Page 401 - APPLIED PROCESS DESIGN FOR CHEMICAL AND PETROCHEMICAL PLANTS, Volume 1, 3rd Edition
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Ejectors and  Mechanical  Vacuum Systems                          369

             1  s P <  10 Lorr;  wa  =,  1tD8P0.3 4     (6-12)   flow transition occurs from critical  (sonic)  to subsonic flow
                                                                through any particular leak.  These factors can be calculat-
                                        2
             10 �  P <  100 torr;  w, =  1.2 1tD8Po  6   (6-13)   ed  by  conventional  fluid  flow  methods  if the  size  of the
                                                                leak is estimated, which then is a real problem, or by using
             100 �  P < 760 torr;  w, =  3.98 1tD8      (6-14)   the data of Table 6-8 and applying fluid flow head losses.
                                                                   The  hydraulic  effects  for  the  submerged  portions  of
          where        D  =  sealed diameter,  in.  (estimates of nominal   the vessel or system  can  be  ignored when  the  total  static
                           diameter,  acceptable)               head  on  the  submerged portion  is  not greater than  0.53
                       w, = acceptable air-leakage rate assigned to  a   times atmospheric pressure plus the hydraulic  head  [22],
                           system component,  lb/hr             i.e., r,
                       8  =  specific air leakage rate,  lb/hr/in.
                       P  =  system operating pressl!re,  torr
                W10  =  Wr =  total  calculated air inleakage, lb/hr   P,  =  (p/760)  +  (hLPd34)            (6-16)

             3.  Calculate  the  total  acceptable  air  leakage  rate,  WT,   where  P,  = static pressure, atm
               lb/hr  by  adding  D,V'  a  to  the  sum  of the  leak  rates   P  =  atmospheric pressure, mm Hg
               assigned to the individual  system components,  w3     hL  =  liquid height,  fl,  below liquid surface
                                                                      PL  =  specific gravity of liquid,  relative to water =  1.0
             'Wr =  l:W'  a  +  LW lb/hr                (6-15)
                          0,
                                                                Acceptable Air /nleakage Rates {24}
             To determine the capacity of the vacuum pump,  the val-
           ues  of "\,VT  above  should  not  be  used.  It  is  necessary  to   In  order  to  estimate  an  acceptable  air  inleakage  rate
           apply over-design or safety factors to ensure reliability  [26]   for sizing a vacuum pump for use in the medium to high
           because  pump capacity decreases with  time and wear and   vacuum system,  consider:
           air inleakage surges can occur due to a wide variety of leak
           developing  situations  that result in  more  air or surges  of
           air  inleakage.  The  over-design  factor  should  be  applied   100 Microns (0.10 Torr)  to  1.0 Torr Range
           only  to  the  pump  inlet throughput specification.  The rec-
          ommended  [22]  over-design  factor  should  be  1.5  to  2.0   Estimate  W' a:
           times  the  air  inleakage  rate  [22],  and  should  also  be
           applied  to  saturated  vapors  entering  the  vacuum  equip-   0.1  �  P <  1  torr;  w', =  0.026P0.6 "0).60   (6-17)
                                                                                            4
           ment at the suction conditions required.  Do not put a safe-
           ty factor on tile suction condition of temperature or pres-
          sure,  provided  the worst expected conditions of operation   Estimate  air  inleakage  for  individual  system  specific
           are  specified.  This  requires  a  close  examination  of  the   leak rates, 8, from Table 6-8  [22]  and from  (w �  5  lb/hr)
           process flow sheet range of  operation. A safety factor of 2.0
           is  recommended  for multistage  steam jets  with  compres-   0.1  �  p <  1  torr:  Wa  =  7t  D8P0.6 4   (6-18)
          sion ratio above 6:1; while a  1.5 factor is adequate for most
           mechanical  pumps  and  single-stage jets  with  a  compres-   Note that estimating maximum acceptable differs from
           sion ratio of under 4: 1  [22]. The above  procedure can be   the design equations for Wa  and W'a·
           simplified for preliminary inleakage calculations  [22]:   Calculate  total  acceptable air inleakage rate, WT.

             Multiply W'a  X  2
                                                                                                              (6-19)
             For  equipment  with  rotary  seals  allow  additional  5
           lb/hr for  each  conventional  seal  (packing  type)  and  2   A  simplified  alternate  to  the  previously  cited  proce-
           lb/hr for each mechanical seal and 0-ring.           dures  is  suggested  by  Gomez  [29]  for  calculating  air
             To  account for air inleak a for vessels containing a  liquid   inleakage,  but it is not presented  in detail here.
           level  (portion of vessel submerged), the following applies.
             If there  is  a  large  pinhole  leak a few  inches  below  the
           liquid surface,  it will  behave  like  a leak  above  the  liquid.   Total Capacity at Ejector Suction
          However,  a  small  pinhole  leak  in  the  same  location  may
          have zero  inleakage  due to capillary effects.  The  problem   The  Lota)  capacity  is  the  sum  of all  the  expected con-
          becomes  complicated  as  the  depth  becomes  large,  and   densables  and  non-co nde nsable  flow  quantities  (in
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