VIB ANALYSIS & UNBALANCING-JUN 2008.pdf

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    JUNE 2008

    FEED BACK: 2

    PROJECT: Unit - 2 , NTPC Ramagundam

    PROBLEM: Vibration analysis and balancing

    NTPC Ramagundam units 1 to 3 are Ansaldo Units of rating

    200 MW . The turbine consists of Combined HP IP and LP

    Modules . The first stage of the combined HP-IP turbine is

    Curtis stage .The HP-IP rotor is of single journal at

    bearing 1 and LP rotor is supported at bearing 2 and 3.

    The thrust bearing location is at bearing 1 and pedestals 1

    and 2 are sliding type. The generator bearing are end

    shield mounted .

    The unit had undergone capital overhaul during May

    June. 08 first time by BHEL . LP rotor was replaced

    during Overhaul. The unit was rolled on 14th June after

    overhaul. The turbine rotor system is soaked at 1000 rpm

    for about 1 hour and at 2500 rpm for 10 minutes duringrolling to 3000 rpm.

    Vibration monitoring is carried out with permanently

    mounted shaft rider probes at turbine and generator

    bearings . Each bearing is instrumented with one shaft

    rider probe mounted at approximately 60 degrees to the

    horizontal . In addition an eccentricity probe is provided at

    pedestal 1 .

    During the initial rolling at 3000 rpm , Bearing 2 (LP

    front ) and Bearing 3 (LP rear ) vibrations shaft

    vibrations exceeded the alarm levels 160 microns pk-pk .

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    The coast up plot of LP Rear shaft vibrations are given in

    Fig.1. The vibrations were predominantly of running

    speed component. Since the vibration increase had a steep

    slope around 1500 rpm which is in the zone of LP 1st

    critical speed and were predominantly 1X, it was decided tocarry out balancing at site using LP plane.

    A total of 9 numbers of balancing weights each of 60 grams

    weight were used for balancing LP rotor using LP front

    plane..

    The LP shaft vibration levels after balance correction ,

    were brought around 90 microns peak to peak and bearing

    vibrations around 20 microns peak to peak, which are wellwithin acceptable limits. The coast up plot of LP Rear

    shaft vibrations after balance correction is given in Fig.1.

    The Unit was loaded to rated load and the vibration levels

    were found steady.

    Observation

    Incidentally this LP rotor underwent Slow speed balancing

    at 250 RPM carried out by customer. This has not yielded

    desired results and the rotor once again had to be balanced

    at 3000 rpm. Slow speed balancing may help for rotors

    whose criticals are above operating speed but for flexible

    rotors it is always recommended to carry out balancing at

    operating speeds.

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