Page 333 - Pressure Swing Adsorption
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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
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