Page 143 - Air and Gas Drilling Manual
P. 143

a) Surface location at sea level.
                                   The total fixed ratio  across  all  three  stages  that  is  needed.    The  atmospheric
                               pressure  at  sea  level  (i.e.,  assuming  API  Mechanical  Equipment  Standard
                               atmospheric pressure) is               Chapter 4: Compressors    4-29
                                      p = 14 696.  psia
                                       i
                               Thus, the output pressure is
                                                            .
                                      p o  = 240  + 14 696  = 254 696 psia
                                                   .
                               The total fixed compression ratio across all three stages of the compressor, r st, is
                                              .
                                                      .
                                      r st  =  254 696  = 17 33
                                            14 696
                                             .
                               This  is  the  fixed  mechanical  ratio  designed  into  the  compressor  and  must  be
                               determined at the standard conditions of the compressor specifications.  The  above
                               total fixed ratio will  be needed to  determine the maximum  pressure available  from
                               the compressor when the compressor system is  operated at surface elevations above
                               sea level (part b of this example).
                                   The specific heat ratio for air is
                                      k = 14
                                           .
                                                                                 3
                                   The rated volumetric flow rate  into  the  compressor  is  900  ft /min.    For  this
                               example the compressor is located at sea level, thus,
                                      q = 900 scfm
                                       i
                                   The number of stages are

                                      n = 3
                                       s
                                   With the above terms the theoretical shaft horsepower required to  compress the
                               air moving through the machine is  given by Equation 4-35a.   Thus,  the theoretical
                               shaft horsepower is
                                                . ( ) (14
                                            () 31 4  .696 ) (900 )      254 .696  ()( . (04 )   
                                       ˙
                                      W =                               31 . ) 4  −1
                                        s
                                               . (04 )  229 .17    14 .696    
                                                                              
                                       ˙
                                      W = 189 .1
                                        s
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