Page 158 - Improving Machinery Reliability
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130   Improving Machinery Reliability

                       17. Discharge pressure and brake horsepower versus ICFM curves at rated condi-
                          tions for each section or casing on multiple section or casing units in addition
                          to composite curves at 80%, 90%, loo%, and 105% of rated speed
                            For variable molecular weight (MW) gases, curves also shall be furnished at
                          maximum  and minimum MW. For air compressors, curves also shall be fur-
                          nished at three additional specified inlet temperatures.
                       18. “Pressure above suction pressure behind the balance drum” versus “unit load-
                          ing of the thrust shoes,” both in pounds per square inch (bar), using rated con-
                          ditions as the curve basis
                            The curve shall extend from a pressure equal to suction pressure behind the
                          drum to a pressure corresponding to at least 500 pounds per square inch  (35
                          ata) unit  loading  on  the thrust  shoes.  Balance  drum OD, effective  balance
                          drum area, and  expected  and  maximum  recommended  allowable pressure
                          behind the balance drum shall be shown on the curve sheet.
                            Will balance drum labyrinth wear cause overloading of the thrust bearing?
                          What happens when fouling (polymerization) occurs in the balance line? Is the
                          design safe for a wide range of suction pressures?
                       19. Speed versus starting torque curve
                            Will the motor be  designed to safely  start the  compressor? Even  more
                          important for gas turbine drivers!
                       20. Vibration analysis data, including:
                          a. Number of vanes-each   impeller
                          b. Number of vanes-each  guide vane
                          c. Number of teeth-gear-type  couplings
                            These are required  for machine signature “real time” on line diagnostic or
                          spectrum analysis. They will allow identification of  relevant frequencies, and
                          possibly be useful in determining which component has undergone deteriora-
                          tion. Refer also to the illustrative example in Chapter  1, “How to Deal with the
                          Typical API Data Sheet.”
                       21. Lateral critical analysis, including:
                          a. Method used
                          b. Graphical display of  bearing and support stiffness and its effect on critical
                            speeds
                          c. Graphical display of rotor response to unbalance
                          d. Graphical display of overhung moment and its effect on critical speed
                            Reviews will identify whether there is risk of operating too close to critical
                          speed, or whether rotor is likely to vibrate at the slightest sign of unbalance. If
                          gear couplings  are used, the effective (instantaneous) overhung moment may
                          change as  a function  of  tooth  loading  or tooth  friction.  The probability  of
                          encountering critical speed problems as a function of gear-coupling deteriora-
                          tion can be investigated by examining graphical displays of effective overhung
                          moment versus critical speed.
                       22. Torsional critical speed analysis for all motor and gear units, including:
                          a. Method used
                          b. Graphical display of mass-elastic system
                          c. Tabulation identifying the mass-moment torsional stiffness for each compo-
                            nent in the mass-elastic system
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