Page 217 - Steam Turbines Design, Applications, and Rerating
P. 217

196   Chapter Eleven

            TABLE 11.1 Comparison between Vibration Testing and NASTRAN Analysis
            of a Particular Design
                                                      NASTRAN
                              1st rotor  2nd rotor                   Maximum
                               test fn,  test fn       analysis      estimated
                 Mode           Hz        Hz       fn, Hz   Error,* %  error, %
            1 1st TAN           835.       790.      799.      2        5
            2 1st AXIAL        1420       1423.     1274      10       10
            2 AXIAL ROCKING      —        1675.     1447      14       15
            4 TAN FIXED        3020       2860      2879       2        5
               SUPPORTED
            5                                       2931
            6                                       3007
            7                                       3047
            8                  3090       3153      3058       2        5
            9 Axial “U”        3580       3546      3531       2        5
            10 2nd TAN                              4047      —        —
            11 AXIAL, FIXED      —        3880.     4483      16       20
               SUPPORTED         —
            12                                      4688
            13                   —        4125.     4765      16       20
             * Error is that compared to be average test value.
             SOURCE: Dresser-Rand Company, Wellsville, N.Y.


            quency above the fourth harmonic of running speed excitation for vari-
            able speed turbines. For constant speed turbines it is conceivable to
            have a blade frequency that is less than four times the running speed,
            but it will be tuned between exciting harmonics at the operating r/min.
              Nozzle-passing frequency excitation is caused by the steam wakes at
            the trailing edges of nozzle vanes as the blade passes from one nozzle
            to the next. The first harmonic of nozzle-passing frequency is equal to
            (r/min/60 × number of nozzles in 360°) in units of Hertz.
              Partial admission excitation is similar to nozzle-passing frequency
            excitation, except instead of each nozzle causing one pulse of excita-
            tion, a group of active nozzles will be causing the exciting force. As a
            blade passes from inactive nozzling to an active group of nozzles back
            to inactive nozzling, it will receive one pulse of excitation. Partial
            admission nozzling will provide a low harmonic of running speed exci-
            tation that is dependent on the number and spacing of the nozzle
            groups.
              There are other exciting frequencies that occur in turbines besides
            these three most common discussed earlier. Struts or support ribs in
            casings can cause disturbances in the steam flow. Diaphragm manu-
            facturing variations can cause both nozzle passing and low harmonics
            of running speed excitations; sharp turns in the steam path can cause
            random excitations.
              The vibratory stress at a resonant condition depends on the
            strength of the exciting force, the resonant mode shape of the blades,
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