Page 99 - Intro Predictive Maintenance
P. 99

90       An Introduction to Predictive Maintenance

         complete revolutions (720 degrees) are required for all cylinders to complete a full
         cycle.

         Piston orientations. Crankshafts on positive-displacement reciprocating compressors
         have offsets from the shaft centerline that provide the stroke length for each piston.
         The orientation of the offsets has a direct effect on the dynamics and vibration ampli-
         tudes of the compressor. In an opposed-piston compressor where pistons are 180
         degrees apart, the impact forces as the pistons change directions are reduced. As one
         piston reaches top dead center, the opposing piston also is at top dead center. The
         impact forces, which are 180 degrees out-of-phase, tend to cancel out or balance each
         other as the two pistons change directions.

         Another configuration, called an unbalanced design, has piston orientations that are
         neither in-phase nor 180 degrees out-of-phase. In these configurations, the impact
         forces generated as each piston changes direction are not balanced by an equal and
         opposite force. As a result, the impact energy and the vibration amplitude are greatly
         increased.

         Horizontal reciprocating compressors (see Figure 5–9) should have X-Y data points
         on both the inboard and outboard main crankshaft bearings, if possible, to monitor the
         connecting rod or plunger frequencies and forces.

         Screw. Screw compressors have two rotors with interlocking lobes and act as posi-
         tive-displacement compressors (see Figure 5–10). This type of compressor is designed
         for baseload, or steady-state, operation and is subject to extreme instability if either
         the inlet or discharge conditions change. Two helical gears mounted on the outboard
         ends of the male and female shafts synchronize the two rotor lobes.

         Analysis parameters should be established to monitor the key indices of the com-
         pressor’s dynamics and failure modes. These indices should include bearings, gear
         mesh, rotor passing frequencies, and running speed; however, because of its sensitiv-
         ity to process instability and the normal tendency to thrust, the most critical monitor-
         ing parameter is axial movement of the male and female rotors.

         Bearings. Screw compressors use both Babbitt and rolling-element bearings. Because
         of the thrust created by process instability and the normal dynamics of the two rotors,
         all screw compressors use heavy-duty thrust bearings. In most cases, they are located
         on the outboard end of the two rotors, but some designs place them on the inboard
         end. The actual location of the thrust bearings must be known and used as a primary
         measurement-point location.

         Gear mesh. The helical timing gears generate a meshing frequency equal to the
         number of teeth on the male shaft multiplied by the actual shaft speed. A narrowband
         window should be created to monitor the actual gear mesh and its modulations. The
         limits of the window should be broad enough to compensate for a variation in speed
         between full load and no load.
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