Page 68 - Advanced Gas Turbine Cycles
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44                         Advanced gas turbine cycles

                55
                50

                48
              5
              tiu
              2
              $35
              Y
              Y
              Ym
              4
              2 25
              z
                20
                15

                10
                 800    800   looo   1200   1400   1600   1800   Moo   2200   2400
                                      MAXIMUM TEMPERATURE ( "C)
          Fig. 3.14.  Overall efficiency of [CBVI~ cycle as a function of temperature T3 with pressure ratio r as a parameter.

          plant [CHTII as a function of x  and  e). Fig. 3.13 is quite similar to Fig.  3.9, where the
          optimum pressure ratio increases with T3, but the values are now more realistic.
            The [CBTIIG efficiency is replotted in Fig. 3.14, against (T3/T1) with pressure ratio as a
          parameter. There is an indication in Fig.  3.14 that there may be  a limiting maximum
          temperature for the highest thermal efficiency, and this was observed earlier by Horlock
          et al. [8] and Guha [9]. It is argued by the latter and by Wilcock et al. [ 101 that this is a real
          gas effect not apparent in the a/s calculations such as those shown in Fig. 3.9. This point
          will be dealt with later in Chapter 4 while discussing the turbine cooling effects.


          3.4.2.  Comparison of several types of gas turbine plants

            A set of calculations using real gas tables illustrates the performance of the several
          types of gas turbine plants discussed PreViOUSlY, the [CBTIIG, [CBTX]IG, [CB~TX]IG,
          [CICBTXIIG and [CICBTBTXIIG plants. Fig. 3.15 shows the overall efficiency of the five
          plants, plotted against the overall pressure ratio (r) for T3 = 1200°C. These calculations
          have been  made with  assumptions similar to  those made  for Figs.  3.13  and  3.14.  In
          addition  (where  applicable),  equal  pressure  ratios  are  assumed  in  the  LP  and  HP
          turbomachinery, reheating is set to the maximum temperature and the heat exchanger
          effectiveness is 0.75.
            The first point to note is that the classic Hawthorne and Davis argument is reinforced-
          that the optimum pressure ratio for the [CBT]IG plant (r = 45) is very much higher than
          that for the [CBTXIIG plant (r = 9). (The optimum r for the latter would decrease if the
          effectiveness  (E) of the heat exchanger were increased, but it would increase towards that
          of the [CBTIIG plant if  E fell towards zero.)
            While the lowest and highest optimum pressure ratios are for these two plants, the
          addition of reheating and intercooling increases the optimum pressure ratios above that of
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