Page 198 - Subyek Teknik Mesin - Forsthoffers Best Practice Handbook for Rotating Machinery by William E Forsthoffer
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Be st Practice 3 .18          Compressor Best Practices

        Table 3.18.1 Typical compressor oil film bearing parameters (Courtesy of Elliott Co.)
        4   1.6"tilt 20.5" TB 3.0" shaft end 7.5e6.5" shaft Bendix coupling
        Static bearing load (lbs)     897                     diameter (inches)                   4.00
        Bearing station               12                      length (inches)                     1.60
        Bearing location              thrust                  diam assembly clearance (inches)    5.7487Ee03

        Bearing type                  tilt pad                diam machined clearance (inches)    8.7500Ee03
        Location of load              between pads            inlet oil temperature (deg F)       120.0
        Preload                       0.343                   type of oil                         DTEelight
                                                                                                  (150SSU @100 F)
















































       modeling the rotor and bearings, most rotor response calcula-  When selecting machinery, the best practice is to request
       tions also include the following additional inputs:
                                                            specific vendor experience references for installed equipment
       - Bearing support stiffness                          with similar design parameters as follows:
       - Oil film seal damping effects                       - Bear span O major shaft diameter
                                                            - Speeds
          Of all the input parameters, the effects of bearing and seal oil
       film parameters are the most difficult to calculate and measure.  - Bearing design
                                                            - Seal design
       Therefore, a correlation difference will always exist between the
       predicted and actual values of critical speed. Historically,  - Operating conditions (if possible)
       predictedvaluesofNC 1 (firstcriticalspeed)generallyagreewithin  Once the rotor system is adequately modeled, the remaining
         5%. However, wide variations between predicted and actual  input parameter is the amount and location of unbalance. Since
       values above the first critical speed (NC 1 ) exist for NC 2 ,NC 3 ,etc.  the objective of the rotor response study is to accurately predict

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