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Effects of porosity change of gas diffuser on performance of proton exchange membrane fuel cell

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Effects of porosity change of gas diffuser on performance

of proton exchange membrane fuel cell

Hsin-Sen Chu

a,

, Chung Yeh

a

, Falin Chen

b

aDepartment of Mechanical Engineering, National Chiao Tung University, Hsinchu 300, Taiwan, ROC bInstitute of Applied Mechanics, National Taiwan University, Taipei 106, Taiwan, ROC

Received 30 July 2002; accepted 29 October 2002

Abstract

An investigation is made of the effects of the change of the porosity of the gas diffuser layer (GDL) on the performance of a proton exchange membrane (PEM) fuel cell. The analysis of fuel cell performance with non-uniform porosity of GDL is a necessity because the presence of liquid water in the GDL leads to a non-uniformly distributed porosity in the GDL. To implement this performance analysis, a half-cell model which considers the oxygen mass fraction distribution in the gas channel, the GDL and the catalyst layer, and the current density and the membrane phase potential in the catalyst layer and the membrane is investigated. Four continuous functions of position are employed to describe the porosity, and differential equations are derived based on oxygen transportation and Ohm’s law for proton migration and solved numerically. Results show that a fuel cell embedded with a GDL with a larger averaged porosity will consume a greater amount of oxygen, so that a higher current density is generated and a better fuel cell performance is obtained. This explains partly why fuel cell performance deteriorates significantly as the cathode is flooded with water (i.e. to give a lower effective porosity in the GDL). In terms of the system performance, a change in GDL porosity has virtually no influence on the level of polarization when the current density is medium or lower, but exerts a significant influence when the current density is high. This finding supports the scenario proposed by previous studies that the polarization at high current density corresponds mainly to mass transfer through (or the concentration activation of) the membrane assembly. © 2002 Elsevier Science B.V. All rights reserved.

Keywords: Proton exchange membrane; Fuel cell; Variable porosity; Gas diffuser layer; Performance; Current density

1. Introduction

Proton exchange membrane (PEM, originally referred as solid polymer electrolyte) fuel cells are considered to be promising and environmentally friendly power sources for both mobile and stationary applications. This because of the attributes of high energy density at low operating tempera-ture (70–90◦C), good performance in intermittent operation, quick start-up capability, zero emissions, and minimal prob-lems from component corrosion or electrolyte leakage. Nev-ertheless, polarization occurs during operation of PEM fuel cells and this influences dramatically both the performance and the commercialization of the technology. Accordingly, the development of a theoretical model of the PEM fuel cell, as well as corresponding analyses, are crucial to gain a good understanding of the effect of the operating conditions on the cell potential so that the polarization level can be well

Corresponding author. Tel.:+886-3-571-2121x55115;

fax:+886-3-572-7930.

E-mail address: [email protected] (H.-S. Chu).

controlled. An extensive review of the development of such a model is provided in[1–3].

Bernardi [4] studied the humidification of the inlet gas

that is required to maintain a water balance in a PEM fuel

cell. Verbrugge and Hill[5,6]developed a one-dimensional

model for the proton exchange membrane (MEA) based

on the Nernst–Plank equation. Bernardi and Verbrugge[7]

employed gas-phase transport and membrane models to investigate the performance of a gas-fed porous cathode bonded to a polymer electrolyte, and later they developed a one-dimensional isothermal model for the cell[8]. Springer

et al. [9,10] also derived an isothermal, one-dimensional,

steady-state model of a PEM fuel cell to simulate perfor-mance with a partially dehydrated membrane. Following the work of Bernardi and Verbrugge[8], Singh et al.[11] devel-oped a two-dimensional isothermal model to investigate the effect of two-dimensionality on fuel cell performance. Rowe

and Li [12] produced a one-dimensional non-isothermal

model of a PEM fuel cell. It was found that the temperature distribution within the cell is affected by the phase change of water in the electrodes, and that the partially humidified

0378-7753/$ – see front matter © 2002 Elsevier Science B.V. All rights reserved. PII: S 0 3 7 8 - 7 7 5 3 ( 0 2 ) 0 0 6 0 5 - 5

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reactants decrease the hydration and thus increase the resis-tance of the membrane. To consider the above-mentioned models, however, it is necessary to solve the coupled non-linear differential equations by complicated numeri-cal computations. Also, difficulties may be encountered in that the mass transfer limitations in the gas diffuser layers

(GDLs) and gas channels can be underestimated[13].

To avoid these difficulties, a simplifying approach has

been proposed[13–15] in which the average surface

over-potential across the catalyst layer is used as a set parame-ter in the model. This approach can actually decouple the governing equation and result in an easier-to-solve prob-lem, so that a more complex gas channel topology or a higher dimension of the cell system can be taken into ac-count. A good example can be seen from the research of

Yi and Nguyen[15], who used this approach to investigate

multi-component transport in the porous electrodes of PEM fuel cells using the interdigitated gas distributors. The model describes the two-dimensional flow patterns and the distri-butions of the gaseous species in the porous electrode. The model predicts the current density generated at the interface between the electrode and the membrane as a function of various operating conditions and design parameters. It was shown that the averaged current density generated at the positive electrode (cathode) increases with higher gas flow rates, with a thinner electrode, and with a narrower shoulder between the inlet and outlet channels of the interdigitated gas distributor.

Most of the studies mentioned above have assumed for simplicity that the porosity of the GDL is constant. This, however, may not reflect the importance of GDL porosity on fuel cell performance. In fact, the GDL is composed of a thin layer of carbon black mixed with polytetrafluoroethy-lene (PTFE), a carbon paper consisting of rigid carbon

fib-bers with a diameter of about 10␮m, and a porous structure

formed by carbon fibbers with a pore size of 20–50␮m and

70–80% porosity of volume. Any change in the composi-tion or the morphology of the GDL can lead to a substan-tial influence on fuel cell performance owing to a porosity change[16–19]. In practice, the presence of water generated in the GDL during fuel cell operation can also change the effective porosity, and this change may vary with time and position. Although it has been recognized that the change of content and morphology of the GDL can influence sig-nificantly the optimum performance of the fuel cell, rele-vant studies, especially those with a systematical approach, are still rarely reported in the literature. Accordingly, to consider the effect of the porosity change in terms of the non-uniformity of porosity in GDL on fuel cell performance, it is necessary for work to be done for a precise fuel cell design.

To consider the non-uniformity of the porosity of the

GDL, Gurau et al. [20] developed a one-dimensional

half-cell model in which the concept of the so-called effec-tive porosity was employed to account for the fact that the pores may be partially filled with liquid water. To simplify

the problem so that an analytical solution could be obtained, the authors divided the GDL into a series of parallel layers, in each of which the porosity was considered to be uniform but of a different value. The results showed that the value of the limiting current density decreased when the GDL was flooded with water (a smaller porosity). In the present study, fuel cell performance is investigated by considering the so-called ‘half-cell model’[20]; special attention is paid to the effect of non-uniform porosity on fuel cell performance in terms of physical parameters such as oxygen consump-tion, current density, power density, etc. The non-uniformity of the porosity is accounted for by four different continuous functions of position, each of which has a different averaged value of porosity and a different type of distribution across the GDL.

In the following, the mathematical model and

corre-sponding assumptions are given inSection 2, in which the

governing equations and associated boundary conditions for both the oxygen mass fraction and the membrane phase potential are presented. Mathematical models of porosity

are also discussed. In Section 3, the computational

re-sults are presented to illustrate the effect of non-uniform porosity on the distribution of the oxygen mass fraction across the GDL and the catalyst, as well as on the current density and membrane phase potential across the catalyst

layer and the membrane. In Section 4, the performance

of the fuel cell in terms of the polarization curve is dis-cussed by again focusing on the effect of porosity. It is also shown that the present numerical results serve well to explain the physical meaning of the performance model

proposed previously. Finally, in Section 5, several

con-cluding remarks are made, where the relation between fuel cell performance and the porosity of the GDL is explicitly identified.

2. Mathematical model and assumptions

A schematic of the positive electrode (cathode) side of a PEM fuel cell is shown inFig. 1. This consists of four dif-ferent regions, namely, the gas channel, the GDL, the cata-lyst layer, and the membrane. In the GDL (usually a carbon fiber paper), the morphology varies widely, as determined by the proportions of the constituents. Moreover, in order to consider the presence of the water in the GDL, the effective porosity is taken into account. Since the presence of liquid water is intrinsically non-uniform in the GDL, the porosity of the GDL will be a function of position, instead of a uni-form porosity or a piece-wise uniuni-form model as considered by previous studies, see for example[14,20]. In the present paper, four different models of the porosity of the GDL are considered, and are described by four different mathemati-cally continuous functions (Fig. 2).

(1) Model 1 represents constant porosity and the mean porosity of the GDLεd(x) = 0.4 is considered.

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Fig. 1. Physical model and coordinate system.

(2) Model 2 is a linear function described by εd(x) =

−1.143 × 10−3x + 0.7, which is a mean porosity equal

to 0.523.

(3) Model 3 is a convex exponential function described by

εd(x) = exp 

−7.5 × 10−6x2− 2.04 × 10−4x − 0.357,

which is a mean porosity equal to 0.551.

(4) Model 4 is a concave exponential function described by

εd(x) = exp 

7.5 × 10−6x2− 5.05 × 10−2x − 0.357, which is a mean porosity equal to 0.472.

Fig. 2. Porosity distribution function of four models considered.

Model 1 of uniform porosity allows a comparison to be made between the present numerical results and the

ana-lytical results of Gurau et al. [20]. The other three

mod-els are chosen to account for the effective porosity influ-enced by the presence of water in the GDL during fuel cell operation. The use of an exponential function is primar-ily due to the convenience of the mathematical derivation. There are no existing experimental data by which the real change of porosity with the presence of water in the GDL can be confirmed. Accordingly, no model is thought to be particularly suitable for a cell under a certain operational condition. The present exponential models are therefore be-lieved to be able to account for real conditions to a certain extent.

The mathematical model of the present system is made

on the basis of several assumptions [20]: (a) the model is

one-dimensional; (b) the system is isothermal and steady; (c) the air is taken as an ideal gas; (d) the air is fully saturated with water vapor; (e) the membrane is maintained in a fully hydrated condition; (f) oxygen is transported to the catalyst site as a gaseous component; (g) diffusion is the only mode of transport.

2.1. Governing equations of oxygen mass fraction

The species are transported through the gas channel, the GDL and the catalyst layer only by diffusion. The governing equation for the oxygen mass fraction in the gas channel is: d dx  ρDO2 dYg dx  = 0, 0 ≤ x ≤ Lg (1)

whereρ is the density of mixed gases, DO2 the diffusion

coefficient of oxygen, Yg the oxygen mass fraction in the

gas channel and x the position. In the GDL, the equation is d dx  [εd(x)]τdρDO2 dYd dx  = 0, Lg≤ x ≤ Ld (2)

whereεd(x) and τdare the porosity function and tortuosity

factor of the GDL, respectively, and Ydis the oxygen mass

fraction in the GDL. Since the GDL is a porous medium, a

Bruggeman-type correction[21]can be applied to account

for the effective diffusion coefficient. In the catalyst layer, the oxygen is consumed and the governing equation is:

d dx  ετcc ρDO2 dYc dx  = j 4FMO2 Ld≤ x ≤ Lc (3)

where εc and τc are the uniform porosity and tortuosity

factor of the catalyst layer, respectively, Yc is the oxygen

mass fraction in the catalyst layer, F = 96,487 the

Fara-day constant, MO2 = 32 the molecular mass of oxygen,

j = 2FκYcexp[2αFη/RT] the cathode transfer current

den-sity, in whichκ is the reaction rate constant, α the transfer

coefficient, η the surface overpotential, R = 8.314 is the

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The boundary conditions at different positions accounted for by the oxygen mass fraction are:

Yg= Y0, x = 0 (4a) DO2 dYg dx = [εd(x)] τdD O2 dYd dx , x = Lg (4b) Yg= Yd, x = Lg (4c) [εd(x)]τdDO2 dYd dx = ε τc cDO2 dYc dx , x = Ld (4d) Yd= Yc, x = Ld (4e) dYc dx = 0, x = Lc (4f)

The densityρ is calculated from the ideal gas law[21], i.e.

ρ = PM

RT (5)

where P is the pressure and M the molecular mass. The molecular mass of the gas mixture is obtained by:

M = 1

(Yi/MO2) + (Yw/Mw) + ((1 − Yw− Yi)/MN2)

,

i = g, d, c (6)

where Yw is the water vapor mass fraction, the subscripts

O2, w and N2mean oxygen, water vapor and nitrogen,

re-spectively. The mass fraction of the saturated water vapor is given by:

Yw= P sat w Mw

PM (7)

where the water saturation pressurePwsatis calculated from the following expression[22]:

ln(Pwsat) = −5800.2206

T + 1.3914993

− 0.048640239(T +0.41764768 × 10−4)T2 − 0.14452093×10−7(T3+6.5459673)ln(T ) (8)

The oxygen diffusion coefficient is a function of the binary diffusion coefficients, namely:

DO2= 1−Yi (Yw/(DO2–wMw))+((1−Yw−Yi)/(DO2–N2MN2)) 1 M, i = g, d, c (9)

The binary diffusion coefficientsDO2–wandDO2–N2are then

calculated by using the Slattery and Bird estimation[21]:

Dk,m= 10.13 × a(T/ 

Tcr,kTcr,m)b(Pcr,kPcr,m)1/3(Tcr,kTcr,m)5/12((1/Mk) + (1/Mm))1/2

P (10)

where a, b are the constants in the Slattery and Bird estima-tion for the binary diffusion coefficients and the subscript cr accounts for the critical values.

2.2. Governing equations of membrane phase potential

The membrane phase potential exists in the membrane and the catalyst layer, and accounts for the difference be-tween the surface overpotential and the potential of electron-ically conductive carbon. In the present system, the averaged surface overpotential across the catalyst layer is considered constant, and is used as a parameter of the model. In the membrane, the governing equation of the phase potential is given as: d dx  σdΦm dx  = 0, Lc≤ x ≤ Lm (11)

whereσ is the ionic conductivity of the membrane and Φm

the membrane phase potential in membrane. In the catalyst layer, the equation becomes:

d dx  ετionσdΦc dx  = j, Ld≤ x ≤ Lc (12)

where ε and τion are the porosity and tortuosity of the

ionomer in the catalyst layer, respective1y,Φcthe membrane

phase potential in the catalyst layer.

The boundary conditions applied at different positions are: dΦc dx = 0, x = Ld (13a) ετiondΦc dx = dΦm dx , x = Lc (13b) Φc= Φm, x = Lc (13c) Φm= 0, x = Lm (13d)

In above equations, the membrane ionic conductivityσ can

be obtained by the empirical expression[9]:

σ = (0.5139λ − 0.326)exp  1268  1 303− 1 T  (14)

whereλ is the membrane water content at the interface. A

typical function form ofλ measured for Nafion 117 can be

found in[9], and has a value between 14 and 22, as dictated by the temperature of water.

2.3. Governing equations of current density

In the membrane and the catalyst layer, the current den-sity is governed by Ohm’s law for proton migration. The

equations are written as:

ic= ετionσ

dΦc

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im= σ

dΦm

dx , Lc≤ x ≤ Lm (16)

where i is the current density; the subscripts c and m mean catalyst layer and membrane, respectively, After obtaining the values of the membrane phase potential, the calculation for current density can be carried out easily fromEqs. (15) and (16)without employing boundary conditions. The above

equations are the same as those used by Gurau et al.[20],

except that the porosity of the GDL is considered as a func-tion of posifunc-tion, as shown in the beginning ofSection 2.

3. Effects of change of porosity

The resulting steady-state, non-linear, differential equa-tions shown in the previous section are solved by a fi-nite difference numerical approach. The central differencing scheme is applied, which is a routine procedure and is de-scribed many numerical textbooks. Thus, it is not necessary to show explicitly the discretized equations. The base case conditions are the same as those used by Gurau et al.[20]; the reader is referred to their Table 1 for the details. 3.1. Effects on oxygen mass fraction

The effects of porosity change on the oxygen mass frac-tion across the gas channel and the GDL catalyst layer are examined for three different surface overpotentials, namely,

η = 0.25, 0.28 and 0.36. The computational results are

given inFig. 3. Results show that, for the same porosity in

the GDL, a higher surface overpotentialη leads to a lower

oxygen mass fraction in the gas channel. This is due to the

Fig. 3. Effects of porosity change on distribution of oxygen mass fraction across gas channel, GDL and catalyst layer for three different surface overpotentials.

fact that a larger surface overpotential,η, corresponds to a more active electrochemical reaction, which leads to an in-crease in the oxygen consumption in the gas channel. On the other hand, for the same overpotential, a higher aver-aged porosity of the GDL results in a smaller oxygen mass fraction in the gas channel. This is because a larger poros-ity of the GDL allows a higher consumption of oxygen in the catalyst layer. For the same reason, when the overpo-tential is smaller, the consumption of oxygen is smaller and the oxygen consumption is significantly less influenced by the porosity change in the GDL. See, for example, the case of η = 0.25, in which the oxygen mass fractions in the gas channel given by the four different porosity models are virtually the same. Under such circumstances, the electro-chemical reaction is dominated by the surface kinetics in the catalyst layer.

In the GDL, the effect of a continuous change of

poros-ity can be seen. Whenη = 0.36, for example, the oxygen

mass fraction changes with position and follows closely the porosity distribution across the GDL, i.e. as stated previ-ously, the oxygen mass fraction is smaller when the poros-ity is larger, and vice versa. To some extent, this reflects the fact that the oxygen mass fraction is not uniform across the GDL, especially in the region adjacent to the face between the GDL and the catalyst layer. It is inter-esting to note that the difference in oxygen mass fraction

due to the porosity change in the GDL decreases asη

be-comes larger because, for a largerη, the electrochemical re-action is more active and more oxygen is consumed. When

η = 0.36, the electrochemical reaction is so strong that the

oxygen is almost depleted completely in the catalyst layer, and differences in the oxygen mass fractions between the

four models disappear. For low η, the difference remains

because under such circumstances, the electrochemical re-action is dominated by the surface kinetics, so that less oxygen in the catalyst layer is consumed and the amount of oxygen remaining increases as the porosity decreases.

Consequently, the difference becomes more significant asη

decreases.

The change in the oxygen mass fraction across the

cata-lyst layer due to the porosity change in the GDL forη =

0.25, 0.28, 0.36 is illustrated inFig. 4. Note that, because the catalyst layer is very thin and the electrochemical reaction within the layer prevails, the variation in the oxygen mass fraction across the layer is not at all significant for all three

values of η, and cannot be detected on the decimal scale.

On a logarithmic scale, however, the variation in the case of

η = 0.36 can be clearly seen, i.e. the oxygen mass fraction

decreases exponentially from the GDL to the membrane. Al-though all the variations are very small, the averaged

oxy-gen mass fraction of η = 0.36 is the smallest because the

oxygen mass fraction decreases as η increases due to the

dominance of the electrochemical reaction. By contrast, the effect of the porosity change in the GDL on the oxygen mass fraction is insignificant for all the three values ofη. This is because virtually all the oxygen has been consumed within

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Fig. 4. Variations of oxygen mass fraction in catalyst layer for three different surface overpotentials and four different porosity models.

the catalyst layer. Thus, the differences between the oxygen mass fractions in the four porosity models are insignificant. 3.2. Effects on current density

The current density distributions in the catalyst–layer– membrane domain of the four porosity models of the GDL whenη = 0.25, 0.28, 0.36 are given inFig. 5. The current density increases significantly in the catalyst layer and ap-proaches to the limiting value in the membrane, which

in-Fig. 5. Effects of porosity change on distribution of current density across catalyst layer and membrane for three different surface overpotentials.

creases with η because a higher overpotential results in a

more active electrochemical reaction and thus a higher resul-tant electronic current. For the sameη but different porosity model of the GDL, the current density increases with the av-eraged porosity. Again, this is obviously due to the fact that a larger porosity in the GDL leads to a larger consumption of oxygen in the catalyst layer, and thus a larger current density is generated. The difference between the highest and lowest

current density can be as much as 16% whenη = 0.36 and

the averaged porosity differs by about 30% (the difference between models 3 and 4). The effect of variable porosity on the current density is not seen at all inFig. 5. This is because the electronic current occurs only in the catalyst layer, in which the chemical reaction is influenced only by the amount of oxygen transported from the GDL into the catalyst layer, and is independent of the porosity distribution in the GDL. 3.3. Effects on membrane phase potential

The variation of the membrane phase potentialΦ in the

catalyst–layer–membrane domain for the different porosity

models and surface overpotentialη = 0.25, 028, 0.36 is

il-lustrated inFig. 6. The membrane phase potential is lower

when the porosity of the GDL is higher. For instance, model 3 is for the highest averaged porosity but the lowest phase potential among the four models considered; whereas model 4 is for the lowest averaged porosity but highest phase po-tential. The difference between the highest and lowest

mem-brane phase potential is 24% when η = 0.36. A higher

porosity in the GDL leads to a larger current density, and thus a higher loss of the membrane phase potential. As a result, model 3 (i.e. highest averaged porosity, lowest mem-brane phase potential) represents the best cell performance

Fig. 6. Effects of porosity change on membrane phase potential across catalyst layer and membrane for three different surface overpotentials.

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among the four porosity models. For the same physical rea-sons, when the same model of porosity is considered, the loss of membrane phase potential is larger when the overpo-tential is larger, which again results in a better performance of the fuel cell.

4. Physical explanation of performance model

Models to describe the steady-state performance of the PEM fuel cell have been developed by other workers

[1,10,22–24]. The complexity of the model varies

consider-ably. A typical model proposed by Lee et al.[24]presents

a comprehensive empirical relation between voltage and current, i.e. V = V0− b ln i − Ri − m exp(ni) − b ln  P PO2  (17)

where b, R, m and n are empirical parameters to be deter-mined experimentally. The first term on the right-hand side ofEq. (17)is the open-circuit voltage, usually 1.2 V for a hy-drogen fuel cell. The remaining four terms on the right-hand side ofEq. (17) account for different kinds of polarization (or irreversibilities) of the cell. The second term is called the ‘activation polarization’, caused mainly by the slowness of the reaction on the electrode surface. The third term is the ‘ohmic polarization’ due to the resistance to the flow of ions through the electrolyte. These first three terms are essen-tially the same for the different models proposed before and can provide a good prediction of the performance when the current density is lower than the limiting value. The last two terms, usually the concentration polarization, are proposed particularly for the performance when the current density is close to the limiting current density and the voltage experi-ences a rapid drop. Recently, a large effort has been devoted to discussing the mathematical form of the fuel cell perfor-mance in this high current density regime. There is, however, a lack of physical justification of the corresponding math-ematical expression. For example, the exponential term of

Eq. (17), first proposed by Kim et al.[23], turns out to serve merely as a tool for curve fitting so that the parameters m and n have to be recalculated for any change in the operation conditions. The logarithmic term proposed by Lee et al.[24]

is a form of the Nernst equation; it is of a more clear physical sense and accounts for the influence of the oxygen fraction on the voltage drop. Namely, a smaller oxygen mass fraction leads to a larger voltage drop, and this is supported by the present results. Actually, the present computational results indicate that the level of polarization, or the voltage drop, in the high current density regime corresponds largely to the transport of oxygen at the cathode, and this, as shown by the results discussed in the previous section, is related closely to the porosity of the GDL. A limiting case of this scenario is that as soon as the oxygen is consumed completely, the voltage shall drop to zero because the fuel cell is expected

Fig. 7. Polarization and power density curves corresponding to four different porosity models.

to cease functioning due to the lack of oxygen. This occurs when the system approaches the limiting current.

The above scenario is examined in the present analysis by considering the four porosity models and the fuel cell perfor-mance is discussed with the aid of polarization curves. For the base case conditions[20], there are various relationships between any two of the following parameters: the external load, the cell voltage, the cell operating current density, the surface overpotential across the cathode catalyst layer. When the surface overpotential is taken as the governing parameter of the system[20], the polarization curve can be described parametrically by the relation between V(η) and i(η), where

V(η) = V0− Φ(η) − η is the cell voltage and V0 is the

open circuit voltage. The power density curves also can be

described parametrically by the relation between PW(η) and

i(η), where PW(η) = V(η) × i(η) is the power density. The curves of polarization and power density corresponding to

the four porosity models are shown in Fig. 7, in which a

comparison between the polarization curve of the present model 1 and that of the analytical work of Gurau et al.[20]

for a uniform porosityεd(x) = 0.4 is also shown. It is found

that the present numerical results are in excellent agreement with the analytical results of Gurau et al.[20], which con-firms that the present numerical approach has been correctly implemented.

The polarization curves consist of three regions of differ-ent voltage drop, which is typical for a PEM fuel cell. They are: (i) the region on the left (first sharp drop) corresponds to the activation polarization, accounted for by the second term of Eq. (17); (ii) the region in the middle (decreasing linearly) corresponds to the ohmic polarization, accounted for by the third term ofEq. (17); and (iii) the region on the right (second sharp drop) corresponds to the concentration polarization, accounted for by the last two terms ofEq. (17). Note that, the polarization curves of the four porosity

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mod-els overlap in the region of low-to-medium current density (the linear regime), while at higher current density close to the limiting value, differences between the four models be-come significant. This implies that the porosity of the GDL exerts no influence on fuel cell performance when the cur-rent density is of a medium or low value, but has a signifi-cant when the current density is close to the limiting value. The explanation suggested by the present results is that a larger porosity in the GDL results in a larger oxygen trans-fer from the gas channel to the catalyst layer, and thus a larger current density is generated. Thus, for example, for the model of the highest porosity, i.e. model 3, the limiting current density is the largest. This finding implies that the polarization curve in the regime close to the limiting current density is governed by the performance of the mass transfer across both the GDL and the catalyst layer, as commonly

proposed in previous studies[23–25]. Similar phenomena

were also found by Rho et al.[26], who indicated that the

drastic drop of voltage is due to the transport limitation of oxygen through the GDL, and a mixed gas with a higher oxygen leads to a higher limiting current density. Rho et al.

[27]further pointed out that the departure of cell potential from the linear regime is caused by partial flooding of the GDL, which decreases the oxygen diffusion in the GDL and thus the voltage of the cell.

It is also seen fromFig. 7that the power density increases virtually linearly with current density. When the latter ap-proaches the limiting value, the power density reaches a maximum and then decreases sharply because of the deple-tion of oxygen in the catalyst layer. The maximum power density increases and corresponds to a higher current den-sity as the poroden-sity of the GDL is increased. Consequently, a fuel cell can generally deliver better performance when a GDL of larger porosity is used.

5. Concluding remarks

The influence of the porosity of the GDL on the perfor-mance of a PEM fuel cell has been investigated. Four poros-ity models which represents different continuous functions of position are considered so that the porosity influence can be studied in a systematic way. Due to the complexity caused by the porosity models considered, the resultant simultane-ous differential equations are solved numerically. Results corresponding to the uniform porosity model are in excel-lent agreement with the analytical results of Gurau et al.

[20], and thus confirm the accuracy of the present analyses. It is also found that the influence of the porosity change in the GDL generally reflects the oxygen transfer from the gas channel to the GDL and catalyst layer, i.e. greater porosity leads to higher consumption of oxygen such that higher cur-rent density is generated and a better fuel cell performance is obtained. The present analyses also serve to explain the physical meaning of the performance model in the high cur-rent density regime, which has been an issue discussed in

many previous publications. In summary, the following con-clusions have been drawn.

1. A higher averaged porosity of the GDL results in a smaller oxygen mass fraction in the gas channel because a higher consumption of oxygen in the catalyst layer occurs. Consequently, a fuel cell with a higher surface

overpotential, η, may require a GDL of larger porosity

so that a larger quantity of oxygen can be provided from the gas channel to the catalyst. This is because, due to

the higher η, more oxygen is required to support the

active electrochemical reaction.

2. A continuous change in the porosity of the GDL may be necessary to accommodate the fact that the oxygen mass fraction is not uniform across the GDL, especially in the region adjacent to the interface between the GDL and the catalyst layer. This effect is less significant whenη is large because the electrochemical reaction is then more active and more oxygen is consumed, which leads to a smaller difference oxygen in the oxygen mass fraction across the GDL.

3. Across the catalyst layer, the current density increases rapidly from zero at the interface between GDL and cata-lyst to the limiting value at the interface between catacata-lyst and membrane. The limiting current density increases withη because a higher η leads to a more active electro-chemical reaction as well as a higher current. The current density also increases with the averaged porosity of the GDL because of the larger consumption of oxygen in the catalyst layer.

4. A higher porosity in the GDL leads to a larger current density and therefore a higher loss of the membrane phase potential, which also corresponds to a larger overpotential and a better performance of the fuel cell.

5. A change in the porosity of the GDL has virtually no in-fluence on the polarization level when the current density is at a medium or low value. On the other hand, it has a significant effect on the polarization when the current density is close to the limiting value. This is obviously due to the fact that a larger porosity in the GDL results in a larger oxygen transfer from the gas channel to the catalyst layer, and thus a larger current density is gen-erated. This result supports the fact that the polarization curve in the regime close to the limiting current den-sity is governed by the performance of the mass transfer across both the GDL and the catalyst layer, as proposed in previous studies[22–24].

Although the present results indicate coherently that a larger porosity of the GDL leads to a higher current den-sity, and to some extent a better performance of the fuel cell, a high porosity is accompanied by water flooding in the

GDL and this decreases markedly the cell voltage[16].

Be-sides, as concluded by the present paper, a fuel cell with a higher surface overpotential,η, may require a GDL of greater porosity because more oxygen is necessary to support the active electrochemical reaction. Gurau et al.[20]indicated,

(9)

however, that a higherη induces a higher ohmic resistance in the catalyst layer, which in turn decreases the fuel cell voltage under moderate current density because ohmic re-sistance dominates the cell performance.

It is also noted that optimization of the GDL depends not only on porosity morphology, but also on the thickness and the content of the GDL. Giorgi et al.[18]have shown that a change in the content of PTFE of GDL results in a change in porosity, and thus affects the cell performance, although the influence was insignificant in their experiments. They further pointed out that the thickness of the GDL has a more substantial effect, i.e. a thick GDL may decrease the cell performance because the oxygen path is too long; a thin GDL may also decrease the cell performance because of the contact resistance at the GDL| catalyst interface.

In summary, there is an optimum porosity level for the GDL so that the fuel cell has the best performance. This optimization is beyond the scope of present study, which can only be implemented when the whole fuel cell system is considered and a more thorough mathematical model is analyzed.

Acknowledgements

Financial support for this research from National Science Council of Taiwan through Grant no. 90-2212-E-002-202 is gratefully acknowledged.

References

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[4] D.M. Bernardi, J. Electrochem. Soc. 137 (1990) 3344–3350. [5] M.W. Verbrugge, R.F. Hill, J. Electrochem. Soc. 137 (1990) 886–893. [6] M.W. Verbrugge, R.F. Hill, J. Electrochem. Soc. 137 (1990) 1131–

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[7] D.M. Bernardi, M.W. Verbrugge, AIChE J. 37 (1991) 1151–1163. [8] M.W. Verbrugge, D.M. Bernardi, J. Electrochem. Soc. 139 (1992)

2477–2490.

[9] T.E. Springer, T.A. Zawodzinski, S. Gottesfeld, J. Electrochem. Soc. 138 (1991) 2334–2342.

[10] T.E. Springer, M.S. Wilson, S. Gottesfeld, J. Electrochem. Soc. 140 (1993) 3513–3526.

[11] D. Singh, D.M. Lu, N. Djilali, Int. J. Eng. Sci. 37 (1999) 431–452. [12] A. Rowe, X. Li, J. Power Sources 102 (2001) 82–96.

[13] V. Gurau, H. Liu, S. Kakac, AICHE J. 44 (1998) 2410–2422. [14] J.S. Yi, T.V. Nguyen, J. Electrochem. Soc. 146 (1999) 38–45. [15] S. Um, C.Y. Wang, K.S. Chen, J. Electrochem. Soc. 147 (2000)

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[16] L.R. Jordan, A.K. Shukla, T. Behrsing, N.R. Avery, B.C. Muddle, M. Forsyth, J. Power Sources 86 (2000) 250–254.

[17] L.R. Jordan, A.K. Shukla, T. Behrsing, N.R. Avery, B.C. Muddle, M. Forsyth, J. Appl. Electrochem. 30 (2000) 641–646.

[18] L. Giorgi, E. Antolini, A. Pozio, E. Passalacqua, Electrochim. Acta 43 (1998) 3675–3680.

[19] M. Wohr, K. Bolwin, W. Schnurnberger, M. Fischer, W. Neubrand, G. Eigenberger, Int. J. Hydrogen Ener. 23 (1998) 213–218. [20] V. Gurau, F. Barbir, H. Liu, J. Electrochem. Soc. 147 (2000) 4485–

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[21] R.B. Bird, W.E. Stewart, E.N. Lightfoot, Transport Phenomena, Wi-ley, New York, 1960.

[22] ASHRAE Handbook, Fundamentals, American Society of Heating, Refrigerating and Air-Conditioning Engineers Inc., 1981.

[23] J. Kim, S.-M. Lee, S. Srinivasan, J. Electrochem. Soc. 142 (1995) 2670–2674.

[24] J.H. Lee, T.R. Lalk, A.J. Appleby, J. Power Sources 70 (1998) 258– 268.

[25] R.F. Mann, J.C. Amphlett, M.A.I. Hooper, H.M. Jensen, B.A. Pep-pley, P.R. Roberge, J. Power Sources 86 (2000) 173–180. [26] Y.W. Rho, O.A. Velev, Y.T. Kho, S. Srinivasan, J. Electrochem. Soc.

141 (1994) 2084–2088.

[27] Y.W. Rho, Y.T. Kho, S. Srinivasan, J. Electrochem. Soc. 141 (1994) 2089–2096.

數據

Fig. 2. Porosity distribution function of four models considered.
Fig. 3. Effects of porosity change on distribution of oxygen mass fraction across gas channel, GDL and catalyst layer for three different surface overpotentials.
Fig. 4. Variations of oxygen mass fraction in catalyst layer for three different surface overpotentials and four different porosity models.
Fig. 7. Polarization and power density curves corresponding to four different porosity models.

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