Page 204 - Air and Gas Drilling Manual
P. 204

5-46    Air and Gas Drilling Manual
                                                  .
                                            148 3 .
                                      r =
                                       s
                                            12 685
                                      r = 342 .     05
                                            .
                                       s
                               The  volumetric  efficiency  (only  for  the  reciprocating  piston  compressor),  ε , is
                                                                                          v
                               determined  from  Equation  4-38.    The  compressor  clearance  volume  ratio,  c, is
                               assumed to be 0.06.  Equation 4-38 becomes
                                                             1    
                                      ε  = 096 1  − (006   .     − 1
                                               
                                                     .
                                            .
                                                         
                                       v                ) (342 )14 .   
                                                                  
                                      ε  = 0 879
                                            .
                                       v
                                                                     ˙
                               From Equation 4-39, the actual shaft horsepower,  W ,  required by  each compressor
                                                                      as
                               is
                                      W ˙ as  =  114 .1
                                             09
                                            (. ) (. 0879 )
                                      W ˙  as  = 144 .3
                                   The above determined  144.3  horsepower  is  the  actual  shaft  power  needed  by
                               each of the two compressor to  produce the 148.3  psia pressure output  at the surface
                               location elevation of 4,000  ft above sea level.  At  this  surface  location,  the  input
                               horsepower available from  each  of  the  prime  mover  of  the  compressor  units  is  a
                               derated value (derated from the rated 270 horsepower  available  at  1,000  rpm).    In
                               order for the compressor units  to  operate at this  4,000  ft  surface location elevation,
                               the derated input power available must be greater than the actual shaft power needed.
                               Figure 4-15 shows that for 4,000 ft surface elevation the input  power of each of the
                               turbocharged  prime  movers  must  be  derated  by  approximately  10  percent.    The
                                                     ˙
                               derated  input  horsepower,  W ,  available  from  each  prime  mover  of  each  of  the
                                                     i
                               compressor units is
                                                    .
                                      W = 270 1(  − 0 10)
                                       i
                                       ˙
                                      W = 243 .0
                                       i
                                   For this example, the prime mover of each of the two compressor units  derated
                               input power is greater than the actual shaft horsepower needed.  This  shows that the
                               compressor units  have sufficient power to  operate at a surface elevation of 4,000  ft
                               above sea level.
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