Page 212 - Steam Turbines Design, Applications, and Rerating
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Campbell, Goodman, and SAFE Diagrams for Steam Turbine Blades  191
























            Figure 11.2 Calculating a factor of safety using the Soderberg dia-
            gram. (Dresser-Rand Company, Wellsville, N.Y.)



            Most manufacturers limit the minimum acceptable factor of safety to
            1.50 to cover variations due to machining tolerances, nonhomogenous
            material and other unpredictable factors. There is usually a limit to the
            steam bending stress which in turn helps to minimize the vibratory
            stresses in a stage.
              If the calculated factor of safety of a turbine blade is less than 1.50,
            there are several alternatives: (1) Use a better blade material to
            improve the endurance limit and yield strength; (2) use a less dense
            material (like titanium) to reduce the centrifugal stress; (3) change to
            a different blade section to reduce stresses.
              The Soderberg diagram is used to determine the factor of safety not
            only in blades but also in the shroud, rivet, root, and wheel rim of every
            turbine produced by experienced turbine manufacturers.


            11.3 Campbell Diagram
            The Campbell diagram, or interference diagram, is used to indicate
            what the vibratory stress level may be in a given stage. Since almost all
            blade failures are caused by vibratory stress, many reliability-conscious
            purchasers are requesting Campbell diagrams with turbine quotes or
            orders. A Campbell diagram is a graph with turbine speed (r/min) plot-
            ted on the horizontal axis and frequency, in cycles per second, plotted on
            the vertical axis. Also drawn in are the blade frequencies and the stage-
            exciting frequencies. When a blade frequency and an exciting frequency
            are equal, or intersect, it is called a resonance (see Fig. 11.3).
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