Page 33 - Petroleum Production Engineering, A Computer-Assisted Approach
P. 33

Guo, Boyun / Computer Assited Petroleum Production Engg 0750682701_chap02 Final Proof page 22 22.12.2006 7:08pm




               2/22  PETROLEUM PRODUCTION ENGINEERING FUNDAMENTALS
               compressibility factor, gas density, gas formation volume  where p ci and T ci are critical pressure and critical tempera-
               factor, and gas compressibility. The first two are com-  ture of component i, respectively.
               position dependent.The latter four are pressure dependent.
                                                         Example Problem 2.2 For the gas composition given in
                                                         the following text, determine apparent molecular weight,
               2.3.1 Specific Gravity of Gas             specific gravity, pseudo-critical pressure, and pseudo-
               ‘‘Specific gravity gas’’ is defined as the ratio of the appar-  critical temperature of the gas.
               ent molecular weight of the gas to that of air. The molecu-
               lar weight of air is usually taken as equal to 28.97 ( 79%
               nitrogen and 21% oxygen). Therefore, the gas-specific  Component  Mole Fraction
               gravity is
                                                                C 1                0.775
                   MW a                                         C 2                0.083
               g g ¼   ,                          (2:18)
                   28:97                                        C 3                0.021
                                                                i-C 4              0.006
               where MW a is the apparent molecular weight of gas, which
                                                                n-C 4              0.002
               can be calculated on the basis of gas composition. Gas
                                                                i-C 5              0.003
               composition is usually determined in a laboratory and
                                                                n-C 5              0.008
               reported in mole fractions of components in the gas. Let
                                                                C 6                0.001
               y i be the mole fraction of component i, and the apparent
                                                                C 7þ               0.001
               molecular weight of the gas can be formulated using a
                                                                N 2                0.050
               mixing rule such as
                                                                CO 2               0.030
                     Nc
                     X                                          H 2 S              0.020
               MW a ¼  y i MW i ,                 (2:19)
                     i¼1
                                                         Solution Example Problem 2.2 is solved with the
               where MW i is the molecular weight of component i, and
                                                         spreadsheet program MixingRule.xls. Results are shown
               N c is number of components. The molecular weights of
                                                         in Table 2.2.
               compounds (MW i ) can be found in textbooks on organic
               chemistry or petroleum fluids such as that by Ahmed  If the gas composition is not known but gas-specific
               (1989). Gas-specific gravity varies between 0.55 and 0.9.  gravity is given, the pseudo-critical pressure and tempera-
                                                         ture can be determined from various charts or correlations
               2.3.2 Gas Pseudo-Critical Pressure and Temperature  developed based on the charts. One set of simple cor-
               Similar to gas apparent molecular weight, the critical  relations is
               properties of a gas can be determined on the basis of the
                                                         p pc ¼ 709:604   58:718g g         (2:22)
               critical properties of compounds in the gas using the mix-
               ing rule. The gas critical properties determined in such a  T pc ¼ 170:491 þ 307:344g g ,  (2:23)
               way are called ‘‘pseudo-critical properties.’’ Gas pseudo-
               critical pressure ( p pc ) and pseudo-critical temperature  which are valid for H 2 S < 3%, N 2 < 5%, and total content
               (T pc ) are, respectively, expressed as   of inorganic compounds less than 7%.
                                                          Corrections for impurities in sour gases are always
                   X
                   N c
               p pc ¼  y i p ci                   (2:20)  necessary. The corrections can be made using either charts
                   i¼1                                   or correlations such as the Wichert and Aziz (1972)
                                                         correction expressed as follows:
               and
                                                                                            (2:24)
                                                         A ¼ y H 2 S þ y CO 2
                   X
                    N c
               T pc ¼  y i T ci ,                 (2:21)
                                                         B ¼ y H 2 S                        (2:25)
                    i¼1
               Table 2.2 Results Given by the Spreadsheet Program MixingRule.xls
               MixingRule.xls
               Description: This spreadsheet calculates gas apparent molecular weight, specific gravity, pseudo-critical pressure,
               and pseudo-critical temperature.
               Instruction: (1) Update gas composition data (y i ); (2) read result.
               Compound     y i     MW i     y i MW i  p ci (psia)  y i p ci (psia)  T ci ,(8R)  y i T ci (8R)
               C 1         0.775    16.04    12.43       673      521.58       344       266.60
               C 2         0.083    30.07     2.50       709       58.85       550        45.65
               C 3         0.021    44.10     0.93       618       12.98       666        13.99
               i-C 4       0.006    58.12     0.35       530        3.18       733         4.40
                           0.002    58.12     0.12       551        1.10       766         1.53
               n-C 4
                           0.003    72.15     0.22       482        1.45       830         2.49
               i-C 5
                           0.008    72.15     0.58       485        3.88       847         6.78
               n-C 5
                           0.001    86.18     0.09       434        0.43       915         0.92
               C 6
               C 7þ        0.001   114.23     0.11       361        0.36      1024         1.02
                           0.050    28.02     1.40       227       11.35       492        24.60
               N 2
               CO 2        0.030    44.01     1.32     1,073       32.19       548        16.44
               H 2 S       0.020    34.08     0.68       672       13.45      1306        26.12
                           1.000   MW a ¼    20.71     p pc ¼     661         T pc ¼     411
                                   g g  ¼     0.71
   28   29   30   31   32   33   34   35   36   37   38