Page 169 - Handbook of Energy Engineering Calculations
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the fuel input and oxygen consumed, using the gas specific-heat method.


               Calculation Procedure:


               1. Determine the air equivalent in the exhaust gases
               In gas-turbine–based cogeneration/combined-cycle projects, the HRSG may
               be fired to generate more steam than that produced by the gas-turbine exhaust
               gases.  Typically,  the  gas-turbine  exhaust  gas  contains  14  to  15  percent

               oxygen by volume. So the question arises: How much fuel can be fired to
               generate more steam? Would the oxygen in the exhaust gases run out if we
               fired  to  a  desired  temperature?  These  questions  are  addressed  in  this

               procedure.
                  If 0 percent oxygen is available in W  lb/h (kg/h) of exhaust gases, the air-
                                                               g
               equivalent W  in lb/h (kg/h) is given by: W  = 100(W )(32O )/[23(100)(29.5)]
                               a
                                                                                       x
                                                                               g
                                                                   a
               = 0.0417 W (O). In this relation, we are converting the oxygen from a volume
                             g
               basis  to  a  weight  basis  by  multiplying  by  its  molecular  weight  of  32  and
               dividing  by  the  molecular  weight  of  the  exhaust  gases,  namely  29.5.  Then
               multiplying by (100/23) gives the air equivalent as air contains 23 percent by
               weight of oxygen.


               2. Relate the air required with the fuel fired using the MM Btu (kJ) method

               Each MM Btu (kJ) of fuel fired (HHV basis) requires a certain amount of air,
               A. If Q = amount of fuel fired in the turbine exhaust gases on a LHV basis
               (calculations for turbine exhaust gases fuel input are done on a low-heating-

               value basis), then the fuel fired in lb/h (kJ/h) = W  = Q/LHV.
                                                                          f
                                                                              6
                  The heat input on an HHV basis = W (HHV)/(10 ) = (Q/LHV)(HHV)/10                          6
                                                                 f
               Btu/h (kJ/h). Air required lb/h (kg/h) = (Q/LHV)(HHV)(A), using the MM
               Btu, where A = amount of air required, lb (kg) per MM Btu (kJ) fired. The
               above quantity = air available in the exhaust gases, W  = 0.0417 W (O).
                                                                                a
                                                                                                g

               3. Simplify the gas relations further
                                                                         6
               From the data in step 2, (Q/LHV)(HHV)(A)/10  = 0.0417 W (O). For natural
                                                                                         g
               gas  and  fuel  oils  it  can  be  shown  that  (LHV/A   HHV)  =  0.00124.  For
                                                                              x
               example, LHV of methane = 21,520 Btu/lb (50,055.5 kJ/kg); HHV = 23,879
               Btu/lb (55,542.6 kJ/kg), and A = 730 lb (331.4 kg). Hence, (LHV/A HHV) =
                                                                                                  x
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