Page 143 - APPLIED PROCESS DESIGN FOR CHEMICAL AND PETROCHEMICAL PLANTS, Volume 1, 3rd Edition
P. 143

Fluid Flow                                           129

              Total line pressure drop:                             The majority of industrial chemical and petrochemical
                                                                 plants’  vacuum  operations  are  in  the  range  of  100
                                                                 microns to 760 torr. This is practically speaking the rough
              APvac = [F) = 0.794 in. water (for 350’)           vacuum range noted above. For reference:
                              (350)
                   = (0.794/13.6)  = 0.0584 in. Hg                  1 torr  = 1 mm mercury (mmHg)
                                                                    1 in. mercury  (in. Hg)  = 25.4 torr
                                                                    1 micron  (pm Hg)  = 0.0010 torr
           Final calculated pressure  = 0.6 + 0.0584 = 0.6584 in. Hg   For other conversions, see Appendix.
            10% of 0.658 = 0.0658 in. Hg                            In general, partially due to the size and cost of maintain-
              Therefore the system is applicable to the basis of  the   ing vacuum in a piping system, the lines are not long (cer-
           method, since the  calculated  pressure  drop is  less than   tainly not transmissions lines), and there is a minimum of
            10% of the final pressure, and w/d  = 25.5, which >20.   valves, fittings, and bends to keep the resistance to flow low.
                                                                   The  procedure  recommended  by  Reference  [18]  is
           Low Absolute Pressure Systems for Air [54]            based on the conventional gas flow equations, with some
                                                                 slight  modifications. The  importance  in  final  line  size
              For piping with air in streamline flow at absolute pres-   determination is to determine what is a reasonable pres-
           sures in the range between 50 microns and 1 millimeter   sure loss at the absolute pressure required and the corre-
           of mercury, the following is a recommended method. Cal-   sponding  pipe  size  to  balance  these.  In  some  cases  a
           culation  procedures  in  pressure  regions  below  atmos-   trial/error  approach is necessary.
           pheric are very limited and often not generally applicable
           to broad interpretations.                               Method  [ 181, by permission:
              For this method 10  be applicable, the pressure drop is
           limited to 10% of the final pressure.                    1. Convert mass flow rate to volumetric flow rate, q,.
                                                                      q,  = M7 (359/M)  (760/P,)  (T/(32 + 460)  (1/60),
           Method [54]
                                                                          cu ft/min                           (2-1 28)
              Refer to Figure 2-44 for low pressure friction factor and
           air viscosity of Figure 2-45 to correspond to Figure 2-44.   where  P, = pressure, torr
                                                                            T = temperature, “R
                                                                           W = mass flow, lbs/hr
                                                                            M = molecular weight
                         4f Lpv 2
                 - pg   1 ___-                         (2-127)
                        2gD (144)’ psi
                                                                    2. Calculate section by section from the process vessel to
                                                                      the vacuum pump (point of lowest absolute pressure).
           where    = upstream static pressure, psi abs.            3. Assume a velocity, v, ft/sec  consistent with Figure 2-
                  lPlz  = downstream static pressure, psi abs.        46. Use Table 2-21 for short, direct connected con-
                   f = friction factor, from Figure 2-44.             nections to the vacuum pump. Base the final specifi-
                   E = length of pipe (total equivalent), ft, incl. valves
                      and fittings                                    cations for the line on pump specifications. Also the
                   p  = average density, Ibs/cu ft                    diameter of the line should match the inlet connec-
                   v = average velocity, ft/sec                       tion for the pump. General good practice indicates
                   g = acceleration due to gravity, 32.17 ft/sec-sec   that velocities of 100 to 200 ft/sec are used, with 300
                  D  = inside diameter of pipe, ft                    to 400 ft/sec being the upper limit for the rough vac-
                   p = abs. viscosity of air, Ibs/ft-sec              uum classification.

                                   ~
           V     ~ for other Gases and Vapors                        Sonic velocity, v,  = (kg [1544/M]  T)l/*, ft/sec.
                       c
                             ~
                                                                     Use v from Figure 246, and qm from Equation 2-128.
                ans and Roper  categorize  [18] vacuum in  process
           systems as:                                             4. Determine pipe diameter,
           Category             Absolute Vacuum (Absolute Pressure)   D  = 0.146d  q,/v                      (2- 129)
           Rough vacuum                760 torr to 1 torr
           Medium vacuum               I  to   torr                     Round this to the nearest standard pipe size. Recal-
           High vacuum                     to io-’  torr             culate v based on actual internal diameter of the line.
           Ultra hiel? vacuum          IO-’  torr and below
                                                                                                 (text continued on page 132)
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