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International Journal of Chemical Engineering and Applications, Vol. 1, No. 2, August 2010
                                                              ISSN: 2010-0221




      Dynamic Modeling and Simulation of Catalytic
                Naphtha Reforming
                                                     H.M.Arani1, S.Shokri2, M.Shirvani3


                                                                                 surface.
   Abstract—In this paper, according to the recent progresses in                    More recently Jorge [5] presented a twenty-four lumps
naphtha reforming technology, dynamic modeling of catalytic                      model with 71 reactions and Taskar [6] proposed a more
naphtha reforming process is studied. The dynamic model is                       detailed thirty-five lumps model used for the optimization of
composed of the reforming reaction model, the heat exchanger
model, furnace model, which together, are capable to capture
                                                                                 semi-regenerative naphtha catalytic reformers. Generally
the major dynamics that occur in this process system. Kinetic                    speaking, detailed models are theoretically sound but quite
modeling of the reactions of the fixed bed reactors connected in                 complicated, consequently difficult for application because
series form the most significant part of the overall simulation                  of very complex lumping scheme and parameter estimation to
effort. MATLAB software in SIMULINK mode is used for                             maintain a good balance between kinetics, simplicity and
dynamic simulation. Hougen-Watson Langmuir-Hinshelwood                           applicability of the model [7].
type reaction rate expressions are used to represent rate of each
reaction.The results show models are in fair agreement with the
                                                                                    On the other hand, dynamic modeling was performed by
actual operating data.                                                           Yongyou et al. [15] by a 17 lumps kinetic model and solution
                                                                                 was performed after linearization. Actually, very limited
  Index Terms—Catalytic reforming, Dynamic modeling,                             attempt on dynamic simulation of this process have been
Simulation, Naphtha                                                              appeared in the literature. A modeling and dynamic
                                                                                 simulation on the catalytic reforming process was carried out
                                                                                 by Ansari [16] using Smith's kinetic scheme.
                          I. INTRODUCTION
                                                                                 A. Process Description
   Catalytic naphtha reforming is an important process for
producing high octane gasoline, aromatic feedstock and                              Catalytic naphtha reforming contains three reactors in
hydrogen in petroleum-refining and petrochemical                                 series, as shown in Fig. 1. It is generally carried out in
industries.                                                                      three/four fixed or moving bed reformers. The catalyst used
   Advanced process control and process optimization                             in reformer is commonly a bifunctional bimetallic catalyst
strategies are important to be considered in catalytic                           such as Pt-Re/Al2O3, providing the metal function and the
reforming of naphtha due to its impacts on refineries profit.                    acid function. The product stream from the first reactor after
These are achieved mostly via a reliable mathematical                            preheating enters the second reactor and similarly the product
dynamic model.                                                                   stream from the second reactor after preheating enters the
   The catalytic reforming process came into operation in                        third one. Thus, the reactor feeds are raised to the proper
refineries in the late 1940s. The reforming of naphtha feed                      temperature by heaters located before the reactors, since the
stocks over platinum catalysts was pioneered by Universal                        reactions are endothermic. The product stream from the final
Oil Products (UOP), with the plat forming process introduced                     reactor enters a separator wherein hydrogen rich gas stream is
in 1947.                                                                         separated from the products which is then recycled back and
   Concerning the kinetic modeling of the naphtha processes                      mixed with the first reactor fresh feed. Reactors are of
Smith [1] firstly proposed a four lumps model by considering                     different sizes, with the smallest one located in the first stage
naphtha as being composed of naphthenes, paraffins,                              and the largest one in the last. Temperature profile of the
aromatics and light hydrocarbons (<C5), lumps with average                       reactors is shown in Fig. 2.
carbon number properties in 1959. However, it is not much
precise because of its limited lumps. Kmak [2] developed a
detailed model (Exxon model) including twenty-two lumps,
which was refined by Froment [3] who developed a more
detailed twenty-eight lumps model with 81 reactions.
Ramage [4] developed the Mobile thirteen lumps model that
considered the adsorption of chemical lumps on the catalyst

  1,2
      Research Institute of Petroleum Industry (RIPI), West Blvd. Azadi
Sport Complex, Tehran, Iran
  3
    Assistant Professor, School of Chem. Eng., Iran Univ. Sci. Tehran., Iran
  Corresponding author: Tel.:+982148252503; fax: +982144739713                        Figure 1. Process flow scheme of the catalytic naphtha reformer
  E-mail address: Shokris@ripi.ir



                                                                               159
International Journal of Chemical Engineering and Applications, Vol. 1, No. 2, August 2010
                                                            ISSN: 2010-0221




                                                                       Where, Pi in the above equations is the partial pressure of the
                                                                       components and T is the temperature. As done by Hu et al.
                                                                       (2003) [9] and Taskar (1996) [6], all constants of adsorption
                                                                       terms were obtained by studying the reforming of C7
                                                                       hydrocarbons. Thermodynamics of reactions are considered
                                                                       in another work [10].
                                                                         B. Reactors Dynamic Model
          Figure 2.Temperature distribution in reactors length
                                                                          A dynamic mathematical model with the kinetics
                                                                       described above is developed by assembling the mass and
                                                                       energy balance on the system of reforming reactions. The
                      II. DYNAMIC MODEL
                                                                       mass balance provides the variation of the concentrations of
   There are a number of different methods for modeling the            the components along the reactors, and the energy balance
catalytic reforming process, and the main idea behind all of           gives the variation of temperature. Mass and energy balances
them is to determine the operating conditions of the                   for each reformer are both nonlinear partial differential
reforming unit and to predict the yield of reformate and the           equations in space and time. By taking component material
temperature profile accurately.                                        balances as well as energy balanc on a differential element
   A model must predict the behavior not only within the               “dw” of catalyst bed the following system of differential
reactor, but in the auxiliary areas of the unit as well. It should     equations can be obtained.
also consider the complex nature of the process and the                Mass balance equations for an element of catalyst weight in
reactions which take place during the process of reforming.            a plug flow reactor (proved in appendix A) are:
  A. Reaction Kinetic Model
   Reactions of catalytic naphtha reforming are elementary                                 dFi nr              ε d ( ci )
                                                                                       −      + ∑ γ i , j rj =
and Hougen-Watson Langmuir- Hinshelwood type of                                            dw j =1             ρ b dt
reaction rate expressions are used to describe the rate of each                                                                       (1)
reaction.
   Rate expressions of this type explicitly account for the                Where:
interaction of chemical species with catalyst and contain                                              ci                    Fi
                                                                                             yi =     nc
                                                                                                                      =    nc
                                                                                                                                      (2)
denominators in which characteristic terms of adsorption of
reacting species are presented. The reaction rate coefficients                                       ∑c
                                                                                                     i =1
                                                                                                                  i        ∑F
                                                                                                                           i =1
                                                                                                                                  i
obey the Arrhenius law. All reaction rate equations are
shown in Table 1.                                                                                     m
                                                                                              Ft =                                    (3)
                                                                                                     M av
                TABLE 1: REACTION RATE EQUATIONS
                                                                                                           nc
                                                                                             M av = ∑ yi M i                          (4)
                                                                                                           i =1

                                                                                              Fi = yi Ft                              (5)
                                                                           The energy balance equation for the reactor shown in
                                                                           Fig. 1 can be written (proved in appendix B) as:
                                                                                             nc                        nc
                                                                                                          dT nr
                                                                                        − ( ∑ Fi C pi )      − ∑ rj ( ∑ H iγ i , j )
                                                                                  dT        i =1          dw j =1     i =1           (6)
                                                                                      =
                                                                                  dt                         ε nc
                                                                                                 ( C pcata +   ∑ ci C pi )
                                                                                                                      ρb   i =1

                                                                         Where, ni is the number of moles of ith lump for element
                                                                       with dw of catalyst weight.
                                                                       Where,
   In the above table, adsorption terms for the metal function                                              T
(θ), and for the acid function (Γ), are defined as follows (Van.                       H i = H 0 + ∫ C pi dT                          (7)
Trimpont, Marin and Froment, 1988 )                                                                         T0
                                                                         In Hu et al. [9] catalyst heat capacity in the denominator of
                                                                       energy equation was ignored, while this has great influence
                                                                       on dynamic response of reactors.



                                                                     160
International Journal of Chemical Engineering and Applications, Vol. 1, No. 2, August 2010
                                                                      ISSN: 2010-0221

  C. Furnace ِ Model:                                                                                    Assuming perfect mixing results in achieving a lumped
  Simple model of fired heater furnaces are used here.                                                 parameter model for the heat exchanger, as bellow:
  In the mathematical model of this system the following
assumptions are used:                                                                                  d (C p , cold M cold Tcold , o )
1) Outlet gas temperature from the furnace is equal to tube                                                       dt                                                   (12)
    wall temperature                                                                                   = Fcold ( H cold ,i − H cold , o ) − q
2) The temperature of the tube wall is equivalent over the
    length of tube                                                                                                  d (C p , hot M hotThot , o )
3) Variation of gas temperature inside tube is linear                                                                                                                         (13)
                                                                                                                            dt
  We consider the tubes for heat transfer according to fig.3
                                                                                                                  = Fhot ( H hot ,i − H hot , o ) − q
                                                                                                            The heat transferred q is:
                                                                                                                                                                              (14)
                                                                                                                q = F U A Δ Tm

                                                                                                            Where, ΔTm is logarithm of mean temperature difference.
                                                                                                                     (Thot ,i − Tcold ,o ) − (Thot ,o − Tcold ,i ) (15)
                                                                                                                ΔTm =
                                   Figure 3. Furnace tube.
                                                                                                                                                Thot ,i − Tcold ,o
  Unsteady state energy balance with the considered                                                                                       ln(                      )
assumptions is as:                                                                                                                              Thot ,o − Tcold ,i

                               d (mwC p wTw + m f C p f T f , m )
                                                                                                         E. Octane Number:
                                                    dt                                         (8)
                                                                                                         Octane number of the product from naphtha reforming unit
                                                                             .
                              = q − (T f , out − T f , in )C p f m f                                   can be expressed by concentrations as follows [14]:
                                                                                                                                    n
                                                                                                                                                            (16)
Where,                                                                                                                      RON = b W               ∑       r   r

                                           (T f , in + T f , out )                                                                                   r =1

                              T f ,m =                                                         (9)     Where, br are coefficients and Wr are weight concentrations.
                                                         2                                                 TABLE 2: GROUP DEFINITION AND REGRESSION COEFFICIENTS OF LINEAR
   Supposing linear variation of gas temperature, tube exit                                                            RON MODEL DEVELOPED BY WALSH AND
temperature is equal to Tf,out and Tf,m. Substituting equation (9)                                                                  COWORKERS.

into (8) results in:

                                                             •
                                                                     m f C p f d (T f ,in )
          d (T f ,out )       q − (T f ,out − T f ,in )C p f m f −                            (10)
                          =                                              2          dt
              dt                                             mf Cp f
                                              (mwC p w +                 )
                                                                 2
  In the above equations q is the amount of heat absorbed
by tubes. If the amount of heat generated by fuel is denoted
by Q and the efficiency of the furnace by η, then:
                        q =η Q                          (11)

  D. Heat Exchanger Model:
  Low order lumped parameter model of heat exchangers
were used. Mathematical modeling plays an important role
not only in designing and optimizing chemical engineering
processes but also in studying the dynamic characteristics
and controllability of existing equipment.
  Fig. 4 depicts the thermal shell balance scheme on heat
exchanger for developing the required model.
                                                                                                                                          III. SIMULATION
                                                                                                         Level-1 M-files of S-function in MATLAB software are
                                                                                                       used in this paper for simulating the above equations.
                                                                                                       Distribution of nodes in the space of reactor plays an
                                                                                                       important role in converging to the solution when solving the
                                                                                                       equations. Nodes in beginning of reactor are very close
                                                                                                       together according to Fig. 5.
                                Figure 4. Heat Exchanger.



                                                                                                     161
International Journal of Chemical Engineering and Applications, Vol. 1, No. 2, August 2010
                                                           ISSN: 2010-0221

                                                                                                                714.5




                                                                               Output temp. of first reactor
                                                                                                                 714




                                                                                                                713.5




                                                                                                                 713




             Figure 5. Node distribution in reactor length.
                                                                                                                712.5
                                                                                                                        0   2000    4000      6000      8000   10000   12000
                                                                                                                                           time (sec)
   Derivative terms in the right hand side of partial                        Figure 7. Comparison of plant data with simulated model for 3 o C
differential equations are fitted by second order polynomial.                                  temperature rise in reactor 1.
                                                                                                                744.7

        y = cx 2 + bx + a                                     (17)
                                                                                                                744.6




                                                                               Output temp. of second reactor
                                                                                                                744.5

  Slope is calculated from the equation:                                                                        744.4


                                                                                                                744.3
        dy                                                    (18)
           = 2cx + b                                                                                            744.2
        dx
                                                                                                                744.1



   Constants b and c can be calculated using the values of                                                       744


three consecutive nodes.                                                                                        743.9
                                                                                                                        0   2000    4000      6000      8000   10000   12000
   Fig. 6 shows a flow diagram of the system simulated via                                                                                 time (sec)
MATLAB SIMULINK.                                                             Figure 8. Comparison of plant data with simulated model for 3 o C
                                                                                               temperature rise in reactor 2.
                                                                                                                763.8


                                                                                                                763.7
                                                                               Output temp. of third reactor




                                                                                                                763.6


                                                                                                                763.5


                                                                                                                763.4


                                                                                                                763.3


                                                                                                                763.2


                                                                                                                763.1



Figure 6. Dynamic model and simulation of model by MATLAB software.                                              763
                                                                                                                        0   2000    4000      6000      8000   10000   12000
                                                                                                                                           time (sec)
                                                                             Figure 9. Comparison of plant data with simulated model for 3 o C
   In the SIMULINK mode all variables can be plotted versus                                    temperature rise in reactor 3.
time. The Solver type used in simulation is ode23tb with                    SATISFACTORY FITTING between PLANT AND MODEL IS
variable steps.                                                         DETECTED FROM THE FIGURES.

                IV. RESULTS AND DISCUSSION
   Results of simulated model are compared with                                                                                    V. CONCLUSION
experimental data obtained from the operation data sheets of               In this paper, simulation of the dynamic model of the
a refinery plant in Iran and are shown in Fig. 7. In order to           catalytic naphtha reformer process by MATLAB software is
validate the dynamic model, output temperatures of the                  presented. The kinetic parameters of model are based on the
reactors for input temperatures of three degrees centigrade             steady state condition and are obtained from a commercial
are compared with the data of a refinery in Iran. Plant data are        plant data furnished by a domestic petroleum refinery. This
collected at every 600 seconds. The results of simulation and           dynamic model is in form of partial deferential equations.
comparison are shown in figures 7, 8 and 9.                             The nonlinear model of the system was solved numerically
                                                                        by MATLAB software.
                                                                           The simulation results reveals of satisfactory fitness
                                                                        between data and the model.



                                                                      162
International Journal of Chemical Engineering and Applications, Vol. 1, No. 2, August 2010
                                                                      ISSN: 2010-0221

                                    NOMENCLATURE                                                        nc
                                                                                                     d (∑ Fi H i )                            nc
                                                                                                                                                          dH i
                                                                                               −        i =1
                                                                                                                            dw = −(∑ Fi                        )dw                                (24)
Ac                                                              Catalyst bed area                         dw                                 i =1         dw
ci (kmol / m3 )                                 Particle i mole concentration                                                               nc
                                                                                                                                                          dFi
                                                                Catalyst diameter
                                                                                                                                   − (∑ H i                   )dw
d p( m )                                                                                                                                    i =1          dw
E Aj                                                            Activation energy

G( kg / m 2 .s )                                                  Total mass flux                 Internal energy is related to enthalpy and by expansion of
ε                                                      Porosity of catalyst bed
                                                                                               the right hand side of equation (20) we have:
                                                                                                                                                                   nc
μ( pa.s )                                                                Viscosity                                                           d ( Ecata + ∑ ni ( H i − PVi ))
                                                                                                                            dEsys
ri (kmol / kg cat.s)                                                Reaction Rate                                                       =                         i =1
                                                                                                                              dt                      dt
R                                                                    Gas constant                                                         dEcata       nc
                                                                                                                                                           dH i
                                                                                                                                        =        dw + ∑ ni
ρ s ( kg / m 3 )                                    Density of catalyst particle                                                           dt         i =1  dt                                                     (25)
                                                                                                                                                   nc
ρ f ( kg / m )3                                                                                                                                    dn d ( PV )
                                                                    Fluid Density                                                           + ∑ Hi i −
                                                                                                                                              i =1 dt    dt
Ω( m2 )                                                         Catalyst bed Area
                                                                                                                                        =
                                                                                                                                             dEcata       nc
                                                                                                                                                    dw + ∑ ni
                                                                                                                                                              dH i
                                                                                                                                              dt         i =1  dt
Mav (kg / kmol)                                  Average molecular weight
                                                                                                                                                   nc
                                                                                                                                                                 εdw dci d ( PV )
                                                                                                                                            + ∑ Hi (                 )   −
                                                                                                                                                   i =1           ρ b dt    dt
                                        APPENDIX A
                                                                                                 Where V is the volume of catalyst element upon which the
  Mass balance equation for element of catalyst weight in a
                                                                                               balance is performed.
plug flow reactor is:
                                                                                                                                                                 ε
                                                                                                                                                     V =            dw                                             (26)
                                                         nr                                                                                                      ρb
                          Fi.w − Fi , w + dw + ∑ γ i , j rj dw                                    ni is the number of i'th lump mole in the element with dw
                                                         j =1
                                                                                      (19)     of catalyst weight.
                                  d (ni ) d (ci ) ε                                               By equations (19) and (23) the following equation is
                          =              =          dw
                                    dt      dt ρb                                              obtained:
                                                                                                                    dE sys              dE cata                      nc
                                                                                                                                                                                      dH i
                                                                                                                         dt
                                                                                                                                   =
                                                                                                                                         dt
                                                                                                                                                dw +                ∑n           i
                                                                                                                                                                                       dt
                                                                                                                                                                                           +
                                                                                                                                                                                                                   (27)
   In the above equation ni is as bellow:                                                                                                                           i =1
                                                                                                                       nc
                                                                                                                                          dFi             nr
                                                                                                                                                                                            d (P) ε
                                                     ε                                                             ∑H          i   (−         +           ∑γ      i, j jr ) dw −
                                                                                                                                                                                              dt ρ b
                                                                                                                                                                                                     dw
                                             ni = ci    dw                            (20)                          i =1                  dw              j =1

                                                     ρb                                          By equation (7), (20), (23), (25) and (27), and by ignoring
   And in final step the following equation is attained:                                       pressure effects, we reach to the following equation:

                                                                                                                  nc
                                                                                                                                    dT             dT ε                                    nc
                                                                                                                                                                                                              dT
                       dFi nr              ε d (ci )                                                           − (∑ Fi C pi            ) = C pcata   +                                     ∑c C
                     −    + ∑ γ i , j rj =                                            (21)                                          dw             dt ρ b
                                                                                                                                                                                                     i   pi
                                                                                                                                                                                                              dt   (28)
                                           ρb dt
                                                                                                                  i =1                                                                     i =1
                       dw j =1                                                                                                                            nr            nc
                                                                                                                                                     + ∑ r j (∑ H i γ i , j )
                                                                                                                                                          j =1          i =1
                                        APPENDIX B
   Energy balance equation for an element of catalyst weight                                         And the resulted final equation is:
in a plug flow reactor is:                                                                                                         nc                                     nc
                                                                                                                                                               dT nr
                                                                                                                            − ( ∑ Fi C pi )                      − ∑ rj ( ∑ H iγ i , j )
                                                                                                               dT                  i =1                        dw j =1 i =1                                        (29)
                   nc                          nc
                                                                              dEsys                               =
                   ∑ FH                     − ∑ Fi H i                                                                                                  ε                      nc
                                                                         =                                     dt
                   i =1
                              i     i
                                        w      i =1             w + dw
                                                                               dt
                                                                                      (22)                                                  ( C pcata +
                                                                                                                                                        ρb
                                                                                                                                                                               ∑c C
                                                                                                                                                                               i =1
                                                                                                                                                                                       i        pi   )

   Differential form of the above equation is in the form:

                                        nc                                                                                                          REFERENCES
                                  d (∑ Fi H i )                                                [1]     Smith, R.B. (1959). Kinetic analysis of naphtha reforming
                                                                     dEsys
                          −             i =1
                                                         dw =                         (23)             withplatinum catalyst. Chem. Eng. Pm~ e s s5,5 . 6,76.
                                            dw                           dt                    [2]     Kmak, W.S., Stuckey, A.N. (1973). Powerforming process studies with
                                                                                                       a kinetic simulation model. AlChE National Meetmg, New Orleans,
  The following equation is attained by expansion of the left                                          March, PaperNo.56a.
hand side of the above equation:                                                               [3]     Froment, GF.(IY87). Thc Kinetic of Complex Catalytic Reactions.
                                                                                                       Chem. Eng. Sci., 42,5, 1073.


                                                                                             163
International Journal of Chemical Engineering and Applications, Vol. 1, No. 2, August 2010
                                                                ISSN: 2010-0221
[4]    Ramagc, M.P., Graiani, K.R.,K rambeck, F.l.(1980). Developmcnt of
       Mobil's kinetic reforming model. Chem. Eng. Sci., 35, I, 41
[5]    lorge Ancheyta~luarezE, duardo Villafuene-Macias. (2000). Kinetic
       Modeling of Naphtha Catalytic Reforming Reactions. Energy & Fuels,
       14, 5, 1032.
[6]    Taskar, U,, Riggs, J.B. (1997). Modeling and optimization of
       asemiregenerative catalytic naphtharefarmer. AIChEf., 43, 3, 740.
[7]    Hu. Y., Su, H., Chu, 1. (2003). Modeling. Simulation andOptimization
       of Commercial Naphtha Catalytic Reforming Process. Pmceedinxs
       "/the 42"* IEEE Cofifwmce on Decaion and Coniml, 6206-6211,Dec.
       9~12,Hawuii,USA.
[8]    Rahimpour, M.R., Esmaili, S., Bagheri, GN.A., “Kinetic and
       deactivation model for industrial catalytic naphtha reforming”, Iran. J.
       Sci. Tech., Trans. B: Tech., 27, 279- 290(2003).
[9]    Hu, Y.Y., Su, H.Y., Chu, J., “The research summarize of catalytic
       reforming unit simulation”, Contr. Instrum. Chem. Id.2,9 (2),
       19-23(2002). (In Chinese)
[10]   H. M. Arani, M. Shirvani2, K. Safdarian and E. Dorostkar," Lumping
       procedure for a kinetic model of catalytic naphtha reforming" Braz. J.
       Chem. Eng. vol.26 no.4 Oct./Dec. 2009
[11]   HOU Weifen, SU Hongye, H, U Yongyou, CHU Jian, Zhejiang
       University, "Modeling, Simulation and Optimization of a Whole
       Industrial Catalytic Naphtha Reforming Process on Aspen Plus
       Platform", Chinese J. Chem. Eng., 14(5) 584-591 (2006).
[12]   M. R. Rahimpour, "Operability of an Industrial Catalytic Naphtha
       Reformer in the Presence of Catalyst Deactivation",Chem. Eng.
       Technol., 29, No. 5,(2006).
[13]   Yongyou Hu, Weihua Xu, Hongye Su, Jian Chu, Zhejiang
       university,"Modeling, Simulation and Optimization of Commercial
       Naphtha Catalytic Reforming Process", IEEE, (2004).
[14]   George J. fintos, abdullah M. aitan,"Catalytic naphtha reforming,
       second edition, revised an expanded", MARCELD EKKER, INC,
       (2004).
[15]   Yongyou Hu, Weihua Xu, Hongye Su, Jian Chu, Zhejiang university, "
       A Dynamic Model for Naphtha Catalytic Reformers", IEEE, Taiwan,
       September 2-4,2004
[16]   R.M. Ansari, M.O. Tade, "Constrained nonlinear multivariable control
       of a catalytic reforming process", Control Engineering Practice 6 (1998)
       695-706.
[17]   Anderson, P.C.; Sharkey, J.M.; Walsh, R.P. J. Inst. Petr. 1972, 58 (560),
       83.




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Dynamic modeling and simulation of catalytic

  • 1. International Journal of Chemical Engineering and Applications, Vol. 1, No. 2, August 2010 ISSN: 2010-0221 Dynamic Modeling and Simulation of Catalytic Naphtha Reforming H.M.Arani1, S.Shokri2, M.Shirvani3 surface. Abstract—In this paper, according to the recent progresses in More recently Jorge [5] presented a twenty-four lumps naphtha reforming technology, dynamic modeling of catalytic model with 71 reactions and Taskar [6] proposed a more naphtha reforming process is studied. The dynamic model is detailed thirty-five lumps model used for the optimization of composed of the reforming reaction model, the heat exchanger model, furnace model, which together, are capable to capture semi-regenerative naphtha catalytic reformers. Generally the major dynamics that occur in this process system. Kinetic speaking, detailed models are theoretically sound but quite modeling of the reactions of the fixed bed reactors connected in complicated, consequently difficult for application because series form the most significant part of the overall simulation of very complex lumping scheme and parameter estimation to effort. MATLAB software in SIMULINK mode is used for maintain a good balance between kinetics, simplicity and dynamic simulation. Hougen-Watson Langmuir-Hinshelwood applicability of the model [7]. type reaction rate expressions are used to represent rate of each reaction.The results show models are in fair agreement with the On the other hand, dynamic modeling was performed by actual operating data. Yongyou et al. [15] by a 17 lumps kinetic model and solution was performed after linearization. Actually, very limited Index Terms—Catalytic reforming, Dynamic modeling, attempt on dynamic simulation of this process have been Simulation, Naphtha appeared in the literature. A modeling and dynamic simulation on the catalytic reforming process was carried out by Ansari [16] using Smith's kinetic scheme. I. INTRODUCTION A. Process Description Catalytic naphtha reforming is an important process for producing high octane gasoline, aromatic feedstock and Catalytic naphtha reforming contains three reactors in hydrogen in petroleum-refining and petrochemical series, as shown in Fig. 1. It is generally carried out in industries. three/four fixed or moving bed reformers. The catalyst used Advanced process control and process optimization in reformer is commonly a bifunctional bimetallic catalyst strategies are important to be considered in catalytic such as Pt-Re/Al2O3, providing the metal function and the reforming of naphtha due to its impacts on refineries profit. acid function. The product stream from the first reactor after These are achieved mostly via a reliable mathematical preheating enters the second reactor and similarly the product dynamic model. stream from the second reactor after preheating enters the The catalytic reforming process came into operation in third one. Thus, the reactor feeds are raised to the proper refineries in the late 1940s. The reforming of naphtha feed temperature by heaters located before the reactors, since the stocks over platinum catalysts was pioneered by Universal reactions are endothermic. The product stream from the final Oil Products (UOP), with the plat forming process introduced reactor enters a separator wherein hydrogen rich gas stream is in 1947. separated from the products which is then recycled back and Concerning the kinetic modeling of the naphtha processes mixed with the first reactor fresh feed. Reactors are of Smith [1] firstly proposed a four lumps model by considering different sizes, with the smallest one located in the first stage naphtha as being composed of naphthenes, paraffins, and the largest one in the last. Temperature profile of the aromatics and light hydrocarbons (<C5), lumps with average reactors is shown in Fig. 2. carbon number properties in 1959. However, it is not much precise because of its limited lumps. Kmak [2] developed a detailed model (Exxon model) including twenty-two lumps, which was refined by Froment [3] who developed a more detailed twenty-eight lumps model with 81 reactions. Ramage [4] developed the Mobile thirteen lumps model that considered the adsorption of chemical lumps on the catalyst 1,2 Research Institute of Petroleum Industry (RIPI), West Blvd. Azadi Sport Complex, Tehran, Iran 3 Assistant Professor, School of Chem. Eng., Iran Univ. Sci. Tehran., Iran Corresponding author: Tel.:+982148252503; fax: +982144739713 Figure 1. Process flow scheme of the catalytic naphtha reformer E-mail address: Shokris@ripi.ir 159
  • 2. International Journal of Chemical Engineering and Applications, Vol. 1, No. 2, August 2010 ISSN: 2010-0221 Where, Pi in the above equations is the partial pressure of the components and T is the temperature. As done by Hu et al. (2003) [9] and Taskar (1996) [6], all constants of adsorption terms were obtained by studying the reforming of C7 hydrocarbons. Thermodynamics of reactions are considered in another work [10]. B. Reactors Dynamic Model Figure 2.Temperature distribution in reactors length A dynamic mathematical model with the kinetics described above is developed by assembling the mass and energy balance on the system of reforming reactions. The II. DYNAMIC MODEL mass balance provides the variation of the concentrations of There are a number of different methods for modeling the the components along the reactors, and the energy balance catalytic reforming process, and the main idea behind all of gives the variation of temperature. Mass and energy balances them is to determine the operating conditions of the for each reformer are both nonlinear partial differential reforming unit and to predict the yield of reformate and the equations in space and time. By taking component material temperature profile accurately. balances as well as energy balanc on a differential element A model must predict the behavior not only within the “dw” of catalyst bed the following system of differential reactor, but in the auxiliary areas of the unit as well. It should equations can be obtained. also consider the complex nature of the process and the Mass balance equations for an element of catalyst weight in reactions which take place during the process of reforming. a plug flow reactor (proved in appendix A) are: A. Reaction Kinetic Model Reactions of catalytic naphtha reforming are elementary dFi nr ε d ( ci ) − + ∑ γ i , j rj = and Hougen-Watson Langmuir- Hinshelwood type of dw j =1 ρ b dt reaction rate expressions are used to describe the rate of each (1) reaction. Rate expressions of this type explicitly account for the Where: interaction of chemical species with catalyst and contain ci Fi yi = nc = nc (2) denominators in which characteristic terms of adsorption of reacting species are presented. The reaction rate coefficients ∑c i =1 i ∑F i =1 i obey the Arrhenius law. All reaction rate equations are shown in Table 1. m Ft = (3) M av TABLE 1: REACTION RATE EQUATIONS nc M av = ∑ yi M i (4) i =1 Fi = yi Ft (5) The energy balance equation for the reactor shown in Fig. 1 can be written (proved in appendix B) as: nc nc dT nr − ( ∑ Fi C pi ) − ∑ rj ( ∑ H iγ i , j ) dT i =1 dw j =1 i =1 (6) = dt ε nc ( C pcata + ∑ ci C pi ) ρb i =1 Where, ni is the number of moles of ith lump for element with dw of catalyst weight. Where, In the above table, adsorption terms for the metal function T (θ), and for the acid function (Γ), are defined as follows (Van. H i = H 0 + ∫ C pi dT (7) Trimpont, Marin and Froment, 1988 ) T0 In Hu et al. [9] catalyst heat capacity in the denominator of energy equation was ignored, while this has great influence on dynamic response of reactors. 160
  • 3. International Journal of Chemical Engineering and Applications, Vol. 1, No. 2, August 2010 ISSN: 2010-0221 C. Furnace ِ Model: Assuming perfect mixing results in achieving a lumped Simple model of fired heater furnaces are used here. parameter model for the heat exchanger, as bellow: In the mathematical model of this system the following assumptions are used: d (C p , cold M cold Tcold , o ) 1) Outlet gas temperature from the furnace is equal to tube dt (12) wall temperature = Fcold ( H cold ,i − H cold , o ) − q 2) The temperature of the tube wall is equivalent over the length of tube d (C p , hot M hotThot , o ) 3) Variation of gas temperature inside tube is linear (13) dt We consider the tubes for heat transfer according to fig.3 = Fhot ( H hot ,i − H hot , o ) − q The heat transferred q is: (14) q = F U A Δ Tm Where, ΔTm is logarithm of mean temperature difference. (Thot ,i − Tcold ,o ) − (Thot ,o − Tcold ,i ) (15) ΔTm = Figure 3. Furnace tube. Thot ,i − Tcold ,o Unsteady state energy balance with the considered ln( ) assumptions is as: Thot ,o − Tcold ,i d (mwC p wTw + m f C p f T f , m ) E. Octane Number: dt (8) Octane number of the product from naphtha reforming unit . = q − (T f , out − T f , in )C p f m f can be expressed by concentrations as follows [14]: n (16) Where, RON = b W ∑ r r (T f , in + T f , out ) r =1 T f ,m = (9) Where, br are coefficients and Wr are weight concentrations. 2 TABLE 2: GROUP DEFINITION AND REGRESSION COEFFICIENTS OF LINEAR Supposing linear variation of gas temperature, tube exit RON MODEL DEVELOPED BY WALSH AND temperature is equal to Tf,out and Tf,m. Substituting equation (9) COWORKERS. into (8) results in: • m f C p f d (T f ,in ) d (T f ,out ) q − (T f ,out − T f ,in )C p f m f − (10) = 2 dt dt mf Cp f (mwC p w + ) 2 In the above equations q is the amount of heat absorbed by tubes. If the amount of heat generated by fuel is denoted by Q and the efficiency of the furnace by η, then: q =η Q (11) D. Heat Exchanger Model: Low order lumped parameter model of heat exchangers were used. Mathematical modeling plays an important role not only in designing and optimizing chemical engineering processes but also in studying the dynamic characteristics and controllability of existing equipment. Fig. 4 depicts the thermal shell balance scheme on heat exchanger for developing the required model. III. SIMULATION Level-1 M-files of S-function in MATLAB software are used in this paper for simulating the above equations. Distribution of nodes in the space of reactor plays an important role in converging to the solution when solving the equations. Nodes in beginning of reactor are very close together according to Fig. 5. Figure 4. Heat Exchanger. 161
  • 4. International Journal of Chemical Engineering and Applications, Vol. 1, No. 2, August 2010 ISSN: 2010-0221 714.5 Output temp. of first reactor 714 713.5 713 Figure 5. Node distribution in reactor length. 712.5 0 2000 4000 6000 8000 10000 12000 time (sec) Derivative terms in the right hand side of partial Figure 7. Comparison of plant data with simulated model for 3 o C differential equations are fitted by second order polynomial. temperature rise in reactor 1. 744.7 y = cx 2 + bx + a (17) 744.6 Output temp. of second reactor 744.5 Slope is calculated from the equation: 744.4 744.3 dy (18) = 2cx + b 744.2 dx 744.1 Constants b and c can be calculated using the values of 744 three consecutive nodes. 743.9 0 2000 4000 6000 8000 10000 12000 Fig. 6 shows a flow diagram of the system simulated via time (sec) MATLAB SIMULINK. Figure 8. Comparison of plant data with simulated model for 3 o C temperature rise in reactor 2. 763.8 763.7 Output temp. of third reactor 763.6 763.5 763.4 763.3 763.2 763.1 Figure 6. Dynamic model and simulation of model by MATLAB software. 763 0 2000 4000 6000 8000 10000 12000 time (sec) Figure 9. Comparison of plant data with simulated model for 3 o C In the SIMULINK mode all variables can be plotted versus temperature rise in reactor 3. time. The Solver type used in simulation is ode23tb with SATISFACTORY FITTING between PLANT AND MODEL IS variable steps. DETECTED FROM THE FIGURES. IV. RESULTS AND DISCUSSION Results of simulated model are compared with V. CONCLUSION experimental data obtained from the operation data sheets of In this paper, simulation of the dynamic model of the a refinery plant in Iran and are shown in Fig. 7. In order to catalytic naphtha reformer process by MATLAB software is validate the dynamic model, output temperatures of the presented. The kinetic parameters of model are based on the reactors for input temperatures of three degrees centigrade steady state condition and are obtained from a commercial are compared with the data of a refinery in Iran. Plant data are plant data furnished by a domestic petroleum refinery. This collected at every 600 seconds. The results of simulation and dynamic model is in form of partial deferential equations. comparison are shown in figures 7, 8 and 9. The nonlinear model of the system was solved numerically by MATLAB software. The simulation results reveals of satisfactory fitness between data and the model. 162
  • 5. International Journal of Chemical Engineering and Applications, Vol. 1, No. 2, August 2010 ISSN: 2010-0221 NOMENCLATURE nc d (∑ Fi H i ) nc dH i − i =1 dw = −(∑ Fi )dw (24) Ac Catalyst bed area dw i =1 dw ci (kmol / m3 ) Particle i mole concentration nc dFi Catalyst diameter − (∑ H i )dw d p( m ) i =1 dw E Aj Activation energy G( kg / m 2 .s ) Total mass flux Internal energy is related to enthalpy and by expansion of ε Porosity of catalyst bed the right hand side of equation (20) we have: nc μ( pa.s ) Viscosity d ( Ecata + ∑ ni ( H i − PVi )) dEsys ri (kmol / kg cat.s) Reaction Rate = i =1 dt dt R Gas constant dEcata nc dH i = dw + ∑ ni ρ s ( kg / m 3 ) Density of catalyst particle dt i =1 dt (25) nc ρ f ( kg / m )3 dn d ( PV ) Fluid Density + ∑ Hi i − i =1 dt dt Ω( m2 ) Catalyst bed Area = dEcata nc dw + ∑ ni dH i dt i =1 dt Mav (kg / kmol) Average molecular weight nc εdw dci d ( PV ) + ∑ Hi ( ) − i =1 ρ b dt dt APPENDIX A Where V is the volume of catalyst element upon which the Mass balance equation for element of catalyst weight in a balance is performed. plug flow reactor is: ε V = dw (26) nr ρb Fi.w − Fi , w + dw + ∑ γ i , j rj dw ni is the number of i'th lump mole in the element with dw j =1 (19) of catalyst weight. d (ni ) d (ci ) ε By equations (19) and (23) the following equation is = = dw dt dt ρb obtained: dE sys dE cata nc dH i dt = dt dw + ∑n i dt + (27) In the above equation ni is as bellow: i =1 nc dFi nr d (P) ε ε ∑H i (− + ∑γ i, j jr ) dw − dt ρ b dw ni = ci dw (20) i =1 dw j =1 ρb By equation (7), (20), (23), (25) and (27), and by ignoring And in final step the following equation is attained: pressure effects, we reach to the following equation: nc dT dT ε nc dT dFi nr ε d (ci ) − (∑ Fi C pi ) = C pcata + ∑c C − + ∑ γ i , j rj = (21) dw dt ρ b i pi dt (28) ρb dt i =1 i =1 dw j =1 nr nc + ∑ r j (∑ H i γ i , j ) j =1 i =1 APPENDIX B Energy balance equation for an element of catalyst weight And the resulted final equation is: in a plug flow reactor is: nc nc dT nr − ( ∑ Fi C pi ) − ∑ rj ( ∑ H iγ i , j ) dT i =1 dw j =1 i =1 (29) nc nc dEsys = ∑ FH − ∑ Fi H i ε nc = dt i =1 i i w i =1 w + dw dt (22) ( C pcata + ρb ∑c C i =1 i pi ) Differential form of the above equation is in the form: nc REFERENCES d (∑ Fi H i ) [1] Smith, R.B. (1959). Kinetic analysis of naphtha reforming dEsys − i =1 dw = (23) withplatinum catalyst. Chem. Eng. Pm~ e s s5,5 . 6,76. dw dt [2] Kmak, W.S., Stuckey, A.N. (1973). Powerforming process studies with a kinetic simulation model. AlChE National Meetmg, New Orleans, The following equation is attained by expansion of the left March, PaperNo.56a. hand side of the above equation: [3] Froment, GF.(IY87). Thc Kinetic of Complex Catalytic Reactions. Chem. Eng. Sci., 42,5, 1073. 163
  • 6. International Journal of Chemical Engineering and Applications, Vol. 1, No. 2, August 2010 ISSN: 2010-0221 [4] Ramagc, M.P., Graiani, K.R.,K rambeck, F.l.(1980). Developmcnt of Mobil's kinetic reforming model. Chem. Eng. Sci., 35, I, 41 [5] lorge Ancheyta~luarezE, duardo Villafuene-Macias. (2000). Kinetic Modeling of Naphtha Catalytic Reforming Reactions. Energy & Fuels, 14, 5, 1032. [6] Taskar, U,, Riggs, J.B. (1997). Modeling and optimization of asemiregenerative catalytic naphtharefarmer. AIChEf., 43, 3, 740. [7] Hu. Y., Su, H., Chu, 1. (2003). Modeling. Simulation andOptimization of Commercial Naphtha Catalytic Reforming Process. Pmceedinxs "/the 42"* IEEE Cofifwmce on Decaion and Coniml, 6206-6211,Dec. 9~12,Hawuii,USA. [8] Rahimpour, M.R., Esmaili, S., Bagheri, GN.A., “Kinetic and deactivation model for industrial catalytic naphtha reforming”, Iran. J. Sci. Tech., Trans. B: Tech., 27, 279- 290(2003). [9] Hu, Y.Y., Su, H.Y., Chu, J., “The research summarize of catalytic reforming unit simulation”, Contr. Instrum. Chem. Id.2,9 (2), 19-23(2002). (In Chinese) [10] H. M. Arani, M. Shirvani2, K. Safdarian and E. Dorostkar," Lumping procedure for a kinetic model of catalytic naphtha reforming" Braz. J. Chem. Eng. vol.26 no.4 Oct./Dec. 2009 [11] HOU Weifen, SU Hongye, H, U Yongyou, CHU Jian, Zhejiang University, "Modeling, Simulation and Optimization of a Whole Industrial Catalytic Naphtha Reforming Process on Aspen Plus Platform", Chinese J. Chem. Eng., 14(5) 584-591 (2006). [12] M. R. Rahimpour, "Operability of an Industrial Catalytic Naphtha Reformer in the Presence of Catalyst Deactivation",Chem. Eng. Technol., 29, No. 5,(2006). [13] Yongyou Hu, Weihua Xu, Hongye Su, Jian Chu, Zhejiang university,"Modeling, Simulation and Optimization of Commercial Naphtha Catalytic Reforming Process", IEEE, (2004). [14] George J. fintos, abdullah M. aitan,"Catalytic naphtha reforming, second edition, revised an expanded", MARCELD EKKER, INC, (2004). [15] Yongyou Hu, Weihua Xu, Hongye Su, Jian Chu, Zhejiang university, " A Dynamic Model for Naphtha Catalytic Reformers", IEEE, Taiwan, September 2-4,2004 [16] R.M. Ansari, M.O. Tade, "Constrained nonlinear multivariable control of a catalytic reforming process", Control Engineering Practice 6 (1998) 695-706. [17] Anderson, P.C.; Sharkey, J.M.; Walsh, R.P. J. Inst. Petr. 1972, 58 (560), 83. 164