Page 37 - Advanced Gas Turbine Cycles
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14                        Advanced gas turbine cycles
           is Hp4 = (1 + f)hp4. Hence

               ha0 +fh,  = w + (1  +f)hP4.                                     (2.3)
           where w = WIM,  is the specific work (per unit air flow).
             If the same quantities of fuel and air were supplied to a calorific value experiment at To
          (Fig. 1.7) then the steady-flow energy equation for that process would yield
               hao +fhm  = (1 +f)hpo +f [Cvlo,                                 (2.4)
          where [CV],  is the calorific value of the fuel. Combining these two equations yields

               f [CVIO = w + (1 +f NhP4  - hw).                                (2.5)
          This equation is often used as an ‘equivalent’ form to Eq. (2.1),  the calorific value term
          being  regarded  as the  ‘heat supplied’  and  the  gas enthalpy difference term  (I  +f)X
          (hp4 - hw) being regarded as the ‘heat rejected’ term.
             In this chapter we will develop more rigorous approaches to the analysis of gas turbine
          plants using both the first and second laws of thermodynamics.


          2.2.  Reversibility, availability and exergy

             The concepts of reversibility and irreversibility are important in the analysis of gas
          turbine plants. A survey of important points and concepts is given below, but the reader is
          referred to standard texts [ 1-31  for detailed presentations.
             A closed system moving slowly through a series of stable states is said to undergo a
          reversible  process  if  that  process  can  be  completely  reversed  in  all  thermodynamic
          respects,  i.e.  if  the  original  state  of  the  system  itself  can  be  recovered  (internal
          reversibility) and its surroundings can be restored (external irreversibility). An irreversible
          process is one that cannot be reversed in this way.
             The objective of the gas turbine designer is to make all the processes in the plant as near
          to reversible as possible, i.e. to reduce the irreversibilities, both internal and external, and
          hence to obtain higher thermal efficiency (in a closed cycle gas turbine plant) or higher
          overall efficiency (in an open gas turbine plant). The concepts of availability and exergy
          may be used to determine the location and magnitudes of the irreversibilities.


          2.2.1.  Flow in the presence of an environment ut To (not involving chemical reuction)
             Consider first the steady flow of fluid through a control volume CV between prescribed
          stable states X and Y (Fig. 2. I) in the presence of an environment at ambient temperature
          To (Le. with reversible heat transfer to that environment only). The maximum work which
          is obtained in reversible flow between X and Y is given by

               [(WCV)REVG = Bx - BY9                                           (2.6)
          where B is the steady flow availability function
               B = H  - ToS,                                                   (2.7)
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