Page 216 - Chemical process engineering design and economics
P. 216

Compressors, Pumps, and Turbines                               199




            Table 5.3  Fan Efficiencies

                                 Fan Type        Fan Efficiency 3
                                                     TIP,  %
                            Radial"                  65-70
                            Backward inclined
                              Single Thickness 0      84
                              Air Foil"               90
                              Forward Curved         70-75
                            Axial
                              Tube"                  75-80
                              Vane 0                  85

                           a) Includes fluid and mechanical
                             frictional losses
                           b) Source: Reference 7
                           c) Source: Reference 8







                 A  final  consideration  is  the  fan  operating  temperature  and  environmental
            conditions.  Most  axial  fans  contain  the  motor,  bearings,  and  drive  components
            within the duct.  Thus, the gases must be noncorrosive, at a low temperature (-34
            to  82 °C) (-29.2 to  180 °F)  [1],  nonflammable  and without any particulate matter.
            At  low  or  high  temperatures,  most  steels  lose  their  strength  [8].  Thompson  and
            Trickier  [8] discuss  some  elements of duct-system design.  Table  5.3 summarizes
            efficiencies  for approximate sizing of the fans that have been described.

            Fan Power

            The  most  frequently  used  relationship  in  the  design  of  flow  systems  is  the  macro-
            scopic mechanical-energy balance.  This equation is obtained by integrating the mi-
            croscopic  mechanical-energy  balance  over  the  volume  of  the  system  as  shown  by
            Bird et al. [9]. The balance is given by

               2
            A(v /a)  g      f 2  dp
            ————   + —  Az+  I  —— + W + E = 0                           (5.1)
                     gc     Ji  P
              2g c




         Copyright © 2003 by Taylor & Francis Group LLC
   211   212   213   214   215   216   217   218   219   220   221