Page 124 - Advanced Gas Turbine Cycles
P. 124

96                         Advanced  gas turbine cycles
          an increase in turbine work (and heat supplied) with a constant compressor work (and heat
          rejected), leads to an increase in efficiency.
             A further variation of the El-Masri EGT cycle is one in which the evaporation takes
          place both in an aftercooler and within the cold side of  the heat exchanger (Fig. 6.8~).
          Eq. (6.17) is still valid, but the efficiency is increased because more water can be injected
          and the turbine work increased further.
             It was shown in Ref. [5] that the arguments given above for the closed EGT cycles also
          hold  good  for open EGT cycles, but  this  analysis is  not  repeated here.  Some simple
          parametric  calculations  were  given  to  illustrate  the  increased  thermal  efficiency  of
          practical  open EGT cycles, corresponding to  Fig. 6.8a-c.  It  was  assumed  that  water
          injection was
           (a)  in the aftercooler (sufficient to saturate the compressor discharge gas),
           (b)  within the heat exchanger (cold side, to raise the effective specific heat), and
           (c)  in  both  aftercooler and  heat  exchanger (cold side).
             Evaporative  mixing  at  low  velocity  was  assumed  in  the  aftercooler, the  pressure
          remaining constant. Allowance was made for the real gas effects (increased specific heat of
          the products of combustion at high temperature), of turbine cooling and intercooling. A
          method of calculating the turbine work similar to that developed by Cerri and Arsuffi [8]
          for the STIG cycle was used. It was assumed that evaporative cooling was carried out by a
          small quantity of  water so that the temperatures of the working gas carrying the steam
          remain unchanged (except after injection for intercooling and at exit from the hot side of
          the heat exchanger). The additional steam in the turbine was assumed to be superheated (at
          low partial pressure) and its drop in enthalpy was obtained from steam tables knowing the
          original ‘dry’ gas temperature drop.
             Plots  of  efficiency  against  pressure  ratio  for  the  full  injection  EGT  plant,  for  a
          maximum to  minimum temperature  =5,  are  shown in Fig. 6.9, compared with  lower
          values of efficiency in the dry CBTX plant. There are several points to be noted: first that
          an increase in efficiency is worthwhile, up to 10%; secondly that the total water injection is
          up to over 10% of the air mass flow; and thirdly that the optimum pressure ratio increases
          to about 8, from about 5 for that of the dry cycle.
             Similar calculations (Fig. 6.10) were made for intercooled cycles, without and with
          water injection, i.e. comparing the efficiency of the dry CICBTX cycle with an elementary
          recuperated water injection plant, now a simple version of the so-called RWI plant (see
          Section 6.4.2.  I). Again there is an increase in thermal efficiency with water injection, but it
          is  not  as great as for the  simple EGT plant compared with  the dry CBTX plant; the
          optimum pressure ratio, about 8 for the dry intercooled plant, appears to change little with
          water injection.
            These  smaller  effects  are  related  to  the  smaller  amount  of  water  that  can  be
          injected for the intercooled cycle. Applying Eq. (6.19~) to the near optimum condition
          of  Fig.  6.9  (~RY = 0.5,  with  S = 0.1)  yields  (?)wET - ?DRY)  = 0.08. Applying  the
          same  equation  to  the  near  optimum  condition  of  Fig.  6.10   = 0.53,  with
          S = 0.04) yields (m - %RY)  = 0.035. Both  these  approximate estimates are  very
          close to the  detailed calculations of  the  increases in  thermal efficiency shown in  the
          two  figures.
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