Page 237 - Chemical process engineering design and economics
P. 237

218                                                      Chapter 5


                  10                   i  l  l

                                    Isothermal Compression


                                       Second-stage Adiabatic Compression









                           I  i     I  i        i  i     l  i  i  t
                    0      24        6     8    10     12     14    16
                                       Specific Volume of Gas


           Figure 5.17 The effect of operating mode on compressor work.


           phase separator after  the condenser to separate the gas  from  the liquid. The total
           work of compression is equal to the  sum of the work for each stage of compres-
           sion.  Assuming that the compressed gases are cooled to the inlet temperature of
           the compressor after  each stage, we can use Equation 5.18 for each stage.  If it is
           also  assumed  that  the  pressure  drop  across  intercoolers,  phase  separators,  and
           piping is negligible, then the total compressor work,
                                 n
                  zRTi    [ f  P 2  Y ~                    1
           Wp =  —————   |  | ———|                   +  .....           (5.24)
                (n-l)/n   L IP,  )


           where z is the average of the inlet and discharge compressibility factors.
                  Because  the  work  of  compression  should  be  a  minimum,  differentiate
           Equation 5.24 with respect to P, and  then set the derivative equal to zero.
                                    2

                                                        1
           5W P                                      p 3
                                                                       (5.25)
           5P 2                                      P 2  J
                Next, solve for the pressure ratio for the  first  stage, P/Pi.
                                                         2




         Copyright © 2003 by Taylor & Francis Group LLC
   232   233   234   235   236   237   238   239   240   241   242