Hydrogen production by autothermal reforming of ethanol over monolith reactors: multi-channel approach Maria Galiano Tavares Casaca Braga Dissertação para obtenção do Grau de Mestre em Engenharia Química Júri Presidente: Prof. Doutor José Madeira Lopes Orientadores: Prof. Doutor Carlos Henriques (Instituto Superior Técnico) Doutor Didier Pavone (IFP Energies nouvelles) Doutor Nuno Pacheco Magalhães (IFP Energies nouvelles) Vogais: Profª Doutora Ana Paula Dias Doutor Victor Costa Setembro 2010
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Hydrogen production by autothermal reforming of
ethanol over monolith reactors: multi-channel approach
Maria Galiano Tavares Casaca Braga
Dissertação para obtenção do Grau de Mestre em
Engenharia Química
Júri
Presidente: Prof. Doutor José Madeira Lopes
Orientadores: Prof. Doutor Carlos Henriques (Instituto Superior Técnico)
Finally, as established for hydrodynamics, since we are at a 2-D axisymmetri
s considered as axis of symmetry.
gas phase, the gas enters in the monolith channel with a well defined
On the outlet, the gas leaves the channel by convective flux, which transport can be
Eq. 9
As stated before, the orange boundary corresponds to the washcoat, where the surface catalytic
chemical reactions occur. Therefore, this boundary contains the sum of terms of reaction that take
Eq. 10
Eq. 11
Eq. 12
Eq. 13
D axisymmetric geometry the
1.3 Heat transfer inside a monolith channel
The applied heat balance (
convective term and thermal conductive
∇
In the present model the
interior of the channel, the gas phase.
there is no gas flow.
On Eq. 14 it can be seen that the unk
The heat transfer depends on the hydrodynamics (
composition and therefore the parameters
The thermal conductivity of the mixture is calculated by the
thermal conductivities of pure components
equation and assumptions are available on reference Poling et al (Poling et al, 2004).
According to the Review of mathematical modelling of monolith reactors
radiation is considered negligible.
monolith structure are constant and independent of the monolith temperature.
The heat generated by reactions and the heat losses are simulated as a boundary condition.
Figure 22 illustrates the boundary conditions for h
Figure
28
inside a monolith channel
heat balance (Eq. 14) shows that the developed model depends
thermal conductive term:
( ) TuCTkipgg ∇=∇− ρ
odel the heat transport, by convection and conduction,
interior of the channel, the gas phase. On the channel wall occurs heat transfer by conduction since
it can be seen that the unknown variable of the heat balance is the temperature (
The heat transfer depends on the hydrodynamics (u ) and mass transfer, which affects the gas
the parametersreactionQ , ipC andk .
The thermal conductivity of the mixture is calculated by the Wassilijewa Equation
components obtained by the software Component Plus
ssumptions are available on reference Poling et al (Poling et al, 2004).
Review of mathematical modelling of monolith reactors
s considered negligible. In addition, it is also assumed that the physical prop
monolith structure are constant and independent of the monolith temperature.
The heat generated by reactions and the heat losses are simulated as a boundary condition.
illustrates the boundary conditions for heat balance equations on the monolith channel.
Figure 22. Heat transfer boundary conditions.
depends on the thermal
Eq. 14
heat transport, by convection and conduction, only occurs in the
On the channel wall occurs heat transfer by conduction since
is the temperature (T ).
) and mass transfer, which affects the gas
Wassilijewa Equation, using the
Component Plus. The method
ssumptions are available on reference Poling et al (Poling et al, 2004).
Review of mathematical modelling of monolith reactors, the heat transfer by
s also assumed that the physical properties of the
The heat generated by reactions and the heat losses are simulated as a boundary condition.
eat balance equations on the monolith channel.
29
On the yellow domain, the gas phase, the gas enters in the monolith channel with a well defined
injection temperature (injT ). It is established, on the pink boundary, that the gas leaves the channel by
convective flux, which transport is represented by Eq. 15:
( ) 0=∇− Tkn Eq. 15
As established for hydrodynamics and mass transfer, since we are at a 2-D axisymmetric
geometry the green boundary is considered as axis of symmetry.
Like stated before, the orange boundary corresponds to the washcoat, where the surface
catalytic chemical reactions occur. Therefore, this boundary corresponds to the heat generated by
reactions that take place ( )reactionQ .
On the blue domain, the channel wall, only occurs heat transfer by conduction. According to the
Review of mathematical modelling of monolith reactors, the single channel approach assumes that the
monolith external wall in insulated once all channels are similar and therefore no heat exchanges
occur. However, previous studies (Pacheco, 2010) have shown that only the top and the bottom of the
monolith channel can be considered insulated, which correspond the black boundaries. For the lateral
monolith wall, red boundary, this boundary condition was changed to heat flux, to simulate the heat
losses of the monolith reactor. The simulations of heat losses, however, are not trivial. The deduction
is explained below (Section 1.4).
30
1.4 Mechanism of heat transfer between zones of homogeneous temperature
For the mechanism of heat transfer between zones, it is assumed that these zones exchange
energy according to Eq. 16, in analogy to heat exchangers:
TAUQ ∆⋅⋅= Eq. 16
Where U is the overall heat transfer coefficient ( KmW ⋅2 ), A the surface area of heat
exchange ( 2m ) and T∆ the temperature difference between zones (K ).
Each homogeneous temperature zone is composed by N number of channels. Therefore, the
energy exchanged by each channel is an Nth part of the total energy exchanged between zones, Eq. 17:
NTAUQchannel /∆⋅⋅= Eq. 17
The heat exchanged by each channel needs to be converted in a heat flux to be employed as a
boundary condition. This heat is the integral of the flux along the exchange surface. Therefore, the
following differential equation, Eq. 18, can be established to obtain the heat flux across the lateral
surface of the channel:
channel
ringchannelHL
ringchannelchannel
channelchannel
NR
TRUF
dzRN
TUdzRF
dAN
TUdAF
∆=⇔
⇔∆=⇔
⇔∆=
:
22 ππ Eq. 18
Hence, the heat flux that is employed as a boundary condition on Figure 22 to simulate the heat
loss per channel is calculated by Eq. 18, channelHLF : .
The overall heat transfer U is a measure of the overall ability of a series of conductive and
convective barriers to heat transfer and can be calculated as the reciprocal of the sum of a series of
thermal resistances (Bird et al, 2001). Therefore, several questions arise in calculation of U: which
transfer mechanisms to consider, which media offer thermal resistance, and how to estimate the mean
thermal resistance.
On Figure 23, a schematic representation of the transversal section of a monolith is shown:
Figure 23. Schematic representation of the transversal cross
As can be schematically seen on
that are separated from each other by channel walls.
the channels is feasible and consequently, no convective heat transfer in this direction occurs. On the
other hand, the monolith channels are co
transfer heat by conduction with each other. Therefore, the monolith presents resistance to the heat
transfer by radial conduction.
The thermal resistance is determined by the ratio between the
zones,x , and the thermal conductivity of the two phases of the monolith: solid
to the monolith walls, and gas phase.
conductionR
In order to simplify the determination of
monolith, Borger et al (Borger et al
conductivity apk in monolith structures based on th
monok of the monolith walls, assuming that monolith behaves like a homogeneous media (
(
= monoap kk
Roh et al (Roh et al, 2010)
conductivity of a reactor bed with metal monolith catalyst for the steam reforming of natural gas.
31
. Schematic representation of the transversal cross-section of a monolith reactor.
As can be schematically seen on Figure 23, a monolith is represented by a number
that are separated from each other by channel walls. On one hand, no radial exchange of gas between
the channels is feasible and consequently, no convective heat transfer in this direction occurs. On the
other hand, the monolith channels are connected by their walls throughout the entire diameter, which
transfer heat by conduction with each other. Therefore, the monolith presents resistance to the heat
The thermal resistance is determined by the ratio between the thickness of the heat transfer
, and the thermal conductivity of the two phases of the monolith: solid phase that
to the monolith walls, and gas phase.
( )gmonomonolithconduction kkf
x
,_ =
to simplify the determination of the thermal conductivity of both components of the
Borger et al, 2005) applied a correlation to calculate the effective radial
in monolith structures based on the void fraction, ε, and the thermal conductivity
of the monolith walls, assuming that monolith behaves like a homogeneous media (
( )
1
1
1
−
+−
+−εε
εε
mono
G
k
k
l, 2010) applied the same correlation, Eq. 20, for the estimation
conductivity of a reactor bed with metal monolith catalyst for the steam reforming of natural gas.
section of a monolith reactor.
, a monolith is represented by a number of channels
o radial exchange of gas between
the channels is feasible and consequently, no convective heat transfer in this direction occurs. On the
nnected by their walls throughout the entire diameter, which
transfer heat by conduction with each other. Therefore, the monolith presents resistance to the heat
thickness of the heat transfer
phase that corresponds
Eq. 19
both components of the
applied a correlation to calculate the effective radial
, and the thermal conductivity
of the monolith walls, assuming that monolith behaves like a homogeneous media (Eq. 20):
Eq. 20
estimation of thermal
conductivity of a reactor bed with metal monolith catalyst for the steam reforming of natural gas.
The correlation of Eq. 20
their study of the effective thermal conductivity of monolith honeycomb structures.
To model the heat transfer on the monolith reactor it i
centre of a zone of homogeneous temperature
interface between the two zones (
performed on a 1/8 of monolith channel:
Figure 24. Radial temperature profile for a 1/8 of monolith. The blue arrows represent the r
direction between zones of homogeneous temperatu
Based on Figure 24, knowing which media offers resistance to heat transfer and how to
calculate the monolith thermal conductivity, it is possible to esta
equations, for each zone:
zone 3 to zone 2:
32
was also tested and validated by Hayes et al (Hayes et al
their study of the effective thermal conductivity of monolith honeycomb structures.
er on the monolith reactor it is considered that it occurs between the
homogeneous temperature ( 'iR ) to the centre of the adjacent zone
interface between the two zones (iR ), as schematically shown on Figure
a 1/8 of monolith channel:
Radial temperature profile for a 1/8 of monolith. The blue arrows represent the r
between zones of homogeneous temperature (from top to bottom): zone 1 to zone 2; zone 2 to zone 3;
zone 3 to exterior.
, knowing which media offers resistance to heat transfer and how to
calculate the monolith thermal conductivity, it is possible to establish the overall heat transfer
to zone 2:
'23
3'2
3'3
'33
23
1
→→
→ −+
−=
apap k
RR
k
RRU
Hayes et al, 2009) in
their study of the effective thermal conductivity of monolith honeycomb structures.
s considered that it occurs between the
to the centre of the adjacent zone ( '1+iR ), across the
Figure 24 for a simulation
Radial temperature profile for a 1/8 of monolith. The blue arrows represent the radial heat transfer
re (from top to bottom): zone 1 to zone 2; zone 2 to zone 3;
, knowing which media offers resistance to heat transfer and how to
blish the overall heat transfer
Eq. 21
33
zone 2 to zone 1:
'12
2'1
2'2
'22
12
1
→→
→ −+
−=
apap k
RR
k
RRU Eq. 22
zone 1 to exterior:
1'1
'11
1
1
→
→ −=
ap
ext
k
RRU Eq. 23
Eq. 21, Eq. 22 and Eq. 23, integrated on Eq. 16, allow to couple zones of homogeneous
temperature by heat transfer terms and, consequently, the representative channels of each zone by Eq.
17.
To summarize, the simulation of heat losses using the multi channel approach is not trivial. A
heat flux per channel needs to be established to simulate the global heat loss. Furthermore, the heat
loss per channel depends on the global heat transfer coefficient of each zone that depends on gas
composition and temperature. This strategy allows accurately simulating the heat loss using the multi--
-channel modelling approach.
1.5 Multi-channel model unknown variables
For each channel there are 3 unknowns for hydrodynamics ( zu , ru andp ), 6 mass balance
variables ( igY ), and the energy balance with 1 unknown (T ), which adds up to 10 coupled unknowns
per channel. Since there are three channels plus the external thermal model, which accounts for one
more unknown, the model developed in this work accounts for 31 unknown that are intrinsically
coupled. As a result, to solve the reactor model the software COMSOL Multiphysics3.5a has been
used, which has showed that it is adapted to solve multiphysics problems of this dimension.
34
2 Multi-channel modelling approach on COMSOL Multiphysics
As stated before, the software COMSOL Multiphysics3.5a is adapted to solve a multiphysics
problem as the presented one. To obtain the simulation results it is required to perform the following
simulation steps:
1. geometry draw, where the object dimensions and shape are defined;
2. mesh, where the geometry mesh is established in order to obtain accurate simulation results;
3. domain conditions, where the mathematical equations are defined for each physical and chemical phenomena;
4. boundary conditions, where the defined boundary conditions are introduced;
5. solver, where the adequate solving method is chosen and performed to obtain the numerical solution;
6. post-processing, where the numerical solution results are given and analyzed;
Figure 25 shows the COMSOL Multiphysics interface, where each channel is defined, as well as
the thermal model developed by Pacheco et al (Pacheco et al, 2010):
Figure 25. COMSOL interface. Each tab contains each channel geometry and the first tab concerns to the
thermal model.
Among all the steps that are required to implement the multi-channel model, there are two that
can be pointed out: the mesh size and the boundary condition that lets couple the channels through the
heat transfer terms defined above. These two modelling steps are presented bellow.
35
2.1 Mesh size for accurate simulations
In order to obtain the maximum accuracy of the simulation solution it is necessary to size the
mesh correctly: minimize the computational time, while at the same time have elements small enough
to capture the sharp gradients (Hayes et al, 1992).
For the monolith channels for hydrogen production by ATR of ethanol the mainly chemical
phenomena occur near to the entrance of the channel, as often in tubular reactors. This leads naturally
to the use of a variable mesh size, with small elements near to the monolith entrance and larger
elements elsewhere. Figure 26 shows the mesh used in this work for a monolith channel:
Figure 26. Element distribution for the monolith channel. The mesh contains 490 elements.
Using this mesh, 40-cm-long reactor contains 490 elements. In each finite element mesh, each
unknown, such as temperature or velocity, is quadratic with respect to the independent coordinates, r
and z. In each vertex of the mesh the model need to solve the intrinsically coupling hydrodynamics,
mass transfer and heat transfer mathematical equations, as well as account for the effects of catalytic
chemical reaction and heat transfer between the channels and the exterior.
36
2.2 Channels coupling by heat transfer terms
As stated on the section Mechanism of heat transfer between zones of homogeneous
temperature, the channels are coupled by heat flux terms, as defined on Eq. 24:
channel
ringchannelHL NR
TRUF
∆=:
Eq. 24
Therefore, each channel depends on its own temperature and the temperature of the adjacent
zones, as schematically represented on Figure 27:
Figure 27. Representative schema that shows the variables that each channel depends on.
So, it is required to transfer the information relative to the channel temperature to the
boundaries of the adjacent channels. That can be done using a COMSOL option called Extrusion
variables. In order to simplify the model and reduce the computational resources it is considered that
there is no radial gradient of temperature in the channels. Therefore, it can be made a temperature
boundary extrusion instead of temperature domain extrusion.
( )ii
ringiiiiii RN
RTTUF
−= +→+
+→11
1
( )11
111
−−
−→−→−
−=
ii
ringiiiiii RN
RTTUF
i
( )ii
ringiiiiii RN
RTTUF
−= +→+
+→11
1
( )11
111
−−
−→−→−
−=
ii
ringiiiiii RN
RTTUF
i
37
a)
b)
Figure 28. COMSOL interface to transfer the boundary information to the adjacent channels: a) to indentify the
variables to transport; b) to choose the destination.
As shown on Figure 28a), the first step is to define on geometry i±1 the variable that is going to
be extruded to geometry i. The second step (Figure 28b) is to define the destination of the extruded
variable to geometry i, where the heat fluxes are calculated.
Summarizing, with this COMSOL tool it is possible to transport the information between the
different geometry tabs, as developed on this work.
38
Results and discussion
To study the heat losses of a monolith reactor for hydrogen production by ATR of ethanol, a
new multi-channel modelling approach has been developed. In order to accurately represent the
monolith reactor behaviour, the model consists in dividing the monolith into three zones of
homogeneous temperature, as represented on Figure 18, which exchange energy between them. For
each zone it has been modelled a representative single channel that are coupled to each other by heat
flux terms. Hence, in addition to heat transfer, the representative channels also take into account the
hydrodynamics and the mass transfer phenomena, with chemical reaction, that occur in a monolith
reactor.
After establishing the mathematical equations for each physical and chemical reactions and
model boundary conditions, several computer simulations took place in order to estimate the unknown
variables of the model:
• hydrodynamics: velocity (u ) and pressure (P )
• mass transfer: components concentration (iC )
• heat transfer: temperature (T )
In this point of the report, the simulations results are presented and discussed. In addition, the
calculated gaseous components concentrations (H2, CO, CO2, CH4, O2 and N2) are compared with
experimental data.
It is important to refer that the presented results correspond to a simulation realized with the
same injection conditions that the one of the experiments performed by Pacheco (Pacheco, 2010),
which are presented on Table 1:
Table 1. Experimental injection conditions.
Pressure (Pa) Temperature (ºC) FAir (Nm3/s) FH2O (kg/s) FEtOH (kg/s)
7.48x105 350 1.19x10-5 2.27 x10-5 8.21 x10-6
Due to heat losses presented by the monolith reactor for hydrogen production, arose the need to
develop a new model that characterize the reactor behaviour. Hence, it can be said that the temperature
is the most interesting variable to analyse, so it is by this variable that begins this results analysis.
1.1 Temperature profiles
Figure 29 shows the temperature profiles inside the three representative reactor channels, as
function of r (radial coordinate) and
CT º350= ).
Figure 29. Temperature profile inside the three representative monolith channels: the right channel corresponds
to the outer channel and the left channel corresponds to the inner channel.
39
Due to heat losses presented by the monolith reactor for hydrogen production, arose the need to
w model that characterize the reactor behaviour. Hence, it can be said that the temperature
is the most interesting variable to analyse, so it is by this variable that begins this results analysis.
Temperature profiles
the temperature profiles inside the three representative reactor channels, as
(radial coordinate) and z (axial coordinate), for the given injection temperature (
Temperature profile inside the three representative monolith channels: the right channel corresponds
to the outer channel and the left channel corresponds to the inner channel.
Due to heat losses presented by the monolith reactor for hydrogen production, arose the need to
w model that characterize the reactor behaviour. Hence, it can be said that the temperature
is the most interesting variable to analyse, so it is by this variable that begins this results analysis.
the temperature profiles inside the three representative reactor channels, as
(axial coordinate), for the given injection temperature (
Temperature profile inside the three representative monolith channels: the right channel corresponds
to the outer channel and the left channel corresponds to the inner channel.
40
As expected, there is a radial temperature profile inside the monolith reactor, where the inner
channels are hotter than the outer channels, as consequence of the heat losses to the exterior that were
observed experimentally by Pacheco (Pacheco, 2010) on the monolith reactor for hydrogen
production. On each channel the radial temperature profile inside is negligible, as shown on Figure 30:
Figure 30. Radial temperature profile of each channel.
As represented on Figure 29, the temperature raise observed at the entrance of the channels,
particularly at the inner channel, is due to the heat released by the exothermic ethanol partial
oxidation. Hence, the observed temperature decrease derives from two effects: the endothermic
reactions that consume part of the heat, and the reactor heat losses, as expected.
It is also interesting to compare simulated axial temperature profile with the axial profile
obtained experimentally. However, it is very difficult to measure the temperature inside the monolith
reactor and unfortunately those measurements were not made on experiments with the same injection
values. Nevertheless, the temperature trend lines can be compared to other experimental case, as
illustrated on Figure 31, as function of z (axial coordinate) and T (temperature coordinate).
370.70
370.75
370.80
370.85
370.90
370.95
371.00
371.05
371.10
371.15
0.0000 0.0001 0.0002 0.0003 0.0004 0.0005 0.0006
r (m)
T (
°C)
T interior channel
T middle channel
T external channel
41
a)
b)
Figure 31. Comparison between the temperature axial profile: a) simulated for each channel; b) experimental.
Although the represented axial temperature profiles do not correspond to the same injection
conditions, it can be observed similar temperature trend lines along the reactor: the initial peak that
corresponds to the exothermic partial oxidation, and the continuous temperature decrease due to the
endothermic reactions and reactor heat losses.
330
350
370
390
410
430
450
-0.05 0 0.05 0.1 0.15 0.2 0.25 0.3 0.35 0.4
z (m)
T (
°C)
T interiorchannel
T middlechannel
T externalchannel
250
300
350
400
450
500
550
600
650
-0.05 0 0.05 0.1 0.15 0.2 0.25 0.3 0.35 0.4
z (m)
T (
°C)
T experimental
1.2 Velocity profiles
Figure 32 illustrates the velocity profiles inside the three representative reactor channels, as
function of r (radial coordinate) and
Figure 32. Velocity profile inside the three representative monolith channels: the right channel corresponds to
the outer channel and the left channel corresponds to the inne
As expected, the fluid flows inside the channels with a Poiseulle
is maximum at the channel centre and zero along the
(Figure 33).
42
illustrates the velocity profiles inside the three representative reactor channels, as
(radial coordinate) and z (axial coordinate), for the given injection conditions (
. Velocity profile inside the three representative monolith channels: the right channel corresponds to
the outer channel and the left channel corresponds to the inner channel.
As expected, the fluid flows inside the channels with a Poiseulle-like profile, where the velocity
the channel centre and zero along the wall, as consequence of the laminar gas flow
illustrates the velocity profiles inside the three representative reactor channels, as
(axial coordinate), for the given injection conditions (Table 1).
. Velocity profile inside the three representative monolith channels: the right channel corresponds to
r channel.
profile, where the velocity
wall, as consequence of the laminar gas flow
43
Figure 33. Radial velocity where a laminar gas flow can be seen.
On Figure 34 it can be observed that at the channel entrance, particularly at the inner channel,
there is a significant raise of fluid maximum velocity. According to the perfect gas law, this velocity
increase is the consequence of two effects: the gas thermal expansion due to temperature increase, and
the chemical reactions that cause molar gas expansion.
Figure 34. Axial velocity for each monolith channel.
As stated before, it can be observed an initial velocity peak as consequence of gas thermal and
molar expansion. As expected, once the interior channel reaches higher temperatures, the thermal
expansion is higher in this channel, which corresponds to the highest peak. Therefore the lowest peak
corresponds to the outer channel. Further, it can be observed a velocity increase that is consequence of
the temperature decrease. Then, it can also be observed a new velocity increase, as consequence of the
molar expansion.
0
0,05
0,1
0,15
0,2
0,0E+00 1,0E-04 2,0E-04 3,0E-04 4,0E-04 5,0E-04
velo
city
(m/s
)
r (m)
Velocity radial centre channel
Velocity radial middle channel
Velocity radial exterior channel
0.14
0.15
0.16
0.17
0.18
0.19
0 0.1 0.2 0.3 0.4
z (m)
velo
city
(m
/s)
Velocity interior channel
Velocity middle channel
Velocity exterior channel
1.3 Product profiles and comparison with chemical data
There are 8 different species in the monolith reactor for hydrogen production by ATR of
ethanol: H2, H2O, CO, CO2, CH4, EtOH, O
Figure 35 shows the hydrogen composition profile, as function of
(axial coordinate), for the given injection conditions (
Figure 35. H2 concentration profile (%mol/mol) inside the three representative monolith channels: the right
channel corresponds to the outer channel and the left channel corresponds to the inner channel.
Figure 35 illustrates a fast hydrogen production at the reactor entrance, which is consequence of
the reactions that take place: partial oxidation and ethanol decomposition (
fact can be enhanced by Figure
consumed close to the reactor entrance. Further, until the outlet of the reactor, there is a decrease on
44
Product profiles and comparison with chemical data
There are 8 different species in the monolith reactor for hydrogen production by ATR of
, EtOH, O2 and N2.
shows the hydrogen composition profile, as function of r (radial coordinate) and
(axial coordinate), for the given injection conditions (Table 1), for each representative channel.
concentration profile (%mol/mol) inside the three representative monolith channels: the right
channel corresponds to the outer channel and the left channel corresponds to the inner channel.
t hydrogen production at the reactor entrance, which is consequence of
the reactions that take place: partial oxidation and ethanol decomposition (Eq. 10
Figure 36, where it is shown that the oxygen and ethanol are completely
the reactor entrance. Further, until the outlet of the reactor, there is a decrease on
There are 8 different species in the monolith reactor for hydrogen production by ATR of
(radial coordinate) and z
), for each representative channel.
concentration profile (%mol/mol) inside the three representative monolith channels: the right
channel corresponds to the outer channel and the left channel corresponds to the inner channel.
t hydrogen production at the reactor entrance, which is consequence of
10 and Eq. 11). This
hanol are completely
the reactor entrance. Further, until the outlet of the reactor, there is a decrease on
45
the hydrogen concentration, due to the incomplete steam reforming of methane (or methanation
reaction) and WGS reactions (Eq. 12 and Eq. 13), which are reversible and therefore consume
hydrogen to produce the reaction reagents, whose concentration profiles are presented on Figure 37.
On Figure 35 it can also be observed that there is a greater hydrogen production in the inner
channel, when compared with the two others. In fact at higher temperatures, the methanation reaction
equilibrium favours the hydrogen side because it is endothermic in this reaction direction. However,
the differences that are observed are not very distinct.
In addition, it can be observed that at the reactor outlet all the channels have the same hydrogen
concentration. This fact is due to the thermodynamic equilibrium that is reached.
Figure 36 shows the ethanol and oxygen conversion profiles along the monolith reactor,
comparing the simulated results, for the centre channel and the experimental data, obtained by
Pacheco (Pacheco, 2010).
Figure 36. Conversion profile for EtOH and O2 along the reactor, for each channel, and comparison with
experimental data.
Figure 36 shows that the simulation results for both components match the experimental results,
which mean that the model accurately simulates the experimental results.
The oxygen profile shows that its consumption is very fast, which allows to confirm that the
POX reaction takes place near to the reactor entrance. The same observation can be made for ethanol
profile, which is completely consumed at the reactor inlet, although after the oxygen. Therefore, it can
be said that the two main reactions for hydrogen production occur at the reactor entrance, nevertheless
the POX reaction occurs before the ethanol decomposition reaction.
0
20
40
60
80
100
0 0,05 0,1 0,15 0,2 0,25 0,3 0,35 0,4
Con
vers
ion
(%)
z (m)
EtOH simulation
O2 simulation
EtOH experimental
O2 experimental
46
To understand the behaviour of the monolith reactor it is also interesting to compare all
components concentration profiles, for each channel. In addition, a comparison between the simulated
results and experimental data, obtained by Pacheco (Pacheco, 2010), is also important to analyse.
Therefore, Figure 37 illustrates all component profiles along the monolith reactor, for each channel, as
well as a comparison between the simulated results and experimental data, as function of z (axial
coordinate) and gas composition (%mol/mol).
Figure 37. H2,CO, CO2, , CH4, O2 and N2 composition profiles, along the ATR reactor, for each channel, and
comparison with experimental data.
On Figure 37 it can be observed that methane concentration increases along the reactor, as a
consequence of the inverse reaction of incomplete steam reforming of methane, which consumes
hydrogen (Eq. 12). Therefore, when the methane concentration increases the hydrogen concentration
decreases.
Figure 37 also shows that the carbon monoxide produced by ethanol decomposition and partial
oxidation is then consumed by the reverse reaction of methane incomplete steam reforming.
0.0
0.2
0.4
0.6
0.8
0 0.1 0.2 0.3 0.4
z (m)
Gas
com
posi
tion
(%m
ol/m
ol)
H2 centre channel
H2 middle channel
H2 external channel
CO centre channel
CO middle channel
CO external channel
CO2 centre channel
CO2 middle channel
CO2 external channel
CH4 centre channel
CH4 middle channel
CH4 external channel
O2 centre channel
O2 middle channel
O2 external channel
N2 centre channel
N2 middle channel
N2 external channel
Exp H2
Exp CO
Exp CO2
Exp CH4
Exp O2
Exp N2
47
It can also be observed that the carbon monoxide concentration increases significantly at the
reactor entrance due to the inverse WGS reaction favoured by high temperatures. Further, its
composition stabilizes as consequence of its consumption by the reverse reaction of methane
incomplete steam reforming.
Summarizing, for all gas components, Figure 37 shows that the concentration trend lines are
similar in levels and in shapes. Therefore, it can be stated that the model correctly represents the
monolith reactor behaviour despite some mismatches that are related to the difficulty to get
experimental data.
48
Conclusions and perspectives
The first conclusion of this work is that the new modelling approach, the “multi-channel model”
was successfully developed to describe the monolith reactor for hydrogen production.
Simulations have shown that the developed model accurately represents the behaviour of the
monolith reactor for hydrogen production by ATR of ethanol, showing a radial temperature gradient,
as consequence of the heat losses present on the reactor. Comparing the simulated temperature axial
profile with the experimental one it can be concluded that the two profiles present similar trend lines.
For the gas composition profile, for each compound, the results agree with the expected ones, where
the ethanol and oxygen are completely consumed for producing hydrogen. A comparison between the
simulated results and experimental data was also made, which showed that the model fits to
experimental data, and represent the monolith reactor behaviour.
To improve the multi-channel model several adjustments could be made in the future, namely to
increase the number of zones and try different thickness of the zones. An improved chemical model
can be also introduced in order to get even more similarities between the simulation and the
experimental results.
Hence, a new model to represent the monolith reactor for hydrogen production by ATR of
ethanol is now available and will be able to be applied in the next future.
49
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