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Chapter 9: Aerated Fluid Drilling    9-73
                                   The above determined  322.5  horsepower  is  the  actual  shaft  power  needed  by
                               each of the two compressors to  produce the 420 psia pressure output  at the surface
                               location elevation of 4,000 ft above sea level (while drilling  at a depth of 7,000  ft).
                               At this  surface location, the input  horsepower available from the Caterpillar Model
                               D398  prime  mover  is  a  derated  value  (derated  from  the  rated  760  horsepower
                               available at 900 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 elevation the input
                               power of a turbocharged prime mover must  be derated by approximately 10 percent.
                                                       ˙
                               The derated input horsepower,  W , available from the prime mover is
                                                       i
                                      W ˙ i  760  (1  . 0 10 )
                                      W ˙ i  684 .0
                                   For this  illustrative example, the prime mover of  the  compressor  unit  derated
                               input  power is  greater than  the  actual  shaft  horsepower  needed,  thus,  the  selected
                               compressor unit  can be operated  at  this  4,000  ft  surface  location  elevation  (while
                               drilling at a depth of 10,000 ft).
                                   The  volumetric  flow  rate  of  gas  to  create  an  aerated  drilling  fluid  is  very
                               dependent upon the flow resistance in the circulation system.    This resistance is  the
                               sum of the major and minor flow friction losses in  the flow system.   This  friction
                               resistance creates choking of the system and, therefore, generally increases the average
                               pressure and in turn increases the average specific weight of the aerated drilling  fluid
                               in the annulus and elsewhere in the circulation system.  Therefore, if it  is  required to
                               maintain a constant bottomhole pressure limit, more gas volumetric flow rate will be
                               required to reduce the average pressure and the specific weight in the annulus.
                                   A major contributor to  this  choking effect is  the inside diameter of the surface
                               return flow line (relative to the annulus inside of diameter).  In Illustrative Example
                               9.3 the surface return flow line inside diameter was 5.625 inches.  For this  example,
                               the  required  maximum  volumetric  flow  rate  when  drilling  at  10,000  ft  was
                               determined  to  be  1,168  acfm.    If  the  surface  return  flow  line  inside  diameter  is
                               changed to 4.00  inches the required maximum  volumetric flow rate becomes 1,575
                               acfm.  This is a 35 percent increase in  gas volumetric flow rate required.   Thus,  the
                               design  of  the  surface  return  flow  line  and  the  drill  string  to  reduce  choking  can
                               dramatically  reduce  the  gas  volumetric  flow  rate  needed  to  provide  the  required
                               aerated drilling fluid.

                               9.5  Prime  Mover  Fuel  Consumption
                                   In this  section  the  fuel  consumption  of  the  prime  mover  for  the  compressor
                               system  will  be  discussed.    Illustrative  examples  of  the  fuel  consumption  were
                               discussed in  detail in  Chapter  4.    In  this  section  the  illustrative  example  in  this
                               chapter will be completed with the calculation of the approximate fuel needed on the
                               drilling location for the compressor system.
                                   Illustrative Examples 9.3 describe the implementation of the basic planning step
                               No. 12 given in Section 9.1.
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