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Guo, Boyun / Computer Assited Petroleum Production Engg 0750682701_chap13 Final Proof page 189  3.1.2007 9:07pm Compositor Name: SJoearun




                                                                                           GAS LIFT  13/189
                       rotary compressors (vane or impeller type) are generally  The theoretical formula for volumetric efficiency is
                       driven by electric motors. Large-volume positive compres-  1=k
                       sors operate at lower speeds and are usually driven by  E v ¼ 1   (r    1) C l ,  (13:21)
                       steam or gas engines. They may be driven through reduc-  where
                       tion gearing by steam turbines or an electric motor. Re-
                       ciprocation compressors driven by steam turbines or  E v ¼ volumetric efficiency, fraction
                       electric motors are most widely used in the petroleum  r ¼ cylinder compression ratio
                       industry as the conventional high-speed compression ma-  C l ¼ clearance, fraction.
                       chine. Selection of compressors requires considerations of  In practice, adjustments are made to the theoretical
                       volumetric gas deliverability, pressure, compression ratio,  formula in computing compressor performance:
                       and horsepower.
                                                                            z s  1=k
                                                                 E v ¼ 0:97    r    1 C l   e v ,   (13:22)
                       13.4.3.1 Reciprocating Compressors                   z d
                       Two basic approaches are used to calculate the horse-  where
                       power theoretically required to compress natural gas. One
                       is to use analytical expressions. In the case of adiabatic  z s ¼ gas deviation factor at suction of the cylinder
                       compression, the relationships are complicated and are  z d ¼ gas deviation factor at discharge of the cylinder
                                                                   e v ¼ correction factor.
                       usually based on the ideal-gas equation. When used for
                       real gases where deviation from ideal-gas law is appre-  In this equation, the constant 0.97 is a reduction of 1 to
                       ciable, they are empirically modified to take into consid-  correct for minor inefficiencies such as incomplete filling
                       eration the gas deviation factor. The second approach is  of the cylinder during the intake stroke. The correction
                       the enthalpy-entropy or Mollier diagram for real gases.  factor e v is to correct for the conditions in a particular
                       This diagram provides a simple, direct, and rigorous pro-  application that affect the volumetric efficiency and for
                       cedure for determining the horsepower theoretically neces-  which the theoretical formula is inadequate.
                       sary to compress the gas.
                         Even though in practice the cylinders in the reciprocating  13.4.3.1.2 Stage Compression  The ratio of the dis-
                       compressors may be water-cooled, it is customary to con-  charge pressure to the inlet pressure is called the pressure
                       sider the compression process as fundamentally adiabatic—  ratio.Thevolumetricefficiencybecomesless,andmechanical
                       that is, to idealize the compression as one in which there is  stress limitation becomes more, pronounced as pressure
                       no cooling of the gas. Furthermore, the process is usually  ratio increases. Natural gas is usually compressed in stages,
                       considered to be essentially a perfectly reversible adiabatic,  with the pressure ratio per stage being less than 6. In field
                       that is, an isentropic process. Thus, in analyzing the  practice, the pressure ratio seldom exceeds 4 when boosting
                       performance of a typical reciprocating compressor, one  gas from low pressure for processing or sale. When the total
                       may look upon the compression path following the  compression ratio is greater than this, more stages of
                       general law
                                                                 compression are used to reach high pressures.
                         k
                       pV ¼ a constant:                   (13:19)  The total power requirement is a minimum when the
                                                                 pressure ratio in each stage is the same. This may be
                       For real natural gases in the gravity range 0:55 < g g < 1,  expressed in equation form as
                       the following relationship can be used at approximately     1=N s
                       150 8F:                                   r ¼  p d  ,                        (13:23)
                                                                     p s

                       k 150 F     2:738   log g g        (13:20)
                                2:328                            where
                       When a real gas is compressed in a single-stage compres-  p d ¼ final discharge pressure, absolute
                       sion, the compression is polytropic tending to approach  p s ¼ suction pressure, absolute
                       adiabatic or constant-entropy conditions. Adiabatic com-  N s ¼ number of stages required.
                       pression calculations give the maximum theoretical work
                                                                   As large compression ratios result in gas being heated to
                       or horsepower necessary to compress a gas between any
                                                                 undesirably high temperatures, it is common practice to
                       two pressure limits, whereas isothermal compression cal-
                                                                 cool the gas between stages and, if possible, after the final
                       culations give the minimum theoretical work or horse-
                                                                 stage of compression.
                       power necessary to compress a gas. Adiabatic and
                       isothermal work of compression, thus, give the upper
                       and lower limits, respectively, of work or horsepower  13.4.3.1.3 Isentropic Horsepower The computation is
                       requirements to compress a gas. One purpose of intercool-  basedontheassumptionthattheprocessisidealisentropicor
                       ers between multistage compressors is to reduce the horse-  perfectly reversible adiabatic. The total ideal horsepower for
                       power necessary to compress the gas. The more  a given compression is the sum of the ideal work computed
                       intercoolers and stages, the closer the horsepower require-  for each stage of compression. The ideal isentropic work can
                       ment approaches the isothermal value.     be determined for each stage of compression in a number of
                                                                 ways.Onewaytosolveacompressionproblemisbyusingthe
                                                                 Mollier diagram. This method is not used in this book
                       13.4.3.1.1 Volumetric Efficiency The volumetric effi-
                       ciency represents the efficiency of a compressor cylinder  because it is not easily computerized. Another approach
                       to compress gas. It may be defined as the ratio of the  commonly used is to calculate the horsepower for each
                       volume of gas actually delivered to the piston displacement,  stage from the isentropic work formula:
                                                                                         #
                                                                               "
                       corrected to suction temperature and pressure. The principal  k     (k 1)=k
                       reasons that the cylinder will not deliver the piston  w ¼  k   1  53:241T 1  p 2   1 ,  (13:24)
                       displacement capacity are wire-drawing, a throttling effect  g g  p 1
                       on the valves; heating of the gas during admission to the  where
                       cylinder; leakage past valves and piston rings; and re-
                       expansion of the gas trapped in the clearance-volume space  w ¼ theoretical shaft work required to compress the
                       from the previous stroke. Re-expansion has by far the  gas, ft-lb f =lb m
                       greatest effect on volumetric efficiency.   T 1 ¼ suction temperature of the gas, 8R
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