Page 622 - Air and Gas Drilling Manual
P. 622

11-60    Air and Gas Drilling Manual
                                            t
                                      L
                                           0 0113 ft
                                      L t t  l 12
                                            .
                               The nozzle depth along the periphery of the stator,  L , is
                                                                      d
                                            .
                                      l d  0 280 inches
                                            l d
                                      L
                                       d
                                            12
                                            .
                                      L d  0 0233 ft
                                   Assuming  that 16 of the nozzles are plugged, then the  total  nozzle  flow  area,
                                A , is
                                 tn
                                                            0
                                      A tn  (23  16 ) ( .0113 ) ( .0233 )
                                                     0
                                      A tn  0 00185 ft 2
                                             .
                                   Assuming  sonic gas flow conditions at the throats of each of the  remaining  7
                               nozzles in the stator, Equation 6-62 can be used to  determine the pressure above the
                               turbine stator.  Equation 6-62 becomes

                                                       2
                                                                41
                                                      (.635 ) (604 . )  . 05
                                      P ias
                                                                         . 24  . 05
                                                     (32 . ) ( . ) ( . )  2  . 04
                                                        2
                                                               1
                                                                0
                                                           1
                                                            4
                                             0
                                            (.00185 )
                                                         53 .36      . 24
                                                     2
                                      P ias  65 790 lb/ft abs
                                              ,
                                            P ias
                                      p ias
                                            144
                                               .
                                      p ias  456 9 psia
                                   The ratio of the pressure  below  the  turbine  to  the  pressure  above  the  turbine
                               (stator) is
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