Page 151 - Petroleum Production Engineering, A Computer-Assisted Approach
P. 151

Guo, Boyun / Computer Assited Petroleum Production Engg 0750682701_chap11 Final Proof page 146  3.1.2007 8:54pm Compositor Name: SJoearun




               11/146  EQUIPMENT DESIGN AND SELECTION
                  Oil-specific gravity:                  equations that are noniterative or explicit. This has in-
                                                         volved substitutions for the friction factor f M . The specific
                                141:5                    substitution used may be diameter-dependent only
                           g o ¼      ¼ 0:85
                              131:5 þ 35                 (Weymouth equation) or Reynolds number–dependent
                                                         only (Panhandle equations).
                  Reynolds number:

                              6  (1:66)(0:85)(62:4)      11.4.1.2.1 Weymouth Equation for Horizontal Flow
                    N Re ¼ 1,488  12       ¼ 13,101      Equation (11.97) takes the following form when the unit of
                                   5
                                                         scfh for gas flow rate is used:
                       > 2,100 turbulent flow                    s ffiffiffiffiffiffis ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi
                                                                        2
                                                                           2
                                                            3:23T b  1  ( p   p )d  5
               Equation (11.89) gives                    q h ¼          1  2  ,             (11:98)

                                                              p b  f M  g g T zzL
                                                                         T
                 1             0:0006   21:25                q ffiffiffiffi
               p ffiffiffiffiffiffi ¼ 1:14   2 log  þ   0:9  ¼ 5:8759,     1
                 f M             6     (13,101)          where  f M  is called the ‘‘transmission factor.’’ The friction
                                                         factor may be a function of flow rate and pipe roughness.
               which gives                               If flow conditions are in the fully turbulent region, Eq.
                              f M ¼ 0:02896:             (11.89) degenerates to
                                                                  1
               Equation (11.93) gives                    f M ¼          2  ,                (11:99)

                p 1 ¼ 50 þ 0:433(0:85)(5)(5,280) sin (15 ) þ 1:15   10  5  [1:14   2 log (e D )]
                                                         where f M depends only on the relative roughness, e D .
                                    2
                      (0:02896)(0:85)(5,000) (5)(5,280)
                                                         When flow conditions are not completely turbulent, f M
                               (6) 5                     depends on the Reynolds number also.
                                                          Therefore, use of Eq. (11.98) requires a trial-and-error
                  ¼ 2,590 psi:
                                                         procedure to calculate q h . To eliminate the trial-and-error
                                                         procedure, Weymouth proposed that f vary as a function
                                                         of diameter as follows:
               11.4.1.2 Gas Flow
               Consider steady-state flow of dry gas in a constant-diam-  f M ¼  0:032     (11:100)
               eter, horizontal pipeline. The mechanical energy equation,  d 1=3
               Eq. (11.78), becomes                      With this simplification, Eq. (11.98) reduces to
               dp  f M ru 2  p(MW) a fu 2                          s ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi
                                                                         2
                                                                      2
                 ¼     ¼           ,              (11:94)   18:062T b  ( p   p )D 16=3
               dL  2g c D  zRT  2g c D                   q h ¼        1    2  ,            (11:101)
                                                                        TzzL
                                                               p b     g g T
               which serves as a base for development of many pipeline
               equations. The difference in these equations originated  which is the form of the Weymouth equation commonly
               from the methods used in handling the z-factor and fric-  used in the natural gas industry.
               tion factor. Integrating Eq. (11.94) gives  The use of the Weymouth equation for an existing
               ð             ð                           transmission line or for the design of a new transmission
                    (MW) a f M u 2  p                    line involves a few assumptions including no mechanical
                dp ¼            dL:               (11:95)
                      2Rg c D  zT                        work, steady flow, isothermal flow, constant compressibil-
                                                         ity factor, horizontal flow, and no kinetic energy change.
               If temperature is assumed constant at average value in a
               pipeline, T ¯ , and gas deviation factor, z ¯, is evaluated at  These assumptions can affect accuracy of calculation
               average temperature and average pressure, p ¯, Eq. (11.95)  results.
                                                          In the study of an existing pipeline, the pressure-mea-
               can be evaluated over a distance L between upstream
                                                         suring stations should be placed so that no mechanical
               pressure, p 1 , and downstream pressure, p 2 :
                                                         energy is added to the system between stations. No me-
                          2
                      25g g Q   T zzf M L                chanical work is done on the fluid between the points at
                           T
                2
                   2
               p   p ¼          ,                 (11:96)
                1  2      d 5                            which the pressures are measured. Thus, the condition of
                                                         no mechanical work can be fulfilled.
               where
                                                          Steady flow in pipeline operation seldom, if ever, exists
                 g g ¼ gas gravity (air ¼ 1)             in actual practice because pulsations, liquid in the pipeline,
                 Q ¼ gas flow rate, MMscfd (at 14.7 psia, 60 8F)  and variations in input or output gas volumes cause devi-
                 T ¯ ¼ average temperature, 8R           ations from steady-state conditions. Deviations from
                 z ¯ ¼ gas deviation factor at T ¯ and p ¯  steady-state flow are the major cause of difficulties experi-
                 p ¯ ¼ (p 1 þ p 2 )/2                    enced in pipeline flow studies.
                 L ¼ pipe length, ft                      The heat of compression is usually dissipated into the
                 d ¼ pipe internal diameter, in.         ground along a pipeline within a few miles downstream
                 F ¼ Moody friction factor               from the compressor station. Otherwise, the temperature
                                                         of the gas is very near that of the containing pipe, and
               Equation (11.96) may be written in terms of flow rate
               measured at arbitrary base conditions (T b and p b ):  because pipelines usually are buried, the temperature of
                     s ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi          the flowing gas is not influenced appreciably by rapid
                           2
                        2
                       ( p   p )d  5                     changes in atmospheric temperature. Therefore, the gas
                  CT b
               q ¼      1  2  ,                   (11:97)  flow can be considered isothermal at an average effective

                         T
                   p b  g g T zzf M L
                                                         temperature without causing significant error in long-
               where C is a constant with a numerical value that depends  pipeline calculations.
               on the units used in the pipeline equation. If L is in miles  The compressibility of the fluid can be considered con-
               and q is in scfd, C ¼ 77:54.              stant and an average effective gas deviation factor may be
                The use of Eq. (11.97) involves an iterative procedure.  used. When the two pressures p 1 and p 2 lie in a region
               The gas deviation factor depends on pressure and the  where z is essentially linear with pressure, it is accurate
               friction factor depends on flow rate. This problem  enough  to  evaluate  z ¯  at  the  average  pressure
               prompted several investigators to develop pipeline flow    p p ¼ ( p 1 þ p 2 )=2. One can also use the arithmetic average
   146   147   148   149   150   151   152   153   154   155   156