing by means of a finer control valve. The pressure gauges mounted in

    the downstream pipes of these finer control valves indicate the jacking oil pressure

    required for lifting. A check valve provided in the jacking oil supply pipings prevent

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    Fig.No.6 Jacking oil system

    the lub oil from flowing out of the bearings into the header during the normal

    operation of turbine since the jacking oil pumps are out of service.

    The finer control valve, the check valve and the pressure gauge for each line

    are arranged in boxes, which are connected laterally to the bearings. At the

    generator free end bearing alone, they are arranged in the hacking oil piping

    outside the bearing housing.

    The lift in mm of the shaft at the bearings is about 0.04 to 0.08 mm.

    Bearing Jack oil pressure (in ksc) where the shaft lifts.

    (When JO header pressure is 120ksc)

    Hp front 40

    Hp Rear journal cum thrust 60

    IP Rear a) 62 b) 82

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    LP Rear a) 50 b) 36

    Generator Front a) 80 b) 70

    Generator Rear 40

    The values are given above for the purpose of indication only.

    6.0 Logics:

    6.1 Hydraulic Turning Gear:

    6.1.1 Sub Loop Control Of Turning Gear: a) Bringing SLC of Turning gear to ON.

    i. SLC of Turning gear can be made ON by giving manual command

    from the control desk.

    ii. When Sub Group Control (SGC) Oil supply is ON and the start up

    programme is at STEP 4, SLC of Turning gear is made ON

    automatically.

    b) Bringing SLC of Turning gear to OFF.

    i. SLC of Turning gear can be made OFF by giving manual command

    from the control desk.

    ii. SLC of Turning gear gets switched OFF automatically when any one

    of the following conditions appears.

    1. Fire Protection 2 Channel 1 has operated. (OR),

    2. Fire Protection 2 Channel 2 has operated. (OR),

    3. When SGC Oil supply is ON and the shut down programme at

    STEP 51, is executed.

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    FIG.NO.7 HYDRAULICTURNINGGEAR&JACKINGOILSYSTEMCONTROLDESK

    ON/OFF

    OFFON FAULT

    SHUTDOWN ON/OFF STARTUP

    PUSHBUTTON INDICATION

    JACKOILPUMP1

    JACKOILPUMP2

    GATEVALVEGEARING

    SLCJ.O.P1 SLCJ.O.P2 SLCTURNINGGEAR

    SUBGROUPSHUTDOWN

    SUBGROUPSTARTUP

    SGC OILSUPPLY

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    6.1.2 Gate Valve Gearing: 1. Protection close:

    When the lub oil pressure before the thrust bearing becomes less than 1.2

    ksc (MAV 43 CP 012), the gate valve gearing will protection close.

    2. Permissives for manual and auto operation of gate valve gearing are

    as under.

    Differential pressure between the generator seal oil and hydrogen gas should be greater than 0.9 KSc. (as sensed by PS MKW 01 CP 003)

    Generator seal oil pressure (turbine side) should be greater than 3.8 KSc (as sensed by pressure switch MKW 01 CP 001).

    Generator seal oil pressure (Excitation side) should be greater than 3.8 KSc (as sensed by the pressure switch MKW 01 CP 002).

    (OR)

    Turbine speed should be greater than 15 RPM. (as sensed by MYA 01 FS 001)

    3. Manual open

    The gate valve gearing can be opened manually from the control

    desk (after keeping SLC of Turning Gear in OFF position) provided that the

    permissives detailed in Sec.2. are available.

    4. Automatic Open

    When SLC of Turning Gear is ON and the turbine speed is less than 200

    rpm (MYA 01 FS 001), the gate valve gearing will open automatically

    provided that the permissives detailed in Sec.2 are available.

    5. Manual close

    The gate valve gearing can be closed manually from the control desk

    after keeping in SLC of Turning Gear in off position.

    6. Automatic close

    When SLC of Turning Gear is on and the turbine speed is greater than

    250 rpm (MYA 01 FS 001), the gate valve gearing will close automatically.

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    6.2 Jacking Oil Pumps:

    6.2.1 SLC of JOP-A: a. Bringing SLC of JOP A to ON

    (i) SLC of JOP A can be made ON by giving manual command from the

    control desk (or)

    (ii) SLC of JOP A is made ON automatically when SGC oil supply is ON

    and the start-up programme is at STEP 5.

    b. Bringing SLC of JOP A to OFF

    (i) SLC of JOP A can be made ON by giving manual command from the

    control desk (or)

    (ii) SLC of JOP A gets switched OFF automatically when any one of the

    following conditions exits.

    1. Fire Protection 2 Channel 1 has operated. (or)

    2. Fire Protection 2 - Channel 2 has operated. (or)

    3. When SGC oil supply is ON and the shut down programme is at STEP

    54.

    (or)

    4. Auto start command for JOP B exists.

    6.2.2 SLC OF JOP B: a. Bringing SLC of JOP B to ON:

    (i) SLC of JOP B can be made ON by giving manual command from the

    control desk. (or)

    (ii) SLC of JOP B is made ON automatically when SGC oil supply is ON

    and the start-up programme is at STEP 5.

    b. Bringing SLC of JOP B to OFF

    (i) SLC of J.O.P. B can be made OFF by giving manual command from

    the control desk. (or)

    (ii) SLC of J.O.P. B gets switched off automatically when any one of the

    following conditions exists.

    1. Fire protection 2 Channel 1 has operated (or)

    2. Fire protection 2 Channel 2 has operated (or)

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    3. When SGC oil supply is ON and that shut down programme is at

    STEP 54.

    6.2.3 JACKING OIL PUMP A a. Protection.

    JOP A will trip on actuation of any one of the following protections

    i. Fire protection 2 Channel 1 has operated (or)

    ii. Fire protection 2 Channel 2 has operated

    b. Manual Starting.

    JOP A can be started manually from the control desk provided that

    JOPB is off (irrespective of SLC of JOPA position).

    c. Automatic starting.

    JOP A gets started automatically when all the following conditions exist.

    i. SLC of JOP A is ON.

    ii. Turbine speed is less than 510 rpm (MYA 01 FS 001) (OR) (MYA 01 DS

    001) and

    iii. JOP B is off.

    d. Manual Stopping.

    JOP A can be stopped manually from the control desk after keeping

    SLC of JOP A in off position.

    e. Automatic stopping.

    JOP A gets stopped automatically when any one of the following

    conditions exists.

    i. SGC oil supply is ON and shut down programme STEP 54 is

    executed.

    ii. SLC of JOP A is ON and

    Turbine speed is greater that 540 rpm (MYA 01 FS 001) or (MYA 01 DS

    001) (OR)

    Auto start command for JOP B exists.

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    6.2.4 JACKING OIL PUMP B a. Protection starting

    JOP B will be protection started on actuation of any one of the following

    protections.

    i. Fire protection 2 Channel 1 has operated

    ii. Fire protection 2 Channel 2 has operated

    b. Manual starting

    JOP B can be started manually from the control desk provided that JOP

    A is off. (irrespective of SLC of JOP B position)

    c. Automatic starting of JOP B along with stopping of JOP A

    On occurrence of any one of the following conditions.

    1. JOP B gets started automatically.

    2. JOP A gets stopped automatically &

    3. SLC of JOP A is made off.

    Conditions:

    1. (i) SLC of JOP B is ON.

    (ii) JOP A is off.

    (iii) JOP A Discrepancy.

    (or)

    2. (i) SLC of JOP B is ON.

    (ii) Turbine speed is less than 510 rpm.

    (MYA 01 FS 001) (OR) (MYA 01 DS 001).

    (iii) Jacking oil pressure is less than 100 Ksc. (Time delay 5 Sec) (MAV 35 CP

    001)

    (OR)

    3. (i) SLC of JOP B is ON.

    (ii) Turbine speed is less than 2800 rpm (MYA 01 FS 001).

    (iii) A.C. Voltage for JOP A failed.

    d. Manual stopping

    JOP B can be stopped manually from the control desk after keeping SLC

    of JOP B in off position.

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    6.3. Alarms: 1. SLC Turning Gear System Not on alarm will appear when SLC gate valve

    gearing is off and temperature of HP casing top (50%) is greater than

    1200C (MAA 50 CT 053A)

    2. Gate Valve Gearing Not closed alarm appears if the turbine speed is

    greater than 540 rpm and the valve remains open.

    3. SLC Jacking System not ON alarm will appear when SLC of JOP A is

    off SLC of JOP B is off and when the turbine speed is greater than 15

    rpm. (MYA 01 FS 001)

    4. Jacking oil pressure low alarm appears when the jacking oil header

    pressure drops to a value less than 100 Kg/Cm2.

    7.0 Guide Lines For Turning Gear Operation:

    1. After shut down of turbine, turning gear should be kept in operation till the

    maximum metal temperature comes down to 120 C.

    2. The mechanical barring gear shall be operated only after the turbo-

    generator shaft system has been lifted with the jacking oil. If it is hard to

    start turning by means of the mechanical barring gear, this may be due to

    incorrect adjustment of the jacking oil system or due to rubbing of shaft.

    Corrective action must be taken before steam is admitted into the turbine.

    3. Emergency operation of Hydraulic Turning Gear.

    On admission of the oil for driving the hydraulic turning gear (after opening

    of Gate Valve Gearing), if the Turbo-generator rotor fails to rotate, Manual

    barring of the rotor should be immediately started.

    After manual rotation of TG rotor for a short interval, if the rotor begins

    to rotate due to hydraulic turning gear, manual barring gear can be

    stopped.

    In case that the rotor does not rotate at all, due to hydraulic turning

    gear, even after manual barring for some time, manual barring has to be

    continued such that the rotor is rotated by 180 for every five minutes. This

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    has to be continued until the rotor becomes straight due to its own cooling

    and begins to rotate due to hydraulic turning gear.

    8.0 Technical Data:

    8.1 Jacking Oil Pump: Number of pumps per unit : 2

    Type :SDF 40 R54

    Manufactured by :M/S AllWeiler

    Capacity : 1.26 dm cubes/sec

    Discharge Pressure :120 Bar

    Speed : 49.16/sec.

    8.2 Motor Of Jacking Oil Pump: 1. Rated Voltage : 415 V

    2. Rated Power : 30 KW

    3. Rated Current : 57 A

    4. Starting Current : 365 A

    5. Manufactured by : M/S Siemens.

    Bearing No of lines