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PROGRESS IN HIGH-TEMPERATURE ELECTROLYSIS FOR HYDROGEN
PRODUCTION
Third Information Exchange Meetingon the Nuclear Production of Hydrogen
Oarai, JapanOctober 6, 2005
J. Stephen HerringJames E. O’Brien, Carl M. Stoots, Grant L. Hawkes, Paul Lessing, William Windes, Daniel Wendt, Michael McKellar, Manohar Sohal (INL) and Joseph Hartvigsen (Ceramatec)
Herring NEA 3rd IEM 6Oct05 2
High temperature electrolysis using nuclear electricity and heat
• Advantages– Builds on existing Solid Oxide Fuel Cell
technology– Lower operating temperatures than
thermochemical cycles– Less corrosive operating conditions
• Disadvantages– May have lower efficiencies than
thermochemical cycles– Cells are relatively small (100 mm x 100 mm)
Herring NEA 3rd IEM 6Oct05 3
Theoretical Efficiency of High Temperature Electrolysis
35%
40%
45%
50%
55%
500 600 700 800 900Reactor Outlet Temperature (C)
Effic
ienc
y
Electrical generation eff.Hydrogen production eff.
P=1 atm
0
2
4
6
8
10
12
14
16
0
0.5
1
1.5
2
2.5
3
3.5
0 200 400 600 800 1000
Ener
gy D
eman
d pe
r uni
t mas
s of s
team
kWh/m3H2
T (C)
liquid steam
ΔHR, Total Energy Demand
ΔGR, Electrical Energy Demand
TΔSR, Heat Demand
MJ/kg H2O
Energy Input to Electrolyser
Herring NEA 3rd IEM 6Oct05 4
High Temperature Electrolysis Plant
Herring NEA 3rd IEM 6Oct05 5
Porous Anode, Strontium-doped Lanthanum Manganite
Gastight Electrolyte, Yttria-Stabilized Zirconia
Porous Cathode, Nickel-Zirconia cermet
2 H20 + 4 e- → 2 H2 + 2 O=
2 O= → O2 + 4 e-
2 O=
↓
H2O↓ ↑
H2
O2↓
4 e-→
0.10 mm 0.01 mm
0.05 mm 1.500 mm
0.05 mm 0.05 mm
90 v/o H2O + 10 v/o H2 10 v/o H2O + 90 v/o H2
Typical thicknessesElectrolyte- Cathode-supported supported
Interconnection
H2O + H2 →
← Ο2
1 – 2.5 mm
Next Nickel-Zirconia Cermet CathodeH2O↓
↑H2
Herring NEA 3rd IEM 6Oct05 6
Schematic of Stack Testing Apparatus
N2
H2 + Ar + H2O
Air + O2
H2
Air
H2O + Ar + H2
P
TTdp
Tdp
TA
V+-
Humidifier
Furnace
3-way valve
Humidifier bypass
Stack
T
T
T
T
CoolingWater
Condenser
H2 Exhaust
PowerSupply
Herring NEA 3rd IEM 6Oct05 7
Stack Internal Components
Herring NEA 3rd IEM 6Oct05 8
Metal Interconnect Details
Separator Plate, Ferritic SS, alloy 441, ~ 460 μm thickness
Air Side• Rare Earth Element Surface Treatment• Formation of low-growth-rate conductive oxide scale• Perovskite Coating (screen printing or plasma sprayed)
yields low and stable electronic resistance in air• Ferritic SS Flow Field (also surface treated)
Steam/hydrogen side• Ni metal coating on separator plate (spall
resistant)• Nickel flow field
Edge Rails• Ferritic SS, 1.02 mm
thickness• Brazed in place
Herring NEA 3rd IEM 6Oct05 9
22-cell stack used in July-August 2005 test
Herring NEA 3rd IEM 6Oct05 10
Hydrogen Production at 800° C
0
500
1000
1500
2000
0 0.05 0.1 0.15 0.2
based on stack currentbased on dewpoint measurements
H2 P
rodu
ctio
n R
ate,
sccm
current density, A/cm2
H2 Production R
ate, NL/hr
90
30
60
120
sccm N2 = 4027sccm H2 = 412T
f = 800 C
The stack continued producing102 normal liters per hour for 197 hours
Herring NEA 3rd IEM 6Oct05 11
22-cell stack performance, July-August 2005
0
5
10
15
20
25
30
35
0
20
40
60
80
100
120
140
0 50 100 150 200
Stac
k V
olta
ge o
r Cur
rent
Hydrogen Production R
ate, NL/hr
elapsed time, hr
H2 Production Rate
Stack Current
Stack Voltage
Herring NEA 3rd IEM 6Oct05 12
Overall hydrogen production efficiencies as a function of power-production thermal efficiency and electrolyzer per-cell operating voltage
0.25
0.3
0.35
0.4
0.45
0.5
0.55
0.6
0.65
0.7 0.8 0.9 1 1.1 1.2 1.3 1.4 1.5
ηT
Vop
0.30
0.35
0.40
0.45
ηP = 0.50
Eo
Te = 800 C
Vtn
Herring NEA 3rd IEM 6Oct05 13
operating voltage, V
current density, A/cm2he
atflu
x,W
/cm
2
-1.4-1.2-1-0.8-0.6-0.4
-0.3-0.2-0.100.10.20.30.4
-0.2
0
0.2
0.4
reactionohmicnet
thermal neutralvoltage
open-cellpotential
electrolysisfuel cell
Energy Budgets in fuel-cell and electrolysis modes
Stack ASR = 1.25, T = 927 C, yH2,i = 0.1, yH2,o = 0.95
FhV R
tn 2Δ−=
(1.291 V at 1200 K)
Herring NEA 3rd IEM 6Oct05 14
Stack and furnace temperatures during sweep
780
785
790
795
800
805
810
815
820
18 20 22 24 26 28 30 32 34
TfurnaceTair inletTinternal1Tinternal2Tinternal3Tinternal4Tinternal5
T (C)
Stack Voltage
Herring NEA 3rd IEM 6Oct05 15
FLUENT Single-Cell SOEC Model
Herring NEA 3rd IEM 6Oct05 16
Top view, showing 42 x 42 element grid
Details of 3D numerical mesh
Closeup of corner, showing vertical element stacking
Herring NEA 3rd IEM 6Oct05 17
FLUENT Single-Cell SOEC Model DetailsSeparator plates (Ferritic SS)• half thickness (symmetry boundary); k = 27 W/m K, σ = 8.50 x 105 Ω-1m-1
Flow Fields
• High-porosity anisotropic porous media; ε = 0.87, K1 = 2 x 10-4 m2; K2 = 2 x 10-5 m2
• Nickel metal properties (steam/hydrogen side): k = 72.0 W/m K, σ = 2.20 x 106 Ω-1m-1
• Ferritic SS properties
Steam/hydrogen electrode (Ni-YSZ cermet)
• isotropic porous media, 25 µm thickness, K = 10-13 m2, ε = 0.37, tortuosity Lt = 3.0, k= 13.1 W/m K, σ = 1.129 x 105 Ω-1m-1
YSZ electrolyte
• 2-D planar element in the FLUENT SOEC module• Ionic conductivity: ρ(T) = 3.685 x 10-4 + 2.838 x 10-5exp(10300/T(K))
Air electrode (LSM)
• isotropic porous media, 25 µm thickness, K = 10-13 m2, ε = 0.37, tortuosity Lt = 3.0, thermal conductivity k = 9.6 W/m K, and electrical conductivity σ = 7.045 x 103 Ω-1m-1
Herring NEA 3rd IEM 6Oct05 18
0.8
0.9
1
1.1
1.2
1.3
0.00 0.05 0.10 0.15 0.20 0.25
FLUENTExperimental
Per-
Cel
l Ope
ratin
g V
olta
ge (V
)
Current Density (A/cm2)
Voltage-current characteristics of actual electrolysis stack and FLUENT model
Electrode exchange current densities and several gap electrical contact resistances were determined empirically by comparing
FLUENT predictions with stack performance data
Herring NEA 3rd IEM 6Oct05 19
CFD Contour Plots
H2/H2O
Air
Herring NEA 3rd IEM 6Oct05 20
near thermal minimum near thermal neutral above thermal neutral
Electrolyte/insulator temperature contours0.156 A/cm2; 1.164 V 0.2344 A/cm2; 1.306 V 0.4688 A/cm2; 1.640 V
1091
1100
1104.5
1105.5 1197
1139
Electrolyte current density contours
-1404
-1878
-2097
-2734
-3892
-5158
Herring NEA 3rd IEM 6Oct05 21
near thermal minimum near thermal neutral above thermal neutral
Nernst Potential contours
0.156 A/cm2; 1.164 V 0.2344 A/cm2; 1.306 V 0.4688 A/cm2; 1.640 V0.910
0.847
0.932
Hydrogen mole fraction contours0.212
0.0757
0.278
0.0757
0.478
0.0759
0.8380.847
0.986
⎥⎥
⎦
⎤
⎢⎢
⎣
⎡⎟⎟⎠
⎞⎜⎜⎝
⎛⎟⎟⎠
⎞⎜⎜⎝
⎛−=
− 2/1
2/122
2lnstdOH
OHo P
Pyy
yjFRTEE
Herring NEA 3rd IEM 6Oct05 22
Internal Stack Components
Corroded post-test edge rail
Technical Issue: corrosion of metallic interconnect during test contributed to performance degradation and stack failure.
Herring NEA 3rd IEM 6Oct05 23
Inevitable Comparison:Liquid hydrocarbons are very good fuels for transportation
• Liquid over range of ambient temperatures• Pumpable: gas pump: 20 liters/min = 11 MWth
• Energy dense: 34 MJth/liter at 0.1 MPa– H2 gas: 9.9 MJth/liter at 80 MPa,– H2 120 MJth/kg, gasoline: 40 MJth/kg
• Storable: little loss, small explosion hazard• Transportable by pipeline: 0.91 m oil pipeline: 70 GWth
Hydrogen will be used primarily to enhance gasoline, diesel and jet fuel production until the on-board storageproblem can be solved.
Herring NEA 3rd IEM 6Oct05 24
Conclusions• Experimental results from a 22-cell stack, 64 cm2,
fabricated by Ceramatec, – Hydrogen production rates in excess of 100 NL/hr were maintained with a
22-cell solid-oxide electrolysis stack for over 196 hours over the time period from July 26 to August 3, 2005.
– The stack endurance test was terminated due to instrumentation failure (an uninterruptible power supply failed), not due to any problem with the stack itself.
– Stack performance as measured by the per-cell ASR was good, although a lower value of ASR would be desirable.
• Carbon-based liquid fuels will be dominant for decades.• Hydrogen from nuclear energy will first be used to
upgrade and synthesize feedstocks.