Page 334 - Pressure Swing Adsorption
P. 334

310   PRESSURE SWING ADSORPTION   APPENDIX A                           311

              By  wnting  tile  same  equation  for  component  B,  an  eau1vaicnt  l1ut  not
 Y,
           identical  expression  1s  obtained,  which  can  be  solved  fo.r  the  1nterst1t1al
           veiocity ahead of the shock wave  m terms of the vei'oc1ty behind  n. The result
 t,   t,   ,s Ea. 4.8.


           References

 Y1NIT
           I.  H.-K.  Rhee,  R.  Ans,  and  N.  R.  Amundson.  First  Order  Part1al  Diff'ererma!  Equarwm.  1,
              Prent1ce-Hall,  Englewood Cliffs,  NJ (1986).
 z
           2.  A.  Acnvos, "Method of Charactensttcs Technique,"  Ind.  Eng. Chem.  48.  703-10 (1956).
 (a/
           .J.  M.  C.  Bustos  and  F.  Concha,  "Boundary Conditions  for  the  Conunuous  Sedimentat10n  of
              Ideal Suspensions," A/Ch£ J.  38,  1135-38 (1992).
 Y,
           4.  V.  R.  Dabholkar,  V.  Ba!ako1aiah,  and  D.  Luss,  '"Travelling  Waves  in  Multi-Reaction
              Systems," Chem.  Eng.  Sci. 43, -945-55 (1988).
 z   z,   z,
           5.  A.  KJuwick,  "The Anatytical  Method  of Charactenst1cft,"  Prog.  Aero.mace  Sci.  19,  197-313
             (1981).
           6.  R.  Herman and  I.  Prigogme, "A Two Fluid Approach  IO Town Traffic,"  Science  204.  148-51
             (1979).
 Y-!NIT

 t
 (b/
 Figure A.I  (a)  Composition  front  for  an  adsorption  step, shown  as  three  instanta-
 neous  profiles,  as  It  passes  through  an  eiement of adsorbent.  (b) Composition  front
 for an adsorption step, shown as  histories recorded at three axial  positions within the
 adsorbent.


 case,  a  matenal  t>alance  "around the  front"  1s  written  m  the same form  as
 Eq. 4.1

 ,(· APyA I + A,vPyA I]+ RT(l - e) AnA I ~ O   (A.7)
 Al  '   AZ  I,   Al  I,
 where Al,  represents the shift in  a sliver observed at a specific time, and  6.lz
 represents  the  shift  over  a  motnent  at  a  given  position,  and  that  d.yAi,  =
 -6.y)z,  as  shown  m  the  figure.  When  that  substitution  is  made  and  the
 Ii   definition of OA  ts  applied at constant pressure, the following equation for the
 I   shock veloc1ty,  VsH•  is obtained:
 llzl
 I   VsH  = tit a1•  =  OA  AyA   (A.8)
 AvyA
 I   where  the  shift  ,s  taken  with  respect  to  position  or  time,  but  must  be
 consistent.

 I
   329   330   331   332   333   334   335   336   337   338   339