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Experimental and Modeling Study of NO and NO2 Storage and Release Characteristics of a Diesel-Cold Start Catalyst

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Abstract

A 2013 6.7L Cummins ISB (209 kW) diesel engine was used to quantify the NO, NO2, and NOx storage and release performance of the diesel cold start catalyst (dCSC™). The NOx storage experiments were performed over a range of temperatures from 80 to 250°C and NOx release experiments were performed at temperatures from 200 to 450°C. A 2-D diesel cold start catalyst (d-CSC) model was developed to predict NO, NO2 storage, and release characteristics along with the temperature distribution within diesel cold start catalyst (d-CSC) and the pressure drop across the d-CSC. This d-CSC model was calibrated using eight runs of experimental data that consisted of storage temperatures ranging from 80 to 250°C and release temperatures ranging from 200 to 450°C. The validation results show that the new d-CSC model can predict 200-s NOx storage and total NOx release capacity with a maximum root mean square (RMS) error of 0.02 and 0.10 NO2 g/L of substrate, respectively. The NO2/NOx ratio RMS error was within 24%. The RMS temperature errors for storage and release phases were within 3°C and the pressure drop model error was within 0.2 kPa. It is found that the dCSC™ shows significant low temperature NOx storage capability with a peak storage occurring from 125 to 150°C. The rapid NOx release was observed at temperatures above 200°C which is well within the operating range of the aftertreatment system after cold start period.

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Abbreviations

ANPR:

Advanced notice of proposed rule

CARB:

California Air Resources Board

CPF:

Catalyzed particulate filter

CO:

Carbon monoxide

CO2 :

Carbon dioxide

CTI:

Clean Truck Initiative

dCSC™:

Diesel cold start catalyst

d-CSC:

Diesel cold start catalyst model (Johnson-Matthey)

DOC:

Diesel oxidation catalyst

DPF:

Diesel particulate filter

ECU:

Electronic control unit

EPA:

Environmental Protection Agency

FTP:

Federal test procedure

HC:

Hydrocarbons

LLC:

Low load cycle

MECA:

Manufacturers of Emission Controls Association

MTU:

Michigan Technological University

NO:

Nitrogen monoxide

NO2 :

Nitrogen dioxide

NOx:

Oxides of nitrogen

O2 :

Oxygen

OBD:

On-board diagnostics

PM2.5:

Particulate matter of 2.5 micrometers and smaller

PNA:

Passive NOx Adsorber

RMC:

Ramp modal cycle

RMS:

Root mean square

SCAQMD:

South Coast Air Quality Management District

SCR:

Selective catalytic reduction

SCRF™:

SCR catalyst on a filter (Johnson-Matthey)

SCR-F:

Selective catalytic reduction catalyst on a DPF

SET:

Supplemental emission test

SwRI:

Southwest Research Institute

\(\Delta\) P:

Pressure drop

1-D:

One-dimensional

2-D:

Two-dimensional

3-D:

Three-dimensional

Abbreviations

\({A}_{ads, NO}\) :

Pre-exponential for NO adsorption [m3 gmol1 s1]

\({A}_{{ads, NO}_{2}}\) :

Pre-exponential for

\(N{\mathrm{O}}_{2}\) :

adsorption [m3 gmol1 s1]

\({A}_{ads,y}\) :

Pre-exponential of species

\(\mathrm{y}\) :

for adsorption [m3 gmol1 s1]

\({A}_{des, NO}\) :

Pre-exponential for NO desorption [m3 gmol1 s1]

\({A}_{{des, NO}_{2}}\) :

Pre-exponential for NO desorption [m3 gmol1 s1]

\({A}_{des,y}\) :

Pre-exponential of species

\(\mathrm{y}\) :

for desorption [m3 gmol1 s1]

\({A}_{amb}\) :

Surface area of outer shell [m2]

\({A}_{g}\) :

Geometric surface area [m2]

\({Ar}_{i,j}\) :

Area normal to the heat transfer in the radial direction [m2]

\(a\) :

Channel width [m]

\({CFA}_{i,j}\) :

d-CSC frontal area at each zone [m2]

\({C}_{{f}_{i,j}}\) :

Skin friction coefficient [-]

\({c}_{f}\) :

Specific heat of d-CSC substrate material [J kg1 K1]

\({C}_{{C}_{3}{H}_{6}}\) :

d-CSC inlet

\({C}_{3}{H}_{6}\) :

concentration [mol m3]

\({C}_{CO}\) :

d-CSC inlet

\(CO\) :

concentration [mol m3]

\({C}_{{H}_{2}O}\) :

d-CS inlet

\({H}_{2}O\) :

concentration [mol m3]

\({C}_{NO}\) :

d-CSC inlet

\(NO\) :

concentration [mol m3]

\({C}_{{NO}_{2}}\) :

d-CSC inlet

\({NO}_{2}\) :

concentration [mol m3]

\({C}_{s,y}\) :

Solid phase concentration for the species

\(y\) :

[mol m3]

\({C}_{s,NO}\) :

d-CSC substrate

\({NO}\) :

concentration [mol m3]

\({C}_{s,NO2}\) :

d-CSC substrate

\({NO}_{2}\) :

concentration [mol m3]

\({C}_{{O}_{2}}\) :

d-CSC inlet

\({O}_{2}\) :

concentration [mol m3]

\({c}_{{p}_{i,j}}\) :

Specific heat of exhaust gas at each zone [J kg−1 K−1]

\({C}_{s,y}\) :

d-CSC solid concentration along y direction [mol m3]

\({C}_{g,y}\) :

d-CSC gaseous concentration along y direction [mol m3]

\({D}_{h}\) :

Hydraulic diameter of the d-CSC channel [m]

\({E}_{NO}\) :

Activation energy for

\(\mathrm{NO}\) :

oxidation [J gmol1]

\({E}_{NO2}\) :

Activation energy for

\({\mathrm{NO}}_{2}\) :

oxidation [J gmol1]

\({E}_{des,NO}\) :

Activation energy for

\(\mathrm{NO}\) :

desorption [J gmol1]

\({E}_{{des,NO}_{2}}\) :

Activation energy for

\(N{\mathrm{O}}_{2}\) :

desorption [J gmol1]

\({E}_{{des,NO}_{2}}\) :

Desorption activation energy for species

\(\mathrm{y}\) :

[J gmol1]

\({G}_{4}\) :

Inhibition factor [-]

\({h}_{amb}\) :

Ambient heat transfer coefficient [W m−2 K−1]

\({h}_{g}\) :

Internal heat transfer coefficient [W m−1 K−1]

\({K}_{i,j}\) :

Fanning friction factor [-]

\(k\) :

Species reaction index [-]

\({k}_{mtc,y}\) :

Mass transfer coefficient of species

\(\mathrm{y}\) :

[m2 s−1]

\({K}_{p}\) :

Equilibrium constant [-]

L:

Length of the d-CSC [m]

M:

Number of radial zones [-]

\(\dot{m}\) :

Instantaneous exhaust mass flow rate [kg s1]

\({\dot{m}}_{i,j}\) :

Mass flow rate at each zone [kg s1]

N:

Number of axial zones [-]

\({N}_{y,k}\) :

Stoichiometric coefficient [-]

\({N}_{u}\) :

Nusselt number [-]

\({P}_{in}\) :

d-CSC inlet gas pressure [kPa]

\({P}_{r}\) :

Prandtl number [-]

\({\dot{Q}}_{cond,axial}\) :

Axial conduction [W]

\({\dot{Q}}_{cond,radial}\) :

Radial conduction [W]

\({\dot{Q}}_{conv}\) :

Convection between channels gases and substrate wall [W]

\({\dot{Q}}_{rad}\) :

Radiation between channel surfaces [W]

\({\dot{Q}}_{reac}\) :

Exothermic reactions within d-CSC [W]

\({rc}_{i}\) :

Radial distance of the nodes [m]

\(R\) :

Universal gas constant [J mol1 K1]

\({R}_{{e}_{i,j}}\) :

Reynolds number [-]

\({R}_{ads,y}\) :

Adsorption rate of species

\(y\) :

[mol m3 s1]

\({R}_{ads,NO}\) :

Adsorption rate of NO [mol m3 s1]

\({R}_{ads,NO2}\) :

Adsorption rate of NO2 [mol m3 s1]

\({R}_{des,y}\) :

Desorption rate of species

\(y\) :

[mol m3 s1]

\({R}_{des,NO}\) :

Desorption rate of NO [mol m3 s1]

\({R}_{des,NO2}\) :

Desorption rate of NO2 [mol m3 s1]

\({R}_{mat 1}\) :

Thermal resistance of the inner mat [K/W]

\({R}_{mat 2}\) :

Thermal resistance of the outer mat [K/W]

\({R}_{nfz}\) :

Thermal resistance of the no flow zone [K/W]

\({R}_{shell 1}\) :

Thermal resistance of the inner shell [K/W]

\({R}_{shell 2}\) :

Thermal resistance of the outer shell [K/W]

\({R}_{total}\) :

Total thermal resistance of the insulation material [K/W]

\({R}_{y,k}\) :

Reaction rate of species

\(y\) :

[mol m3 s1]

\({T}_{amb}\) :

Ambient temperature [K]

\({Ts}_{i,j}\) :

Solid phase temperature at each zone [K]

\({Tg}_{i,j}\) :

Gas phase temperature at each zone [K]

\({u}_{{g}_{i,j}}\) :

Exhaust gas velocity [m s1]

\({\dot{V}}_{i,j}\) :

Actual volumetric flow rate of the channel [m3 s1]

\({V}_{{e}_{i,j}}\) :

Empty volume (volume occupied by the exhaust gas) at each zone [m3]

\({V}_{{s}_{i,j}}\) :

Substrate volume with washcoat at each zone [m3]

\({t}_{ins+can}\) :

Thickness of the insulation + inner can [m]

\({T}_{amb}\) :

Ambient temperature [K]

\({T}_{{g}_{i,j}}\) :

d-CSC solid phase temperature at each zone [K]

\({T}_{in}\) :

d-CSC inlet temperature [K]

\({T}_{{s}_{i,j}}\) :

d-CSC solid phase temperature at each zone [K]

\({T}_{w}\) :

d-CSC substrate temperature at each zone [K]

\(z\) :

Axial zone length [m

\({\Delta }_{i}\) :

Effective radial zone radius [m]

\({\Delta }_{j}\) :

Effective axial zone length [m]

\({\Delta L}_{i,j}\) :

axial length of the channel at each zone [m]

\({\Delta P}_{i,j}\) :

Pressure drop across d-CSC at each zone [kPa]

\(\Delta x\) :

Discretization length in axial direction [m]

\(\varepsilon\) :

Void fraction [-]

\({\varepsilon }_{r}\) :

Emissivity of the metal surface [-]

\({\theta }_{1,NO}\) :

Fraction of sites covered with NO molecules [-]

\({\theta }_{1,NO2}\) :

Fraction of sites covered with NO2 molecules [-]

\({\theta }_{y}\) :

Fraction of sites covered with species

\(y\) :

[-]

\({\lambda }_{i,j}\) :

Thermal conductivity of the substrate [W m-1 K−1]

\({\mu }_{{g}_{i,j}}\) :

Dynamic viscosity of exhaust gas [Ns m2]

\({\mu }_{i,j}\) :

Dynamic viscosity of exhaust gas at each zone [Ns m2]

\({\rho }_{f}\) :

d-CSC substrate density [kg m3]

\({\rho }_{{g}_{i,j}}\) :

Exhaust gas density [kg m3]

\(\sigma\) :

Stefan-Boltzman constant [W m-2 K4]

\({\tau }_{wall}\) :

Wall shear stress [N m2]

\({\Omega }_{1, NO}\) :

Total storage capacity of NO sites [gmol m−3]

\({\Omega }_{1, NO2}\) :

Total storage capacity of NO2 sites [gmol m−3]

\({\Omega }_{y}\) :

Total storage capacity of species

\(y\) :

[gmol m−3

i :

Radial Direction

j :

Axial Direction

y :

Species Index

k :

Reactions Index

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Appendices

Appendix 1 Thermocouple Layout and Thermal Insulation Arrangement

Figs. 12

Fig. 12
figure 12

dCSC™ thermocouple layout

12,

Fig. 13
figure 13

Illustration of the dCSC™ thermal insulation arrangement

13

Appendix 2 Additional d-CSC Submodel Equations

2.1 Solid and Gas Phase Temperature Solver

In the substrate temperature submodel in Equation (1), \({\dot{Q}}_{cond.radial}\) at the outermost zone of the d-CSC model is calculated accounting for the multilayers of thermal insulation shown in Fig. 13. The \({\dot{Q}}_{cond.radial}\) at the outermost radial zone is give as

$${\dot{Q}}_{cond.radial} \text{=}{ \lambda }_{i,j}{Ar}_{i,j}\frac{{Ts}_{i-1,j}{- Ts}_{i,j} }{In\left(\frac{{rc}_{i}}{{rc}_{i-1}}\right)}+\frac{\left({ T}_{amb}-{Ts}_{i,j}\right)}{{R}_{total}}+{\mathrm{h}}_{amb}{A}_{amb}\left({ T}_{amb}-{Ts}_{i,j}\right)+ {\varepsilon }_{r}\sigma {A}_{amb}\left({T}_{amb}^{4}-{Ts}_{i,j}^{4}\right)$$
(B.1)
$${R}_{total}={R}_{nfz}+{R}_{mat 1}+{R}_{shell 1}+{R}_{mat 2}+{R}_{shell 2}$$
(B.2)

where, \({\lambda }_{i,j}\) is the thermal conductivity of the substrate, \({Ar}_{i,j}\) is the area normal to the heat transfer in the radial direction, \({Ts}_{i,j}\) is the substrate temperature,\({rc}_{i}\) is the radial distance of the nodes, \({T}_{amb}\) is the ambient temperature, \({R}_{total}\) is the total thermal resistance of the insulation materials shown in Fig. A 2, \({R}_{nfz}\) is the thermal resistance of the no flow zone of the d-CSC, \({R}_{mat 1}\) is the thermal resistance of the inner mat, \({R}_{shell 1}\) is the thermal resistance of the inner shell, \({R}_{mat 2}\) is the thermal resistance of the outer mat , \({R}_{shell 2}\) is the thermal resistance of the outer shell, \({h}_{amb}\) is the ambient heat transfer coefficient, , \({A}_{amb}\) is the surface area of outer shell , \({\varepsilon }_{r}\) is the emissivity of the metal surface, and \(\sigma\) is the Stefan-Boltzman constant

2.2 d-CSC Species Solver Equations

Table

Table 8 Summary of chemical reactions and rate expressions used in the d-CSC species solver model

8 shows the summary of the chemical reactions and rate expressions used in the d-CSC species solver model.

Table 8

where \({R}_{ads,NO}\) is the adsorption rate of NO, \({R}_{ads,NO2}\) is the adsorption rate of NO2, \({R}_{des,NO}\) is the desorption rate of NO, \({R}_{des,NO2}\) is the desorption rate of NO2, \({A}_{ads,NO}\) is the NO adsorption pre-exponential, \({A}_{ads,NO2}\) is the NO2 adsorption pre-exponential, \({C}_{s,NO}\) is the sold phase concentration of NO, \({C}_{s,NO2}\) is the solid phase concentration of NO2, \({\theta }_{1,NO}\) is the fraction of sites covered with NO molecules, \({\theta }_{1,NO2}\) is the fraction of sites covered with NO2 molecules, \({\Omega }_{NO}\) is the total storage capacity of NO sites, \({\Omega }_{NO2}\) is the total storage capacity of NO2 sites, \({E}_{des,NO}\) is the activation energy for the NO desorption, \({E}_{des,NO2}\) is the activation energy for the NO2 desorption, \({A}_{NO}\) is the NO oxidation pre-exponential, \({A}_{NO2}\) is the NO2 oxidation pre-exponential, \({E}_{NO}\) is the activation energy for the NO oxidation reaction, \({E}_{NO2}\) is the activation energy for the NO2 oxidation reaction, \({C}_{O2}\) is the gaseous O2 concentration (gaseous concentration is used instead of solid phase concentration to reduce computational complexity and is available in excess in diesel exhaust), \({K}_{p}\) is the equilibrium constant, \(R\) is the universal gas constant, \({G}_{4}\) is the inhibition factor and \(Ts\) is the solid phase temperature of the d-CSC. The detailed formulation of terms used in Table 8 for NO oxidation equations are available in reference [18].

2.3 Pressure Drop Model

The pressure drop across the d-CSC is calculated using the fully developed laminar flow equations for a square channel from the previous research [18] and it is given as

$${\Delta P}_{i,j}=\frac{1}{{\varepsilon }_{i,j}}\left(\frac{2{\mu }_{{g}_{i,j}}{K}_{i,j}{\Delta L}_{i,j}{\dot{V}}_{i,j}}{{CFA}_{i,j}{ D}_{h}^{2}}\right)$$
(B.3)
$${K}_{i,j}={R}_{{e}_{i,j}}{C}_{{f}_{i,j}}$$
(B.4)
$${C}_{{f}_{i,j}}=\frac{{\tau }_{wall}}{\frac{1}{2}{\rho }_{{g}_{i,j}}{u}_{{g}_{i,j}}^{2}}$$
(B.5)

where \({\Delta P}_{i,j}\) is the pressure drop across the channel at each zone \((i,j)\), \({\varepsilon }_{i,j}\) is the void fraction representing open frontal area at each zone, \({\mu }_{{g}_{i,j}}\) is the exhaust gas viscosity, \({K}_{i,j}\) is the fanning friction factor, \({\Delta L}_{i,j}\) is the axial length of the channel at each zone, \({\dot{V}}_{i,j}\) is the actual volumetric flow rate of the channel, \({CFA}_{i,j}\) is the frontal area at each zone, \({D}_{h}\) is the hydraulic diameter of the channel, \({C}_{{f}_{i,j}}\) is the skin friction coefficient, \({R}_{{e}_{i,j}}\) is the Reynolds number, \({\tau }_{wall}\) is the wall shear stress, \({\rho }_{{g}_{i,j}}\) is the gas density, \({u}_{{g}_{i,j}}\) is the exhaust gas velocity, \({D}_{h}\) is the hydraulic diameter of the channel and \({\mu }_{{g}_{i,j}}\) is the exhaust gas viscosity.

Appendix 3 d-CSC Model Calibration Parameters Summary

Tables

Table 9 Temperature solver calibration parameters – Single set for all experiments

9,

Table 10 Species solver calibration parameters – Single set for all experiments

10,

Table 11 Species solver calibration parameters – Varying based on storage capacity of the d-CSCTM

11

Appendix 4 Model Discretization Study – 3 × 3, 4 × 4 and 5 × 5 Models

The d-CSCTM temperature varies axially and radially as shown in Figure 14

Fig. 14
figure 14

Experimental temperature distribution for S250/R350 experiment at 108 min (2 min after the start of Phase IV)

14 for S250/R350 experiment. The experimental axial temperature variation is upto 12°C and the radial temperature variation is about 8°C. The simulation of axial and radial temperature distribution is necessary to accurately capture the storage and release charecterstics of the d-CSC. Based on the experimental data presented in Section 5 of this work, the 20°C variation in temperature could alter the 200-second storage capacity by 0.06 gNO2/L.sub (in 200-250°C storage temperature range) and release capacity by 0.08 gNO2/L.sub (comparing S080/R300 and S150/R200 experiments). Hence, in order to capture the temperature dependent storage and release charecterstics accurately, axial and radial distribution modelling is necessary. However, the higher level of model discretization increases the computational time. From earlier research by same authors, the computational time varies linearly with the number or elements used in the model [22]. In case of an 1-D 3x1 model (3 elements in total), with 3 axial discretization and 1 radial discretization, the computation time is 1/3rd of the 3x3 2-D model with 3 axial and 3 radial discretization (9 elements in total). Comparing 2-D 3x3 discretization with 2-D 10x10 discretization, 10x10 discretization will be 11 times slower than 3x3 model. The 3x3 d-CSC model used in this work for S250/R350 experiment took 70 hours to simulate 1.3 hours of test data. Hence, considering the accuracy and the computational time, the 3x3 axial and radial discretization was selected for 2-D d-CSC modeling presented in this research. The comparison of experimental and model temperature distribution for S250/R350 experiment at 3x3,4x4 and 5x5 discretization levels are shown in Figs. 14,

Fig. 15
figure 15

Model temperature distribution for S250/R350 experiment at 108 min (2 min after the start of Phase IV) – 3 × 3 Discretization

15,

Fig. 16
figure 16

Model temperature distribution for S250/R350 experiment at 108 min (2 min after the start of Phase IV) – 4 × 4 Discretization

16 and

Fig. 17
figure 17

Model temperature distribution for S250/R350 experiment at 108 min (2 min after the start of Phase IV) – 5 × 5 Discretization

17, respectively. The model discretization plots in Figs. 15, 16 and 17 shows that the 3x3 model is able to capture axial and radial distribution similar that of 5x5 model. Comparing 3x3, 4x4 and 5x5 models, the maximum temperature difference is about 8°C at the outer most radius (dCSCTM length of 122 mm and dCSCTM radius of 124 mm) between 3x3 and 5x5 models. The max difference in 200-second NOx storage capacity is about 0.07 gNO2/L.sub and the total NOx release capacity is about 0.02 gNO2/L.sub compared to 3x3 model.

Figs. 14, 15, 16, 17

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Mahadevan, B.S., Berndt, C.T., Johnson, J.H. et al. Experimental and Modeling Study of NO and NO2 Storage and Release Characteristics of a Diesel-Cold Start Catalyst. Emiss. Control Sci. Technol. 8, 41–62 (2022). https://doi.org/10.1007/s40825-022-00208-7

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