Properties of laminar premixed hydrogen- added ammonia/air flames

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5 th Annual Ammonia Fuel Conference Minneapolis, MN, USA, 29-30 September 2008 Properties of laminar premixed hydrogen- added ammonia/air flames J.H. Lee, J.H. Park and O.C. Kwon * School of Mechanical Engineering Sungkyunkwan University Suwon, Kyunggi-do, Korea Acknowledgments: Supported by the Ministry of Environment, Korea

Sungkyunkwan University & ME Sungkyunkwan Univesity: The oldest university in Korea, founded in 1398. One of the leading universities, among the top 5 in Korea. Private university strongly supported by Samsung. 2 School of Mechanical Engineering: Established in 1967. Natural sciences campus. Faculties: 32. Undergraduate students: 727. Graduate students: 135.

Global warming

CO 2 emissions in Korea Korea Metrological Administration report (July 2007): the average amount of CO 2 at the national air monitoring station in Anmyeondo, Chungcheong Province, in 2006 was 388.9 ppm: Korea's CO 2 level has been on the rise for seven 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 (Only NOx) Energetic (120 MJ/kg) Abundant (Renewable) Wide flammable limit Low ignition energy Fast burning velocity High specific heat

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 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.

SWOT of use of ammonia as a fuel in Korea 암모니아이용기술분석 Strengths Weaknesses CO/CO 2 free High hydrogen density: transport and storage Established infrastructure Public concern over toxicity 100% imported No earlier works for ammonia as a fuel Opportunities Threats Initial stage of research on ammonia as a fuel even in advanced countries Increasing public concern on the environment: the Kyoto protocol Price increase of ammonia Development first, the environment later policies

Use of ammonia as a fuel: the present project Heat recovery Thermal dissociation without catalysts Heat recirculation Use of outwardly propagating spherical flames at constant pressure for measurements of fundamental parameters Parabolic mirror (Typ.) Light source: mercury arc lamp Flame Light path Fill/vent line Ground Spark ignitor Pressure transducer Window (Typ.) High-speed camera Parabolic mirror (Typ.) Lens +H 2 NH 3 combustion CO 2 /CO free H 2 -added NH 3 combustion

Originalities of the present project 1 Use of ammonia as a fuel 2 Combustion characteristics of ammonia as a fuel 3 Combustion characteristics of hydrogen-added ammonia 4 No catalytic, thermal dissociation of ammonia 5 Use of ammonia for both combustion and reforming 6 Accurate measurements of burning velocities of ammonia

Objective (within 3 years) Goal Development of CO 2 /CO-free hydrogen generation technology using combustion and reforming of ammonia (miniature/portable size of efficiency of 10-30% and power of 5-30 W)

Research plan 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 thermal 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

Research Years 1-21 Studies on combustion characteristics of ammonia Setup of experimental apparatus Parabolic mirror (Typ.) Light source: mercury arc lamp Flame Spark ignitor Pressure transducer Window (Typ.) Measurements/predictions of combustion characteristics of hydrogen-added ammonia Understanding of reaction kinetics of ammonia-air via numerical simulations Light path Fill/vent line Ground High-speed camera SL /S /SL = 1 + MaKa S = (ρ ( /ρ )dr L /dt Ka = K/(S b u f L /δ) K = (2/r )dr f /dt δ = D/S f L Parabolic mirror (Typ.) Lens

Research Years 2-32 Studies on reforming characteristics of ammonia A study on combustion and heat transfer characteristics in a small combustor via 2/3-D numerical simulations Setup of a small heatrecirculating combustor Setup of experimental apparatus for ammonia reforming

Research Year 3 Studies on hydrogen generation technology using ammonia Setup of a combustorreformer integrated hydrogen generation system Performance evaluations of hydrogen generation system Demonstration of hydrogen generation technology using ammonia

Technological challenges to overcome Combustor: Burning temperature high enough for combustion stability and performance but suppressing NOx formation Heat losses quenching flames Ignition (delay) Maintenance: no catalyst heat recirculation concept applied but with NH 3 Reformer: Uniform and steady heating: residence time and array Erosive to some materials such as metals Combustor-reformer reformer integrated system: Effective heat transfer between a combustor and a reformer Simple structure with heat recirculation

Expected benefits Technological Environmental Economic Combustion and reforming technologies for using ammonia as a fuel Technologies for portable H 2 and power generation systems with rapid response time Reduction of carbon dioxide to prevent global warming Replacement of fossil fuels by ammonia, reducing costs to remove greenhouse gases CO 2 credit price of 3 cents/kg (2005)

Present status of work

Laminar burning velocities This provides strong motivation for accurate measurements of laminar burning velocities.

Nonequidiffusion

Local-conditions conditions hypothesis Laminar burning velocity/stretch interactions are related, following Markstein (1964): S = S L L - LK (1) Application of the local-conditions conditions hypothesis of Kwon et al. (1992) then yields: S /S L L = 1 + Ma Ka (2) where Ka = K δ D /S L, Ma = L/δ D, δ D = D u /S L (3)

Flame/stretch response Linear response conveniently yields constant Markstein numbers at each reactant condition: 4.0 i-c8h18/air FLAMES @ P = 1 ATM & T = 298 K MEASUREMENTS 0.9 = φ 1.5 1.0 STABLE 4.5 = φ 1.8 0.9 3.0 UNSTABLE 0.6 S L /S L 2.0 STABLE 1.0 S L /S L 0.5 0.0 SIMULATIONS: MUELLER ET AL.(1999) MECHANISM H2/AIR FLAMES @ NTP 4.5 1.1 1.5 STABLE 1.0 1.2 1.4 1.0 1.8 0.9 1.6 UNSTABLE 0.0 0.00 0.04 0.08 0.12 0.16 KARLOVITZ NUMBER 0.6 = φ 0.5 UNSTABLE MEASUREMENTS 0.0 0.00 0.05 0.10 0.15 KARLOVITZ NUMBER

Turbulent flame speed evolution Preferential diffusion affects even strongly turbulent premixed flames: This provides strong motivation to find laminar flame response to stretch.

Objectives Study effects of H 2 -addition on properties of laminar premixed NH 3 /air flames: Measure laminar burning velocities for various values of stretch, fuel-equivalence ratios and hydrogen concentrations. Use the measurements to find fundamental unstretched laminar burning velocities and flame response to stretch (Markstein numbers). Use the measurements to evaluate contemporary models of flame structure based on detailed chemical reaction mechanisms. These fundamental data can be used for designing ammonia-fueled hydrogen generation systems.

Experimental methods Flames are spark ignited at the center of a 320 mm diameter spherical chamber: Motion picture Schlieren photographs indicate flame stability, rates of propagation and stretch. Measurements are limited to flame radii of 5-305 mm to provide thin, quasi-steady steady constant-pressure flames.

Data reduction Data is reduced where effects of curvature and unsteadiness are small (δ( D /r f << 1) and the following relationships apply: Laminar burning velocity S L = (ρ( b /ρ u ) dr f /dt Flame stretch K = (2/r f ) dr f /dt Results are limited to unwrinkled flames where effects of ignition and buoyancy are small.

Numerical simulations Codes treating variable properties, multicomponent diffusion and thermal diffusion with detailed chemical kinetics are used: PREMIX: steady laminar one-dimensional flame code developed by Kee at al. of Sandia National Laboratories. COSILAB: steady and unsteady laminar one-dimensional flame code developed by Rogg of Ruhr-Universit Universität Bochum. A detailed N/H/O reaction mechanism of Miller et al. (1989; 73 steps and 19 species) is considered.

Flame/stretch response: NH 3 /H 2 /air flames Linear response conveniently yields constant Markstein numbers at each reaction condition (predicted results only):

Unstretched laminar burning velocities Hydrogen functions by increasing light radical concentrations (predicted results only): Laminar burning velocities increase as hydrogen concentrations increase due to enhanced light radical concentrations.

Markstein numbers Increased hydrogen concentrations enhance unstable nonequidiffusion/stretch interactions for fuel-lean lean and stoichiometric conditions (predicted results only):

Predicted flame structure

Concluding remarks The local-conditions conditions hypothesis yielded a simple correlation of flame/stretch interactions with Ma independent of Ka for moderate and even high levels of stretch. Flame/stretch interactions were substantial for hydrogen-added ammonia/air flames with laminar burning velocities varying in range 0.4-1.7 the unstretched value for Ka < 0.8. Hydrogen acts to increase light radical concentrations and thus laminar burning velocities, which is desirable for intensifying burning of pure ammonia. Once combustion characteristics of ammonia are investigated, a heat-recirculating ammonia-fueled combustor will be designed.