Page 114 - Improving Machinery Reliability
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86    Improviiig Machinery Reliability

                    Generally, each significant shaft diameter change is represented by one or more sta-
                    tions. A  station is generally  located at each added mass or inertia, at each bearing
                    and  seal location,  and  at  each potential  unbalance  location.  A  typical  rotor  shaft
                    drawing and the computer model are given in Figure 3-1.
                      Rotating elements such as wheels and impellers are modeled as added masses and
                    inertias  at the  appropriate  locations  on the  shaft. The polar and  transverse  mass
                    moments of inertia are included in the analyses to simulate the gyroscopic effects on
                    the rotor.  The gyroscopic  effects are particularly  significant  on  overhung  rotors
                    where the impeller or disk produces a restoring moment when whirling in a deflected
                    position.
                      Couplings are simulated as concentrated added weights and inertias. Normally the
                    half  coupling weight is placed  at the center  of  gravity of  the  half  coupling. When
                    necessary, the entire train, including the driver and driven equipment, can be  mod-
                    eled by using programs that can simulate the shear loading across the coupling with-
                     out transferring the moments. Once the shaft model is completed, the critical speed
                     map can be calculated.
                     Critical Speed Map. This is a logarithmic plot  of  the undamped  lateral  critical
                     speeds versus the combined support stiffness, consisting of the bearing and support
                     structure as springs in series. The critical  speed map for a seven-stage compressor
                     rotor is given in Figure 3-2. The critical speed map provides the information needed
                     to understand  the  basic response  behavior  of  rotors; therefore,  it  is important to
                     understand how the map is developed.
                       For large values of  support stiffness, the rotor critical speeds are called the rigid
                     bearing critical  speeds. If  the bearing stiffness is infinity, the vibrations are zero at
                     the bearings,  and the first natural  frequency  for shafts that do not have  overhung
                     impellers or disks is analogous to a simply supported beam.
























                                 Figure 3-1. Typical shaft drawing and computer model.
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