Vibration analysis at Vijajawada.pdf

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    PROJECT: VIJAYAWADA TPS

    PROBLEM: VIBRATION ANALYSIS OF UNIT 5, 210 MW

    SIEMENS TURBINE - SIEMENS GENERATOR

    VTPS unit 5 was rolled on 23-05-08 after rectification works carried

    out for Generator Earth fault. Bently Nevada ADRE Vibration analyzer

    system was used for vibration measurements and analysis. During coast

    up of the unit, Generator front and rear vertical vibrations were

    recorded. The coast up vibration values both amplitude in microns and

    phase are given in figure 1. The bode plot shows that the run up of

    generator rotor is very smooth.

    Table 1 and 2 gives the bearing pedestal vibration levels for Turbine,

    Generator and Exciter both in velocity and displacement units. The

    table gives 1X running speed vibration component , corresponding

    phase and overall vibration levels which is a sum of all vibration

    frequency components. The bearing vibrations on all pedestals are

    satisfactory except for exciter primarily in horizontal direction. Theexciter vibrations which were 85 microns peak - peak at 3000 RPM

    showed a steady increase after synchronization and at rated load were

    128 microns peak - peak. Figure 2 shows the velocity and displacement

    spectrums of exciter bearing in horizontal direction. The spectrum

    shows that the bearing vibrations are predominantly of running speed

    component.

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    Table 3 gives the control room vibration levels at rated load. The

    Bearing and shaft vibrations are satisfactory except at exciter bearing.

    The Exciter bearing vibrations are above alarm values . The increase in

    exciter vibrations with time before stabilization could be because of the

    following reason.

    Design diametrical clearance between spigot and recess in Generator -

    Exciter coupling should be 0.03mm to 0.05mm . But the measured

    clearance at site is 0.12 mm . A 0.05 mm shim has been introduced

    between recess in Generator rotor and Spigot in exciter rotor . This

    was not providing a desired solution to the high exciter vibration

    problem.

    A permanent solution suggested would be to ream and introduce dowels

    at 120 degrees apart positions on Generator Exciter couplings as

    being followed in Hyderabad 120 MW units. Till such time customer

    was advised to operate the unit with close monitoring of exciter

    vibration levels.

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    Fig 1. Generator Front Vertical and Rear vertical Bode Plot

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    Figure 2. Exciter Pedestal Vibrations Horizontal, Velocity and

    Displacement spectrums

    Table 1. Bearing vibrations in Velocity and Displacement units at 3000 RPM

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    Velocity in mm/sec Displacement in microns

    pk-pk

    1X Phase Overall 1X Phase Overall

    Vertical 1.2 243?

    6 7 333?

    10Horizontal 1.0 171? 2 6 260? 8

    HP

    FrontAxial 1 228? 2.6 6 317? 9

    Vertical 1.2 89? 3.8 8 176? 10

    Horizontal 1.6 287? 2.1 10 16? 10

    HP

    Rear

    Axial 0.4 98? 1.2 3 186? 5

    Vertical 0.6 302? 1.5 4 32? 5

    Horizontal 0.1 --- 1.2 1 --- 3IP

    RearAxial 0.7 284? 1.1 4 14? 6

    Vertical 1.8 358? 2.5 10 84? 12

    Horizontal 3.6 163? 4.4 23 252? 26LP

    RearAxial 5.2 294? 5.3 33 22? 34

    Vertical 4.2 309?

    4.2 26 41?

    28Horizontal 2.4 297? 3.1 15 26? 16

    Gen

    FrontAxial 1.5 157? 1.8 10 246? 11

    Vertical 4.4 142? 4.9 29 230? 30

    Horizontal 2.3 52? 2.4 15 141? 16Gen

    rearAxial 1.5 317? 1.9 9 49? 11

    Vertical 0.4 180? 1.3 2 263? 5

    Horizontal 13 22? 14 85 110? 86Exciter

    Axial 6.2 32? 6.6 38 122? 40

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    Table 2. Bearing vibrations in Velocity and Displacement units at 215 MW Load

    Velocity in mm/sec Displacement in microns

    pk-pk

    1X Phase Overall 1X Phase OverallVertical 1.0 --- 3 7 313? 8

    Horizontal 1.0 --- 3.5 6 242? 9HP

    Front Axial 0.9 --- 3.0 5 295? 10

    Vertical 0.5 --- 7 4 198 10

    Horizontal 1.7 --- 4 10 51? 12HP

    Rear Axial 0.8? 2 2 --- 5

    Vertical 1.0 --- 0.3 7 120?

    11Horizontal 0.5 --- 1.8 3 257 6

    IP

    Rear Axial 0.3 ---- 1.5 1--- 4

    Vertical 4.0 330? 6.2 27 62? 29

    Horizontal 5.4 177? 7.2 34 263? 35LP

    RearAxial 11 161? 11 70 248? 72

    Vertical 7.0 319? 7.9 46 51? 48

    Horizontal 2.0 300? 3.6 12 36? 17Gen

    Front Axial 2.6 156? 3.9 17 240? 19

    Vertical 3.3 128? 5.4 21 213? 27

    Horizontal 0.3 --- 3.2 4 146? 12

    Gen

    rear

    Axial 1.3 ---- 2.3 9 47? 11

    Vertical 1.7 ---- 3.3 10 339? 15

    Horizontal 21 7 21 128 96? 128Exciter

    Axial 7 33? 9 47 126? 53

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    Table 3. Control room vibration values

    24-05-0812.53 hoursLoad: 215.3 MW

    Speed : 2954 RPM

    Vacuum: -0.885 kg/cm2

    Bearing Vibrations Shaft Vibrations

    in microns peak

    HP Front 1.3 47.3

    HP Rear 2.5 39.9

    IP Rear 2.4 38.7

    LP Rear 2.5 56.0

    Gen Front 18.4

    Gen Rear 8.3

    Exciter 43.4 89.7

    Bearing temp

    HP front Thrust HP Rear IP Rear LP Rear Gen Front Gen Rear Exciter

    62.3 63.3 61.3 86.3 83.3 78.2 78.9 54.767.2 61.5 59.3 75.1 85.6 72.4 73.6 59.7

    54.1 69.0 59.975.7 68.8 57.2