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                    248                                                    Lawrence K. Wang et al.

                          the air will be required. Such pretreatment of the air will affect two important design
                          parameters:
                          1. Maximum flow rate at actual conditions (Q ) = 100,000 acfm
                                                                e,a
                          2. Temperature (T ) = 400°F
                                         e
                       D. Projected Venturi Pressure Drop
                          The suppliers of the Venturi scrubber system supplies the operating data curves (see
                          Fig. 5). These curves can be used to estimate the pressure drop, P , for the proposed
                                                                                v
                          Venturi scrubber, at a given removal efficiency.
                                                    P = 47 in. H O
                                                     v         2
                          Also previously noted, if this pressure drop exceeds 80 in. H O, alternative control
                                                                            2
                          technology needs to be considered, as the  Venturi scrubber will most likely not
                          achieve the desired removal efficiency.
                       E. Proposed Material of Construction
                          Selection of material used to actually fabricate a Venturi scrubber is normally recom-
                          mended by the system supplier. A useful first estimate of the type of material required
                          can also be made by consulting Table 14.
                                        Material of construction = 316L stainless steel
                       F.  Proposed Venturi Scrubber Sizing
                          Performance curves supplied by system suppliers may be derived for saturated emis-
                          sion stream flow rate (Q ). If so, Q  may be determined:
                                              e,s      e,s
                                          Q  = [Q  (T  + 460) / (T + 460)] + Q                (28)
                                           e,s   e,a  e,s       e          w
                          where Q  is the saturated emission stream flow rate (acfm), T  is the temperature of
                                 e,s                                        e,s
                          the saturation emission stream (°F), T is the temperature of the emission stream at
                                                         e
                          inlet air (°F), Q  is the actual emission flow rate from Eq. (24) (acfm), and Q is the
                                       e,a                                               w
                                               3
                          volume of water added (ft /min or cfm).
                          T  is estimated to be 127°F using the psychrometric chart shown in Fig. 4 with values
                           e,s
                          for L  and T . The inlet lb of H O per lb of dry air (L ) is determined by convert-
                              w,a    e               2                 w,a
                          ing M (now known to be 5%) from percent volume to the lb of H O per lb of dry air
                               e                                               2
                          as follows.
                           L   = (M / 100) (18/29) = (5/100) (18/29) = 0.031 lb H O / lb dry air (Fig. 4)
                            w,a    e                                    2
                          The adiabatic saturation line is determined on the psychrometric chart by determining
                          the intersection of the humidity (L  = 0.031) and the inlet emission stream tempera-
                                                      w,a
                          ture (T = 400°F). This adiabatic saturation line is followed to the left until it intersects
                                e
                          the 100% relative saturation line. At this intersection, the temperature of the saturat-
                          ed emission (T ) is read from the ordinate and the saturated emission L  is read from
                                      e,s                                          w,s
                          the abscissa.
                                                      T  = 127ºF
                                                       e,s
                                            Q = Q    (D ) (L  − L ) (1/D )                    (29)
                                              w   e,ad  e  w,s  w,a    w
                          where

                                 Q    = (1 − L ) Q  = (1 − 0.031) (110,000) = 106,590 acfm   (29a)
                                   e,ad      w,a  e,a
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