design sr analysis catalytic converter -...
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Design & Analysis of Catalytic Converter
3.1 Design Aspects of Catalytic Converter.
The design of catalytic converters for 2-stroke engines requires a system
approach because of trade-offs involved in arriving at the optimum design.
The following requirements must be satisfied in designing the catalytic
converters:
01. Should provide enough surface area to meet conversion
efficiency requirement for both HC + N02 and CO.
02. Power loss due to backpressure created by the converter should
be minimized.
03. Should not interfere with engine operation.
04. Must meet durability requirements.
05. Heat generated by the catalytic reactions must not raise safety
converters.
06. Must fit in the available space.
07. Should be affordable.
3.2 Robust Design and Analysis of Substrate.
Robust design is a methodology that addresses product quality issues early in
the design cycle. The goal of robust design is to deliver customer
expectations at profitable cost regardless of customer usage, degradation
over product life and variation in manufacturing, suppliers, distribution,
delivery and installatton Since randomness and scatter is a part of reality
5X
everywhere, probabilistic design techniques are necessary to engineer quality
into designs Traditional deterministic approaches account for uncertainties
through the use of empirical safety factors. The safety factors are derived
based on past experience; they do not guarantee safety or satisfactory
performance and do not provide sufficient information to achieve optimal use
of available resources. The probabilistic design process has not been widely
used because it has been intimidating and tedious due to its complexity. In
this research effort, probabilistic modeling of manufacturing and material
variations for a catalytic converter substrate was considered. Typical shapes
of catalytic converter substrates are shown in Figure 3.1.
Figure 3.1 -Typical shapes of catalytic converter substrates
The substrate used in this study has a cylindrical cross section and is
enclosed in a cylindncal steel cover If the substrate is not a perfect cylinder
59
the steel cover applies a non-uniform pressure along the circumference.
Assuming that the maximum diameter of the substrate is Dmax and the
minimum diameter is Dm;n, we can characterize the variation in circularity or
roundness d with their difference
Due to manufacturing variations d is considered a random input variable.
Figure 3.1 Typical shapes of catalytic converter substrates In this study, it was
assumed that a Gaussian distribution with mean value md and standard
variation sd characterizes the variation in circularity d. Due to both material
and manufacturing variation the ultimate shear stress 'tult exhibits
randomness. A pure shear test was performed on several substrates to
determine the ultimate shear stress variation. The mean value of ultimate
shear stress is m'tult = 0.2868 MPa (41.6 psi), the standard deviation is S'tu1t =
0.01724 MPa (2.5 psi), the minimum value of the sample was ('tu1t) min = 0.255
MPa (37.0 psi) and the maximum value of the sample was ('tu1t) max = 0.31
MPa (45.0 psi).
The objective of this study is to identify the supplier specification (sd) max
(maximum standard deviation of variation in circularity d) in order to achieve a
robust design of a des1red sigma quality level.
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The Parametric Deterministic FEA Model
A parametric finite element model of the substrate is shown in Figure 3.2 and
was developed considering the following assumptions:
1. The material of the honeycomb ceramic substrate is isotropic,
linear elastic and the behavior is within small deflection linear
theory limits. The modulus of elasticity is E = 4800 MPa and
Poisson's ratio is 11 = 0.25.
2. Plain Strain Analysis is sufficient to accurately predict the
maximum shear stress.
3. There is no temperature effect on the material properties.
4. The geometry, loading and behavior are symmetric about the
horizontal and vertical axes, thus a quarter symmetry model can
be used.
5. The angle between the maximum and minimum diameter is 90°.
6. The geometry of the FEA model can be represented by the first
quadrant of an ellipsoid with the horizontal lower edge length
equal to F/2 + d/4, and the vertical left edge length equal to F/2 -
d/4, where F = 105.0 mm.
7. The maximum pressure Pmax (in MPa) is a function of .8 (in mm)
and can be computed by the following equation:
Pmax(o) = a5,)5 + a4 84 + a3 ,i3 + a2 &2 + a1 <i1 +aO
where:
ao = -0.8155
a1 = 5.5840
a2 = -8.3864
a3 = 4.0882
a4 = -0.0694
a5 = 0.0004
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Figure 3.3 shows a plot of this function (the maximum pressure
Pmax versus 6) and the data-points used for the curve fitting.
8. As shown in figure 3.2 the maximum pressure is applied at the
point of maximum diameter and varies sinusoidal to zero at the
point of minimum diameter:
P(fl) = Pmax *COS (8)
Figure 3.2 -Finite Model and Loading of the Substrate
·r- ----r--
'
'
'
0 ''
J v 1/
v _.,.. /
..,...,.,.. v -I 1 1 :! 1 1 I ,J 1 -. I 1, I (
s l11Hlll
Figure 3.3 Maximum Pressure P m" versus I>
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The input parameters of the model are variation in circularity d and ultimate
shear stress tu 11• For any combination of the input parameters the solution to
the parametric model can compute the maximum shear stress tmax- Figure 3.4
shows a typical distribution of the magnitude of the displacements and figure
3_5 shows a typical maximum shear stress distribution_
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1\N
Figure 3.4 Typical Displacement Distribution
1\N or;-.· • n"4
'·.:. }I
Figure 3.5 Typical Maximum Shear Stress Distribution
We define a performance function G as the difference between ultimate shear
stress and the maximum computed stress or G = tun -'tmax· If G remains positive
at all times we will have a safe design. The performance function G is
considered as the output variable and is a function of the input variables d and
3.3 The Probabilistic FEA Model
Uncertainty in the input parameters of the FEA model can be introduced by
assuming certain randomness in the input parameters. In this study, it was
assumed that a Gaussian distribution with mean value md and standard
variation sd characterizes the variation in circularity d.
The mean value md was considered uncontrollable or a noise parameter with
a constant value of md = 1.05 mm. The standard variation sd was considered
as a controllable parameter and it was declared as an optimization design
variable. For various values of the standard variation sd one may obtain a
distribution for d. Figure 3.6 shows the Probability Distribution of the input
variable 8 with a standard variation sd = 0.01 mm.
>. u
Histogram of Circularity Var tatwn,;; ·1'-',----,---,---,--..... -.---.---,---,
;; ,. lf----1--+--5-~
u. ''lif--+--+--,, -~ ~ Jl"··ll---t--+-;;; a:
"' Figure 3.6. Probability Distribution of the Input Variable 8
It was also assumed that truncated Gaussian distribution characterizes the
ultimate shear stress of the substrate material. The mean value of ultimate
65
shear stress mt .. 11 = 0.2868 MPa, the standard deviation S<ult = 0.01724 MPa,
and the range 0.255- 0 310 MPa were determined experimentally. Figure 3.7
shows the Probability Distribution of the input variable Stu11 with these values.
Ht"it(HJI :.m of Ult1matf! Shear Stress t\111
•,(·,------,-----, ~-~
llll11nate ShP.ar St1ess '••ll MPa
Figure 3. 7 - Probability Distribution of the Input Variable <ult
Since the two input variables are random the performance function G (where
G = (<u11 - (<u11) max) exhibits randomness and is considered the output variable.
H1stogram uf Pedormance Function G for a6 = 0.01mm
• .!,-1 c------+---+----1--t--
., ' ,,.-,, ., ,-, F·
Perfor manc.e Func.t!Oil G MPa
Figure 3.8 Probability Distribution of the Performance
Function G for Standard Variation 0, = 0.01 mm.
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H~-:>IOUI am of PelfOIITii'lllCP. Funct1011 G foro~= 0.05 mm
1_1 '.
"' ', f ~--11----11--~t--
gLc-,~~.,"7,,~~- 0(J5 •J1 (I~' Perf01 manca- Function G MPa
Figure 3.9 Probability Distribution of the Performance
Function G for Standard Variation cr, = 0.05 mm.
Monte Carlo and the Central Composite Design response surface sampling
techniques were implemented in determining the response distribution of the
output variable for various values of the standard variation cr,. The probability
distribution of the performance function G for standard variation cr, = 0.01 mm
is shown in Figure 3.8. The mean value of the performance function is m0 =
0.08312 MPa and the standard deviation is Sc; = 0.01521 MPA. One may
observe that the entire distribution of the performance function G remains on
the positive side, indicating that for cro = 0.01 the maximum shear stress does
not exceed the ultimate shear stress. In this case the probability that the
performance function G is less than zero is 0 %, P[G<O] = 0%. Figure 3.9
shows the probability distribution of the performance funct1on G for standard
variation n,, = 0.05 mm The mean value of the performance function is mG =
0.07849 MPa and the standard deviation is sG = 0.04026 MPa. One may
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observe that part of the distribution of the performance function G remains on
the positive side indicating that for cr0 = 0.05 the maximum shear stress
exceeds the ultimate shear stress. The area to the left of the zero (red line)
indicates the probability of failure. In this case the probability that the
performance function G is less than zero is 4.24 %, P[ G< 0]:: 4.24%.
3.4 Further Analysis Of Substrate
If the catalyst coating is the same, the first three design considerations
depend on substrate parameters. Higher cell density is desirable from a
conversion efficiency point of view. However the pressure drop, i.e., power
loss, will be greater with higher cell density Table-3.1, show the values of
geometric surface area and flow resistance parameters for different cell
density. It was found that 100 cells/in2 is an optimum cell density for
motorcycles to meet surface area and pressure and requirements.
Table 3.1: Geometric Surface Area and Flow Resistance Parameters.
I Cpsi !Wall thickness GSA RF i I
I Cell/in2 ! M2/m3 1/m2 :Mm
I
I
I
[100 , ______
i 0.30 1386 7.34 I ' '200 ! 0.20 1975 14.23
' I
350 ' 0.14 2643 23.79
'
400 : 0.17 2740 30.74 ! I
6X
Once the cell density is chosen, the next step in the design process is the
selection of the size and aspect ratio of the ceramic substrate. Typically the
volume of the ceramic substrate for motorcycle application ranges from 75-
200 ml depending on the size of the engine and available space. If the
substrate volume and cell density is held constant, the aspect ratio of a
cylindrical converter affects the pressure drop in the following manner.
Pressure drop a L/02
Where, L and D are substrate length and diameter, respectively. The aspect
ratio is also important in determining the mat/substrate contact area, which is
important in determining the holding force provided by the mat for cylindrical
converters, at constant volume. The mat contact area decreases with
increase in diameter of the substrate. Depending on the available space and
location of the converter, the aspect ratio (LID) of motorcycle converters can
vary from 0.8 to 2.5.
3.5 Durability
The durability of a catalytic converter can be limited by either the catalyst
durability or the phys1cal durability of the converter package. Factors that
determine catalyst durability are
01 Temperatures w1th1n the converter
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02. Impurities in the fuel and lubricating oil.
03. Wash-coat composition and method of application composition and
distribution of precious metals within the wash-coat
04. Geometric surface area of the converter.
The temperatures within the converter of a 2-stroke engine can reach 1050°C
due to exothermic heat generated by the oxidation of hydrocarbons and CO.
State-of-the-art catalysts can withstand this temperature for short duration
(@25 hours). The catalyst loses its activity due to loss of surface area of the
wash-coat Sometimes chemical interactions between the precious metals
can also lower the activity of the catalyst Therefore, it is necessary to
minimize temperature excursions within the converter to maintain longevity of
the catalyst coating. If the temperatures within the converter are maintained
below 900°C, it is possible to obtain long-term durability in motorcycle
application. This assumes that the impurities in the fuel and lubrication oil do
not deteriorate the catalyst
Physical durability, i.e., the converter's ability to withstand thermal and
mechanical stresses, is an important consideration in determining its life. The
parameters that determine the physical durability of the ceramic catalytic
converter are:
01. H1gh temperature physical properties of the ceramic substrate
02 The magnitude of the holding force provided by the mat
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03 Mat durability
04. High temperature creep resistance and thermal expansion of the
stainless steel can
Strength, thermal expansion coefficient and elastic properties are the main
physical properties that govern the durability of the ceramic substrate. The
physical properties of the ceramic substrate (EX-22) are given in table 3.2 and
figure 3.1 0. For comparison, the high temperature strength behavior of
metallic substrates is shown in figure 3.11. The biaxial compressive strength
of the ceramic substrate is ten times greater than the radial compressive
stress imposed by the mat (500 KPa), and therefore, the failure of the
substrate due to mechanical loads is not a significant concern. The same is
true with respect to thermal stress failures.
Table 3.2. The physical properties of the ceramic substrate
,.---··· ·-,. Thermal Expansion RT-1000°C (10 -7f'C) Elastic Modulus (GPa)
1000°C 1100°C
I Density (g/cc) I l_l3iaxial Strengtll (f<.i=>_a_l __j
-- --
Substrate
Bare With
Catalyst 5.2 10.4
9.3 13 14.5 18
, I 0~51 0.8 i 6500 i
--- ----
., 7
~ 6 ;; 5
"' c: 4 ~ Ul 3 iii 2 ~
;l 1 Q)
iL 0
Axial direction
~ .--.
..._<:><:> n,<:><:; ""<:;<:;
Temperature (oC)
71
I
___... _._...
' ' ! I
Figure 3.10: High temperature strength behavior of EX-22 ceramic
substrates .
., 800 ~ 700 ;; 600 c, 500 c: ~ 400 Ul 300 .21 200 ·~ 100 ~ 0
0
I
""' I
""-. ' ' """-. ' " I
\ I \. I
~ I
500 1000 1500 Temperature (oC)
Figure 3.11: High temperature strength of metal substrates.
The Magnitude of thermal stresses depends on the temperature gradient
across the substrate. thermal expansion coefficient, elastic modulus and
Poisson's ratio of the coated substrate. Since the size of motorcycle
converters is much smaller than the automotive converters, the temperature
gradients w1ll be lower. Failure of the substrate due to thermal stresses in
motorcycle application is unlikely because ceramic substrates have been
performing reliably for the last 20 years in car application. As mentioned
earlier, the temperatures inside the catalytic converter of a 2-stroke
motorcycle can reach 1 050°C. For satisfactory performance, the high
temperature strength of the substrate must be adequate, As seen from the
data in figure 3.10 and 3.11 the ceramic substrate maintains its strength up to
1200 °C. Whereas the strength of the metallic substrates drops significantly
above 600 °C. Distortion of the cell walls can occur if the high temperature
strength is not adequate. Cell distortion can increase pressure drop across
the convector, which in turn causes an increase in power loss of the vehicle.
Another issue that needs to be addressed is the sudden rise in converter
temperature due to unburned fuel entering the converter. The melting
temperature of the substrate should be high enough to withstand the
temperature rise. The melting temperature of the substrate should be high
enough to withstand the temperature rise. The ceramic substrate (EX-22)
melts at 1465'c which 1s 400'c higher than the maximum allowable
temperature for the catalyst.
3.6 Mat
Because of the large thermal expansion difference between the
substrate and the stainless steel can, a mat is needed to secure the ceramic
substrate in the steel can. The mat must exert enough radial force on the
7.1
substrate to hold it in place in the exhaust enVIronment of a 2-stroke engrne. It
is possible to estimate the forces on the converter due to chassis vibrations
and pressure drop across the converter. The total force, F on the ceramic
substrate in the·direction of gas flow is given by
F=W (V/G) + PA --------- (1)
Where W, is the mass of the coated substrate, V is the maximum
vibrational acceleration experienced by the ceramic substrate, G is the
gravitational acceleration. P is the backpressure, and A is the cross sectional
area of the substrate. If one assumes V as 120 G and P as 30 g/cm2 (30 em
of water). the maximum force on a 55 x 40 mm long substrate is 96 N. The
shear stress at the substrate I mat interface due to this force is 14kPa. The
radial stress. i.e .. holding pressure to be provided the mat can compute p,
computed from the shear stress and the coefficient of friction, ftJ. p =shear stress I j.l------------- (2)
Assuming mas 0.2. the minimum radial pressure to be provided by the
mat is 70 kPa. It will be shown later in the paper that non-intumescent mats
can provide the necessary holding force. Before moving to design aspects of
the stainless steel can. rt is necessary to mention that the forces generated on
the substrate would be much higher if the vibrational frequencies encountered
by the converter coincrdes with the resonance frequency of the conversion.
The vibrational frequencres encountered by the converter can be measured
by mountrng accelerometers on the surface of the steel can.
7-1
3.7 Stainless Steel Can
The steel can is exposed to high temperatures because of the heat
generated within the converter. It is necessary to select steels that have low
thermal expansion coefficient and excellent creep resistance to maintain the
holding force provided by the mat. The holding force can decrease if the steel
shell expands too much or if the steel undergoes permanent deformation.
Ferrite stainless steels 409 and 439 are commonly used for catalytic converter
cans. The thermal expansion of this steel is 30% lower than 300 series
stainless steels. The yield strength of these two alloys at different
temperatures are given in table 3.3. The hoop stress generated in the steel
can depend on the radial pressure provided by the mat, the diameter of the
can and thickness of the can. For circular cans, the hoop stress, a is given by
0 = p d,J 2 t -----------------(3)
Where p is the radial pressure exerted by the mat, d is the diameter of the
substrate and t is the thickness of the steel can. Assuming p= 700 kPa, d=60
mm and t=1.2 mm, the hoop stress in the steel can is 17.5 Mpa. The yield
strength data in table 3.3 indicate that the permanent deformation at 17.5 Mpa
will be negligible up to 800oC for 409 steel and up to 875oC for 439 steel. In
most cases, the motorcycle catalytic converters are mounted inside the
mufflers and therefore. the skin temperature of the converter can reach 700-
800oC 1n 2-stroke veh1cles
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Table 3.3: Yield Strength of 409 and 439 Steels (Mpa)
Temperature °C 409 Steel 439 Steel ---- --
25 244.7 302.6
204 173.7 245.4
316 169.6 253.0
482 147.5 215.1
538 135.1 179.9
593 111.7 191.0
649 92.4 137.2
704 46.9 82.7
760 29.0 57.9
816 22.1 42.7
871 15.2 30.3
I 927 6.2 17.2
I , ___ --- ----
3.8 Results
The objective of this study is to establish that it is possible to achieve the
following performance targets using catalytic converters on 2-stroke
Motorcycles and scooters.
01. HC+ N02 and CO emission levels below 60% of year 2004 standard on
I DC. ie .. HC + No2 < 0.9 g/km and CO < 1.2 g/km.
02. Less than 5% power loss over the entire speed range
03. Must fit in available space without interfering with normal operation of
the b1ke
04 Meet the des1red on-the road durability.
7h
The progress made to date in achieving the above objectives will be
discussed in this section. Additionally, the results of several new tests that
were conducted to characterize the mat durability are also included in this
paper.
3.9 Emission Results
Engine out emissions from motorcycles and scooters in IDC vary considerably
depending on engine design, engine size, carburetor design, and air/fuel ratio.
The HC + N02 values of different vehicles can range from 3 to 6 g/km and for
CO from 1 to 7 g/km. Depending on engine out emissions, conversion
efficiencies greater than 60% are needed to meet the year 2000 emission
standards. Mass emissions tests were conducted on a 150 cc scooter and a
110 cc motorcycle using a chassis dynamometer. As prescribed, emissions
were collected over six measuring cycles after four warm up cycles. The
variables in the experiments were, cell density, size of the ceramic substrate,
catalyst formation. secondary air injection, catalyst location, carburetor
adjustment and a pre-converter to increase the exhaust gas temperature.
Tables 3.4 and 3.5 provide emission results obtained on these two vehicles
for the 11 o cc motorcycle, eight warm up cycles were used prior to emission
measurement although catalyst light off occurred in the fourth cycle.
Table 3.4: Emission Test results of 150 cc Scooter:
Conversion Efficiency
f.--------Baseline (engine out)
Idling CO at 0.62%
Idling CO at 1.2%
·-----
---+---
--
HC c 0
g/km g/k m
3.07 2. 63 --------
1.1 0. 70
1.1 0. 90
(%) ---- --
HC
-----
--
64
64
Table 3.5: Emission Test results of 110CC motorcycle:
HC (g/km)
----------· Baseline (engine out ) with 100 cpsi, 55 x 40mm 5.65
..
1.69 1------------Catalyst
1----- -- - . - --~-Conversion Efficiency (%) 70
--
-- - -----
co
---
74
66
co (g/km) -
1.2
0.54
55
77
It can be seen from these results that both HC and CO emissions were
reduced significantly using ceramic catalytic converters. The emissions levels
of N02 in 2-stroke engines are generally bellow 0.02 g/km and therefore, is
not a big concern. The emission data in table 4 suggests that carburetor
adjustments in idling condition can affect CO conversion efficiency.
The em1ssion levels of the 110 cc motorcycle could not be reduced below the
year 2000 standard because of higher baselme HC emissions an limited
catalyst volume By mcreasing the size of the catalyst or by secondary air
injection, it should be possible to reduce HC emissions of the motorcycle to
year 2000 standard.
3.10 Power Loss
The power of 2-stroke engines is very sensitive to any modifications in •
the exhaust system. Two-stroke engines do not have valves and therefore,
the backpressure created by the catalytic converter can interfere with engine
operation. Since vehicle power is an important performance parameter, the
installation of a catalytic converter in the exhaust system should ideally have
minimal effect on engine power. Realizing that the vehicle power can vary as
much as 2% due to statistical variations in muffler dimensions, it was decided
that the power loss due to the catalytic converter should be less than 5% over
the speed range of the vehicle.
The vehicle power was measured on a chassis dynamometer for both the 150
cc scooter and the 110 cc motorcycle. The scooter had two catalytic
converters in the exhaust system one small converter closer to the exhaust
port to raise the gas temperature to light off the main catalyst. Note that the
emission results in table-4 were obtained with a similar catalyst arrangement.
The power of the motorcycle was measured with a converter, which had a 55
x 40 mm 100 cell/in 2 substrate Figures 3.12 and 3.13 show the change in
engine power at drfferent speeds due to the catalytic converter. In these
graphs. values above zero represent power gain and values below zero
represent power loss
7'1
~ .. 8 ;: 6 0 a. 4 • .. .!: 2 • • Cl-
.TI~ 0
.!: -2 'V ,..,. 0 .. -4 Cl
t:
"' -6 .t: u -8
• I • •
Speed (km/h)
Figure 3.12: Power loss of 150 cc scooter with ceramic catalytic
converter.
~ 15 . . .. .. "' ;: 0 10 a. "' = 5 m_ =~ W'!... • • I <: 0
"' Cl -5 <:
• ~ 20 40 liP 100 120 1 0
"' .s;:: 0 -10
Speed (km/h)
Figure 3.13: Power loss of 110 cc motorcycle with ceramic catalytic
converter.
For both vehicles the power loss varied with vehicle speed. Note that at
certain speeds the veh1cle power was greater with a catalytic converter. With
the exception of one speed, 40 km/h for the scooter and 85 km/h for
motorcycle. the power loss target of 5% was met for both vehicles. These
results suggest that by JUdicious selection of catalyst location cell density size
xo
an aspect ratio of the substrate ceramic catalytic converters can be installed
with minimal effect on vehicle power.
3.11 Durability Of Ceramic Converter
Several aspects of the catalytic converter need to be considered to achieve
the required durability. The first one is the deterioration in conversion
efficiency. Conversion efficiency depends on factors such as the maximum
temperature within the converter, the impurities in fuel and lubricating oil, and
geometric surface area. In addition to these, the change in engine-out
emissions due to deterioration of carburetor and spark plug performances will
determine the overall effectiveness of the catalytic converter. It is necessary
to utilize a system approach in prolonging the life of catalytic converter.
Taiwan manufacturers have shown that the catalytic converters can be
durable up to 15,000 km by conducting road tests on 2-stroke motorcycles.
Long-term durability is expected to be better with ceramic catalytic converters
because of superior wash-coat adhesion.
The second aspect of durability is the mechanical integrity of the catalytic
converter. Thermal and vibration conditions that prevail in the exhaust system
of 2-stroke engines can cause cell wall deformation failure of joints at the cell
junctions or separat1on/slid1ng of the honeycomb substrate from the can. In
hot vibrat1on tests (1 050 °C and 75g's) conducted, at the Southwest Research
Institute. d1stort1on of cell walls was observed in metallic substrates. This
XI
deformation of cell walls increased the pressure drop by 30%. Since
temperatures as high as 1050 °C were measured inside the catalytic
converter of the
Kanthal heating Force
element
~-~···at
Thermocouple location Substrate
Figure 3.14: Ceramic converter with heating elements.
110 cc 2-stroke motorcycles, cell deformation can be an issue with metallic
converters. In the case of ceramic converters, cell deformation does not occur
up to 1200 °C.
Separation of the honeycomb substrate from the stainless steel can could
occur due to the failure of brazed joints in the case of metallic substrates or
due to mat failure in the case of the ceramic substrate. To assess mat
durability. three different laboratory tests were employed. The converter was
heated by installing electric heating elements in the periphery of the ceramic
substrate (85 x 80 mm ) as shown in figure 3.14 A tourniquet method was
used to mount ceramtc substrates in 409 stainless steel cans. Temperature
was measured in the outermost cell half way into the substrate, figure 3.15 A
heat shield was provided around the converter to raise the can temperature.
In all the tests, substrate/maUcan interfaces were subjected to shear stress by
applying a load to the substrate in the direction of the honeycomb channels. A
linearly increasing load was applied in the first test to measure the maximum
load required to push the substrate out of the can (high temperature shear
test). In the second test, a static load (45.5 kg) was applied for 100 hours
(static fatigue test). The shear stress at the substrate/mat interface due to this
load was 20.8 KPa. In the third test, a cyclic shear stress was
Shear strength
Static fatigue
Load Cyclic fatigue
Time
Figure 3.15: Schematic load-time curve in the three laboratory
tests.
Applied to the substrate/mat interface to simulate the cyclic nature of vibration
loads (cyclic fatrgue test) The three loading patterns used in these tests are
illustrated m figure 3 15
The effect of temperature on the shear strength of the ceramic converter
package, i.e., the maximum shear stress required to push the substrate out of
the can, is shown in figure 3.16. With increasing test temperature, the shear
strength of the converter package decreases. The decrease in the elastic
properties of the· mat at elevated temperatures is the primary reasons for the
observed decrease in shear strength. The maximum expected shear stress is
14Kpa from the data in figure 3.16 it is evident that the measured shear
strengths are higher than the design stress by more than a factor of 2.
1\ 100 : 90
;;:_ 80 -"' 70 J::: 60 c, 50 t: ~ 40 y; 30 :;; 20 ~ 10 rn 0
-. i f-.
' i
"' l ~
···~
' ~ l
"~ i
""· ' ·~ ~ .. ~
'
~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~
Substrate Skin Temperature (oC) ·->
Figure 3.16: A Graph of Shear strength Vs. Temperature (0C).
Static fatigue tests were conducted at 900'C and 1 050'C by applying a
constant shear stress of 20.8kPa. This stress is 50% higher than the design
stress. Five specimens were tested at each temperature. To make the test
more severe. the converter was cooled to room temperature every 10 hours.
The test was discont 1nued 1f the substrate slipped or when the total test time
X·l
The test was discontinued if the substrate slipped or when the total test t1me
reached 100 hours. Substrate slippage did not occur at this stress level up to
1 OOhours at both the temperatures. To assess mat degradation, shear
strength of the ·fatigued specimens was measured at 550'C under isothermal
conditions using a furnace. Figure 3. 17 shows shear strength of the converter
package before and after the static fatigue test. The degradation in the initial
shear strength of the converter package is less than 8%, indicating that the
mat is durable.
A triangular wave load cycle at a frequency of 1 Hz was used in the cyclic
fatigue tests. At 900'C three specimens were cooled to room temperature at
10 hours intervals. The tests were stopped at 100 hours and as before the
residual shear strength were measured at 550'C. No degradation in the shear
strength of the converter package was observed after the 900'C cyclic fatigue
tests. Tests were also conducted at 1050'C under a stress cycle of -15.6 to-
15.6 KPa and the specimens survived for more than 1.3 million cycles (>360
hours) without slipping from the can.
Total time= 100 h
I) _:_ 40 "' ~ 35
~ .30
~ 25 Ol)
ro 20
£ 15 Ol
~ 10 ~
ii) 5 ~
~ 0 .<: (f)
" " " ' " " " , . ,,
. <:> .._<:><:> <f'<:> .,~:~<:> ~<:> .,~:~~:~ ro<:><:> '\~<:> co<:>~ o,<:><:> <:><:><:>
" Substrate Skin Temperature (oC) -->
Temperature cycle = 1 0 h on /1 h off.
X'i
I .
" I
Figure 3.17: Shear strength of ceramic converter package
before and after static fatigue test.
The above data suggest that the mechanical integrity of the ceramic catalytic
converter is adequate to withstand the thermal and mechanical stresses
present in the exhaust systems of 2-stroke motorcycles and scooters.
Another issue that needs to be discussed is the rise in temperature of the
exhaust gases due to exothermic heat generated in the converter. Depending
on the speed of the veh1cle. the rise in exhaust gas temperatures can be 250-
400'C. The temperatures on the surface of the exhaust pipe can reach 700-
sso·c especially 1n w1de-open throttle condition For safety reasons these high
temperatures need to be Isolated from the passengers and the vehicle
footboard Additionally tt1e m1ld steel that 1s used in most exhaust systems
will not last long at these temperatures. It is therefore, necessary to use
stainless steel exhaust pipes with heat shields to address durability and safety
concerns.
3.12 Turbulent Catalysts
Mass transfer for regular catalyst shows a laminar flow after intrusion in the
catalytic converter after a short time. If the change in the metallic substrate
allows the change from laminar flow into turbulent one, longer residence time
and more unconverted gases from the core of the channel come closer to the
catalyst surfaces and more reaction takes place. The higher flow velocity
corresponds to a higher mass transfer. The correspondence between flow
velocity and mass transfer is shown in Figure 3.18.
r1~" ,.,;;n, lt•·'l.~., ...
Figure 3.18: Flow velocity- Mass transfer diagram
The scope of work m this publication covers the analysis of turbulent catalyst
with transversal foil structure (TS) and longitudinal foil structure (LS) with the
focus for use in 2 & 3 wheeler vehicles
X7
3.13 TS- Structure
Transversal Foil Structure (TS) catalyst is the second generation of metallic
substrates. The first generation had straight and unstructured channels. This
TS design is · commercially produced and widely used in regular mass
production for automobile application. In this type, the corrugated foils are
embossed with secondary micro- corrugations (Figure 3.19), which are
provided transverse to the direction of flow i.e. at 90 degree to the flow
direction (see above described mass transfer to the wall).
Figure 3.19: TS structure design with flow details
These micro-corrugations help intense exchanges of unconverted gases in
the core of channel with the converted gases close to the walls.
3.13.1 LS- Structure
Longitudinal Structure (LS) is the third generation of metallic substrate
structure. which has been developed by EMITEC. In the LS design the
corrugated foil is characterized by additional cuts and depressions to provide
shovel like shapes (Figure 3.20)
Figure 3.20: LS structure design with flow details
These counter corrugations projecting into the basic channels create the
effect of additional channels within the same given volume, which results in
turbulent mass transfer to the channel walls and an increased catalytic
reaction . Thus, without increasing the actual surface area of a catalyst, a
higher catalytic efficiency is achieved by the LS design.
3.13.2 Test Bench Analysis
During stationary and dynamic tests catalysts with applied TS as well as LS
metallic substrate structure have been analyzed. To exclude the influence of
production, all converters were preconditioned 4 hours under 950°C ambient
air.
Converters with dimensions as defined in table beneath were analyzed on test
bench:
~
c:~ J::. f,-.
0 a: ~ 0 al 0 £ > _ _, ... (l_
II) )( ;;; :1 Q) ~ U> c: '- a. u f g; c: .... I) 2 ::;) ~ ~ ii E - iii <.) nl "" Of > 0 Q
cu (,) _, §,
33x60 100 Std 5 1 . 4 1 25
33x60 100 TS 51 . 4 1 25
3311:50 8 100 TS 43 -15 •(; 4 I 25
33x508 100 LS 43 - 15% 4 1 25
Table 3.6: Dimensions of tested catalytic converters
All substrates had the same diameter, cpsi, coating and loading. For
analyzing the influence of the structure in combination with the substrate
length, two shorter metallic substrates were applied. Besides, the benefit of
15% reduction· in substrate volume could be achieved. All catalysts were
conditioned at 950°C, 4h in ambient air.
3.13.3 Stationary Measurements
The main task of the engine test bench analysis was to define the exact
conversion rates for several lambda values and different engine speed and
load. Lambda is defined as the actual air-fuel ratio divided by the
stoichiometric air-fuel ratio. If e is smaller than 1, the engine runs with air
deficiency or rich mixture, if e is more than 1, the engine is running lean. The
definition of lambda is shown in the equation below:
[ J -AFR AFR st =e Equation 1: Lambda e................ . . . . ........... lambda[-] AFR ........... air-fuel ratio in the cylinder[-] st AFR ......... stoichiometric air-fuel ratio[-]
Thus a 50cc 4-stroke engine with a free applicable ECU with the possibility to
focus on the selected operation points was mounted on the test bench (Figure
3.21 ).
Figure 3.21: Engine with special exhaust system mounted on engine test bench
The engine configuration is listed in Table 3.7.
Prototype 1 cyhnder 4 stroke eng1ne
Displacement {cm3] 49.8
Bore x Stroke [mm) 40 X 39.8
Compression ratio f ·) 11.1
Coohng system 1quid
v'alve tra.n ~ Valves , OHC. chair
Carburet1on [:-uel inJe~t1on
Table 3. 7 Engine operation points driven on engine test bench
90
In addition, a special assembly of the exhaust system to meet all the
measurement conditions was designed. An important requirement was the
possibility to measure the exhaust gas components before and after the
catalytic converter at the same time during engine operation. Thus, special
heated exhaust pipes, for simultaneous measurement before and after the
catalytic converter, were applied between the exhaust system and the
exhaust gas analyzer. The temperatures before and after catalyst were
examined in the same areas In Table 3. 7 representative engine operation
points, as driven on the engine test bench, can be seen. These points
91
represent the most common operating engine speed and load points for a
scooter vehicle during the ECE-R47 homologation cycle.
Lambda Eng1ne speed [rpm) • BIJIEP fbar)
0.9 5000 rpm - B bar 7000 rpm - 8 bar
1.0 5000 rpm - 8 bar 7000 rom - 7 bar
1.1 5000 rpm - 8 bar 7000 !pm - 5 bar
Table 3.8: Map points for stationary measurements Lambda 0.9
The results of rich operation points represent acceleration phase of 2 & 3-
wheeled vehicles. Turbulent catalysts with different substrate lengths were
compared with the standard catalyst between 5000 and 7000-rpm engine
speed. The standard catalyst shows moderate conversion rates for all three-
emission factors at 5000-rpm operation point (Figure 3.22). Turbulence in the
substrate improves the conversion efficiency for more than 100% in the case
of HC and CO emission factors. Even better conversion rates are represented
for NOx, where a conversion rate of about 50% can be reached. The best
results are presented for the 0 33 x 60 mm catalyst with
TS substrate.
Figure 3.22: Conversion rates 5000 rpm I 8bar I Lambda 0.9
92
Figure 6 shows the results of the 7000-rpm rich operation point. The best HC
conversion is achieved by TS 0 33 x 60 mm substrate all other turbulent
substrates show lower conversion rates. A conversion improvement for TS as
well as LS substrate is seen for the CO and NOx emission factors.
J ~·
§ro~~~~L---------~ !~.~ -~--------------~~ B~r-------------~~ ~ 04-t------------~ >Jt-------------8 tot--.,.----
Figure 3.23: Conversion rates 7000 rpm I 8bar I Lambda 0.9
In general, all conversion rates for rich operation points could be improved
with the turbulent catalysts. The eye-catching improvement is visible for the
NOx conversion rates.
3.13.4 Lambda 1.0
Lambda 1.0 is a typical operation point for the 20-km/h sections in the ECE
R47 homologation cycle (see Figure3t~). This driving point has about 32%
share of the emission factors in the homologation cycle. Standard catalyst
reaches approximately 30% conversion rates for HC and CO, whereas all
turbulent converters exceed these conversion efficiencies (Figure 3.24).
Compared to lambda 0.9, all catalysts reach much higher conversion rates for
HC and CO. NOx conversion for turbulent substrates reaches remarkable
60%. Conversion Rates: 5000 rpm I 8 bar
93
Lambda=1.0
Preconditioned: 4h I 950°C Ambient Air Ageing
Figure 3.24: Conversion rates 5000 rpm I 8bar I Lambda 1.0
A similar behavior than at the operation point with lambda 1.0 and engine
speed 5000 rpm and at lambda 1.0 I 7000 rpm operation point (Figure 3.25)
can be observed. Higher conversion efficiencies were reached for all three
emission factors.
~
j~~~~~~~---=·
•"'!-------., t. t----=.----=-~:AJ ~ P' ~ " ..
Figure 3.25: Conversion rates 7000 rpm I 7bar I Lambda 1.0
Also at this operation point the TS 0 33 x 60 mm substrate shows the best overall
conversion efficiency, compared to other converters.
3.13.5 Lambda 1.1
Engines mounted in a scooter vehicle usually reach their break away point at
lean engine operation to allow use of oxidation catalysts. Therefore these
results represent typical engine operation at wide-open throttle and break
94
away point. The conversion rates for HC and CO show respectable results.
Compared to the standard catalyst (Figure-3.26), TS 0 33 x 60 mm substrate
reaches 25 % improvement of conversion efficiency. The NOx conversion of
TS and LS substrates stagnates.
Figure 3.26: Conversion rates 5000 rpm I 8bar I Lambda 1.1
In the case of high engine speed and lean operation (Figure 1 0), high CO
conversion is representative for all catalysts. Moderate NOx conversion for
two turbulent 0 33 x 50.8 mm substrates can be seen. TS 0 33 x 60 mm
substrate shows much higher HC conversion rates than the standard one.
:! ~~~:=L--1-=--------j " ,.,~-IIJ----
" -~------=--t~+--~ i"
10
Figure 3.27: Conversion rates 7000 rpm I 5bar I Lambda 1.1
It can be stated, that the turbulence in the channels (TS substrate) improves
the overall efficiency of all operating points about 33% at the same substrate
length compared with standard substrate. Shorter TS substrate (0 33 x 50.8
mm) shows similar or slightly better conversion rates than the standard one.
95
LS substrate with 0 33 x 50 8 mm d1mens1ons enhances the convers1on
efficiency compared to the same-dimensioned TS substrate.
3.13.6 Turbulent catalyst backpressure
Exhaust gas mass flow of the small capacity engines rarely reaches values
over 20 kg/h. FigureJ~9 shows, that the backpressure for these values is the
same for turbulent as well as for standard substrates. The backpressure for
significantly increased mass flow values shows a disadvantageous
backpressure behavior of turbulent substrates. No increase in fuel
consumption would be observed for turbulent structures.
,_ , ~ ..; ti • ·•: '" .:br>: ,;ul J
-~ '\; : ~A:;.,, r~ I _/ . 1 ' ·II ( "\
v / 1 .---/_ I ~
/ .L---1 ~ . ' > •
:-""' Ui) ..:4 ~ .... , ... ..I
~\oi!IV.Y ~., .. ~
Figure 3.28: Catalyst backpressure as function of the mass flow
3.13. 7 Dynamic measurements
The modified exhaust system, already used for stationary measurement, has
been ~pplied in a series 50cc 4-stroke scooter vehicle (Figure 3.29). The
technical data of the tested vehicle are presented in Table 3.9. The dynamic
measurements were carried out on a chassis dyno test bench with a Constant
Volume Sampling (CVS) device to detect the exhaust emission
characteristics.
Figure 3.29: Measurement setup for dynamic Tests
Series 50 cc vehJcle V•'ltl, 1 cyl1nder 4 stroke ~ncune (Eum 2 llomolooauon)
r=:arourellon system Constant pressure ca1 bttretor
::oolinq system Air !=>dl aust gas after Ox1dalion catalyst and reatment secondarv ah ~o'd start syslem Tf'lermo s,.~ltch ct ott:e
lr tans1russion CVT secondary gear •JehJcle reference
170 [kg] 1l8SS
Pov.·er ot.~lput 2. 54 [k!~\1 at 7250 [rp1'lj
1.4ea:l fuel con-surnptioo 111 the 42.7 [ktl/1) ht:Pnoloqabon cvcle Homologation Euro 2
.. . . . . . ..
Table 3.9: Technical data of the test vehicle
The standard ECE R47 driving cycle was used for the testing program, in
which the same catalysts were tested during the stationary measurements.
The complete homologation cycle ECE R4 7 consists of eight identical cycles.
The first four cycles are warm up cycles for the homologation
procedure and are at the same time used for sampling the
1)7
exhaust emissions for the hypothetrcal cold start phase for Euro 3. The
complete ECE R4 7 homologation cycle rs shown in Figure 3 30
r: .... , , ........... ••a ·~·::~:..·,-..:.~.~~ .. . .. - ........... -.-· ,...., ,..., ,..., ,...., ,...., ,..... ,...,
! .. I ~
! -~
t ~· 1 l l ...., ....,
l 1 '1 .. . • ,,., , ... .;., • ,., ..
...... f .. c:
Figure 3.30: ECE R47 homologation cycle with defined cold start phase
All emissions, measured separately for the warm and the cold start cycle, were
collected in the emission bags as well as recorded with an online measurement tool.
The emission factors (HC, CO and NOx), resulting of the bag measurements, were
analyzed for each catalytic converter separately. The online measurements provided
an insight into cold start behavior and allowed detailed analysis of the warm-up
phase for tested catalysts.
3.14 Measurement Result
The standard catalyst serves as basis for the comparison with turbulent converter. In
the cold start cycle slightly improved CO emission factors of the TS and LS substrate
(0 33 x 50.8 mm) can be seen. TS substrate with the dimensions 0 33 x 60 mm
shows the best CO emission factor of all substrates. HC+NOx are for both catalysts,
LS and TS with dimensions 0 33 x 50.8 mm, about 18% lower compared to the
standard catalyst. TS substrate with dimensions 0 33 x 60 mm shows 38% better
HC+NOx values than the standard catalyst.
'JX
Figure 3.31 : ECE R47 cold start cycle results
The emission factors in the homologation cycle (Figure 3.32) are limited according to
the Euro2 legislation to 1.0 g/km CO and 1.2 g/km HC+NOx. The focus of the
analysis was not put on the achievement of homologation limits, but to clearly point
out the difference in the catalyst performance. Due to the fact, that standard catalyst
exceeds the limited CO value, a standard catalyst without coating has been used to
make the analysis of turbulent catalyst possible. Nevertheless the standard catalyst
with coating reduces the CO emissions to the half and lowers the HC+NOx. The TS
and LS substrates with the dimensions 0 33 x 50.8 mm show moderately higher CO
values for both short type turbulent catalysts. As expected, the TS 0 33 x 60 mm
substrate shows a 48% better CO emission factor than the standard substrate and is
the only one that falls below the limited Euro 2 value.
Figure 3.32: ECE R47 homologation cycle results
1}<)
The HC + NOx factor of the 0 33 x 50 8 mm TS 1s 14% lower and of the 0 33 x 60
mm LS 32% lower in comparison with the standard catalyst TS substrate w1th the
dimensions 0 33 x 60 mm shows 21% improvement m HC + NOx conversion
3.14.1 Online recorder measurement
The online recorder measurement of lambda as function of the time is shown in
Figure 3.33. With this tool the exact duration of the cold start enrichment phase and
the calibration of the carburetion with secondary air induction were observed.
Furthermore, the predefined lambda values for stationary measurements could be
defined according to the dynamic measurements.
c=J'
'---~ --..- ----.-J . ~ ~ ~ • U
:...tf'-"
Figure 3.33: Lambda history in the ECE R47 cold start cycle
With the help of online measurement temperatures progression before and after
catalytic converter was recorded too. Delta T, presented as substitution between the
temperature after and before the catalyst, shows the starting time of conversion in
the catalyst, which directly impacts the cold start emission factors in the cycle. The
results show that the turbulent LS substrate starts the conversion after 150 s in the I
second cycle followed by the TS (0 33 x 50.8 mm) substrate. The standard
converter starts with conversion after 400 s in the fourth cycle. The eye-catching
100
effect is the peak of the delta T for LS substrate that is twice as h1gh as for the
standard converter, which can be traced back to higher turbulence in the substrate
channel and subsequently a higher mass flow to the substrate walls. The TS 0 33 x
60 mm substrate shows the highest peaks of delta T in the cycle. It starts with the
conversion at the same time as LS substrate.
Figure 3.34: Delta T flow during the ECE R47 homologation cycle
The fuel consumption in the ECE R47 homologation cycle can be seen in Figure
3.35. Due to the fact that similar fuel consumption values can be seen for all
converters, no influence of the turbulent substrates on the engine operation
compared to the standard catalyst was detected. This can be attributed to the
backpressure results, which are shown in Figure 3.28, where no significant
backpressure change at maximum engine mass flow (20 kg/h) was measured.
::
•. r . "
Figure 3.35: Fuel consumption in the ECE R47 homologation cycle