Page 307 - Fluid Mechanics and Thermodynamics of Turbomachinery
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288 Fluid Mechanics, Thermodynamics of Turbomachinery
                            The overall efficiency can now be written as
                                                                          2
                                     W    KU 2       KU  2            U       c 2 1
                                  0 D           D   h      D   h  2K
                                        gH E           gH g           c 1    2gH E
                                                 2              2
                              ∴   0 D   R   N  2K  N   D   N .  R  2K  /.                 .9.11/
                          Hence, the mechanical efficiency is,
                                          2
                                m D 1  2K  /  R .                                         (9.12)
                          It can be seen that according to eqn. (9.12), as the speed ratio is reduced towards
                          zero, the mechanical efficiency increases and approaches unity. As there must be
                          some bearing friction at all speeds, however small, an additional term is needed in
                                                    2
                                                          2
                          the loss equation of the form Ac C kU , where A is another dimensionless constant.
                                                    0
                          The solution of this is left for the student to solve.
                            The variation of the overall efficiency based upon eqn. (9.11) is shown in
                          Figure 9.9 for several values of K. It is seen that the peak efficiency:
                          (1) is progressively reduced as the value of K is increased;
                          (2) occurs at lower values of   than the optimum determined for the runner.

                          Thus, this evaluation of overall efficiency demonstrates the reason why experimental
                          results obtained of the performance of Pelton turbines always yields a peak efficiency
                          at a value of  < 0.5.
                            Typical performance of a Pelton turbine under conditions of constant head and
                          speed is shown in Figure 9.10 in the form of the variation of overall efficiency
                          against load ratio. As result of a change in the load the output of the turbine must
                          then be regulated by a change in the setting of the needle valve in order to keep the
                          turbine speed constant. The observed almost constant value of the efficiency over
                          most of the load range is the result of the hydraulic losses reducing in proportion to
                          the power output. However, as the load ratio is reduced to even lower values, the
                          windage and bearing friction losses, which have not diminished, assume a relatively
                          greater importance and the overall efficiency rapidly diminishes towards zero.

                                       1.0




                                      h 0                              0.2 K = 0
                                                    Locus of maxima  0.4



                                         0
                                                 0.2     0.4     0.6     0.8     1.0
                                                              n
                          FIG. 9.9. Variation of overall efficiency of a Pelton turbine with speed ratio for several
                                               values of windage coefficient, K.
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