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Fuel Cells Lecture 2.pdf - Curtin University

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Effects of Pressure<br />

• The change in Gibbs Free Energy with pressure of the fuel<br />

cell reaction H 2 + (½)O 2 H 2 O is given by<br />

⎡ a ⋅ a ⎤<br />

1/2<br />

H O<br />

0<br />

2 2<br />

Δ g f = Δg f − RT ln ⎢ ⎥<br />

⎢⎣ aH2O<br />

⎥⎦<br />

Where R is the universal gas constant 8.314 JK-1mol-1 , T<br />

is the absolute temperature in K, is the change in<br />

Gibbs free energy at standard pressure and at<br />

temperature T, ‘a’ is the activity of the gas given by P/P0 where P is the pressure or partial pressure of the gas, P0 0<br />

Δg<br />

f<br />

is the standard pressure, 0.1 Mpa= 1 bar.<br />

S. Rajakaruna 2007 Renewable Energy Systems 402 1


Effects of Pressure<br />

• If the pressure of hydrogen and oxygen increase, Δg<br />

becomes more negative and hence releases more<br />

energy become available for conversion to electricity.<br />

• If the pressure of steam increases, less energy will be<br />

available for the conversion to electricity.<br />

• Note here that the effect of change of temperature is<br />

0<br />

represented by the change in the value of Δg<br />

with f<br />

changing temperature. The second term only represents<br />

the effect of pressure change.<br />

• The effect of temperature on maximum EMF can be<br />

−Δg<br />

f<br />

seen by substituting the above equation in<br />

E =<br />

S. Rajakaruna 2007 Renewable Energy Systems 402 2<br />

2F<br />

f


Change in EMF with Pressure -The<br />

Nernst Equation<br />

0<br />

1/2 1/2<br />

−Δg<br />

f RT ⎛ aH ⋅ a ⎞ O 0 RT ⎛ aH ⋅ a ⎞ O<br />

E = + ln = E + ln<br />

2F 2F a 2F<br />

a<br />

E<br />

0<br />

2 2 2 2<br />

⎜ ⎟ ⎜ ⎟<br />

⎜ ⎟ ⎜ ⎟<br />

⎝ H2O ⎠ ⎝ H2O ⎠<br />

Where is the maximum EMF at standard pressure<br />

0<br />

and temperature T (K). Note E<br />

drops with the<br />

increasing temperature as seen in Table 2.2. This is<br />

called ‘The Nernst Equation’ and some of its other forms<br />

are as given below.<br />

S. Rajakaruna 2007 Renewable Energy Systems 402 3


Nernst Equation<br />

E E<br />

0<br />

= +<br />

RT<br />

2F<br />

1<br />

⎛ ⎞<br />

2<br />

⎜ PH ⎛ P<br />

2 O ⎞ 2 ⋅⎜<br />

⎟<br />

⎜ 0 0 ⎟<br />

P P ⎟<br />

ln ⎜<br />

⎝ ⎠<br />

⎟<br />

P<br />

⎜ H2O ⎟<br />

⎜ 0 ⎟<br />

⎜ P ⎟<br />

⎝ ⎠<br />

If all the pressures are expressed in ‘bar’, then, P 0 =1. Hence above equation<br />

can be expressed as:<br />

E E<br />

RT<br />

⎛ ⎞<br />

⎜ PH ⋅ PO<br />

1<br />

2<br />

⎟<br />

( )<br />

0<br />

2 2<br />

= + ln ⎜ ⎟<br />

2F<br />

⎜<br />

PH<br />

2O<br />

⎟<br />

⎝ ⎠<br />

S. Rajakaruna 2007 Renewable Energy Systems 402 4


Nernst Equation<br />

• In nearly all the cases, pressures of gases in above<br />

equation are partial pressures as there are many gases<br />

in the mix both at anode and cathode.<br />

• Furthermore, the overall pressure in the mix of gases at<br />

the cathode and anode is the same. Because this<br />

simplifies the design of the cell. If this system operating<br />

pressure is ‘P’, then the partial pressures can be<br />

expressed as a ratio of P.<br />

P = α ⋅ P P = β ⋅ P P = δ ⋅ P<br />

H O H O<br />

2 2 2<br />

α, β and δ<br />

Where are constants depending on the<br />

concentration of gases in the mix.<br />

S. Rajakaruna 2007 Renewable Energy Systems 402 5


Nernst Equation<br />

1 1 1<br />

⎛ ⎞ ⎛ ⎞<br />

2 2 2<br />

0 RT α ⋅ β ⋅ P 0 RT α ⋅ β RT<br />

E = E + ln<br />

⎜ ⎟<br />

= E + ln<br />

⎜ ⎟<br />

+ ln P<br />

2F ⎜ δ ⎟ 2F ⎜ δ ⎟<br />

⎜ ⎟ ⎜ ⎟ 4F<br />

⎝ ⎠ ⎝ ⎠<br />

This form of Nernst equation gives the effect of system<br />

pressure P on the EMF as a separate term. It also shows<br />

how partial pressures influence the EMF.<br />

( )<br />

Example: On the cathode, oxygen is usually supplied as<br />

air. The partial pressures of air at 0.1MPa are: N 2 =0.0781<br />

MPa, O 2 =0.02095 MPa, Argon = 0.00093 MPa etc. Thus,<br />

β=0.2095 and P=0.1MPa= 1 bar<br />

The partial pressure of H 2 depends on how fuel processor<br />

produces hydrogen.<br />

S. Rajakaruna 2007 Renewable Energy Systems 402 6


<strong>Fuel</strong> and Oxygen Utilization<br />

• As hydrogen passes through the anode, it is used in the<br />

reaction. So the partial pressure of hydrogen will<br />

progressively decrease as it flows from one end to the<br />

other end of the anode.<br />

• The same is true for oxygen. As oxygen flows from one<br />

end to the other on the cathode, its partial pressure will<br />

also gradually decrease.<br />

• Since α and β both decrease, the EMF generated<br />

continues to drop as the gases flow from the entry (inlet)<br />

to the exit (outlet). It will be worst near the outlet.<br />

S. Rajakaruna 2007 Renewable Energy Systems 402 7


<strong>Fuel</strong> and Oxygen Utilization<br />

• Since the bipolar plates on the electrode are good<br />

conductors, there cannot be different voltages in the<br />

same cell. Therefore, it is the current density that drops<br />

as the gases flow towards outlet.<br />

⎛ ⎞<br />

1<br />

2<br />

0 RT α ⋅ β<br />

E = E + ln<br />

⎜ ⎟ RT<br />

+ ln P<br />

( )<br />

2F ⎜ δ ⎟<br />

⎜ ⎟ 4F<br />

⎝ ⎠<br />

• Due to the RT term, it is also clear that the effects of<br />

decreasing partial pressures is more at high<br />

temperature fuel cells such as ‘Solid Oxide <strong>Fuel</strong> Cell’.<br />

S. Rajakaruna 2007 Renewable Energy Systems 402 8


<strong>Fuel</strong> Utilization<br />

• For high fuel efficiency, it is required that all the fuel<br />

supplied to the cell used in the reaction. But at the same<br />

time it can be seen from the above discussion that the<br />

pressure of H 2 at outlet should not be reduced to very<br />

low levels. As a result, fuel and oxygen utilization need<br />

careful optimising, especially in high temperature fuel<br />

cells.<br />

• <strong>Fuel</strong> Utilization Ratio (u) is defined as,<br />

N N − N<br />

u = =<br />

N N<br />

used in out<br />

H H H<br />

2 2 2<br />

in in<br />

H H<br />

2 2<br />

S. Rajakaruna 2007 Renewable Energy Systems 402 9


<strong>Fuel</strong> Utilization Ratio<br />

where N is the flow rate in moles/s. For a solidoxide<br />

fuel cell the desired range of u is from 0.7<br />

to 0.9.<br />

• Overused-fuel condition: i.e. u> 0.9, will lead<br />

to fuel starvation near the outlet and cause<br />

permanent damage to cells.<br />

• Underused-fuel condition: i.e. u


Terminal Voltage of Practical <strong>Cells</strong><br />

−Δg<br />

• The maximum EMF given by the equation E =<br />

2F<br />

is an ideal value assuming there are no losses.<br />

The practical terminal voltage of a fuel cell is<br />

considerably less than the above value due to<br />

various types of losses.<br />

• At temperatures below 100°C, the maximum EMF<br />

E is about 1.2 V. Figure 3.1 shows the variation of<br />

terminal voltage with current density of a practical<br />

fuel cell operating at 40°C and standard pressure.<br />

S. Rajakaruna 2007 Renewable Energy Systems 402 11<br />

f


Terminal voltage of a low-<br />

temperature fuel cell<br />

S. Rajakaruna 2007 Renewable Energy Systems 402 12


Terminal voltage of a low-<br />

temperature fuel cell<br />

Note the following in the figure.<br />

• Even the open circuit voltage is less than the<br />

theoretical value.<br />

• There is a rapid initial fall in voltage with<br />

increasing current density.<br />

• Then there is a range of current density where<br />

drop of voltage is almost linear. In this linear<br />

region, the slope is less than in the initial region.<br />

• When current density approaches some high<br />

values, the voltage starts to fall rapidly.<br />

S. Rajakaruna 2007 Renewable Energy Systems 402 13


Terminal voltage of a high-<br />

temperature fuel cell<br />

• As discussed earlier, the maximum EMF (E) falls with<br />

the increasing temperature. At about 800°C, E is ab out<br />

1.0 V. Figure 3.2 shows how the terminal voltage of a<br />

practical cell at 800°C varies with the current den sity.<br />

Note the following in the figure.<br />

• Open circuit voltage is almost equal to the theoretical<br />

value.<br />

• There is no rapid drop in voltage at low current densities.<br />

The graph is much more linear.<br />

• At about the same high values of current densities, the<br />

voltage starts to fall rapidly.<br />

S. Rajakaruna 2007 Renewable Energy Systems 402 14


Terminal voltage of a high-<br />

temperature fuel cell<br />

S. Rajakaruna 2007 Renewable Energy Systems 402 15


<strong>Fuel</strong> Cell Irreversibilities – Causes<br />

of Voltage Drop<br />

• There are four main types of irreversibilities that cause<br />

the terminal voltage to drop below the Maximum EMF<br />

(E). E is also called the ‘ideal emf’, ‘no-loss emf’ or the<br />

‘reversible emf’.<br />

1. Activation Loss<br />

2. <strong>Fuel</strong> Crossover and Internal Currents<br />

3. Ohmic Losses<br />

4. Mass Transport or Concentration Loss<br />

S. Rajakaruna 2007 Renewable Energy Systems 402 16


Activation Loss<br />

• Activation Loss is the main reason for rapid drop in<br />

terminal voltage of low-temperature fuel cells at low<br />

current densities. It is caused by the slowness of the<br />

reactions taking place on the surface of the electrode. A<br />

portion of the available energy is lost in driving the<br />

chemical reaction or to supply the ‘activation energy’.<br />

• The activation loss of voltage is described by “Tafel<br />

Equation’ as:<br />

⎛ i ⎞<br />

Δ Va = Aln<br />

⎜ ⎟<br />

i<br />

⎝ 0 ⎠<br />

where A is a constant which is higher for slower<br />

reactions and i 0 is a constant higher for faster reactions.<br />

S. Rajakaruna 2007 Renewable Energy Systems 402 17


Activation Loss<br />

• For the slow<br />

reaction A is higher,<br />

i 0 is smaller.<br />

• For the fast<br />

reaction A is smaller<br />

and i 0 is higher.<br />

• Due to the<br />

logarithmic function<br />

it is i 0 which affects<br />

the voltage drop<br />

more.<br />

S. Rajakaruna 2007 Renewable Energy Systems 402 18


Activation Loss<br />

• The above equation describes the voltage drop only for i<br />

> i 0 . For i < i 0 , the voltage drop is zero. Therefore, higher<br />

the value of i 0 , the lower is the voltage drop.<br />

• The constant i 0 is called the ‘exchange current density’.<br />

This is the current corresponding to the electrode<br />

reaction in equilibrium under open-circuit condition.<br />

Under zero current supplied to the external circuit, the<br />

electrode reaction is still happening, but in both<br />

directions.<br />

At the cathode:<br />

At the anode: 2<br />

O + 4e + 4H ↔ 2H<br />

O<br />

− +<br />

2 2<br />

2H ↔ 4H +<br />

4e<br />

+ −<br />

S. Rajakaruna 2007 Renewable Energy Systems 402 19


Activation Loss<br />

• When the external circuit is switched on, the exchange<br />

current density is readily available so drawing a current<br />

up to i 0 will cause no voltage drop.<br />

• The anode and cathode have two different i 0 values as<br />

i 0a and i 0c respectively.<br />

• For a hydrogen fuel cell, i 0c


Effect of i 0<br />

S. Rajakaruna 2007 Renewable Energy Systems 402 21


Methods to increase i 0<br />

1. Increasing the cell temperature: Increase of<br />

temperature increases the reaction under open-circuit<br />

condition. Therefore i 0 is higher and the voltage drop is<br />

less. By considering low and high values for i 0, the<br />

shapes of V-I characteristics of Figure 3.1 and 3.2 at<br />

low current levels can be described. For a low<br />

temperature cell i 0 is about 0.1 mA and that for a<br />

800°C cell is about 10 mA, which is 100 times large r.<br />

2. Using more effective catalysts.<br />

3. Increasing the contact area of the electrode.<br />

4. Increasing reactant concentration. Ex. Use pure<br />

oxygen instead of air.<br />

5. Increasing the pressure of reactants.<br />

S. Rajakaruna 2007 Renewable Energy Systems 402 22


<strong>Fuel</strong> Crossover and Internal<br />

Currents<br />

• Although the electrolyte is not supposed to allow the<br />

passing of the fuel (H 2 ) and electrons between the two<br />

electrodes, a very small “leakage” does happen in all fuel<br />

cells. Both hydrogen and electron crossovers have the<br />

same effect that they reduce the charges available to the<br />

external circuit.<br />

• Although, this leakage current is not large enough to<br />

affect the energy efficiency, it does cause a very<br />

considerable drop in open-circuit voltage.<br />

• Because of the leakage, the current produced under<br />

open-circuit condition is not zero.<br />

• If i n is the internal current density, it can be considered<br />

in the Tafel equation as:<br />

S. Rajakaruna 2007 Renewable Energy Systems 402 23


<strong>Fuel</strong> Crossover and Internal<br />

Currents<br />

⎛ i + i ⎞ n<br />

V = E − Aln<br />

⎜ ⎟<br />

i<br />

⎝ 0 ⎠<br />

• Thus, the open-circuit terminal voltage is given by,<br />

ln n ⎛ i ⎞<br />

VOC = E − A ⎜ ⎟<br />

i<br />

⎝ 0 ⎠<br />

Using typical values for a low-temperature cell, E=<br />

1.2v, A=0.06 V, i 0 =0.04mA.cm -2 and i n =3 mA.cm-2, V-I<br />

characteristics can be drawn as below.<br />

S. Rajakaruna 2007 Renewable Energy Systems 402 24


Activation and Internal Current<br />

Losses<br />

Compare this with Figure 3.1 and see how closely it matches the V-I<br />

characteristic of a practical cell at low current densities.<br />

S. Rajakaruna 2007 Renewable Energy Systems 402 25


Ohmic Losses<br />

• Ohmic losses are due to the resistance to the flow of (a)<br />

electrons through the electrodes, bipolar plates and<br />

other stack connections and (b) ions through the<br />

electrolyte.<br />

• In most fuel cells, ohmic loss is mainly due to the<br />

electrolyte.<br />

• The voltage drop is directly proportional to the current<br />

density.<br />

Δ V = i ⋅r<br />

o<br />

Where i is the current density and r is the resistance<br />

per unit area.<br />

S. Rajakaruna 2007 Renewable Energy Systems 402 26


Ohmic Losses<br />

• Ohmic losses are important in all types of fuel<br />

cells. To reduce the ohmic losses, following<br />

can be done.<br />

1. Use of electrodes with highest possible<br />

conductivity.<br />

2. Good design and use of suitable material for<br />

bipolar plates.<br />

3. Making the electrolyte as thin as practically<br />

possible while making sure no direct contact<br />

between electrodes is possible and enough<br />

physical strength is available in the stack.<br />

S. Rajakaruna 2007 Renewable Energy Systems 402 27


Mass Transport or Concentration<br />

Loss<br />

• As current is drawn to the external circuit, gases are<br />

consumed, thus causing a reduction in pressure of both<br />

hydrogen and oxygen at the electrodes if the gas supply<br />

rates are constant. This reduction in pressure at<br />

electrodes due to consumption is the reason for the<br />

concentration loss.<br />

i<br />

• If is the limiting current corresponding to zero<br />

l<br />

pressure at the electrodes, the concentration loss can be<br />

expressed using the Nernst equation as,<br />

⎛ i ⎞<br />

Δ V = −B ln ⎜1− ⎟ for i ≤ i<br />

⎝ il<br />

⎠<br />

c l<br />

S. Rajakaruna 2007 Renewable Energy Systems 402 28


Concentration Loss<br />

⎛ i ⎞<br />

V = E + B ln ⎜1− ⎟<br />

⎝ il<br />

⎠<br />

E = 1.2 V , i =<br />

1000mA<br />

S. Rajakaruna 2007 Renewable Energy Systems 402 29<br />

l


Combined Effect of All Losses<br />

• The effects on terminal voltage by all the<br />

irreversibilities that were discussed can be<br />

represented by the following equation.<br />

⎛ i + i ⎞ ⎛ n i + i ⎞ n<br />

V = E − ( i + in ) r − Aln ⎜ ⎟ + B ln ⎜1− ⎟<br />

i i<br />

⎝ 0 ⎠ ⎝ l ⎠<br />

• Where E is the maximum EMF (reversible opencircuit<br />

voltage), V is the terminal voltage, i is the<br />

current density in the external circuit.<br />

S. Rajakaruna 2007 Renewable Energy Systems 402 30


Typical Values of Parameters<br />

S. Rajakaruna 2007 Renewable Energy Systems 402 31

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