Page 389 - Characterization and Properties of Petroleum Fractions - M.R. Riazi
P. 389

P2: IML/FFX
                           QC: IML/FFX
  P1: IML/FFX
                                        T1: IML
                                                        14:25
                                           June 22, 2007
  AT029-09
                        AT029-Manual-v7.cls
            AT029-Manual
                                                                Gas II
                                                                                 Gas III
                                                 Gas I   9. APPLICATIONS: PHASE EQUILIBRIUM CALCULATIONS 369
                                   Reservoir                 Stage II        Stage III

                                     Fluid   Stage I             o                o
                                                 o
                                            T=37.8  C        T=35  C         T=32.2  C

                                             P=21.7             P=5.2         P=1.01
                                        o
                                  T=118.3  C   bar   Liquid I      bar   Liquid II  bar   Liquid III
                                  P=164.5 bar                                        (Crude Oil)
                                    FIG. 9.3—Schematic of a three-stage separator test in a Middle East
                                  production field.
                                                                  The above procedure can be easily extended to LLE or vapor–
            7. Calculate K i values from a more accurate method using x i
              and y i calculated in Step 6. For example, K i can be calcu-  liquid–liquid equilibrium (VLLE) in which two immiscible
              lated from Eq. (6.197) by a cubic equation of state (i.e., SRK  liquids are in equilibrium with themselves and their vapor
                                    L
                                          V
              EOS) through calculating ˆ φ and ˆ φ using Eq. (6.126). Sub-  phase (see Problem 9.1).
                                    i
                                          i
                       L
                             V
              sequently ˆ f and ˆ f can be calculated from Eq. (6.113). For  Once value of V F is calculated in a VLE flash calculation,
                       i     i
              isothermal flash we must have                        the gas-to-liquid ratio (GLR) or gas-to-oil ratio (GOR) can be
                                        	 2                       calculated from the following relation [7]:

                               N    L
                                   ˆ f i
              (9.7)                  − 1   <ε                                                      5
                                   ˆ f  V                                            
      1.33 × 10 ρ L V F
                              i=1  i                             (9.8)       GOR scf stb =
                                                                                             (1 − V F )M L
              where ε is a convergence tolerance, (e.g., 1 × 10 −13 ).           3
            8. Repeat a new round of calculations from Step 4 with calcu-  where ρ L (in g/cm ) and M L (in g/mol) are the density and
              lated V F from the previous round until there is no change  molecular weight of a liquid product, respectively (see Prob-
              in values of V F , x i , and y i and inequality (9.7) is satisfied.  lem 9.2). The best method of calculation of ρ L for a liquid
                                                                  mixture is to calculate it through Eq. (7.4), using pure compo-
              Various other methods of flash calculations for fast con-  nent liquid densities. If the liquid is at atmospheric pressure
            vergence are given in different references [1–4]. For example,  and temperature, then ρ L can be replaced by liquid specific
            Whitson [1] suggests that the initial guess for V F must be  gravity, SG L , which may also be calculated from Eq. (7.4) and
            between two values of V F,min and V F,max to obtain fast conver-  components SG values. The method of calculations is demon-
            gence. Michelsen also gives a stability test for flash calcula-  strated in Example 9.1.
            tions [5, 6]. Accuracy of results of VLE calculations largely
            depends on the method used for estimation of K i values and  Example 9.1 (Three-stage surface separator)—Schematic of
            for this reason recommended methods in Table 6.15 can be  a three-stage separator for analysis of a reservoir fluid to pro-
            used as a guide for selection of an appropriate method for  duce crude oil is shown in Fig. 9.3. The composition of reser-
            VLE calculation. Another important factor for the accuracy  voir fluid and products as well as GOR in each stage and the
                                                                  overall GOR are given in Table 9.1. Calculate final crude com-
            of VLE calculations is the method of characterization of C 7+
            fraction of the petroleum fluid. Application of continuous  position and the overall GOR from an appropriate model.
            functions, as it was shown in Section 4.5, can improve results
            of calculations. The impact of characterization on phase be-  Solution—The first step in calculation is to express the C 7+
            havior of reservoir fluids is also demonstrated in Section 9.2.3.  fraction into a number of pseudocomponents with known
                               TABLE 9.1—Experimental data for a Middle East reservoir fluid in a three-stage separator
                                                 test. Taken with permission from Ref. [7].
                                                               1st-Stage  2nd-Stage  3rd-Stage  3rd-Stage
                              No.           Component   Feed     gas      gas       gas     liquid
                               1              N 2        0.09    0.77      0.16     0.15    0.00
                               2              CO 2       2.09    4.02      3.92     1.41    0.00
                               3              H 2 S      1.89    1.35      4.42     5.29    0.00
                               4              H 2 O      0.00    0.00      0.00     0.00    0.00
                               5              C 1       29.18    63.27    31.78     5.10    0.00
                               6              C 2       13.60    20.15    33.17    26.33    0.19
                               7              C 3        9.20    7.56     18.84    36.02    1.88
                               8              n-C 4      4.30    1.5       4.14    13.6     3.92
                               9              i-C 4      0.95    0.43      1.24     3.62    0.62
                              10              n-C 5      2.60    0.36      0.92     3.50    4.46
                              11              i-C 6      1.38    0.24      0.63     2.46    2.11
                              12              C 6        4.32    0.24      0.57     2.09    8.59
                              13              C 7+      30.40    0.11      0.21     0.43   78.23
                              SG at 60 F                                                    0.8150
                                     ◦
                              Temp, F                  245      105      100       90      90
                                   ◦
                              Pressure, psia          2387      315       75       15      15
                              GOR, scf/stb             850      601      142      107




                                      --`,```,`,``````,`,````,```,,-`-`,,`,,`,`,,`---
   Copyright ASTM International
   Provided by IHS Markit under license with ASTM             Licensee=International Dealers Demo/2222333001, User=Anggiansah, Erick
   No reproduction or networking permitted without license from IHS  Not for Resale, 08/26/2021 21:56:35 MDT
   384   385   386   387   388   389   390   391   392   393   394