BY : Dr S V Zhubrin, CHAM Ltd
DATE : March 2002
FOR : Demonstration case for CHAM-Japan
The case presents the implementation in PHOENICS of an IPSA based model for non-equilibrium two-phase reactive flow of coal particles particles finely dispersed in the carrying air-steam stream. The model uses the Eulerian description of the two interpenetrating continua with the transfer of heat, mass and momentum between them. The processes accounted for are the volatilisation of dispersed phase material, gaseous exothermic oxidation of volatile products, heterogeneuos oxidation of particle char, steam reforming, shift conversion and carbon monoxide reduction.
The devolatilisation of particulate phase is considered as kinetically driven. Turbulent oxidation of volatiles is modelled via two-step reaction of hydrocarbon oxidation, in which carbon monoxide is an intermediate product. The reaction rates are considered as a blend of EBU model and Arrhenius kinetics. The char oxidation is represented by blended mechanism of the oxygen diffusion to the particle and chemical kinetic. The relative amount of char oxidation products are assumed to be dependent on the particle temperature. The reaction rates of steam reforming, shift conversion and carbon monoxide reduction are represented through exemplary EBU/Arrhenius-kinetics blends.
The turbulence is accounted for by conventional K-e model.
The model is applied to the pulverized coal gasification in a wall-fed pressurized reaction chamber.
The independent variables of the problem are the three components of cartesian coordinate system.
The main dependent (solved for) variables are:
For the second, particulate, phase, raw coal, COL2, is consumed during devolatilisation, and char, CHA2, solid, combustible residue of volatilisation, appears as COL2 disappears. The char then disappears as it burnt in the char oxidation. The ash contents of the phase, ASH2, increase to value 1 in a completely reacted particles.
For the first, gas, phase volatile fuel, YCH4, appears as a consequence of volatilisation and carbon monoxide reduction, and then disappears as it oxidized in gas-phase reaction with oxygen and consumed in steam reforming. The water steam along with its vapour, YH2O, appear as a consequence of external supply and volatile oxidation, and then are consumed in steam reforming and shift conversion producing hydrogen, YH2, carbon monoxide, YCO, and carbon dioxide, YCO2. The hydrogen can also dissapear through carbon dioxide reduction releasing methane, YCH4, and water vapour. The carbon monoxide and dioxides are also the products of char and volatile oxidations. The oxygen contents, YO2, decrease as it is consumed in both latter reactions.
The volatilisation of solid-fuel, raw coal, particles, is presumed to follow the one-step irreversible reaction type mechanism:
1 Kg Coal = YVKg Volatiles + ( 1 - YV ) Kg Char
where YV stands for the mass fraction of volatiles in coal which is coal-rank dependent and is, normally, the user specified input.
As a consequence, the rate of coal consumption, Rcoal, in kg m-3s-1, is readily related to the rate of volatiles released through associated stoichiometric coefficient as follows:
Rcoal = RV/YV
where RV is mass source of volatiles originating from the coal particles into the gas phase, kg m-3s-1.
The rate of char formation, Rchar, in kg m-3s-1, is also calculated through the volatilisation rate as:
Rchar = ( 1 - YV )RV/YV
Volatilisation kinetics are coal-rank dependent. The volatilisation rate is modelled through an Arrhenius-type expression:
RV = 2.103e-2829/T2mV2MVPV
Here
mV2 = YVCOL2
The mass of voilatiles per unit of reaction volume is given as:
MVPV = RHO2 YVR2
The volatiles are taken as 100% methane. Combustion of the volatiles is treated as a two-step irreversible chemical reaction of methane oxidation as follows:
Step 1: CH4 + 1.5 ( O2 + 3.76N2) = CO + 2H2O + 5.64N2
Step 2: CO + 0.5( O2 + 3.76N2 ) = CO2 + 1.88N2
The reaction rates of combustion are obtained as the harmonic blend of a Arrhenius kinetics and eddy-dissipation rates:
RcomCH4 = - [ ( RkCH4)-1 + (ReCH4 )-1 ]-1 and
RcomCO = - [ ( RkCO )-1 + ( ReCO )-1 ]-1
where Rk and Re, in kg/m3s, are the kinetic and eddy-dissipation rates:
ReCH4 = 4 RHO1 EP/KE min( YCH4, YO2/3)
ReCO = 4 RHO1 EP/KE min( YCO, YO2/0.57)
RkCH4 =
1.15 109RHO12e-24444/T
YCH4-0.3YO21.3
RkCO =
5.42 109RHO12e-15152/T
YO20.25YH2O0.5YCO
The remaining rates are defined through associated stoichiometric coefficients:
Step 1:
R1O2 =
3 RcomCH4
R1CO =
-1.75 RcomCH4
R1H2O =
-2.25 RcomCH4
Step 2:
R2O2 =
0.57 RcomCO
R2CO2 =
-1.57 RcomCO
The net rates of species generation in volatile combustion are the balances of formation and combustion as appropriate:
RV,CH4 = RcomCH4
RV,CO = RcomCO +
R1CO
RV,O2 = R1O2 +
R2O2
RV,CO2 = R2CO2
RV,H2O = R1H2O
The particle char burns creating carbon oxides according to the reaction:
C + 0.5(1 + w) O2 = ( 1 - w)CO + wCO2
where w is the mole fraction of carbon oxides formed as CO2 which is related to the mass fractions as follows:
w = MCOYCO2/( MCOYCO2 + MCO2YCO )
where MCO = 28 and MCO2 =44, are the molecular masses of carbon monoxide and carbon dioxide, respectively.
The mass split between carbon oxides is assumed to depend on the particle temperature as:
YCO/YCO2 = 2500e-6249/T2
The char burnout rate, RC, in kg m-3s-1, is obtained as an harmonic blend of a kinetic- and diffusion-controlled mass-transfer rates:
RC = Ap [ ( KkC)-1 + (KdC )-1 ]-1PO2
where
Ap = 6R2/SIZE, is volumetric particle surface area, 1/m, and PO2 is partial pressure of O2, N/m2.
The partial pressure PO2 is calculated using Dalton's law:
PO2 = xO2P1
Wherein, the mole fraction of O2, xO2, is related to mass fraction, YO2, through molecular masses of O2, MO2, and the mixture, Mmix, as
xO2 = Mmix/MO2YO2
Kinetic mass transfer coefficient, KkC, in s/m, is calculated as:
KkC = 0.1309 e-26850/T2
Diffusion mass transfer coefficient, KdC, in s/m, is calculated as follows:
KdC = Sh DO2MC/ ( RgasT2SIZE )
where
RC,O2 = - 0.5(1 + w) MO2/MC
The rate of CO produced by char combustion, in kg m-3s-1, is related to RC through its own stoichiometric coefficient:
RC,CO = (1 - w) MCO/MC
The rate of CO2 produced by char combustion, in kg m-3s-1, is related to RC through the stoichiometry as follows:
RC,CO2 = wMCO2/MC
Carbon monoxide emerging from char further burns to carbon dioxide in the gas phase as a participant of the second step of volatile combustion.
The volatile methane reacts with water vapour creating carbon monoxide and hydrogen according to the reaction:
CH4 + H2O = CO + 3H2
The reaction rates are obtained, in exemplary manner, as the minimum blend of an Arrhenius kinetics and eddy-dissipation rates:
RrefCH4 = - min( Rkref, Reref) and
where Rk and Re, in kg/m3s, are the kinetic and eddy-dissipation rates:
Reref = 4 RHO1 EP/KE min( YCH4, 16/18.YH2O)
Rkref =
3.21 102RHO1e-468/T
YH2O1.3YCH4
The net rates of species generation in steam reforming are as follows:
RSR,CH4 =RrefCH4
RSR,H2O = 18/16.RSR,CH4
RSR,CO = -28/16.RSR,CH4
RSR,H2 = -6/16.RSR,CH4
The carbon monoxide reacts with water vapour creating carbon dioxide and hydrogen according to the reaction:
CO + H2O = CO2 + H2
The reaction rates are obtained, in exemplary manner, as the minimum blend of an Arrhenius kinetics and eddy-dissipation rates:
RconCO = - min( Rkcon, Recon) and
where Rk and Re, in kg/m3s, are the kinetic and eddy-dissipation rates:
Recon = 4 RHO1 EP/KE min( YCO, 28/18.YH2O)
Rkcon =
3.21 102RHO1e-468/T
YH2O1.3YCO
The net rates of species generation in steam reforming are as follows:
RSC,CO = RconCO
RSC,H2O = 18/28.RSC,CO
RSC,CO2 = -44/28.RSC,CO
RSC,H2 = -2/28.RSC,CO
The carbon monoxide reacts with hydrogen creating methane and water vapour according to the reaction:
CO + 3H2 = CH4 + H2O
The reaction rates are obtained, in exemplary manner, as the minimum blend of an Arrhenius kinetics and eddy-dissipation rates:
RredCO = - min( Rkred, Rered) and
where Rk and Re, in kg/m3s, are the kinetic and eddy-dissipation rates:
Rered = 4 RHO1 EP/KE min( YCO, 28/6.YH2O)
Rkred =
3.21 102RHO1e-468/T
YH21.3YCO
The net rates of species generation in steam reforming are as follows:
RCR,CO = RredCO
RCR,H2 = 6/28.RCR,CO
RCR,CH4 = -16/28.RCR,CO
RCR,H2O = -18/28.RCR,CO
Only the compilation of the model sources which required non-standard settings is provided below.
Interphase mass transfer, kg/s
CMDOT = Vcell( RV + RC )
Wherein Vcell is a cell volume, m3
2nd phase composition, kg m-3s-1
1st phase composition, kg m-3s-1
1st phase energy, W m-3
The reaction heats, i.e. the heats of combustions for volatile methane, H°CH4, carbon monoxide, H°CO, and char, H°C, are released with the rates of their consumptions.
The steam reforming is supposed to be endothermic reaction with the reaction heat H°SR. The heats of the reactions for shift conversion and carbon monoxide reduction are taken as H°SC and H°CR.
The heat is also transfered from the 2nd phase via interphase heat transfer.
In terms of the transport equation for H1, the resulting source term is:
SH1 = SH1,rea + SH1,int
The contribution from the heats of reactions is:
SH1,rea = RcomCH4H°CH4 + RcomCOH°CO + RCH°C + RrefCH4H°SR + RconCOH°SC + RredCOH°CR
The interphase heat transfer contribution is:
SH1,int = HCOF( T2 - T1 )
2nd phase energy, W m-3
The source term for 2nd phase specific enthalpy, H2, is caculated as:
SH2 = SH2,int
where
SH2,int = HCOF( T1 - T2 )
The specific enthalpies are related to the phase temperatures and specific heats:
H1 = CP,1T1 and
H2 = CP,2T2
The solid-phase density is taken as constant, as the ideal gas law is used for the gas phase as follows:
RHO1 = MmixR-1gasT1-1P1
where the molecular mass of the mixture is composition-dependent:
M-1mix = YCH4/16+YO2/32+YN2/28+YCO/18+YCO2/44+YH2O/18+YH2/2
The solid-phase specific heats are taken as constant, and the gas-phase specific heat, CP,1, is assumed to be equal for all gas components and is a linear function of gas temperature and the operating pressure as follows:
CP,1 = (1059 + 0.25( T1 - 300 )) (1.+ 0.005(P1/Po-1)
wherein Po stands for the datum pressure.
The combustion heats of volatiles and carbon monoxide, reaction heats for steam reforming, shift conversion and CO reduction are taken as constants. The heat of combustion for char is assumed to depend on the product split ratio:
H°C = wH°C2CO2 + (1 - w)H°C2CO
where H°C2CO2 and H°C2CO are the heats of carbon oxidation to CO2 and CO, J/kgC, respectively.
Interphase particle heat transfer is represented by a sphere-law correlation:
NUSS = 2. +0.65 REYN0.5
Volumetric heat transfer coefficient, HCOF, in W m-3 K-1, is then evaluated as:
HCOF = ApkgasSIZE-1NUSS
where, kgas is gas heat conductivity taken as constant.
The pressurised reaction chamber chosen for the present computations, idealised though, retains some features of real-life industrial equipment: twenty four coal-supply openings are located at the lower part on the chamber front wall; steam/air-pulverised coal particles are injected axially into the chamber; reaction products flow towards the outlet at the upper part of the chamber.
The chamber is symmetrical, and only half of it is simulated and represented.
At all inlets, values are given of all dependent variables together with the prescribed flow rates.
At the outlet, the fixed exit pressure is set equal to zero and the computed pressures are relative to this pressure.
At the walls, the condition of zero flux is assumed for all dependent variables.
The problem setting-up has been made via VR-menu.
The model sources are coded in GROUND.FOR. They are activated via PATCH/COVAL commands in Q1 file.
In-Form has been used for the specification of the properties, RHO1 and CP1, calculations of chemical rection rates and related auxiliary variables.
The specific-to-model user inputs are: