Page 112 - Advanced Gas Turbine Cycles
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Chapter 6


       ‘WET’ GAS TURBINE PLANTS







       6.1.  Introduction

         As Frutschi and Plancherel [I]  have explained, there are two basic gas turbine plants
       with water injection; they are illustrated in Fig. 6.1.
         Fig. 6. la shows diagrammatically the steam injection gas turbine (STIG) plant; steam,
       raised in a heat recovery steam generator (HRSG) downstream of the turbine, is injected
       into the combustion chamber or into the turbine nozzle guide vanes.
         Fig. 6. I b shows diagrammatically the evaporative gas turbine (EGT) in which water is
       injected into the  compressor outlet and  is  evaporated there; the  mixture may  then be
       further heated in the ‘cold’ side of a heat exchanger. It enters the combustion chamber and
       then passes through the turbine and the ‘hot’ side of the heat exchanger.
         There are many variations on these two basic cycles which will be considered later. But
       first we discuss the basic thermodynamics of the STIG and EGT plants.



       6.2.  Simple analyses of STIG type plants
       6.2.1.  The basic STIG plant

         Fig. 6.2 shows a simplified diagram of the basic STIG plant with steam injection S per
       unit  air  flow  into  the  combustion chamber; the  state points  are  numbered.  Lloyd  [2]
       presented a simple analysis for such a STIG plant based on ‘heat input’, work output and
       ‘heat rejected’ (as though it were a closed cycle air and watedsteam plant, with external
       heat supplied instead of combustion and the exhaust steam and air restored to their entry
       conditions by heat rejection). His analysis is adapted here to deal with an open cycle plant
       with a fuel inputfto  the combustion chamber per unit air flow, at ambient temperature To,
       i.e. a fuel enthalpy flux of.fifo. For the combustion chamber, we may write
           ha2 +fhfO  + SA,,  = ( 1 +f)hg3 + Sk,,                          (6.1)

       where  subscripts a, g and  s  refer to air, gas (products of  combustion) and  steam. The
       enthalpy  of  the  steam  quantity  (h,)  is  at  the  same  temperature  as  the  gas,  and  for
       convenience  is  carried  separately through the  analysis, i.e.  the  total  enthalpy is H  =
       (I +f)h, + Sh,. In reality, the steam and gas are fully mixed at all stations downstream of
       the combustion process.
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