Page 153 - Petroleum Production Engineering, A Computer-Assisted Approach
P. 153

Guo, Boyun / Computer Assited Petroleum Production Engg 0750682701_chap11 Final Proof page 148  3.1.2007 8:54pm Compositor Name: SJoearun




               11/148  EQUIPMENT DESIGN AND SELECTION
               e ¼ 2.718 and                             where
                                                            q ¼ volumetric flow rate, Mcfd
                  0:0375g g Dz
               s ¼        ,                      (11:107)  p pc ¼ pseudocritical pressure, psia
                       T T  z z                             d ¼ pipe internal diameter, in.
               and Dz is equal to outlet elevation minus inlet elevation  L ¼ pipe length, ft
               (note that Dz is positive when outlet is higher than inlet).  p r ¼ pseudo-reduced pressure
               A general and more rigorous form of the Weymouth equa-  T ¯ ¼ average flowing temperature, 8R
               tion with compensation for elevation is      g g ¼ gas gravity, air ¼ 1.0
                       s ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi       z b ¼ gas deviation factor at T b and p b , normally
                              s 2
                          2
                          p   e p )d  5
                  3:23T b                                       accepted as 1.0.
               q h ¼     (  1  2  ,              (11:108)

                              TzzL
                    p b   f M g g T  e
                                                         Based on Eqs. (2.29), (2.30), and (2.51), Guo and Ghalam-
               where L e is the effective length of the pipeline. For a  bor (2005) generated curves of the integral function
                                                         p
                                         s
               uniform slope, L e is defined as L e ¼  (e  1)L .  Ð r  p r z  dp r for various gas-specific gravity values.
                                          s
                For a non-uniform slope (where elevation change cannot  0
               be simplified to a single section of constant gradient), an  11.4.1.2.6 Pipeline Efficiency All pipeline flow equ-
               approach in steps to any number of sections, n,willyield  ations were developed for perfectly clean lines filled with
                   (e   1)  e (e   1)                    gas. In actual pipelines, water, condensates, sometimes
                    s 1
                               s 2
                             s 1
               L e ¼    L 1 þ       L 2                  crude oil accumulates in low spots in the line. There are
                     s 1       s 2
                                                         often scales and even ‘‘junk’’ left in the line. The net result
                                         n
                    e s 1 þs 2 (e   1)  X                is that the flow rates calculated for the 100% efficient cases
                         s 3
                   þ          L 3 þ .. .. .. :: þ
                        s 3                              are often modified by multiplying them by an efficiency
                                         i¼1             factor E. The efficiency factor expresses the actual flow
                     P
                     i 1
                       s j                               capacity as a fraction of the theoretical flow rate. An
                    e  j¼1  (e   1)                      efficiency factor ranging from 0.85 to 0.95 would
                         s i
                             L i ,               (11:109)  represent a ‘‘clean’’ line. Table 11.1 presents typical
                        s i
                                                         values of efficiency factors.
               where
                                                         Table 11.1 Typical Values of Pipeline Efficiency
                  0:0375g g Dz i
               s i ¼      :                      (11:110)         Factors
                       T T  z z
                                                                        Liquid content
               11.4.1.2.3 Panhandle-A  Equation  for  Horizontal  Type of line  (gal/MMcf)  Efficiency E
               Flow The Panhandle-A pipeline flow equation assumes
               the following Reynolds number–dependent friction factor:  Dry-gas field  0.1  0.92
                                                         Casing-head gas    7.2       0.77
                   0:085
               f M ¼                             (11:111)  Gas and condensate  800    0.6
                   N  0:147
                    Re
               The resultant pipeline flow equation is, thus,
                                1:07881      0:5394      11.4.2 Design of Pipelines
                                        2
                                     2
                      d  2:6182  T b  ( p   p )
               q ¼ 435:87            1  2     ,  (11:112)  Pipeline design includes determination of material, diam-
                      g 0:4604  p b    T T  zzL          eter, wall thickness, insulation, and corrosion protection
                       g
                                                         measure. For offshore pipelines, it also includes weight
               where q is the gas flow rate in scfd measured at T b and p b ,  coating and trenching for stability control. Bai (2001)
               and other terms are the same as in the Weymouth equa-  provides a detailed description on the analysis–analysis-
               tion.
                                                         based approach to designing offshore pipelines. Guo et al.
                                                         (2005) presents a simplified approach to the pipeline
               11.4.1.2.4 Panhandle-B Equation for Horizontal Flow  design.
               (Modified Panhandle) The Panhandle-B equation is  The diameter of pipeline should be determined based on
               the most widely used equation for long transmission and  flow capacity calculations presented in the previous sec-
               delivery lines. It assumes that f M varies as  tion. This section focuses on the calculations to design wall
                   0:015                                 thickness and insulation.
               f M ¼    ,                        (11:113)
                    0:0392
                   N Re
                                                         11.4.2.1 Wall Thickness Design
               and it takes the following resultant form:  Wall thickness design for steel pipelines is governed by
                             1:02 "  2  2  # 0:510       U.S. Code ASME/ANSI B32.8. Other codes such as
                                    2
                                 1
               q ¼ 737d  2:530  T b  ( p   p )   (11:114)  Z187 (Canada), DnV (Norway), and IP6 (UK) have es-
                         p b     T T zzLg 0:961          sentially the same requirements but should be checked by
                                   g
                                                         the readers.
               11.4.1.2.5 Clinedinst Equation for Horizontal Flow  Except for large-diameter pipes (>30 in.), material
               The Clinedinst equation rigorously considers the deviation  grade is usually taken as X-60 or X-65 (414 or 448 MPa)
               of natural gas from ideal gas through integration. It takes  for high-pressure pipelines or on deepwater. Higher grades
               the following form:                       can be selected in special cases. Lower grades such as X-42,
                                                         X-52, or X-56 can be selected in shallow water or for low-
                      z b p b p pc
               q ¼ 3973:0                                pressure, large-diameter pipelines to reduce material cost
                        p b                              or in cases in which high ductility is required for improved
                   v ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi
                           0
                                          1
                   u        p       p                    impact resistance. Pipe types include
                   u   d  5  ð r1   ð r2
                   u
                    t      @  p r  dp r    p r  dp r  A ,  (11:115)
                               z      z                  . Seamless
                       T Tf M Lg g
                             0      0
                                                         . Submerged arc welded (SAW or DSAW)
   148   149   150   151   152   153   154   155   156   157   158