Hydrogen Production via Catalytic Reformation of Landfill Gas and Biogas Nazim MURADOV, Ali T-RAISSI, Franklyn SMITH, Mohamed M. ELBACCOUCH Florida Solar Energy Center, University of Central Florida Cocoa, Florida 32922, U.S.A.
Hydrogen Production via Catalytic Reformation of Landfill Gas and
Biogas
Nazim MURADOV, Ali T-RAISSI, FranklynSMITH, Mohamed M. ELBACCOUCH
Florida Solar Energy Center, University of Central FloridaCocoa, Florida 32922, U.S.A.
ObjectivesObjectives
• The primary objectives of this study are to:– Determine the catalytic activity of a number of
catalysts for reforming of CH4-CO2 mixtures
– Explore catalyst stability issues
– Evaluate the potential for producing hydrogen for NASA-Kennedy Space Center in Florida
CH4 + CO2 → 2H2 + 2CO ∆H298= 247 kJ/mol
Introduction (1)Introduction (1)
• Landfill gas (LFG) and biogas (BG) are important resources for production of renewable hydrogen
• LFG & BG are complex gaseous mixtures that contain CH4 and CO2 as the major constituents and small amounts of H2S & a variety of organic (e.g., alcohols, organic acids, esters) & element-organic (e.g., S-, N-,Si-containing) compounds
• Concentration of CH4 in LFG & BG vary in the range of 40-70 vol.% (the balance being mostly CO2)
Introduction (2)Introduction (2)
• Extensive sources of LFG and BG are available in the U.S.
• Presently, there are no large-scale commercial hydrogen production processes based on LFG & BG in Florida
• In Florida, 59 landfill sites generate 1.6 million m3/day LFG (in methane equivalent), that can yield about 100,000 tons of H2 gas per year
Landfill Locationswithin approximately 80 km from
NASA-KSC in Florida & their output (GJ/hr)
Landfill Locationswithin approximately 80 km from
NASA-KSC in Florida & their output (GJ/hr)
• Total capacity:0.22 million m3/day CH4
• This amount of methane will produce 50t /day H2gas
Daytona Beach, 76
Cocoa, 32
Vero Beach, 26
Winter Haven, 46
Kissimmee, 23
Orlando, 75
Sanford, 51
KSC
Nearest Landfill Site(Cocoa, Florida)
Nearest Landfill Site(Cocoa, Florida)
•• Located approx. 20 km from Located approx. 20 km from NASA/KSC in FloridaNASA/KSC in Florida
•• Capacity: Capacity: approx.approx. 30 m30 m33/min of /min of LFG (potentially, LFG (potentially, approx.approx. 60 60 mm33/min)/min)
•• Expected to produce LFG forExpected to produce LFG forabout 50 yearsabout 50 years
•• The site could potentially The site could potentially provide feedstock for production provide feedstock for production of of about 5 ton/day Habout 5 ton/day H2 2 gasgas
Composition of Cocoa LFG (vol.%):
Methane 48.3Carbon dioxide 37.1Nitrogen 11.3Oxygen 3.3Hydrogen <0.1Hydrogen sulfide <0.1Carbon monoxide <0.01Other hydrocarbons <0.01
Heating value: 490 BTU/CF
Chemical Equilibrium Considerations (1)
Chemical Equilibrium Considerations (1)
• Aspen Technology’s AspenPlusTM
chemical process simulation (CPS) platform was used to calculateequilibria of CO2-methane reacting gas
• Reforming reactions were modeled using a Gibbs reactor & by minimizing the free energies in order to determine conversions at given reaction conditions
• Input parameters were: feed composition & flow rate, inlet temperature & pressure, and reactor temperature & pressure
• Equilibrium compositions of CH4:CO2:H2O mixtures atP=1 atm were determined
CH4:CO2 = 1:1
0
0.1
0.2
0.3
0.4
0.5
0.6
0.7
600 700 800 900 1000 1100 1200
Temperature (K)
Mol
e Frac
tion
CH4H2OH2CO2COC
CH4:CO2 = 1.3:1
0
0.1
0.2
0.3
0.4
0.5
0.6
0.7
600 700 800 900 1000 1100 1200
Temperature (K)
Mol
e Frac
tion
CH4H2OH2CO2COC
Chemical Equilibrium Considerations (2)
Chemical Equilibrium Considerations (2)
CH4:CO2 = 1:1
0
0.1
0.2
0.3
0.4
0.5
0.6
0.7
600 700 800 900 1000 1100 1200
Temperature (K)
Mol
e Frac
tion
CH4H2OH2CO2COC
CH4:CO2 = 1.3:1
0
0.1
0.2
0.3
0.4
0.5
0.6
0.7
600 700 800 900 1000 1100 1200
Temperature (K)
Mol
e Frac
tion
CH4H2OH2CO2COC
• Equilibrium compositions of CH4:CO2:H2O mixtures at P=1 atm
Scenarios for ConvertingLFG to LH2
Scenarios for ConvertingLFG to LH2
∼20 km
LFG
Florida Gas Transmission Pipeline
CO2
LH2CH4
CH4 recovery plant H2 plant H2 liquefaction unit Cocoa landfill site
KSC
Scenario 1 (credit-debit, LH2 plant at NASA-KSC)Scenario 1 (credit-debit, LH2 plant at NASA-KSC)
H2
CH4-CO2 reforming plant
to KSC
to other end-users
LFG
Scenario 2 (trailer truck delivery of LH2 to NASA-KSC)Scenario 2 (trailer truck delivery of LH2 to NASA-KSC)
LH2
H2 liquefaction unit
Process Design Considerations (1)
Process Design Considerations (1)
• Option 1 - LFG reforming with preliminary recovery of CH4
Landfill Gas (CH4 – CO2)
CO2(liquid)
GSU
H2-CO
H2-CO2
H2
CO2(liquid)
H2OH2O
Steam Reformer
Shift Reactor Cryogenicseparation
Liquid CO2 sequestration
CH4
Process Design Considerations (2)
Process Design Considerations (2)
• Option 2 - Direct reformation of LFG
CO2
Landfill Gas
Reformer Shift Reactor PSA,or cryogenicseparation
H2
Sulfur and siloxane trap
H2-CO
H2-CO2
H2OH2O
CO2 sequestration
CH4 – CO2
Experimental (1)Experimental (1)
• A premixed gaseous mixture with the composition of CH4- 56.9, & CO2- 43.1 vol.% was obtained from Holox Inc. and used to mimic LFG composition in all experiments
• Ni- and Fe-based catalysts were obtained from Sud-Chemie and Alfa Aesar
Experimental (2)Experimental (2)
• Alumina-supported (0.5 and 1 wt.%) Pt, Pd &Ru catalysts were from Aldrich Chemical Co.
• Rh (5 wt.%)/Al2O3 was from Strem Chemicals
• Ir (1 wt.%)/Al2O3 was from Alfa Aesar
• A catalyst (0.5 g) was placed inside a quartz reactor (1 cm O.D.) and purged with Ar at 600oC for 1 hr before each experiment
Experimental (3)Experimental (3)
• All the experiments were conducted at the atmospheric pressure
• The flow rate of CH4-CO2 mixture into the reactor was 10 ml/min
• The reaction products were analyzed gas chromatographically
Laboratory Scale Unit for Catalytic Reforming of CH4-CO2 Mixtures
Laboratory Scale Unit for Catalytic Reforming of CH4-CO2 Mixtures
steamgenerator
reactor
catalystAr CH4-CO2
GC
syringe pump
flowmeters
T-controller
heater
pre-heater
Water collector
adsorber dryerthermocouple
vent to shift reactor
Catalytic Reformation of CH4-CO2Catalytic Reformation of CH4-CO2
0
10
20
30
40
50
60
0 100 200 300
Time (min.)
Pro
duct
s (v
ol.%
)
CO2
CH4
H2
CO
0
10
20
30
40
50
60
0 100 200 300
Time (min.)Pr
oduc
ts (v
ol.%
)
CO2CH4H2CO
• Catalytic reforming of CH4-CO2 (56.9-43.1 vol.%) mixture over Ru (0.5 wt.%)/Al2O3 (left) & NiO(15 wt.%)/Al2O3 catalysts at 850oC
Effect of SteamEffect of Steam
0
5
10
15
20
25
0 0.2 0.4 0.6 0.8 1
Steam / methane ratio (mol.)
Car
bon
(mm
ol/g
cat
.)
• To prevent carbon lay down on the NiO/Al2O3catalyst surface, steam was added. The extent of carbon lay down on the Ni-catalyst as a function of steam to methane ratio in the feed is shown in this Figure.
Comparison of CPS &Experimental ResultsComparison of CPS &Experimental Results
AspenTM Simulation Results
CH4:H2O:CO2 = 1.3:1.3:1
0
0.1
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0.5
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0.7
600 700 800 900 1000 1100 1200
Temperature (K)M
ole
Frac
tion
CH4H2OH2CO2COC
0
10
20
30
40
50
60
70
0 60 120 180 240 300
Time (min.)
Pro
duct
s (v
ol.%
)
H2COCO2CH4
Experimental, T=850oCCH4:H2O:CO2=1.3:1.3:1NiO (15 wt.%)/Al2O3
SummarySummary
• Hydrogen production from renewable feedstocks, such as landfill gas and biogas was analytically and experimentally investigated. A wide range of catalysts were tested for reforming CH4-CO2 and CH4-CO2–H2O mixtures at 850oC & 1 atm pressure
• Experiments used a ratio of CH4/CO2 in the feedstock similar to that of the LFG from Cocoa landfill site in Florida
• Noble metal catalysts (i.e., alumina-supported Pt, Pd, Rh& Ir) show both high activity and high selectivity toward CO2 reformation of methane
Conclusions (2)Conclusions (2)• Ni catalysts were very efficient for both reforming &
methane decomposition reactions. But, CH4decomposition reaction resulted in the catalyst deactivation
• The addition of relatively small amounts of steam (steam-to-methane molar ratio of 0.5÷1) preventedNi catalyst deactivation and significantly improved its activity and stability
• The experimental data for Ni-catalyzed reforming are in good agreement with the thermodynamic equilibrium calculations for the CO2-CO4 mixtures with & without steam supplementation
AcknowledgementsAcknowledgements
Support for this work was provided by the National Aeronautics and Space
Administration (NASA) through Glenn Research Center.