Page 475 - Practical Machinery Management for Process Plants Major Process Equipment Maintenance and Repair
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452   Major Process Equipment Maintenance and Repair


                       What is meant by condition monitoring? Quite  simply it is the observa-
                     tion and analysis of externally observable parameters to estimate the in-
                     ternal condition of the machine. As the word “estimate” implies, this is
                     not an exact science, but one that requires a great deal of skill and experi-
                     ence. The technology of condition monitoring is advancing rapidly as
                     lower cost computers make sensing, trending, and analyzing turbine data
                     easier and more accessible. The parameters most closely monitored are
                     performance and vibration.
                       Monitoring may be as simple as the analysis of  a few key variables
                     which are manually recorded on log sheets. It may also be as extensive as
                     the computerized collection and analysis of 150 variables for a single gas
                     turbine train. Process plants which place a high value on outage time and
                     operate unspared single train units can easily justifj the monitoring of every
                     conceivable variable around a gas turbine on the basis of proper identifica-
                     tion of the cause of nips alone (Figure 9-5).
                       Vibration monitoring of  gas  turbines presents a few difficulties not
                     normally encountered on other types of twbomachinery. High tempera-
                     tures in and around the engine require that special precautions be taken to
                     ensure probe wires remain cool. On industrial turbines with noncontact
                     type probes many times this means running the probe leads in the bearing
                     oil drain piping, since this path is cooled by the flow of oil. Monitoring
                     with seismic probes is another option employed by some industrial users
                      and is the only practical method for aircraft derivative units.  On large
                      industrials establishing good locations for these probes in close proximity
                      to the bearing is sometimes difficult. Many users have chosen to retrofit
                      noncontact probes with good success when unavailable through the man-
                      ufacturer.
                        Performance monitoring is carried out in basically the same fashion on
                      each engine, although the analysis of the data taken is quite different de-
                      pending on the type of turbine and control scheme employed. Basically
                      one tries to determine the engine’s ability to produce power for a given
                      amount of fuel. If carried out properly this analysis should not only hdi-
                      cate the deterioration of thermodynamic performance, but give an indica-
                      tion of the mechanical health of the engine. The simplest form of perfor-
                      mance monitoring involves the trending of key variables (e.g.,  pressure
                      ratio, compressor speed, turbine speed, fuel flow) associated with the en-
                      gine and comparing them with a baseline which has been developed. This
                      method is cQmmonly used on fixed geometry engines, both industrial and
                      derivative. kiable geometry engines, however, do not lend themselves
                      easily to this type of analysis making trending extremely difficult in com-
                      parison to the fixed geometry engines. Thermodynamic gas path analysis
                      is really the only good way to establish the performance of  a variables
                      geometry turbine. This involves an iterative process of matching the per-
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