Page 139 - Subyek Teknik Mesin - Forsthoffers Best Practice Handbook for Rotating Machinery by William E Forsthoffer
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Compressor Best Practices    Be st Practice 3.3

                                                                                Fig 3.3.6   Impeller geometry vs. specific speed



























              savings realized by designing a compressor for a higher  bearings. This led to the assumption that only the stiffness of the
              efficiency.                                           rotor supported by rigid bearings needed to be considered in the
                Referring back to Figure 3.3.6, the calculation of specific  analysis of the natural frequency. Countless machinery prob-
              speed for the first impeller by the contractor or end user will  lems have proven this assumption to be false over the years. The
              give an indication of the type of dynamic compressor blading to  concept of the ‘rotor system’ must be thoroughly understood.
              be used. One other comment; Sundstrand Corporation suc-  The rotor system consists of the rotor itself, the characteristics
              cessfully employs an integral high speed gear box design for low  of the oil film that support the rotor, the bearing, the bearing
              flow, high head applications or for low specific speed applica-  housing, the compressor case that supports the bearing, com-
              tions. The use of a speed increasing gear box (for speeds up to  pressor support (base plate), and the foundation. The stiffness
              34,000 RPM) enables the specific speed to be increased, and  and damping characteristics of all of these components together
              therefore resulting in higher efficiency and less complexity than  result in the total rotor system that produces the rotor response
              would be obtained with a multistage compressor design  to excitation forces.
              approach.                                              We will examine a typical rotor response case in this section
                                                                   and note the various assumptions, the procedure modeling, the
                                                                   placement of unbalance, the response calculation output, and
              Critical speeds and rotor response                   discuss the correlation of these calculations to actual test results.

              The term ‘critical speed’ is often misunderstood. In nature, all
              things exhibit a natural frequency, which is defined as that  Critical speeds
              frequency at which a body will vibrate if excited by an ex-
              ternal force. The natural frequency of any body is a function of  The natural frequency of any object is defined by the
              the stiffness and the mass of that body. As mentioned, for  relationship:
              a body to vibrate, it must be excited. A classical example of                     r ffiffiffiffiffi
                                                                                                  K
              natural frequency excitation is the famous bridge ‘Galloping           F NATURAL ¼  M
              Gerty’ in the state of Washington, which vibrated to de-
              struction when its natural frequency was excited by prevailing  Where: K ¼ Stiffness
              winds.                                                 M ¼ Mass
                In the case of turbo-compressor rotors, their natural fre-  When excited by an external force, any object will vibrate at
              quency must be excited by some external force to produce  its natural frequency. If the frequency of the exciting force is
              a response that will result in increased amplitude of vibration.  equal to the natural frequency of the object, and no damping is
              One excitation force that could produce this result is the speed  present, the object can vibrate to destruction. Therefore, if the
              of the rotor itself, which gives rise to the term ‘critical speeds’.  frequency of an exciting force equals the natural frequency of an
              The term ‘critical speed’ defines the operating speed at which  object, the exciting force is operating at the ‘critical frequency’.
              a natural frequency of a rotor system will be excited. All rotor  Rotor speed is one of the most common external forces in
              systems have both lateral (horizontal and vertical) and torsional  turbo-machinery. When the rotor operates at any rotor system
              (twist about the central shaft axis) natural frequencies. Only  natural frequency, it is said that the rotor is operating at its
              lateral critical speeds will be discussed in this section.  critical speed. The critical speed of a rotor is commonly desig-
                In the early days of rotor design, it was thought that the rotor  nated as NC and the corresponding natural frequencies or
              system consisted primarily of the rotor supported by the  critical speeds are: NC 1 ,NC 2 ,NC 3 , etc.

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