Page 122 - Advanced Gas Turbine Cycles
P. 122

94                         Advanced gas turbine cycles

            Firstly, Fig. 6.8a shows the T, s (air property) diagram for an EGT cycle, a ‘wet’ version
          of the CBTX cycle with water injected to cool the compressor discharge air. Frutschi and
          Plancherel argued that the virtue of such evaporative cooling before the heat exchanger is
          to drop the hot gas temperature at the exchanger exit. A closed cycle version of this EGT
          cycle, in which the water injected was condensed after exit from the heat exchanger and
          then  recirculated to complete the cycle, was initially considered by  Horlock  [5]. This
          analysis showed that the temperature of the gas at exit from the heat exchanger was indeed
          reduced in the wet cycle; the total heat rejected (QA)  was unchanged from that in the dry
          cycle, because of  the condensation of the steam which was necessary to close the wet
          cycle. Some of  the heat rejected in the dry cycle is  simply moved from the gas flow
          downstream of the hot side of the heat exchanger to the additional condenser required in
          the wet cycle.
            However, the turbine work has been increased because of the extra water vapour flow
          through the turbine, while the compressor work is unchanged. Thus Eq. (6.17), which is
          still valid, with turbine work equal to the heat supplied, shows that the thermal efficiency
          increases compared with  the dry cycle. It is important to realise that  this efficiency is
          increased not because of a reduction in the heat rejected (QA)  but because of the increase in
          WT. The heat rejected is still equal to the compressor work.
            If, as suggested in  Section 6.2.1, the turbine work is increased by  a factor (1 + 29,
          where S is the water vapour flow, then the dry and wet efficiencies may be written as

               WRY  = 1 - (WC/WT DRY),                                       (6.19a)
          and

               %ET  =  - [wC/(I  f 2S)(WT DRY],                             (6.19b)
          so that

               (WET  - TDRY)~~ - WRY)   2W1 + 2s)                           (6.19~)
          The same expression applies for some of the other variations of the EGT cycle considered
          below (e.g. the recuperative water injection (RWI) plant with intercooling).
            Horlock  then  considered  a  cycle  proposed  by  El-Masri  [6]  in  which  the  water
          evaporation takes place not in an aftercooler but in the cold side of the heat exchanger;
          again a cycle in closed form was considered, with injected water finally condensed and
          recirculated. The continuing evaporation increases the effective specific heat of the cold
          side fluid and can increase the effectiveness of the heat exchanger towards unity [7]. The
          Hawthorne and Davis analysis for the dry [CBTIIXR cycle (and also for the other more
          complex dry cycles) then becomes relevant. For a ‘perfect’ heat exchanger in the closed
          EGT cycle, in which the continued evaporation on the cold side can lead to the hot and
          cold  side  specific heats  becoming  the  same,  the  heat  rejected  is  now  equal  to  the
          compressor work. The temperature-entropy  diagram for the ‘carrying’ gas is now shown
          in Fig. 6.8b. The expression for the air standard efficiency of the closed dry CBTX cycle
          (Eq. (6.17)) is also valid for this EGT cycle, with QA  = WC, the value in a dry cycle. But
          the turbine work WT  (= QB) is increased because of the extra steam passing through the
          turbine, with its associated enthalpy drop. Again this is the essence of the EGT cycle where
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