Page 293 - Machinery Component Maintenance
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Balancing  of  Machinery  Components   275

                     1. The balancing speed should be as low as possible to decrease cycle
                        time, horsepower requirement, wind, noise, and danger to the oper-
                        ator.
                     2.  It should be high enough so that the balancing machine has suffi-
                        cient sensitivity to achieve the required balance tolerance with ease.




                     However, there is one other important consideration to be made before
                   deciding upon a balancing speed substantially lower than the rotor’s ser-
                   vice speed; namely, is the part (or assembly) rigid?
                   Is the Rotor “Rigid”?

                     Theoretically it is not, since no workpiece is infinitely rigid. However,
                   for balancing purposes there is another way of looking at it. (See defini-
                   tion of  “Rigid Rotor” in Appendix 6A.)
                     Any rotor satisfying this definition can be balanced on standard balanc-
                   ing machines at a speed which is normally well below the service speed.
                   When selecting the balancing speed, consider the following guidelines:
                     1.  Determine the proper balance tolerance by consulting Table 6-5 and
                        subsequent nomograms.
                     2.  Select the lowest available speed at which the balancing machine
                        provides at least 1/4  in. amount-of-unbalance indicator deflection or
                        5 digital units of indication for the required balance tolerance. It is
                        usually  of  no  advantage to  select  a  higher  speed  for  achieving
                        greater sensitivity, since the repeatability of a good quality balanc-
                        ing machine is well in line with today’s exacting balance tolerances.
                     Whether a given rotor can be termed “rigid” as defined in Appendix
                   6A depends on numerous factors that should be carefully evaluated. For
                   instance:
                     1.  Rotor  configuration and  service speed.  Technical literature pro-
                        vides  reference  tables  which  permit  approximating  the  critical
                        speed of the first flexural mode from the significant geometric rotor
                        parameters (see Appendix 6D). In most cases it can be assumed that
                        a rotor can be balanced successfully at low speed if its service speed
                        is less than 50 percent of the computed first flexural critical speed.
                     2.  Rotor  design  and  manufacturing  procedures.  Rotors  which  are
                        known to be flexible or unstable may, nevertheless be balanced sat-
                        isfactorily at low speed if certain precautions are taken. Rotors of
                        this type are classified as “quasi-rigid rotors.”
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