Reforming and burning of ammonia in micro hydrogen and power generation systems

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8 th Annual Ammonia Fuel Conference Portland, OR, USA, 18-21 September 2011 Reforming and burning of ammonia in micro hydrogen and power generation systems O.C. Kwon *, J.M. Joo, S.I. Lee and D.H. Um School of Mechanical Engineering Sungkyunkwan University Suwon, Gyeonggi-do, Korea Acknowledgment: Supported by the National Research Foundation of Korea (NRF) grant funded by the Korea government (MEST): No. 2010-0005237.

Sungkyunkwan University & ME Sungkyunkwan Univesity: The oldest university in Korea, founded in 1398. One of the leading universities, among the top 4 in Korea. Private university strongly supported by Samsung. 2 School of Mechanical Engineering: Established in 1967. Natural sciences campus. Faculties: 33. Undergraduate students: 727. Graduate students: 135.

Global warming

CO 2 emissions in Korea Korea Metrological Administration report (2011): the average amount of CO 2 at the national air monitoring station in Anmyeondo, Chungcheong Province, in 2010 was 394.5 ppm: Korea's CO 2 level has been on the rise for eleven straight years since 1999 when the amount was 370.2 ppm. The U.S. Center for Global Development (2007): Korea ranked 10th among the world's greenhouse gas emitters by emitting 185 million tons of such gases annually. The average temperature in Korea has risen by 1.5 degrees over the last 100 years. The Kyoto Protocol in 1997: Under the second phase of the Protocol, Korea may be required to reduce greenhouse gas emissions between 2013 and 2017. In order to reduce 5% of greenhouse gas emissions in 1995, the estimated cost is 8 billion US dollars.

Hydrogen (H 2 ) Clean (Carbon-free) Energetic (120 MJ/kg) Abundant (Renewable) Wide flammability limits Low ignition energy High burning velocity

Hydrogen (H 2 ) Mass production Difficulties of transport/storage Pipelines: infrastructure needed On-site production No transport problem if hydrocarbons used But CO 2 /CO emitted

Ammonia (NH 3 ) Combustion No CO 2 /CO emissions Liquefied @ 370 psi, similar to LPG Storage Reforming NH 3 Low T catalytic or no catalytic reforming 17.8 Hwt% H 2 carrier Costs Reasonable production costs

Ammonia (NH 3 ) Zamfirescu C, Dincer I, Using ammonia as a sustainable fuel, J Power Sources 185 (2008), 459-465.

Ammonia in Korea No earlier works for use of ammonia as a fuel Ammonia has been used for various fields during the last 50 years in Korea: Fertilizers, refrigerants, catalysts and process chemicals. Safety issues associated with handling of ammonia resolved. Related regulations: industrial safety and health regulations and high pressure gas safety regulations. Ammonia is cheaper than other fuels; however, 100% imported due to low demand in Korea.

Use of ammonia as a fuel Catalytic or thermal dissociation Heat recirculation Use of outwardly propagating spherical flames at constant pressure, burner-stabilized flames and counterflow flames for measurements of fundamental parameters CO 2 /CO free H 2 -added NH 3 combustion H 2 NH 3 combustion

Ammonia as a fuel (2008-2011) Development of combustion technology of NH 3 as a heat source 1 Combustion characteristics of NH 3 Combustion characteristics of H 2 -added NH 3 Reaction mechanisms of NH 3 Design of a small combustor for reforming NH 3 Concept generation of a heatrecirculating small combustor Development of reforming technology of NH 3 using catalytic dissociation Concept generation of combustor-reformer integration Characteristics of NH 3 reforming 2 Development of H 2 generation technology using NH 3 combustion and reforming 3 Design of a combustor-reformer integrated H 2 generation system Performance evaluation of H 2 generation system

Technological challenges to overcome Micro-combustor: Burning temperature high enough for combustion stability and performance but suppressing NO x formation Heat losses quenching flames Ignition (delay) Heat recirculation concept and H 2 addition applied Micro-reformer: Uniform and steady heating: residence time and array Erosive to some materials such as metals Combustor-reformer integrated system: Effective heat transfer between a combustor and a reformer Simple structure with heat recirculation

Burning ammonia - summary

Fundamental characteristics: spherical flames Power TR Switch Iginition Coil Power Supply Spark Plug 220V AC Ground

Fundamental characteristics: spherical flames

Fundamental characteristics: spherical flames Hydrogen substitution improves the burning performance with relatively low NO x and N 2 O emissions in fuelrich ammonia/air flames.

Fundamental characteristics: burnerstabilized flames The lower stability limits due to heat losses, while the upper stability limits due to insufficient residence times of injected mixture jet. Reduction of the stability limits with NH 3 substitution in H 2 /air flames. Opposite tendencies of the upper stability limits with and without the coflow.

Fundamental characteristics: burnerstabilized flames Ammonia substitution enhances the NO x formation in general; however, the NO x emission index is almost constant with the enhanced ammonia substitution. At fuel-rich conditions, the NO x emission index is reduced with increasing burner exit velocities of the injected mixtures.

Fundamental characteristics: counterflow nonpremixed flames

Fundamental characteristics: counterflow nonpremixed flames Ammonia is all capable to significantly reduce the high-stretch extinction limits, the maximum flame temperature and the concentration of light radicals with ammonia substitution in hydrogen/air flames. The remarkable reduction of temperature with NH 3 substitution at low strain rates is observed due to the effect of the less reactive NH 3 substitution, while the insignificant reduction of temperature at high strain rates is observed due to the effect of pure stretch regardless of NH 3 substitution. Chemical effects (rather than thermal effects) of NH 3 substitution on flame structure are dominant.

Radial distance, r (mm) Radial distance, r (mm) Design of micro-combustors In order to satisfy the primary requirements for designing the micro-combustor integrated with a micro reforming system (stable burning in the small confinement, maximum heat transfer through the walls and uniform temperature distribution along the wall surface), the micro-combustor that is simply cylindrical to be easily fabricated but twostaged, expanding downstream was designed. 6 4 T (K) 600 1 = 2.0 t w = 0.5 mm 2 800 0-2 0.035 2400 0.005 1600-4 -6 6 4 2 X f T (K) C 3 H 8 -Air Premixed Flame of @ NTP: = 0.9 and V = 0.79 m/s -5 0 5 10 Axial distance, x (mm) 600 800 (a) 1 = 4.0 t w = 0.5 mm 0-2 0.035 2200 0.005 1400-4 -6 X f C 3 H 8 -Air Premixed Flame of @ NTP: = 0.9 and V = 0.79 m/s -10-5 0 5 Axial distance, x (mm) (b)

Design of micro-combustors Preliminary tests of the two-staged micro-combustor for micro reforming systems were conducted for a methanolsteam reforming system the reforming characteristics of which are relatively well known: Improved performance compared to earlier micro methanolsteam reforming systems. But gaseous ammonia reforming does not need a microevaporator.

Radial distance, r (mm) 8.0 6.0 5.0 4.0 Design of micro-combustors A micro-combustor that burns gaseous fuel-air mixtures as a heat source has been designed: A cylinder with an expanded exhaust outlet that facilitates ignition and an annular-type shield that adopts a heatrecirculation concept. [mm] 0.5 d w = 7.0 t w = 0.5 r t g = 1.5 d s = 3.0 x 42.0 6.0 20.0 2.0 l = 22.0 4 C 3 H 8 -Air Premixed Combustion of = 1.0 and t w = 0.5 mm @ NTP: = 1.0 and V= 3.3 m/s T (K) 400 800 1200 1600 2000 2400 2800 0-4 (b) X f -5 0 5 10 15 20 Axial distance, x (mm) 0.002 0.008 0.014 0.02 0.026 0.032 0.038

Reforming ammonia

Objectives Study the potential of using NH 3 as a clean fuel, particularly for portable H 2 -generation systems: Determine a basic configuration of the micro-reformer system, including the heat-recirculating micro-combustor that can feasibly control stable burning and enhance the overall system efficiency and using the catalytic reforming process. Observe the effects of operating parameters (the feed rate of NH 3 and the micro-combustor inlet velocity of fuel-air mixtures) on the performance of the micro-reformer system (the production rate of reformed gas, the conversion rate of NH 3 and the overall system efficiency). Observe the effects of varying the micro-reformer catalyst materials on the performance of the micro-reformer system, considering the cost-effective candidates. Identify the optimized design and operating conditions from the observations.

Experimental methods 2NH 3 3H 2 N 2

Experimental methods (C 3 H 8 -air) Test micro reforming system (SS304) Gaseous fuel-air mixture supply system (MFCs: 0 2,000 sccm, accuracy of 1.0% of full-scale) Gaseous NH 3 feed system (MFCs) Bubble meter and gas chromatography (Agilent 6890) Thermocouples (K-type) Micro-reformer catalysts: Ru (baseline), Ir and Ni/SiO 2 /Al 2 O 3 Test conditions (micro-combustor): V = 2.6 4.1 m/s, = 1.0 C 3 H 8 @ NTP (micro-combustor)

Experimental methods (NH 3 -H 2 -air) Test micro reforming system (SS304) Gaseous sccm, accuracy of 1.0% of fuel-air mixture supply system (MFCs: 0 2,000 full-scale) Gaseous NH 3 feed system (MFCs) Bubble meter and gas chromatography (Agilent 6890) Thermocouples (K-type) Micro-reformer catalysts: Ru Test conditions: V = 1.5 3.0 m/s, = 0.8 1.25 X h = 0.3 0.5 NH 3 /H2 @ NTP (micro-combustor) = 10 ml/min (micro-reformer) m f

Production rate of reformed gas (C 3 H 8 -air) Ru, Ir and Ni/SiO 2 /Al 2 O 3 catalysts were considered. Production rates of reformed gas increase as feed rates of ammonia increase. For Ni/SiO 2 /Al 2 O 3, higher temperature condition in the micro-reformer (and hence in the micro-combustor) than that for Ir and Ru is needed.

Conversion rate of ammonia The conversion rate increases with increasing V until V = 3.1 m/s for Ir and Ru. For Ni/SiO 2 /Al 2 O 3, increases with increasing V up to V = 4.1 m/s. The maximum value of for Ir and Ru is 98.0 % at m f = 5.0-10.0 ml/min and V = 3.1-4.1 m/s. r r

The maximum overall system efficiency is observed at m f = 10.0 ml/min and V = 3.1 m/s: mf < 10.0 ml/min: m is too r small. m f > 10.0 ml/min: not enough residence time. The overall system efficiency for Ni/SiO 2 /Al 2 O 3 is lower than that for Ru and Ir under all the present conditions. Overall system efficiency The maximum overall system efficiency is 13.7%.

Unreacted ammonia mole fraction For Ir and Ru, X NH3 decreases with increasing V until V = 3.1 m/s. For Ni/SiO 2 /Al 2 O 3, higher temperature condition in the micro-reformer (and hence in the micro-combustor) than that for Ir and Ru is needed. The minimum value of unreacted NH 3 mole fraction X NH3 = 0.01 is observed at m f = 5.0-10.0 ml/min and V = 3.1-3.7 m/s.

Optimized condition (C 3 H 8 -air) Operation/performance parameters Materials Catalyst Values Stainless steel (SS304) Ruthenium (Ru) Equivalence ratio of premixed propane-air flame ( ) 1.0 Micro-combustor inlet velocity (V) 3.1 m/s m f Feed rate of ammonia ( ) 10.0 ml/min Production rate of reformed gas ( ) 20.1 ml/min = 5.4 W (based on LHV) Conversion rate of ammonia ( ) 98.0% r Unreacted ammonia mole fraction (X NH3 ) 0.01 Overall system efficiency (η) 13.7% m r

Production rate of reformed gas: = 1.0 (NH 3 -H 2 -air) m r increases with increasing V until a certain condition (which decreases with increasing X h ) due to the increased amount of the supplied fuel and then becomes almost constant since flame is stabilized in the micro-combustor, providing the appropriate amount of heat into the micro-reformer regardless of varying V. The maximum = 20 ml/min. m r

Conversion rate of ammonia: = 1.0 A tendency similar to mr is observed for. The maximum = 97%. r r

Unreacted ammonia mole fraction: = 1.0 X NH3 decreases with increasing V. The minimum X NH3 = 0.015.

Overall system efficiency: = 1.0 increases with increasing V until a certain condition due to the increased amount of the supplied fuel and then decreases since flame is already stabilized in the micro-combustor and thus more enhanced V results in wasting fuel input without increasing hydrogen output. The maximum = 10.4% @ V = 1.63 m/s and X h = 0.5.

Production rate of reformed gas: = 0.8 1.25 A tendency similar to that for = 1.0 is observed for = 0.8 and 1.25. m r The maximum is still 20 ml/min. However, the Vs where the maximum m r reaches increase, particularly for fuel-lean condition.

Conversion rate of ammonia: = 0.8 1.25 A tendency similar to that for = 1.0 is observed for = 0.8 and 1.25. The maximum is still 97%. However, the Vs where the maximum r reaches increase, particularly for fuel-lean condition. r

Unreacted NH 3 mole fraction: = 0.8 1.25 A tendency similar to that for = 1.0 is observed for = 0.8 and 1.25. The minimum X NH3 is still 0.015. However, the Vs where the minimum X NH3 reaches increase, particularly for fuel-lean condition.

Overall system efficiency: = 0.8 1.25 A tendency similar to that for = 1.0 is observed for = 0.8 and 1.25. However, is somewhat reduced, particularly for fuel-rich condition. Also, the Vs where the maximum reaches increase.

Optimized condition (NH 3 -H 2 -air) Operation/performance parameters Materials Catalyst Values Stainless steel (SS304) Ruthenium (Ru) Equivalence ratio of premixed NH 3 -H 2 -air flame () 1.00 Micro-combustor inlet velocity (V) 1.63 m/s Mole fraction of H 2 in fuel gas (x h ) 0.5 m f Feed rate of ammonia ( ) 10.0 ml/min Production rate of reformed gas ( ) 20.1 ml/min = 5.4 W (based on LHV) r Conversion rate of ammonia ( ) 97.0% Unreacted ammonia mole fraction (X NH3 ) 0.015 Overall system efficiency (η) 10.4% m r

Recirculation of reformed gas Approximately 48 52% of the total amount of the reformed gas without the recirculation. The ammonia conversion rate of 97.0% was still measured. Stably working.

Summary An annulus-type micro reforming system which consists of a heat-recirculating micro-combustor as a heat source and a micro-reformer surrounding the micro-combustor has successfully produced hydrogen, using ammonia as a fuel for both reforming and burning. An optimized feed rate of ammonia was determined by preliminary tests using propane as a fuel for the microcombustor (10.0 ml/min). The production rate of reformed gas and the conversion rate of ammonia increase with the increasing inlet velocity of mixtures V until a certain condition since the amount of the supplied fuel increases, intensifying burning in the microcombustor and enhancing heat transfer into the microreformer, and then becomes almost constant since flame is stabilized in the micro-combustor, providing the appropriate amount of heat into the micro-reformer regardless of varying V.

Summary The performance of the micro reforming system is enhanced with the increasing amount of substituted hydrogen. Ru seems to be the most cost-effective among the catalysts considered in the present investigation. The overall system efficiency increases with increasing V until a certain condition due to the increased amount of the supplied fuel and then decreases since flame is already stabilized in the micro-combustor and thus more enhanced V results in wasting fuel input without increasing hydrogen output. Stoichiometric hydrogen-substituted ammonia-air mixtures provide the best performance of the micro reforming system. Under optimized operating conditions, an overall system efficiency of 10.4% was obtained.

Concluding remarks Based on the fundamental characteristics of ammoniafueled flames that were obtained from outwardlypropagating, burner-stabilized and counterflow flame configurations, a micro reforming system integrated with a micro-combustor that reforms and burns ammonia has been successfully designed. Under optimized operating conditions, the micro reforming system produces 5.4 W (based on lower heating value) of hydrogen with a conversion rate of 97.0% and an overall system efficiency of 10.4%. This supports the potential of using ammonia as a clean fuel for both reforming and burning in micro reforming systems.

Further study - applications

Emitter Filter PV cells Thermophotovoltaic (TPV) devices A further study on an ammonia-fueled micro thermophotovoltaic system is also conducted to evaluate the potential of using ammonia in micro power generation systems. Heat Emission Reflection Radiation Reflection e - e - e - e - e - e - e - Electrical power Absorption

Thermophotovoltaic (TPV) devices