Page 295 - Intro Predictive Maintenance
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286       An Introduction to Predictive Maintenance


         14.1 COMMON GENERAL FAILURE MODES
         Many of the common causes of failure in machinery components can be identified by
         understanding their relationship to the true running speed of the shaft within the
         machine-train.

         Table 14–1 is a vibration troubleshooting chart that identifies some of the common
         failure modes.  This table provides general guidelines for interpreting the most
         common abnormal vibration profiles.  These guidelines, however, do not provide
         positive verification or identification of machine-train problems. Verification requires
         an understanding of the failure mode and how it appears in the vibration signature.

         The sections to follow describe the most common machine-train failure modes:
         critical speeds, imbalance, mechanical looseness, misalignment, modulations, process
         instability, and resonance.


         14.1.1 Critical Speeds
         All machine-trains have one or more critical speeds that can cause severe vibration
         and damage to the machine. Critical speeds result from the phenomenon known as
         dynamic resonance.

         Critical speed is a function of the natural frequency of dynamic components such as
         a rotor assembly, bearings, and so on. All dynamic components have one or more
         natural frequencies that can be excited by an energy source that coincides with, or is
         in proximity to, that frequency. For example, a rotor assembly with a natural frequency
         of 1,800 rotations per minute (rpm) cannot be rotated at speeds between 1,782 and
         1,818rpm without exciting the rotor’s natural frequency.

         Critical speed should not be confused with the mode shape of a rotating shaft. Deflec-
         tion of the shaft from its true centerline (i.e., mode shape) elevates the vibration ampli-
         tude and generates dominant vibration frequencies at the rotor’s fundamental and
         harmonics of the running speed; however, the amplitude of these frequency compo-
         nents tends to be much lower than those caused by operating at a critical speed of the
         rotor assembly. Also, the excessive vibration amplitude generated by operating at a crit-
         ical speed disappears when the speed is changed. Vibrations caused by mode shape tend
         to remain through a much wider speed range or may even be independent of speed.

         The unique natural frequencies of dynamic machine components are determined by
         the mass, freedom of movement, support stiffness, and other factors. These factors
         define the response characteristics of the rotor assembly (i.e., rotor dynamics) at
         various operating conditions.

         Each critical speed has a well-defined vibration pattern. The first critical excites the
         fundamental (1¥) frequency component; the second critical excites the secondary (2¥)
         component; and the third critical excites the third (3¥) frequency component.
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