Page 621 - Air and Gas Drilling Manual
P. 621

where  G  is the gear box reduction ratio.  Using Equation 11-3, the runaway speed
                                      r
                               of the drive shaft (drill bit) is
                                            55 642       Chapter 11: Specialized Drilling Equipment    11-59
                                              ,
                                      N  rb
                                                .
                                             112 5
                                               .
                                      N     494 6 rpm
                                        rb
                               The torque developed by the motor at any drive shaft (drill bit) speed is
                                                            N b
                                      Torque  b  Torque  sb  1                         (11-4)
                                                            N rb
                               where  N  is the drive shaft (drill bit) speed (rpm).  Using Equation 11-4, the torque
                                      b
                               at the drive shaft (drill bit) speed of 40 rpm is
                                                             40
                                      Torque    (,980 ) 1
                                                3
                                            b
                                                            494 .6
                                                ,
                                      Torque    3 658  ft  lb
                                            b
                               The drive shaft (drill bit) horsepower developed at any drive shaft (drill bit) speed is
                                             Torque N b
                                                  b
                                      HP b
                                                ,
                                               5 252
                                             3
                                             (,658 ) (40 )
                                      HP b
                                                , 5 252
                                      HP b   27 86
                                              .
                                 Maintaining Sonic Velocity in Nozzle Throat
                                   In order to maintain sonic gas flow in the throat in  each active nozzle, the ratio
                               of the pressure below  the  turbine  device  to  the  pressure  above  the  turbine  device
                               must  be less than the critical  ratio  as  defined  by  Equation  6-62.    To  obtain  this
                               condition, several of the 23 nozzles in  the stator must  be plugged.  Plugging  these
                               nozzles  restricts  the  flow  of  gas  to  only  a  few  nozzles  and,  thus,  increases  the
                               pressure above the turbine stator.
                                   The nozzle throat opening,  L , is
                                                        t
                                      l t  0 136 inches
                                           .
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