Page 220 - Subyek Teknik Mesin - Forsthoffers Best Practice Handbook for Rotating Machinery by William E Forsthoffer
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Be st Practice 3 .22          Compressor Best Practices











































       Fig 3.22.8   Turbo-compressor ‘trapped bushing seal’ (Courtesy of A.C. Compressor Corp.)


       Seal supply systems                                  maintained by a differential pressure control valve located
                                                            downstream of the seal. Seal oil flows in three separate
       As can be seen from the previous discussion, the type of seal  directions:
       system will depend on the type of seal utilized. We will now
       examine five different types of seal systems, each utilizing  - Through the seal chamber (cooling flow)
       a different type of main compressor shaft seal system. As we  - Through the gas side contact seal 38.5e77 liters/day (10e20
       proceed through each type, the function of each system will  gallons/day)
       become clear.                                        - Through the atmospheric seal
                                                              Let’s examine the variants of flows across the equivalent or-
       Example 1: Contact type gas side seal e bushing
                                                            ifice of each portion of this configuration.
       type atmospheric side seal with cooling flow            The gas side contact seal will experience a constant flow,
       This system incorporates a contact seal on the gas side and  which for purposes of discussion, can be assumed to be zero
       a bushing seal on the atmospheric side of each end of the  gallons per minute (since the maximum flow rate will usually be
       compressor. The inlet pressure of the seal fluid on each end is  on the order of ten gallons per day).
       referenced to the suction pressure of the compressor. It should  The atmospheric side bushing seal flow will vary based upon
       be noted that some applications employ different reference  the referenced gas pressure. At low suction pressure conditions,
       pressures on each end of the compressor. The reference pres-  this flow will be significantly less than it will be under high
       sure should be taken off the balance drum end, or high pressure  pressure conditions. The seal system design must consider the
       end of the compressor, to ensure that the oil to gas differential  maximum reference pressure to be experienced in the com-
       pressure is always at a minimum acceptable value. Therefore,  pressor case to ensure that sufficient seal oil flow is available at
       the low pressure end may experience a slightly higher oil to gas  maximum pressure conditions.
       differential than the reference end of the seal. Refer to  The seal chamber through flow in this seal design is used to
       Figure 3.22.9.                                       remove any excess frictional heat of the seals and is regulated
          Proceeding through the seal, the seal oil supply, which is  by the downstream control valve. As an example, let us
       referenced to the gas reference pressure, enters the seal cham-  assume the following values were calculated for this specific
       ber. The differential across the gas side contact seal is  seal application.

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