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194  HEAT TRANSFER  AND  HEAT  EXCHANGERS



                   EXAMPLE 8.8                                          Re = Dh G, /a
                   Pressure Drop  on  the  Shell Side with  25% Open  Segmental   f = 0.0121Re-0.19,  300 <Re < lo6,   25% segmental baffles,
                   Bafiies, by Kern’s Method (1950, p. 147)
                Nomenclature and formulas:                                  fG,2Ds(N  + 1) -fGSD,(N -   + 1)
                                                                        AP =   2gp&     5.22(1010)sD, ’  psi’
                                       1. 1028P:/D,  - Dt,  triangular pitch,   s = specific gravity.
                   hydraulic diameter  Dh =
                                       1.2732P:/Dt  - Dt,  square pitch,
                                                                       Numerical example:
                                     Q                                  rh = 43,800 lb/hr,
                                                                         s = 0.73 sp gr,
                                                                         y = 0.097 lb/ft hr,
                                                                        D, = 1 in.,
                                            \
                                             \                           Pt= 1.25 in.,  triangular pitch,
                                                                         C = 1.25 - 1.00 = 0.25 in.,
                                                                        D,  = 21.25 in., 1.77 ft.,
                                                                        Dh  = 0.723 in., 0.0603 ft.,
                                                                         B=5in.,
                                F  P  1  -  -  i                         N = 38 baffles,
                                                                        A, = 21.25(0.25)(5)/1.25(144) = 0.1476 sqft,
                     D,  = shell diameter,                              G,  = 43,800/0.1476 = 296,810 lb/(hr)(sqft),
                      B = distance between baffles,                     Re = 0.0603(296,810)/0.97 = 18,450,
                     N = number of baffles,                              f = 0.0121(18,450)-0.19 = 0.00187,
                     A, =flow area = D,BC/P,,                               0.00187(296,810)’(1.77)(39)  = 4,95 psi,
                     C,  = m/A,,  lb/(hr)(sqft),                        AP =  5.22( lo1’)  (0.73)(0.0603)




                construction, the plate-and-frame construction cost is 50-70%  that   in  motor  vehicles, the  designs of  Figures 8.6(h)  and  (i)  have the
                of  shell-and-tube,  according to  Marriott  (Chern.  Eng.,  April  5,   great  merits  of  compactness. and  light  weight.  Any  kind  of
                1971).                                              arrangement of  cross and countercurrent flows is feasible, and three
                    A process design of  a plate-and-frame exchanger is worked out   or  more  different  streams  can  be  accommodated  in  the  same
                by  Ganapathy (1982, p. 368).                       equipment. Pressure drop, heat transfer relations, and other aspects
                                                                    of  design are  well  documented,  particularly by  Kays and London
                SPIRAL HEAT EXCHANGERS
                                                                    (1984) and in HEDH (1983, Sec. 3.9).
                As appears on Figure 8.8(c), the hot fluid enters at the center of the
                spiral element and flows to the periphery; flow of  the cold fluid is   AIR COOLERS
                countercurrent, entering at the periphery and leaving at the center.   In such equipment the process fluid flows through finned tubes and
                Heat  transfer  coefficients are high  on  both  sides, and there  is  no   cooling air is blown across them with fans. Figures 8.4(g) and (h)
                correction to  the  log mean  temperature  difference because of  the   show the two possible arrangements. The economics of  application
                true  countercurrent  action.  These  factors  may  lead  to  surface   of  air  coolers  favors  services  that  allow  25-40°F  temperature
                requirements  20%  or  so  less  than  those  of  shell-and-tube  ex-   difference between  ambient  air  and  process  outlet.  In the  range
                changers. Spiral types generally may be superior with highly viscous   above  10 MBtu/(hr),  air  coolers can be  economically competitive
                fluids at moderate pressures. Design procedures for spiral plate and   with water  coolers when water  of  adequate  quality is  available in
                the related spiral tube exchangers are presented by Minton (1970).   sufficient amount.
                Walker (1982) lists 24 manufacturers of  this kind of  equipment.   Tubes  are  0.75-1.00in.  OD,  with  7-11fins/in.  and  0.5-

                COMPACT (PLATE-FIN) EXCHANGERS                      0.625 in. high, with  a total surface 15-20  times bare surface of  the
                                                                    tube.  Fans are 4-12  ft/dia, develop pressures of  0.5-1.5 in. water,
                Units  like  Figure  8.6(h),  with  similar  kinds  of  passages  for  the   and  require  power  inputs  of  2-5HP/MBtu/hr  or  about  7.5HP/
                hot  and  cold  fluids, are  used  primarily for  gas  service. Typically   lOOsqft  of  exchanger  cross  section.  Spacings  of  fans  along  the
                they  have  surfaces  of  the  order  of  1200mz/m3 (353sqft/cuft),   length of  the equipment do not exceed 1.8 times the width of  the
                corrugation height 3.8-11.8  mm, corrugation thickness 0.2-0.6 mm,   cooler. Face velocities are about  10 ft/sec at a depth of  three rows
                and fin density 230-700  fins/m. The large extended surface permits   and 8 ft/sec at a depth of  six rows.
                about four times the heat transfer rate per unit volume that can be   Standard air coolers come in widths of  8, 10, 12, 16, or 20ft,
                achieved  with  shell-and-tube  construction.  Units  have  been  de-   lengths of  4-40ft,  and  stacks of  3-6  rows  of  tubes.  Example 8.8
                signed for pressures up to 80 atm or so. The close spacings militate   employs typical spacings.
                against fouling service. Commercially, compact exchangers are used   Three modes of  control of  air flow are shown in Figure 3.3(e).
                in  cryogenic  services,  and  also  for  heat  recovery  at  high   Precautions may need to be taken against subcooliig to the freezing
                temperatures in connection with gas turbines.  For mobile units, as   point in winter.
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