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168   Chapter Ten

























            Figure 10.3 Bearing support design data. (General Electric Company, Fitch-
            burg, Mass.)

            tion response of the rotor due to assumed unbalanced forces has made
            the response calculation the ultimate criterion for successful turbine
            operation.
              In its basic format, the dynamic stiffness concept assumes that the
            rotor has two bearings with equal support stiffness characteristics. In
            practice, the two bearings are usually the same type and do not differ
            greatly in diameter, length, or reaction loading. A good approximation
            of effective dynamic stiffness is an average of the two. Different verti-
            cal and horizontal bearing stiffnesses are considered separately, which
            theoretically gives rise to pairs of critical speeds. Each pair involves
            the same mode shape, but they occur at different speeds corresponding
            to the vertical or horizontal orientations. The effects of bearing damp-
            ing on critical speeds are usually neglected as are the cross-coupling
            terms. The effects of the casing support stiffness are included in series
            with the bearing oil film stiffness.
              Figure 10.4 shows what happens when both the vertical and hori-
            zontal bearing support stiffness are different. Each rotor mode curve is
            intersected twice; therefore, there will be pairs of critical speeds for
            each mode. The horizontal bearing stiffness is usually lower, and the
            lower critical of the pair will exhibit an elliptical shaft whirl orbit that
            is horizontally oriented. As speed increases, the shaft orbit will rotate
            to a vertically oriented ellipse at the speed where the vertical support
            stiffness curve intersects the rotor mode curve.
              In actuality, many of the discrete theoretical critical speeds are not
            evident in an operating turbine because of damping. In the case of sep-
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