Page 210 - Subyek Teknik Mesin - Forsthoffers Best Practice Handbook for Rotating Machinery by William E Forsthoffer
P. 210

Be st Practice 3 .20          Compressor Best Practices































       Fig 3.20.5   Thrust bearing rated load vs. speed (Courtesy of Kingsbury Corp.)

                                                            Impeller thrust forces


                                                            Every reaction type compressor blade set or impeller produces
                                                            an axial force towards the suction of the blade or impeller. Refer
                                                            to Figure 3.20.7.
                                                              In this example, the net force towards the compressor suc-
                                                            tion is 8,900 N (2,000 lbs) for the set of conditions noted. Note
                                                            that the pressure behind the impeller is essentially constant at
                                                            344.75 kPa (50 psi), but the pressure on the front side of im-
                                                            peller varies from 344.75 to 275.8 kPa (50 to 40 psi), because of
                                                            the pressure drop across the eye labyrinth. Every impeller in
                                                            a multistage compressor will produce a specific value of axial
                                                            force towards its suction at a specific flow rate, speed and gas
                                                            composition. A change in any or all of these parameters will
                                                            produce a corresponding change in impeller thrust.

                                                            Rotor thrust balance

                                                            Figure 3.20.8 shows how a balance drum or opposed impeller
                                                            design reduces thrust force. The total impeller force is the sum of
                                                            the forces from the individual impellers. If the suction side of the
                                                            impellers is opposed, as noted in Figure 3.20.8, the thrust force
                                                            will be significantly reduced and can approach zero. If the suction
                                                            side of all impellers are the same (in series), the total impeller
                                                            thrust force can be very high, and may exceed the thrust bearing
                                                            rating. If this is the case, a balance drum must be mounted on the
                                                            rotor as shown in Figure 3.20.8. The balance drum face area is
                                                            varied such that the opposing force generated by the balance
                                                            drum reduces the thrust bearing load to an acceptable value. The
                                                            opposing thrust force results from the differential between
                                                            compressor discharge pressure (P F ) and compressor suction
                                                            pressure (P 1 ) since the area behind the balance drum is usually
                                                            referenced to the suction of the compressor. This is accomplished
       Fig 3.20.6   The relationship between thrust pad temperature and  by a pipe that connects this chamber to the compressor suction.
                                                                                    ‘
       thrust load (Courtesy of Kingsbury, Inc.)            This line is typically called the balance line’.
           184
   205   206   207   208   209   210   211   212   213   214   215