10. SI and CI Emissions • • • • • • • • Sources of Emissions Nitrogen Oxides Hydrocarbons Carbon Monoxide Particulate Matter Emissions Control Strategies Regulatory Efforts Aftertreatment Devices 10-1 Primary Pollutants • Oxides of Nitrogen (NOx) – Result of unwanted secondary reactions – Affect respiratory tract, increase airway resistance and damage lung tissue • • Carbon Monoxide (CO) – Result from oxygen-deficient combustion of carbonaceous materials – Toxic effects spring from the greater affinity that hemoglobin has for CO than O2 Unburned Hydrocarbons (HC) – Fuel molecules that survive combustion or arise through partial oxidation – Encompasses hundreds of compounds (alkynes, alkenes, alkanes, aromatics, etc…) – Can be carcinogenic, irritates the mucous membranes • Particulate Matter (PM) – Born in soot nuclei of oxygen-deficient core of fuel sprays and grow in size through incorporating gas phase molecules – Very important in C.I. engines, also pertinent in gasoline direct-injection engines – Many particles small enough to bypass the respiratory system defense, can slow ciliary function and cause bronchitis • Oxides of Sulfur (SOx) – Sulfur in fuel converted to gas – Also adsorbed by PM 10-2 Secondary Pollutants • Acid Rain – SOx and NOx are precursors to acid rain – Acidification of lakes and soil damage, forest die-back Simplified Acid Rain Scheme • Smog and Troposphere Ozone – NOx and HC will react in the presence of sunlight to form – Irritation of the eyes, nose and throat, impairment of lung function, coughing, nausea and chest discomfort – Hagen-Schmidt (1950’s) - mechanism of Los Angeles smog – NO2 is the key factor that starts the reactions for photochemical smog in the atmosphere: NO2 + hn → NO + O O + O2 + HC → HC + O3 Smog and Ozone Reaction Scheme 10-3 Greenhouse Gases • Carbon Dioxide (CO2) – Inevitable result of burning fossil fuels, can only be restricted by reducing fuel consumption • Nitrous Oxide (N2O) – Result of unwanted secondary reactions • Methane (CH4) – Relatively stable hydrocarbon, so it does not participate in atmospheric reactions (hence not regulated with HC) 10-4 Sources of Emissions Bulk of the pollutants in the exhaust are associated with combustion, but there are other sources Problem for carbureted engines HC CO Nowadays, we are typically left with only the emissions that result from combustion and incylinder processes HC CO Ring clearances have been reduced, any blow-by will be trapped in a carbon canister and recycled into the intake system Incomplete combustion, rich combustion, dissociation, chemical kinetics HC, CO CO2, N2O PM NOx, SOx 10-5 Effect of F/A on Pollutant Concentration • Faced with the realities of the combustion process • No matter how good a combustion chamber you design and no matter how well you mix the fuel and air, there will be emissions issues lean, stoichiometric and rich – Dissociation, chemical kinetics, crevices, flame quenching, etc… 10-6 SI Pollutant Formation Mechanisms Deposits absorb HC NOx formed in CO forms under high temperatures high temperature and if fuel rich As burned gases cool, burned gas NOx chemistry freezes first, then CO chemistry Deposits desorb HC Oil layers absorb HC HC flow to crevices Unburned mixture forced into crevices Oil layers desorb HC Outflow of HC from crevices (some burns to form CO) Piston scrapes HC off walls (expansion) (exhaust) End gas source of HC if incomplete combustion (compression) (combustion) Boundary conditions and crevices are setup during the compression, combustion and expansion processes which may create sources of emissions 10-7 NOx: Equilibrium vs. Kinetic Rate-Limited • NOx (NO and NO2) forms primarily via slow chemical reactions in the high temperature burned gases • In engine combustion chambers, values of TB and p change very rapidly, crank-angle by crank-angle, before equilibrium can be reached for species that form via slow chemical reactions (e.g. NO and N). SI burned and • Assume that O, OH, O2 and N2 equilibrate instantly. unburned zones – [O]e, [OH]e, [O2]e and [N2]e values are realistic. • However, NO and N have relatively slow kinetics. – [NO]e and [N]e values are reference, long-term equilibrium concentrations not reflective of instantaneous [NO] and [N] in engine chamber – The latter should be determined from rate-controlled kinetic schemes (e.g. the extended Zeldovich scheme) – If [NO] < [NO]e then NO is being formed – If [NO] > [NO]e then NO is being eliminated 10-8 Nitrogen Oxide • Extended Zeldovich Mechanism for NO formation: production and destruction of NO d NO k1 O N 2 k2 N O2 k3 N OH dt (1) k1 NO N k2 NOO k3 NO H k1 Zeldovich N2 O NO N k1 k2 N O2 NO O k2 Heywood k3 where [ ] species concentration in mole/cm3 and k’s have strong temperature dependence N OH NO H k3 The k terms are often called Arrhenius rate expressions and are an exponential function of temperature: production and destruction of N d N k1 O N 2 k2 N O2 k3 N OH dt k1 NO N k2 NOO k3 NO H Assuming [N] quasi-steady, set Then substitute result in (1). (2) E k A exp a RuT d N 0 and solve for [N] in (2). dt 10-9 Nitrogen Dioxide • NO formed in the flame zone can be rapidly converted to NO2 NO HO NO OH 2 2 • Reversion back to NO can occur NO2 O NO O2 – Unless NO2 formed in flame is quenched by mixing with cooler fluid – Explains high NO2/NO ratios occurring at light loads in diesels • NO2 can be 10 to 30% of total nitrogen oxide (NO) emissions in diesel engines, especially at low load 10-10 Illustration of SI Engine NOx Formation Model From Flame Traversing Charge not all combustion happens at same time compression each element that burns has different temp history near spark plug expansion in end gas unburned Measured cylinder pressure (p) and calculated mass fraction burned (xb) The first elements that burn form the bulk of the NO emissions because of time and temperature Calculated temperature of unburned gas (Tu) and burned gas (Tb) in earlyand late-burning elements Once NO is Calculated NO concentrations in formed it needs time and high early- and latetemperatures to burning elements for react back into O2 and N2 – rate-controlled leads to frozen model and at NO equilibrium 10-11 Summary of SI NOx Formation • Nitric Oxides (NOx) form throughout the high-temperature burned gases behind the flame front, through chemical reactions involving nitrogen and oxygen atoms and molecules, which do not attain chemical equilibrium – Flame front is negligible with respect to mass that it does not significantly contribute to NOx emissions • The higher the burned gas temperature, the higher the rate of formation of NOx • The first mixture element to burn is compressed considerably and thus reaches the highest burned gas temperature. Thus, the early burned mixture contributes much more to NOx formation than the later burned mixture • As the burned gases cool during the expansion stroke (below 2000 K), the reactions involving NOx freeze and leave NOx concentrations far in excess of levels corresponding to equilibrium at exhaust conditions. 10-12 Effect of A/F and EGR on SI NOx Emissions EGR acts as a diluent and reduces the flame temperatures which leads to lower NO production (Chapter 4) Excess oxygen and high temperatures leads to NO formation (Chapter 4) Variation of exhaust NO concentration with A/F and fuel/air equivalence ratio. We have already discussed the theory and what should happen, now we see experimental verification Variation of exhaust NO concentration with percent recycled exhaust gas (EGR) (1600 rev/min, v = 50 %, MBT timing) 10-13 Effects of Spark Timing, A/F, Coolant Temperature and Deposits on SI NOx Emissions Compressing early burned elements more – will see higher pressures and temperatures for spark advance As coolant temperature increases, less possibility for heat transfer to take energy away from gas – leads to hotter chamber as a whole deposits can act as insulation Variation of exhaust NO concentration spark retard. (1600 rev/min, v = 50%; lefthand end of curve corresponds to MBT timing for each A/F) Increased coolant temperature or presence of deposits reduce heat losses, both of which increase NOx 10-14 SI NOx Reduction Strategies Brake specific HC and NOx emissions (relative basis) versus air-fuel ratio Effect of exhaust gas recirculation and NOx reducing catalyst on relative brake specific NOx emissions 10-15 Direct-Injection NOx Formation • SI analysis can be directly applied to a diesel engine – NOx still forms in burned gas Lean flame-out Volume: HC Initial rapid combustion: noise Fuel jet mixing with air: rich mixture Burned gas: NO Premixed Burned gas: NO White/yellow flame: soot oxidation Rich zones in fuel jet: soot formation Flame quench on walls: HC Fuel vapor from nozzle sac volume Mixing controlled 10-16 Unburned Hydrocarbon Mechanisms • • • • • • • • • Crevice Flows Oil Layer Absorption/Desorption Wall Wetting/Fuel Puddles Combustion Chamber Temperature/Deposits Exhaust Gas Temperature Partial Burn, Quenching and Misfire Nozzle Sac Volume Overleaning Undermixing 10-17 HC Emissions from SI Engines- Sources • Cartoon of cylinder showing origin of NO, HC and CO Exhaust port burnup Exhaust Liquid fuel cold start HC’s HC’s desorbed from oil layer and crevice HC’s Crevice outgassing CO, HC Bulk gas Slow/partial burns NO and CO (rich) CO, HC Wall effects • Deposits • Oil layers • Liquid fuel during cold start Crevice • Trapping and release of unburned mixture Bulk quenching • Late and partial burns – cold start/transient • Can be minimized by good fuel and air control. 10-18 Conceptual Sources of SI HC Emissions, Including Crevice Volume Flows From J. Eng, SAE 2005-01-3867 10-19 Crevice Flow Mechanism • • • • • Volumes 1 – 4 make up the crevice. The pressure in Volume 1 equals the cylinder pressure Crevice gas temperature is approximately constant (from ~ 400 – 500 K), so to satisfy the ideal gas law, fuel and air fill volume 1 and 2 of the crevice as the cylinder pressure increases during compression. There is some flow from 2 to 3 due to blowby during this time. As peak cylinder pressure drops (post combustion ~ 730 deg), fuel (HC) and air flow out of the crevice into the combustion chamber to again satisfy the ideal gas law. As the top ring lifts and seats on “B” at 760 deg, Volume 1 is isolated from 2. Beyond 760 deg here, the pressure in Volume 2 - 4 decreases due to blowby (to Volume 5) and flow back into the cylinder via Volume 1 due to gas leakage across the top ring Top Ring seats on “C” (Isolates Volume 2 from 3) Top Ring lifts, seats on “B” (Isolates Volume 1 from 2) Top Ring seats on “C” (Isolates Volume 2 from 3) Mass flows into the crevice from the cylinder Top Ring (moves between “B” and “C”) Bottom Ring (always seated on “D”) Top Ring lifts, seats on “B” (Isolates Volume 1 from 2) 10-20 Effect of Crevice Volume on HC Emissions The larger the crevice, the more HC that can fit into this area Piston top-land crevice volume Eventually, it levels off. Crevice becomes large enough for flame to penetrate. Effect of increasing top-land clearance on exhaust hydrocarbon emissions Unthrottled SI engine (N = 6885 rev/min, A/F = 13, MBT timing) 10-21 Effect of Blow-by Flow on HC Emissions • Effect of increasing crankcase blow-by on exhaust hydrocarbon emissions using production pistons and rings. • As blowby increases, the exhaust gas HC emissions decrease • This results in part from flow out of the crevice, into the crankcase, instead of into the combustion chamber SI Engine (N = 1200 rev/min, A/F = 14.2, intake manifold pressure = 0.6 atm) 10-22 Fuel Puddle Formation (SI Engine) • During port fuel injection, the fuel injector spray is targeted towards the intake valve • Liquid films may form on the intake valve and port as well as inside the cylinder • Fuel may vaporize too late for combustion to burn completely – Depends on temperatures of port and cylinder walls • In particular, this is a problem for cold starting 10-23 SI Unburned HC Emissions due to Deposit Growth for Various Fuels • Deposits have been shown to promote unburned HC emissions – Soak up HCs – Release it late in expansion when there is not a flame • Experiment on right shows that as deposits form over time, the unburned HC emissions increase • Additives may help to reduce deposit formation, hence HC absorption Doelling, et al. SI Engine, SAE Paper 720500 (1500 rpm, = 1.1, S.T. = 15º BTC) 10-24 Effect of Combustion Chamber Surface Temperature on SI HC Emissions • The unburned HCs will go down when operating with hotter walls – Flames will not get quenched as easily – Deposits may not form on hot walls – Clearances get smaller (more expansion and less crevice flows) • However, may lead to higher NOx emissions, knock and loss in volumetric efficiency (air density) Wentworth, SAE Paper 710587, SI Engine, SAE Transactions vol. 80 10-25 Effect of Spark Retard on HC Emissions • Increased exhaust temperature because of lower cycle efficiency • Increased port burnup of the hydrocarbons 10-26 Partial Burn, Quenching and Misfire Combustion Efficiency [%] 100 90 C.I. inherent combustion efficiency advantage 80 Diesel Spark Ignition Simple Model 70 Fuel: Isooctane p /p = 1.0 60 i e 0% EGR SI combustion slows with dilution and may not be complete by EVO for high dilution levels c,lean ~ 1 High levels of CO and H2 c,rich ~ 1/ Lean Rich 50 0.0 Figure 3-9 Heywood 0.2 0.4 0.6 0.8 1.0 Equivalence Ratio 1.2 1.4 1.6 10-27 Overleaning (CI Engine) • Associated with Phase 0 and I • Schematic of diesel engine fuel spray showing equivalence ratio () contours at time of ignition. – L = equivalence ratio at lean combustion limit (~ 0.3) – Shaded Volume contains fuel mixed leaner than L Air swirl > 1 (rich) =0 > L Injection nozzle Fuel jet boundary Ignition location =1 Overmixed HC 10-28 HC and Ignition Delay (CI Engines) • Correlation of exhaust HC concentration with duration of ignition delay for DI diesel engines. • Various fuels, engine loads, injection timings and boost pressures at 2800 rev/min Too long of a delay, there is too much overleaning of the mixture on the leading edges. This will lead to more flame-out and higher HC emissions Too short of a delay, there is not enough mixing and more soot is created. 10-29 Nozzle Sac Volume • Effect of nozzle sac volume on exhaust HC concentration, DI diesel engine at minimum ignition delay – Vd = 1 dm3/cylinder, N = 1700-2800 rev/min 10-30 Overfueling or Undermixing • Effect of overfueling on exhaust HC concentration – DI diesel engine, speed = 1700 rev/min, injection timing at full load 15ºBTC 10-31 Carbon Monoxide • Carbon monoxide forms during the combustion process • With rich fuel-air mixtures, there is insufficient oxygen to fully burn all the carbon in the fuel to CO2 • Partial oxidation of crevice and wall layer HC produce CO • In high temperature products, even with lean mixtures, dissociation ensures that there are significant CO levels • Later in the expansion process (below 1500 K), CO oxidation (to CO2) freezes as burned gas temperatures fall • CO is fairly easy to oxidize in catalysts → not a big problem in today’s engines as long as the catalyst is warmed up Drivers for CO Formation * Equivalence Ratio * Dissociation * Reaction Kinetics 10-32 SI Engine Exhaust Composition as a Function of Equivalence Ratio Discussed previously in Chapter 4 10-33 Particulate Matter • Mainly consists of organic compounds that originate from unburned or partially burned fuel and lubricant and sulphates from the sulfur in the fuel. • Formed predominantly during the diffusion burning period, where within the jet the local fuel-air ratios are rich. • Rich combustion results in the formation of carbon particles. • Jacobs, T. J., Pd.D. Thesis, • University of Michigan (2005). 10-34 Particulates • Any substance (other than H2O) that can be collected on filter paper in the exhaust • Consists of two parts: – Solid Carbon (soot) – Organic fraction (compounds that adsorb to soot) CO Soot Formation Model first stage of combustion: C H xO2 CO O2 CO2 Cs O 2 CO 2 1 2 second stage of combustion: H 2 x O2 2 2 2 xCO 2 x C s 2 H2 Clean 2x Sooting 2x < H 2 12 O2 H 2O Bosch Smoke Number A scale that reflects reflectivity of filter paper 0.5 – no smoke 1 – clear 2 – light 4 – dark 8 – very-dark 9 – heavy smoke 10-35 Particulate Matter Conceptual Model Flynn, P. F., et al. (1999) Diesel combustion: An integrated view combining laser diagnostics, chemical kinetics, and empirical validation. SAE Paper No. 1999-01-0509 10-36 Particulate Matter Conceptual Model - 2 • HC and soot emissions are formed within the diesel jet during Phase II combustion • Much of these species are oxidized by the diffusion flame, or during Phase III • Those species that survive oxidation are exhausted as soot, HC and CO emissions Image of Phase II Combustion SAE Paper No. 1999-01-0509 10-37 Diesel Jet-Wall Interaction • There is significant flame wall interaction during the diesel combustion process • We see OH in the diffusion flame (green) quenching as it interacts with the piston bowl wall • Soot (red), CO and hydrocarbons that are not oxidized will be emitted as emissions Piston bowl wall SAE Paper No. 2001-01-1295 10-38 DI NOx and Soot Emissions Tradeoff • • NOx is formed in high temperature burned gases Soot is formed in rich fuel zones within the diesel jet – Most, but not all will be oxidized in the diffusion flame • The NOx soot tradeoff is one of the perennial challenges of diesel combustion Smoke (FSN) – As peak temperature is reduced to decrease NOx, smoke emissions increase Nishimura et al. SAE 981929 10-39 Emissions Control Strategies • Improved Mixture Preparation • Improved Combustion Process • Improved Engine Design • Optimizing Engine Operating Parameters • Improved Control Strategies and Algorithms • After treatment Systems - if we do not succeed in-cylinder 10-40 Tailpipe Regulations CO: 3.4 g/mi Tier 0 : 0.41 HC, 0.7 NO , 7.0 CO, 0.2 PM (1990) x Tier 1 : 0.25 HC, 0.4 NO , 3.4 CO, 0.08 PM x 0.2 TLEV: 0.125 HC, 0.4 NO , 3.4 CO, 0.08 PM x LEV: 0.075 HC, 0.2 NO , 3.4 CO, 0.08 PM CO: 3.4 g/mi x ULEV: 0.04 HC, 0.2 NO , 1.7 CO, 0.04 PM x 0.1 CO: 3.4 g/mi LEV II: 0.075 HC, 0.05 NO , 3.4 CO, 0.01 PM x ULEV II: 0.04 HC, 0.05 NO , 1.7 CO, 0.01 PM x 0 CO: 1.0 g/mi SULEV: 0.01 HC, 0.02 NO , 1.0 CO, 0.01 PM CO: 1.7 g/mi 0 x 0.2 0.4 0.6 NOx Emissions [g/mi] 0.8 1 Emission Standards USA Heavy-Duty Diesel Truck Engines [g/bhp-hr] 12 0.7 10 NOx/NMHC+NOx 0.6 PM 0.5 8 0.4 6 4 2 0.2 0.1 0 1988 0 0.3 Particulate Matter – SI and CI 0.3 LEV II ULEV ULEV II SULEV NMHC: 0.5 • Effectively zero in 2010 and beyond Tier 0 Tier 1 TLEV LEV Nitrogen Oxides 2004: Non-methane hydrocarbons + NOx – ZEV: Zero-emission vehicle CO: 7.0 g/mi 0.4 HC Emissions [g/mi] • Emission regulations are getting more and more restrictive • California leads the way California Air Resources Board Emission Standards (Passenger Car) 0.5 0.0 1990 1 1991 2 1994 3 1998 4 2004a 5 2004b 6 2007 7 2010 10-41 Worldwide Emission Regulations US07/10 NOx emissions are typically more stringent 10-42 Modern Three-Way Catalyst • Consists of a combination of Pt, Rh and Pd noble metals • Three-Way Reduction of HC, CO and NOx • Washcoat provides high surface area of catalytic material – Can also enhance reactions and stabilize the noble metals – Cerium often used • Small channels cause laminar flow – Increases residence time – Negligible pressure drop CO 12 O2 CO2 HC O2 CO2 H 2O CO NO CO2 12 N 2 Ce2O3 NO 2CeO2 12 N 2 10-43 Effect of A/F on SI Three-Way Catalyst Conversion Efficiency • Around stoichiometry we have CO, HC and NOx due to incomplete combustion and dissociation • Any left over oxygen can be used to convert CO and HC • NOx is also a great oxidizer of CO and HC The conversion efficiency of a catalyst is the ratio of the rate of mass removal in the catalyst of the particular constituent of interest to the mass flow rate of that constituent into the catalyst: e.g. for HC cat ,HC mHC,in mHC,out m 1 HC,out mHC,in mHC,in 10-44 Fuel Flow Calculation: Closed Loop • Requires EGO Sensor or UEGO • Reasons – Stoichiometric Fuel Delivery for Three-Way Catalyst Efficiency – Adaptive Fuel Learning Based on Component Tolerances While we are trying to do the best job we can initially (open loop) there will always be changes/errors in the sensors and injectors that require constant adjustment Exhaust Gas Oxygen (EGO) sensor gives us a catch-up opportunity to look for imbalances in O2 due to under fueling or over fueling events Can adaptively learn which cylinders might have a problem (C-T-C variability) 10-45 Direct-Injection Lean-Burn Engines? – Cannot use TWC NOx reduction reactions lean 0.0140 0% EGR 10% EGR 20% EGR 30% EGR 0.0112 Mole Fraction NO • Better fuel economy • Reduction in CO2 emissions as a byproduct • CO and HC emissions nearly negligible • Soot now becomes a problem • NOx issues Increasing EGR Effect 0.0084 0.0056 0.0028 Fuel: Isooctane Initial Temp: 700 K Initial Pres: 10 bars 0.0000 0.0 0.2 0.4 0.6 0.8 1.0 1.2 1.4 1.6 10-46 Controlling NOx Emissions – Fundamental Difficulties of Diesel Engines • High thermal efficiency and compression ratios of diesel cycle cause high peak gas temperatures. • NOx – Particulate trade-off – Suppression of NO formation has a tendency to increase particulates and vice-versa. • Excess oxygen in exhaust prevents the use of standard stoichiometric TWC technology for the reduction of NOx 10-47 Diesel Oxidation Catalyst • Used excess O2 to reduce any CO and HC that exits the engine – SI: incorporated excess air injection – CI: excess air is already present! • Produces NO2 for use with LNT/SCR devices • Will reduce SOF of PM Diesel Oxidation Catalyst CO, HC and SOF Conversion Clean-up of Regeneration Event NO2 Production from NO for DPF CO 12 O2 CO2 HC O2 CO2 H 2O NO 12 O2 NO2 10-48 Ammonia Selective Catalytic Reduction Urea Injection • One possible way to handle NOx – NH3 great reducer for NOx – Vanadium/Zeolite catalysts like to store NH3 • Industrial use of NH3 SCR dates back to 1970s T NH 2 CO NH 2 NH 3 HNCO HNCO H2O NH3 CO2 – Used homogeneous reactions because of higher temperatures • Automobiles use urea injection in exhaust stream • Relatively easy to control – Optimize engine for performance 4NH3 4NO O2 4N2 6H2O 4NH3 2NO 2NO2 4N2 6H2O 4NH3 3NO2 72 N2 6H2O 4NH3 6NO 5N 2 6H 2O 10-49 Ammonia SCR Issues • • • • Packaging Tampering Issues Consumer Conception Urea Infrastructure – Europe “AdBlue” urea availability project – Mercedes Bluetec with urea charge • Cost not directly factored into mpg – Urea takes energy to make – Well-to-wheel efficiency 10-50 Lean NOx Trap • Two Modes of Operation – Lean: NOx storage on Barium or similar material • NO2 is preferred storage species – Rich: NOx regeneration through TWC type of reactions • Platinum Group Metal (PGM) often incorporated • Rich – To regenerate trap need CO, H2 or HC to promote TWC reactions – Two options: • Late in-cylinder fuel-injection • Fuel-injection in exhaust stream NOx Adsorption Catalyst – Take heavy HCs and break down into species more suited for regeneration NOx Storage During Lean Operation on Alkali or Alkali Earth Metal CO, HC and NOx Conversion over PGM During Rich Operation (Regeneration) Lean Operation Rich Operation NO 12 O2 NO2 Ba NO3 2 13 C3H 6 BaCO3 H 2O 2NO BaCO3 2NO 2 12 O 2 Ba NO3 2 CO 2 CO NO CO2 12 N 2 10-51 Lean NOx Trap Issues • Very Hard to Control • SOx Likes to Store More Than NOx – EPA legislated sulfur in fuel (15 ppm as of 2007) • Regeneration Species – Likes CO and H2 for regeneration – Late in-cylinder injection has high temperatures and excess O2 • Breaks down fuel to proper components • Will also oxidize and lower yield – Post cylinder injection • Temperatures lower and less oxidation possible • More heavy HCs into LNT • Direct Fuel Penalty 10-52 Particulate Filter • Alternating Flow Channel Pattern – Exhaust travels through a porous wall • Stores PM on Inlet Channel Walls • At high enough temperatures, soot oxidizes and provides large exothermic reaction • NO2 reduces the light-off temperature of soot • Add catalytic material to wall to promote NO2 generation and other reactions • Nearly 100% Effective at Trapping Soot • Issues: – Increasing pressure drop with soot loading – Possible runaway combustion reaction – Ash accumulation • In use for all 2007 Diesel engine platforms Diesel Particulate Filter Deposit Collection and Oxidation by O2 and NO2 10-53 Catalyzed DPFs Available
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