Page 131 - Air and gas Drilling Field Guide 3rd Edition
P. 131

122     CHAPTER 5 Compressors and Nitrogen Generators




                          The rated volumetric flow rate into the compressor is 448.3 liters/sec. For this
                          example, the compressor is located at 1829 m above sea level, thus
                                                    3
                                         Q i ¼ 0:448 m =sec:
                          With the aforementioned terms, the theoretical shaft horsepower required to
                          compress the air moving through the machine is given by Equation (5-36a). Thus,
                          the theoretical shaft horsepower is
                                                               2                    3
                                                                            ð0:4Þ

                                          ð2Þð1:4Þ             6  1115720:0 ð2Þð1:4Þ  7
                                      _ W s ¼   ð81170:0Þð0:4483Þ 6                1 7
                                           ð0:4Þ               4  81170:0           5
                                      _ W s ¼ 115660 watts:
                          For this example,

                                       e m ¼ 0:95
                          and from Equation (5-39), the actual shaft power is
                                             115660
                                      _ W as ¼        ¼ 130947 watts:
                                           ð0:95Þð0:930Þ
                             The above determined 131.0 kW is the actual shaft power needed by the com-
                                                                     2
                          pressor to match the back pressure of 103.5 N/cm gauge (at the surface location
                          elevation of 1829 m above sea level). At this surface location, the input power
                          available from the prime mover is a derated value (derated from the rated
                          261 kW available at 1800 rpm). In order for the compressor system to operate
                          at this 1829-m surface location elevation, the derated input power available must
                          be greater than the actual shaft power needed. Figure 5-15 shows that for a
                          1829-m elevation the power of a turbocharged prime mover must be derated by
                          15%. The derated input horsepower available from the prime mover _ W i is
                                       _ W i ¼ 261ð1   0:15Þ¼ 221:9 kW:

                             For this example, the prime mover derated input power is greater than the
                          actual shaft power needed, thus the compressor system can be operated at this
                          1829-m surface location elevation.

                          5.6.3 Rotary Compressor System Unit
                          Rotary compressors have fixed compressor ratios for each stage. These machines
                          have a constant pressure output. These compressors cannot adjust output pres-
                          sures to match the back pressure in the exit flow line. The rotary compressors
                          will inject compressed gas into the flow line at the compressor’s rated pressure
                          output. If the back pressure in the exit flow line is less than the rated pressure
                          output, the gas will expand in the flow line (or surge tank upstream of the flow
                          line) to match the back pressure [1, 7].
                             There is no volumetric efficiency term for the rotary compressor. There is a
                          mechanical efficiency term for these compressors (denoted by the term e m ).
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