cngdeisel
TRANSCRIPT
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Development of CNG Direct Injection Diesel-Cycle Engine
Masaki Okada*Senior Specialist, Department No. 1, Engine Design and Development, Isuzu Motors Limited.
Co-researchers: Hiroyuki Sugii and Tetsuya Wakao, Isuzu Motors limited
John Cryer, Robbie Dickson, Buerebista Ursu, Westport Innovations Inc.
Abstract
Isuzu Motors Limited (Japan) and Westport Innovations Inc. (British Columbia, Canada), with support
from the New Energy and Industrial Technology Development Organization (NEDO of Japan) and theJapan Gas Association, completed the worlds first vehicle operating test for the compressed natural gashot surface ignited direct injection (CNG-DI) diesel-cycle engine, providing the feasibility of thetechnology for commercialization.
This project entitled The Commercial Development of High-efficiency, Ultra-low Emission CNG
Vehicles, was carried out from 2001 to March 2004. Objectives of the project were 1., to improvethermal efficiency by 25%or more over the Otto cycle; and, 2., to achieve at least 75% lower emissions
than the minimum standard at the time of initial low-emission regulations (ultra-low-emission vehicles;
ULEV)
The ELF was used as the base vehicle (load capacity: 2 tons) and succeeded in achieving these
objectives. The model vehicle participated in Michelins Challenge Bibendum 2003 in California andwon Gold Awards in the emission and fuel efficiency categories, and a Silver in the vehicle noisecategory, capturing the attention of domestic and international industry watchers with its close-
to-commercialization performance. The ELF uses a 4.5-liter diesel engine as its base engine, with apower and torque of 100kw/2200rpm and 500Nm/1000rpm, respectively. In this case the engine was
equipped with a 25 MPa common-rail CNG (mono fuel) direct injection system, an on-boardcompressor, hot surface ignition system, variable nozzle turbo, a urea-SCR catalyst (NOx reduction)
and an oxidation catalyst (HC reduction) for clean emission.
In the development, Westport provided full support for the fuel supply, ignition and associated control
systems. Many special features are incorporated in the engine. The natural gas compressor was used toraise the injection pressure up to 25 MPa. The natural gas injector uses a magnetostrictive actuator.Some unique features are incorporated in the part of the ignition system. To study the combustion
process, STAR-CD and WC-ERC (the University of Wisconsin-Madison Engine Research Center)program was employed. Today we are able to accurately reproduce the actual combustion on thecomputer.
Although we have overcome significant challenges, in the future, we aim for higher specific output
engines and better customer attributes (reliability, fuel economy, noise and vibration). Here I would liketo continue to provide actual data and present the benefit of the CNG-DI diesel-cycle engine.
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1. Purpose
Isuzu Motors Limited Carried out this project with support from Westport Innovations (prototype fuel,ignition and associated control systems). Moreover, many of development expense were supported bythe New Energy and Industrial Technology Development Organization and the Japan Gas Association.
Japans transportation sector has a very strong dependence on oil, at 98%, compared to other sectors,and the growth rate for oil consumption is also high. It is crucial for Japan, an energy-importing nation,to introduce and develop alternative energies for oil. Urban air pollution problems are driving the
need and the desire for clean natural gas vehicles. The currently available natural gas vehicles,however, are not comparable to conventional diesel vehicles in fuel consumption, a fact that is a major
obstacle to their general acceptance. From the perspectives of alternative energy development, low
emission and the prevention of global warming, it is therefore an important and urgent issue to developa natural gas vehicle with fuel consumption comparable to diesel vehicles as well as ultra-low
emission.
Based on the above, our objective was to develop a high-efficiency, ultra-low emission commercialnatural gas vehicle that would be an alternative to commercial diesel vehicles.
2. Study objective
The objective was to develop an engine with the following target values and demonstrate that it can bea viable alternative through tests using an actual vehicle with the engine.
(1) To improve the engine cycle efficiency by 25% or more:
Parameter for efficiency: CO2 emission Test gas = 13A
G-13 Mode Target for this project (Note) Conventional mixer system
Average emission (g/kWh) 640 or less 800
(2) To reduce emission by 75% or more of the maximum values allowed in the emission regulation at
the time of project commencement. (meeting ultra-low-emission vehicle requirements)
Test gas = 13A
G-13 Mode NOx CO NMHC
Average emission (g/kWh) 0.85 16 0.18
3. Roadmap to the targets
3.1 Different fueling systems of CNGFig. 1 shows different types of CNG fueling systems. They are divided into two major types: Otto
cycle and Diesel cycle. In addition, there are pre-mixing before cylinder input, In-cylinder pre-mixing,and injection immediately before combustion (or during combustion). Fig.2 shows our evaluation ofthe commercial viability of each type.
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0
20
40
60
80
100
0 20 40 60 80 100
Engine Speed (%)
Load
(%)
Idle
1,4
2
3
5
6 7
89
10
11
1213
G13 mode (g/kWh)
Production CNG VehicleProduction CNG VehicleProduction CNG VehicleProduction CNG Vehicleemission performanceemission performanceemission performanceemission performance
InitialInitialInitialInitial
CNG vehicle emissionCNG vehicle emissionCNG vehicle emissionCNG vehicle emissionGuideline 2000Guideline 2000Guideline 2000Guideline 2000
Test gas
OperatingStability
Fuel Economy Reliability/Durability
Cost Packaging Remarks
Carburetor type -
stoichiometric8 5 8 10 9
Efficiency is not great. Can use
TWC for low emissions.
MPI Type -
stoichiometric8 5 8 9 9
Efficiency is not great. Can use
TWC and has better emissions
than above.
Carburetor type -
lean 7 6 8 10 9
Improvement in efficiency, but
not as good as diesel. Stability
not has good, reliability not has
good, HC emissions can be an
Direct Injection
Type with spark
plug5 7 6 7 8
Improvement in efficiency over
all above, not as good as diesel,
not proven, lower r eliability
potential.
MPI Type with pilot 7 8 5 6 6
Efficiency is not great. Can use
TWC and has better emissions
than above.
Direct injection
Type with glow plug8 10 5 5 6
Improvement in efficiency over
all above. Needs optimization.
Very good potential for
efficiency. Single fuel.
Direct Injection
Type with pilot9 10 7 5 5
May have best potential for
reliability and efficiency, more
complex, more expensive, dual
fuel.
Otto CycleOtto CycleOtto CycleOtto Cycle Diesel CycleDiesel CycleDiesel CycleDiesel Cycle
Pre-Mixed Direct Injection
Mono-Fuel
Diesel Oil Pilot Glowplug ignition
Mixer SPI/MPI GDI Dual-Fuel
Fig. 1 Various Combustion Systems for CNG Fig.2 Technical Evaluation for Each Combustion
Systems
3.2 G-13 Mode test cycle and performance of currently available engines
Fig. 3 shows the 13 operating conditions of the G-13 Mode. The sizes of circles depict the relativeweight of each condition toward the composite result. As shown, the G-13 Mode covers a fairly high
load range even though it is supposed to be focused on the low load range.
A currently mass-produced CNG engine that has been very well received in the marketplace producesapproximately 800 g/kWh of CO2. Its NOx, HC, and CO emission values are as shown in Table 1
in the G-13 Mode; it is an extremely clean engine thanks to the use of a three-way catalyst.
Fig. 3 G-13 mode: Japanese Emission Test
Conditions and Weighting
Table 1 Emission of Production CNG Engine
In order to reduce CO2 to 640 g/kWh as targeted, a 25% improvement in thermal efficiency is requiredsince (800 640)/640 = 0.75, which represents an unattainable target when using the well-known
in-cylinder direct injection Otto cycle alone. An introduction of some innovative technologies at the
same time is undoubtedly required.
3.3 Selection of combustion systems and prognosis of target achievement
From the results of a simulation study, it had been known that the suggested approach of conventionaltechnology with modifications, or stratified combustion combined with the pre-mixing in-cylinder
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S c h e m eS c h e m eS c h e m eS c h e m eG 1 3 M o d e F u e l E c o n o m yG 1 3 M o d e F u e l E c o n o m yG 1 3 M o d e F u e l E c o n o m yG 1 3 M o d e F u e l E c o n o m y
D e c r e a s e R a t i o D e c r e a s e R a t i o D e c r e a s e R a t i o D e c r e a s e R a t i o
D i s u s e T h r o t t l e V a l v eD i s u s e T h r o t t l e V a l v eD i s u s e T h r o t t l e V a l v eD i s u s e T h r o t t l e V a l v e 5555
L e a n C o m b u s t i o n = 1 . 4L e a n C o m b u s t i o n = 1 . 4L e a n C o m b u s t i o n = 1 . 4L e a n C o m b u s t i o n = 1 . 4 3333
L e a n C o m b u s t i o n = 2 . 0L e a n C o m b u s t i o n = 2 . 0L e a n C o m b u s t i o n = 2 . 0L e a n C o m b u s t i o n = 2 . 0 9999
C o m p r e s s i o n R a t i o C o m p r e s s i o n R a t i o C o m p r e s s i o n R a t i o C o m p r e s s i o n R a t i o 2222
C o m p r e s s i o n R a t i o C o m p r e s s i o n R a t i o C o m p r e s s i o n R a t i o C o m p r e s s i o n R a t i o 3333
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M i l l e r C y c l eM i l l e r C y c l eM i l l e r C y c l eM i l l e r C y c l e 5555
C o m b u s t i o n I n p r o v e m e n tC o m b u s t i o n I n p r o v e m e n tC o m b u s t i o n I n p r o v e m e n tC o m b u s t i o n I n p r o v e m e n t 1 01 01 01 0
H i g h T o r q u e @ L o w r p mH i g h T o r q u e @ L o w r p mH i g h T o r q u e @ L o w r p mH i g h T o r q u e @ L o w r p m 7777
F u e l S u p p l y L o s sF u e l S u p p l y L o s sF u e l S u p p l y L o s sF u e l S u p p l y L o s s 5 5 5 5
25252525 29292929TotalTotalTotalTotal
S c h e m eS c h e m eS c h e m eS c h e m eG 1 3 M o d e F u e l E c o n o m yG 1 3 M o d e F u e l E c o n o m yG 1 3 M o d e F u e l E c o n o m yG 1 3 M o d e F u e l E c o n o m y
D e c r e a s e R a t i o D e c r e a s e R a t i o D e c r e a s e R a t i o D e c r e a s e R a t i o
D i s u s e T h r o t t l e V a l v eD i s u s e T h r o t t l e V a l v eD i s u s e T h r o t t l e V a l v eD i s u s e T h r o t t l e V a l v e 5555
L e a n C o m b u s t i o n = 1 . 4L e a n C o m b u s t i o n = 1 . 4L e a n C o m b u s t i o n = 1 . 4L e a n C o m b u s t i o n = 1 . 4 3333
L e a n C o m b u s t i o n = 2 . 0L e a n C o m b u s t i o n = 2 . 0L e a n C o m b u s t i o n = 2 . 0L e a n C o m b u s t i o n = 2 . 0 9999
C o m p r e s s i o n R a t i o C o m p r e s s i o n R a t i o C o m p r e s s i o n R a t i o C o m p r e s s i o n R a t i o 2222
C o m p r e s s i o n R a t i o C o m p r e s s i o n R a t i o C o m p r e s s i o n R a t i o C o m p r e s s i o n R a t i o 3333
D e c r e a s e M e c h a n i c a l L o s sD e c r e a s e M e c h a n i c a l L o s sD e c r e a s e M e c h a n i c a l L o s sD e c r e a s e M e c h a n i c a l L o s s 3333
M i l l e r C y c l eM i l l e r C y c l eM i l l e r C y c l eM i l l e r C y c l e 5555
C o m b u s t i o n I n p r o v e m e n tC o m b u s t i o n I n p r o v e m e n tC o m b u s t i o n I n p r o v e m e n tC o m b u s t i o n I n p r o v e m e n t 1 01 01 01 0
H i g h T o r q u e @ L o w r p mH i g h T o r q u e @ L o w r p mH i g h T o r q u e @ L o w r p mH i g h T o r q u e @ L o w r p m 7777
F u e l S u p p l y L o s sF u e l S u p p l y L o s sF u e l S u p p l y L o s sF u e l S u p p l y L o s s 5 5 5 5
25252525 29292929TotalTotalTotalTotal
S c h e m eS c h e m eS c h e m eS c h e m eG 1 3 M o d e F u e l E c o n o m yG 1 3 M o d e F u e l E c o n o m yG 1 3 M o d e F u e l E c o n o m yG 1 3 M o d e F u e l E c o n o m y
D e c r e a s e R a t i o D e c r e a s e R a t i o D e c r e a s e R a t i o D e c r e a s e R a t i o
D i s u s e T h r o t t l e V a l v eD i s u s e T h r o t t l e V a l v eD i s u s e T h r o t t l e V a l v eD i s u s e T h r o t t l e V a l v e 5555
L e a n C o m b u s t i o n = 1 . 4L e a n C o m b u s t i o n = 1 . 4L e a n C o m b u s t i o n = 1 . 4L e a n C o m b u s t i o n = 1 . 4 3333
L e a n C o m b u s t i o n = 2 . 0L e a n C o m b u s t i o n = 2 . 0L e a n C o m b u s t i o n = 2 . 0L e a n C o m b u s t i o n = 2 . 0 9999
C o m p r e s s i o n R a t i o C o m p r e s s i o n R a t i o C o m p r e s s i o n R a t i o C o m p r e s s i o n R a t i o 2222
C o m p r e s s i o n R a t i o C o m p r e s s i o n R a t i o C o m p r e s s i o n R a t i o C o m p r e s s i o n R a t i o 3333
D e c r e a s e M e c h a n i c a l L o s sD e c r e a s e M e c h a n i c a l L o s sD e c r e a s e M e c h a n i c a l L o s sD e c r e a s e M e c h a n i c a l L o s s 3333
M i l l e r C y c l eM i l l e r C y c l eM i l l e r C y c l eM i l l e r C y c l e 5555
C o m b u s t i o n I n p r o v e m e n tC o m b u s t i o n I n p r o v e m e n tC o m b u s t i o n I n p r o v e m e n tC o m b u s t i o n I n p r o v e m e n t 1 01 01 01 0
H i g h T o r q u e @ L o w r p mH i g h T o r q u e @ L o w r p mH i g h T o r q u e @ L o w r p mH i g h T o r q u e @ L o w r p m 7777
F u e l S u p p l y L o s sF u e l S u p p l y L o s sF u e l S u p p l y L o s sF u e l S u p p l y L o s s 5 5 5 5
25252525 29292929TotalTotalTotalTotal
1.00E+00
1.00E+01
1.00E+02
1.00E+03
1.00E+04
1.00E+05
70 90 110 130 150 170
Crank angle (deg)
LocalA/F
TDC
A/F Monitoring point
Average A/F
Start of Injection
31.0
Ignitiontiming
direct injection, would be extremely difficult to handle (refer to Fig. 4). Based on these factors and
the efficiency improvement target, we decided to choose the in-cylinder direct injection diesel cycle.Table 2 shows the components to be modified and improved to the benchmark (current levels) and theirestimated contributions to the improvement in fuel economy (CO2).
The basic approach was to modify the diesel engine combustion system to include natural gas directinjection, hot surface ignition combustion approach. This would allow the engine to retain highthermal efficiency, a hallmark of diesel engines and use Isuzus extensive and proven knowledge of
diesel-type combustion systems. If successful, it would be possible to exceed the targets by a largemargin.
The overall approach was planned in such a way that it would be possible to go back to theconventional technology with additional modifications (pre-mixing in-cylinder direct injection) at
anytime since it was still an untested and unproven technology. We also felt that a high efficiency inthe compressor pump system might become a key to success.
Table 2 Improved Items of CO2 (Fuel Economy)
and The Contribution
Fig. 4 The results of a stratified combustion
study by CFD
4. Engine development4.1 Vehicle and base engine and their target performances
Our target was to produce a vehicle performance equivalent to the currently available CNG vehicle
with a higher torque and lower engine speed for better fuel economy (CO2). Fig. 5 shows the
performance curves of the conventional CNG engine and the CNG-DI engine of this project.
Fig. 6 the vehicle performance curves. The base engine, transmission, and differential gear were
selected from the models currently commercially available so that the study could commence withoutmanufacturing special components. For durability, the target was set to fall within the range alreadyverified by the base engine.
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30
40
50
60
70
80
90
100
110
500 1000 1500 2000 2500 3000 3500
Engine Speed (rpm)
Power(kW)
0
100
200
300
400
500
600
Torque(Nm)
CNG-DI targetpower
CNG Base Eng.Power
CNG-DI Target
torque
CNG Base Eng.
Torque
CNG-DI Vehicle
Base CNG Vehicle
Vehicle speed (Km/h)
RunningResistance&Drivingforce
Enginespeed(rpm)
CNG-DI Vehicle
Base CNG Vehicle
Vehicle speed (Km/h)
RunningResistance&Drivingforce
Enginespeed(rpm)
CNG-DI Vehicle
Base CNG Vehicle
CNG-DI Vehicle
Base CNG Vehicle Base CNG Vehicle
Vehicle speed (Km/h)
RunningResistance&Drivingforce
Enginespeed(rpm)
CNG-DICNG-DICNG-DICNG-DI RemarkRemarkRemarkRemark
Number of cylinderNumber of cylinderNumber of cylinderNumber of cylinder In-line 4In-line 4In-line 4In-line 4
Valve systemValve systemValve systemValve system valves (InletExhaust valves (InletExhaust valves (InletExhaust valves (InletExhaust
Bore StrokeBore StrokeBore StrokeBore Stroke Same as base diesel engine
DisplacementDisplacementDisplacementDisplacement Same as base diesel engine
Air intake systemAir intake systemAir intake systemAir intake system Turbocharger with intercoolerTurbocharger with intercoolerTurbocharger with intercoolerTurbocharger with intercooler Variable nozzle
Injection systemInjection systemInjection systemInjection system Direct injectionDirect injectionDirect injectionDirect injection With fuel compressor system
Injection pressureInjection pressureInjection pressureInjection pressure MaxMPaMaxMPaMaxMPaMaxMPa Variable lift control
Combustion chamberCombustion chamberCombustion chamberCombustion chamber type type type type Same as base diesel engine
Compression ratioCompression ratioCompression ratioCompression ratio Same as base diesel engine
Ignition systemIgnition systemIgnition systemIgnition system Glow plug ignitionGlow plug ignitionGlow plug ignitionGlow plug ignition With closed shield
Swirl ratioSwirl ratioSwirl ratioSwirl ratio Same as base diesel engine
CamCamCamCam Same as diesel engineSame as diesel engineSame as diesel engineSame as diesel engine
CNG-DI VehicleCNG-DI VehicleCNG-DI VehicleCNG-DI Vehicle Base CNG VehicleBase CNG VehicleBase CNG VehicleBase CNG Vehicle
Fuel
Body type
Occupant
Maximum payload
Number of cylinder
Bore Stroke
Displacement
Air intake system Turbocharger with intercooler NA
Injection system Direct injection Gas mixerVenturi type
Compression ratio
Ignition system Glow plug ignition Spark ignition
Power
Torque
Transmission
Overall length
Overall width
Overall height
Wheel base
Tread Front
Rear
Vehicle mass
GVW
Front
Rear Tire size
Weight
Engine
Dimensions
Tilt cab
In-line 4
Fig. 5 Engine Performance Diagram Fig. 6 Vehicle Performance Diagram
The figures show that a very significant difference lies in the torque characteristics. This curve was
considered possible due to cleaner burning nature of CNG such as no smoke even when the excess airratio is small in comparison to diesel.
An ELF with its payload at 2 tons was used as the base vehicle, and the engine was selected based on
4H* - TC at 4.5 liters. Table 3 shows the main specifications of the vehicle, ELF, and Table 4, those of
the engine.
Table 3 Comparison of Main CNG Vehicle
Specifications Between Production and
Prototype
Table 4 Main Engine Specifications
4.2 Target, approach, and results for each systemThe overall engine system configuration is shown in Fig. 7. The sub-systems unique to this prototype
are described below
1. Fuel systemFig. 8 shows the outline of the ISUZU and Westport fuel system configuration. The maximum
pressure for in-cylinder direct injection of fuel was set at 25 MPa. The reasoning behind this is shown
in Fig. 9: the maximum internal pressure of the cylinders of the engine during operation was 15 MPa;fuel can be injected during combustion; and, the injection pressure should be higher than the cylinder
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CNG TANK
SPOOL VALVE
HYDRAULICPRESSURE RELIEVE
VALVE
H62 COMPRESSOR
ACCUMULATOR
PRESSUREREGULATOR
GAS FILTER
HYDRAULICTANK
HYDRAULICAFTERCOOLER
HYDRAULICPUMP
HYDRAULICFILTER
0
5
10
15
20
25
-90 0 90
Crank angle (deg)
Pressure(MPa)
=12boost1.5bar
=18boost1.5bar
Pressure differenceFor nozzle sealMPa
Pressure differenceFor injection control>MPa
internal maximum pressure by 5 MPa at the minimum. The latter is to ensure the stable sealing
capability of gas seal valves under the internal pressure of cylinders. Also considered was the fact thatthis was a technology under development and the possibility of testing the engine up to 18 MPa withEGR, etc.
Spoolvalve
Variable
nozzleturbocharger
Urea tanl moduleUrea tanl moduleUrea tanl moduleUrea tanl module
EGR valve
EGR cooler
Air
Air
Cleaner
Intercooler
Inlet manifold
Common rail Regulator
Water Temp.sensor
Fuel pressuresensor
Crank
anglesensor
Camangle
sensor
Fuel temp.sensor
fuelfilter
Accumulator
Heat exchanger
One-wayvalve
Oil
pressuretank
Main tap
One-wayvalve
Compressor
Silensor
Exhaust gas
Boostsensor
Air temp.
sensor
Air temp sensor
Temp.
sensorNOUrea catlyst
NOx
sensor
Glowplug
Electricalcontrol
Throttle valve
CNGfilling
Oil
pressurepomp
Relief valve
Fuelfilter
Pressure
sensor
Temp
sensor
Manual
Cut-off valve
Pressuresensor
Relief valve
Eletricalcontrol
cut-offvalve
Relief valve
HC catalyst
Urea tankUrea
pump
CH3 catalystNOx
sensor
Temp.
sensor
FUEL CONDITIONING UNITFUEL CONDITIONING UNITFUEL CONDITIONING UNITFUEL CONDITIONING UNIT
HYDRAULICHYDRAULICHYDRAULICHYDRAULIC
CONTROL PANELCONTROL PANELCONTROL PANELCONTROL PANEL
COMPRESSOR MODULECOMPRESSOR MODULECOMPRESSOR MODULECOMPRESSOR MODULE
CNG tank
Heat exchanger
Eletrical
control
cut-offvalveManual
Cut-off valve
Eletrical
control
cut-offvalve
Fig. 7 Entire System of CNG Engine
Fig. 8 Fuel Delivery System Fig. 9 Maximum Combustion Pressure In
Comparison to Fuel Injection Pressure
Fig. 10 shows a prototype injector assembly. The injection characteristics are shown in Fig. 11, whichshows injection can be made over the entire range from idle, torque, and power as targeted
(controllable). The cross section of this injection nozzle is shown in Fig. 12, with a magnetostrictiveelement employed for direct needle lift control. The coil surrounding the element produces a
magnetic field by inputting electrical current from outside. The element has a different degree of
displacement depending on the strength of the magnetic field; it is possible to control the needle liftwith the electrical power input. Fig. 11shows the relationship between the needle lift, duration and
injected quantity.
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0
10
20
30
40
50
60
70
80
90
100
110
120
0 500 1000 1500 2000 2500 3000
Duration sec
Massflow
mg/injection)
100% Lift
75% Lift
50% Lift25% Lift
Flow @ idle mg/Injection@25MPa 13AFlow @ max torque [mg/Injection]@25MPa 13AFlow @ max power [mg/Injection]@25MPa 13A
30CAD at 2200rpm13CAD at 900rpm
0.75CAD at 500rpm
0
10
20
30
40
50
60
70
80
90
100
110
120
0 500 1000 1500 2000 2500 3000Duration sec
Massflow
mg/injection)
100% Lift
75% Lift
50% Lift
25% Lift
Fig. 10 Injector Assembly
Fig. 11Characteristic of Fuel Injection on
Injection Nozzle (25 MPa)
Fig. 12 Sectional Structure of Injector Fig. 13 Characteristic of Fuel Injection on
Injection Nozzle (10 MPa)
This is one of significant features of the common-rail injection system employed in this engine,because one of the primary aims of this project is to control combustion. In other words, it was our
strong desire to retain the feature of diesel engines: while the pre-mixing combustion is relatively
difficult to control, the diesel combustion is controllable from the ignition timing to combustionconditions (diffusion combustion).
Diesel fuel is liquid, and the internal pressure of the common rail (injection pressure into the cylinders)
is fully changeable as intended through a few repeated injections. Gaseous fuels are, on the otherhand, compressive and difficult to control to produce the optimum common rail pressure even with
rapid changes in the operating range on the engine side.
This new injector, however, controls the needle lift and produces the same effect as if the pressure ischanged in the common rail. Fig. 13 shows the injection characteristics at 10 MPa. As a matter of
fact, the comparison between Fig. 11and Fig. 13 indicates that a 50% lift at 25 MPa produces avirtually equal injection volume as a 100% lift at 10 MPa. It represents exactly the same effect offreely changing the common rail pressure cycle by cycle. It has been shown that this feature is
extremely beneficial in noise reduction as well as in stable ignition and combustion in the idling andlight load range (relatively low fuel flow).
Fig. 14 is a schematic of the hydraulic system for the compressor. Fig. 15 shows a cross section of a
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Atmosphere pressure
M
TURBO
SUPPLY
High pressure
Low pressure circuit
TO COMPRESSOR
HYDRAULICMOTOR
PRV
COOLER
FILTER CylinderCylinderCylinderCylinder
FloatingFloatingFloatingFloatingpistonpistonpistonpiston
MagnetMagnetMagnetMagnet SensorSensorSensorSensor
Oil roomGasroom
WorkingWorkingWorkingWorking
oiloiloiloil
Fuel tankFuel tankFuel tankFuel tank
Common railCommon railCommon railCommon rail
CylinderCylinderCylinderCylinder
FloatingFloatingFloatingFloatingpistonpistonpistonpiston
MagnetMagnetMagnetMagnet SensorSensorSensorSensor
Oil roomGasroom
WorkingWorkingWorkingWorking
oiloiloiloil
Fuel tankFuel tankFuel tankFuel tank
Common railCommon railCommon railCommon rail
IntakeIntakeIntakeIntake
ExhaustExhaustExhaustExhaust
AirCleaner
Variable nozzle turboElectrical throttle valve
IntakeIntakeIntakeIntake
ExhaustExhaustExhaustExhaust
intercooler
Air cleaner
Catalyst
EGR cooler
EGR valve
fuel compressor which has a free-floating piston that divides the cylinder into a compression chamber,
which is filled with fuel and a drive chamber which is filled with hydraulic fluid. Meanwhile a use oftwo compressors as a pair replacing the supply pump on the diesel engine with an oil pump forcompressor has produced a highly efficient compressor system
Fig. 14 Compressor System Fig. 15 Cross Section of Compressor
2. Ignition system.
ISUZU and Westport developed the continuous heat, hot surface ignition system that is employed inthis engine. The system utilizes specially shielded glow plug to generate the hot surface. The shieldcompletely encloses the glow plug and is employed for stable ignition, reliability and durability. Fig.
16 shows the relative orientation of injection nozzle with a hot surface system mounted in the cylinderhead at an inclined angle. The successful demonstration of this ignition system in the Elf truck and
the performance and efficiency results achieved in test cells have shown that this concept has greatpotential. However, the selected plug takes somewhat longer to warm up the glow plug. More works
is needed not only in the temperature increase characteristics but also in reliability and durability.
Fig. 16 Installation of Glow Plug to Cylinder
Head
Fig. 17 Intake and Exhaust System
3. Air intake and exhaust systemFig. 17 shows an outline of the air intake/exhaust system. For the purpose of conducting different
studies, an electric air intake controller was installed. The EGR system has its connecting passagewaysand the cooler doubled in size in order to allow up to twice as much volumetric flow as that of base
diesel engine. Note that the EGR mixing point with intake is actually the inlet of the turbo becausethere is no black smoke generated.
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Local area noise (Engine uppper 50cm)
50
55
60
65
70
75
80
85
90
200
250
315
400
500
630
800
1000
1250
1600
2000
2500
3150
4000
5000
Frequency (Hz)
SPL(dBA)
CNG-DI 50% 1000 89.4
DIESEL 50% 1000 87.7
Autospectrum(Top) - Mark 1
Working : CNG_50_1000 : Input : Time Capture Analyzer
0 1k 2k 3k 4k 5k 6k
40m
80m
120m
160m
200m
240m
280m
[Hz]
[dB(A)/20.0u Pa][s] (Nominal Values)
10.0
14.017.220.4
24.4
28.4
32.435.638.842.0
46.049.252.455.6
59.662.866.069.2
73.276.479.682.8
86.890.0
Autospectrum(Top) - Mark 1
Working : CNG_50_1000 : Input : Time Capture Analyzer
0 1k 2k 3k 4k 5k 6k
40m
80m
120m
160m
200m
240m
280m
[Hz]
[dB(A)/20.0u Pa][s] (Nominal Values)
10.0
14.017.220.4
24.4
28.4
32.435.638.842.0
46.049.252.455.6
59.662.866.069.2
73.276.479.682.8
86.890.0
CNG-DI 50%Load 1000rpmAutospectrum(Top) - Mark 1Working : CNG_50_1000 : Input : Time Capture Analyzer
0 1k 2k 3k 4k 5k 6k
40m
80m
120m
160m
200m
240m
280m
[Hz]
[dB(A)/20.0u Pa][s] (Nominal Values)
10.0
14.017.220.4
24.4
28.4
32.435.638.842.0
46.049.252.455.6
59.662.866.069.2
73.276.479.682.8
86.890.0
Autospectrum(Top) - Mark 1
Working : CNG_50_1000 : Input : Time Capture Analyzer
0 1k 2k 3k 4k 5k 6k
40m
80m
120m
160m
200m
240m
280m
[Hz]
[dB(A)/20.0u Pa][s] (Nominal Values)
10.0
14.017.220.4
24.4
28.4
32.435.638.842.0
46.049.252.455.6
59.662.866.069.2
73.276.479.682.8
86.890.0
CNG-DI 50%Load 1000rpmAutospectrum(Top) - Mark 1Working : CNG_50_1000 : Input : Time Capture Analyzer
0 1k 2k 3k 4k 5k 6k
40m
80m
120m
160m
200m
240m
280m
[Hz]
[dB(A)/20.0u Pa][s] (Nominal Values)
10.0
14.017.220.4
24.4
28.4
32.435.638.842.0
46.049.252.455.6
59.662.866.069.2
73.276.479.682.8
86.890.0
Autospectrum(Top) - Mark 1
Working : CNG_50_1000 : Input : Time Capture Analyzer
0 1k 2k 3k 4k 5k 6k
40m
80m
120m
160m
200m
240m
280m
[Hz]
[dB(A)/20.0u Pa][s] (Nominal Values)
10.0
14.017.220.4
24.4
28.4
32.435.638.842.0
46.049.252.455.6
59.662.866.069.2
73.276.479.682.8
86.890.0
CNG-DI 50%Load 1000rpm
Fig. 18 illustrates the variable nozzle-turbo charger system, and a photo of the system is Fig. 19. The
system controls the boost and has a feedback for VNT position.
Fig. 18 Variable Nozzle Turbo Charger (VNT)
System
Fig. 19 Appearance of Variable Nozzle Turbo
Charger (VNT)
4. Other modifications
Principal areas of the engine remain the same as the base diesel engine; for instance, the combustion
chamber of the piston has the same shape, with a compression ratio of= 18.0. Cooling and
lubrication systems are also the same as in the base diesel engine.
4.3 Noise and vibration
Latest diesel engines are common rail types and, combined with pilot injection and other technologicaladvances, are far superior in vibration and noise to conventional diesel engines. Fig. 20 shows a noise
comparison between the latest diesel engine model under development at Isuzu and the engine studiedin this project. It was noted that our engine had a jarring noise (2000 to 4000 Hz), occurring every
two revolutions.
Fig. 20 Comparison of Engine Noise (The
Newest Diesel Engine vs. CNG-DI)
Fig. 21 Search for Noise Source at the Frequency
Band between 2k and 4kHz
Fig. 21 shows one example of such noise. The subsequent study found that the cylinder heads were
acting as speakers for the injectors seating noise. Today it has been improved to a degree such thatthis noise is virtually inaudible. The combustion noise was demonstrated to be sufficiently low in
comparison with that of diesel engines. Fig. 22 shows one example. In fact, the noise heard at thestart of the vehicle is quite mellow, without any resemblance to the noise of the diesel cycle. It is
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Load(Nm)
0
50
100
150
200
250
300
350
400
450
500
Engine Speed (rp m)
800 1000 1200 1400 1600 1800 2000 2200
1.0
1.01.0
4.0
2.0
1.3
1.5
1.0
1.3
1.5
2.0
4.0
(%)
0
20
40
60
80
100
120
140
160
Pmax(MPa),
Comb.
noise(dBA)
Pmax Comb. noise
Full load 1000rpm
; CNG - DI
; Diesel
Pmax Comb. noise
Full load 1500rpm
Pmax Comb. noise
Full load 2200rpm
Converted by *
**** CNL = CPL + SA + ACNL = CPL + SA + ACNL = CPL + SA + ACNL = CPL + SA + A---- weightweightweightweightCNL [dB(A)]: Combustion Noise Level
CPL [dB] : Cylinder Pressure Level
SA [dB] : Structure Attenuation
A weight : (Audibility Compensation - A)
Grasp optimum combustion
condition used CFD*
0
2000
4000
6000
8000
10000
12000
14000
-90 -70 -50 -30 -10 10 30 50
Grasp air flow
compression stroke
Grasp fuel spray in and
around glow plug
Grasp optimum ignition
condition used CFD*
Compression stroke CombustionExpansion strokeTDC
Cylinder pressure
* CFD ; Computational Fluid Dynamics
Grasp optimum combustion
condition used CFD*
0
2000
4000
6000
8000
10000
12000
14000
-90 -70 -50 -30 -10 10 30 50
Grasp air flow
compression stroke
Grasp fuel spray in and
around glow plug
Grasp optimum ignition
condition used CFD*
Compression stroke CombustionExpansion strokeTDC
Cylinder pressure
* CFD ; Computational Fluid Dynamics
likely caused by the fact that CNG has one less physical transition as in gas ignition combustion
than diesel as in liquid gas ignition combustion.
Fig. 22 Differences of Combustion Noise Fig. 23 Coefficient of Variation of Combustion
(COV; Pmax) before Fine Tuning
Fig. 23, on the other hand, shows the fluctuation of maximum combustion pressure, the factor affectingvibration, by coefficient of variation of Pmax (maximum peak cylinder pressure). As seen, there is no
problem since fluctuation is within 5% over the entire range, thereby satisfying the target.
4.4 Combustion related simulation by CAE
1. Simulation approach
Fig. 24 describes the development of simulation in each phase, with the aim of faithfully simulating theairflow compression gas injection mixing/ignition combustion expansion in the cylinder
so that computation can reach the level of sufficient agreement with actual test results. STAR-CD was
employed for flow analysis from compression to spraying/flow, WC-ERC combustion model,developed by the Wisconsin University Engine Research Center, was used in combination with
STAR-CD from ignition to combustion.
Fig. 24 Simulation of Combustion Process
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Factor First Second Third
AIn-cylinder temp.() 400 550 700
BCylinder pressure (bar) 50 70 90
CInjection pressure (bar) 100 120 140
DInjection hole (mm) 0.1 0.15 0.2
EInjection duration (ms) 0.3 0.6 0.9
FInjection angle () 7.6 13.6 19.6
GInjection angle () 7.3 9.7 12.1
HGlow plug temp. () 1050 1200 1350
IShield & Glow gap (mm) 0.100 0.225 0.350
JGlow plug & Shield relative position (mm 0 2 4
Liftporsion
Hole Inlet
Fuel passage
Hole outlet
Sack andhole portion
2. CAE results and engine test
Since not much was known on the relationship between fuel jets and ignition, computation studies wereconducted by changing different factors contributing to combustion at three levels in a 27-runstructured design in order to find out how mixing affected combustion. They were followed by a
study in 9-run design to obtain the contributing ratio to combustion and optimum level of each factor.One such example is presented in Fig. 25. The surface temperature of glow plug and injectionpressure, among other things, were found to have large impacts on combustion.
Fig. 25 A Sample of CFD Analysis
The most difficult part was the transition from ignition to combustion. In the ERC model, CNGcombustion was not calibrated; we selected to determine them out by matching them to test results.
Initially we focused on test results from shock tube experiments. Pressures were successfully simulatedwith great accuracy, but we were troubled by little success in the ignition to combustion process. It was
finally understood that there is a fundamental difference in the subject and actual ignitions. In otherwords, it was a difference between the combustion process of high temperature oxidation at 2000 or
higher of a shock tube and that of low-temperature oxidation premixing/diffusion combustion in thecylinder.
Subsequently this problem was resolved, but this gap between the data and the simulation was awake-up call: the true simulation of combustion is impossible unless the injection characteristics in
actual combustion are accurately reproduced. It was therefore decided that we do some more work onthe accurate simulation of actual injection. Fig. 26 shows such an example. In order to ensure if this
simulation actually matched the real injection, methane was injected into a constant pressure vessel andobserved (Fig. 27), and the result was closely compared with the computation results.
Fig. 26 Duplication of Fuel Injection Fig. 27Injection Visualization
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Reduction by
EGR
g/kWg/kWg/kWg/kWhhhh
Final TargetFinal TargetFinal TargetFinal Target
g/kWg/kWg/kWg/kWhhhh
Reduction ratio by catalyst
(Target)
Before catalystBefore catalystBefore catalystBefore catalyst
TargetTargetTargetTarget
(Engine out)(Engine out)(Engine out)(Engine out)
g/kWg/kWg/kWg/kWhhhh
Reduction by
EGR
g/kWg/kWg/kWg/kWhhhh
Final TargetFinal TargetFinal TargetFinal Target
g/kWg/kWg/kWg/kWhhhh
Reduction ratio by catalyst
(Target)
Reduction by
EGR
g/kWg/kWg/kWg/kWhhhh
g/kWg/kWg/kWg/kWhhhh
Final TargetFinal TargetFinal TargetFinal Target
g/kWg/kWg/kWg/kWhhhh
Reduction ratio by catalyst
(Target)
Before catalystBefore catalystBefore catalystBefore catalyst
TargetTargetTargetTarget
(Engine out)(Engine out)(Engine out)(Engine out)
g/kWg/kWg/kWg/kWhhhh
0
5
10
15
-20 -10 0 10 20 30 40 50 60
C.A.(deg)
P
[MPa]
exp.#1_cyli. 100Nm SOI: -15 ATDCexp.#2_cyli. dittoexp.#3_cyli. dittoCFD -A01 ( 100Nm, SOI: -15 ATDC )exp.#1_cyli. 300Nm SOI: -15 ATDCexp.#2_cyli. dittoexp.#3_cyli. dittoCFD -B01 ( 300Nm, SOI: -15 ATDC )exp.#1_cyli. 475Nm SOI: -15 ATDCexp.#2_cyli. dittoexp.#3_cyli. dittoCFD -C01 ( 475Nm, SOI: -15 ATDC )A01Aft (100_-15)B01Aft (300_-15)C01Aft (475_-15)
Fig. 28 shows the results from the experiment and the computation plotted together in one chart.
Although there are still some differences in the absolute values, a very close simulation to the actualengine data became possible from the start of combustion, timing and profile of pressure changes(thermal generation). Thus it is now indicated that computer simulations are now possible using
different values of different parameters, a very valuable tool indeed from now on. This is one of theinnovations we have led the world. Fig. 29 shows one example of such analysis of injection tocombustion in the cylinder.
Fig. 28 Comparison of Simulation and Actual
Fuel Injection P-
Fig. 29 A Sample of Pictorial Playback
According To Combustion Process
5. Development of aftertreatment
5.1 Allocation of emission between engine and aftertreatmentFig. 30 shows the allocation of emission between the engine (with EGR) and aftertreatment in order to
achieve the target emission levels. In other words, the engine was to reduce NOx to 10 12 g/kWhby itself without any processing in the G 13 Mode, which was then to be further reduced by EGR to 4
4.5 g/kWh.
Fig. 30 Contribution of Emission Reduction
Thus the target level would become reachable by aftertreatment, accomplishing a reduction of 80 to85% in NOx from this level. It was indeed the target for NOx reduction of aftertreatment. The
target for NMHC was a 90% or more reduction through aftertreatment. NMHC was presumed toaccount for 20% of THC, and the THC was tuned to produce 9 g/kWh or less before catalyst.
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0
10
20
30
40
50
60
70
80
90
100
100 150 200 250 300 350 400 450 500 550 600
Catalyst inlet temp.
NO
conversion
%
Urea-SCR low temp active typeLNT High temp active type
Turbo chargerTurbo chargerTurbo chargerTurbo charger
Urea injectorUrea injectorUrea injectorUrea injector
ENGINEENGINEENGINEENGINE
1 Oxidation catalyst : For CH4 conversion (Mianly low load)
2 Oxidation catalyst : For CH4 conversion (Mianly high load)
3 Oxidation catalyst : For chang NONO2 & CH4 conversion
4 SCR catalyst : For NOx conversion
5 Oxidation catalyst : For prevention of ammonia slip
Mainly function of catalystMainly function of catalystMainly function of catalystMainly function of catalyst
TurboTurboTurboTurbo
UreaUreaUreaUrea
ENGINENGINENGINENGINENGINENGINENGINENGIN
1 Oxidation catalyst : For CH4 conversion (Mianly low load)
2 Oxidation catalyst : For CH4 conversion (Mianly high load)
3 Oxidation catalyst : For chang NONO2 & CH4 conversion
4 SCR catalyst : For NOx conversion
5 Oxidation catalyst : For prevention of ammonia slip
Mainly function of catalystMainly function of catalystMainly function of catalystMainly function of catalyst
0
10
20
30
40
50
60
70
80
90
100
50 100 150 200 250 300 350 400 450 500 550 600
Catalyst inlet Temp
CH4conversion
(%)
Pt/Pd system A
NO oxidation catalyst Pt system
Pt/Pd system B
Pt/Pd system C
ItemItemItemItem
No conversionNo conversionNo conversionNo conversionprospectprospectprospectprospect 20 3020 3020 3020 30 60 7060 7060 7060 70 80 9080 9080 9080 90
Fuel economyFuel economyFuel economyFuel economyprospectprospectprospectprospect
2-5%2-5%2-5%2-5% 12%12%12%12% 1.6-2.1%1.6-2.1%1.6-2.1%1.6-2.1%
(Include urea(Include urea(Include urea(Include ureacost)cost)cost)cost)
DurabilityDurabilityDurabilityDurability
Light-off temp.Light-off temp.Light-off temp.Light-off temp. 200-300Pt200-300Pt200-300Pt200-300Pt
seriesseriesseriesseries350-500Base350-500Base350-500Base350-500Basemetal seriesmetal seriesmetal seriesmetal series
300 4 50300 450300 450300 4 50 200 600200 600200 600200 600
Catalyst sizeCatalyst sizeCatalyst sizeCatalyst size times as times as times as times asdisplacementdisplacementdisplacementdisplacement
times as times as times as times asdisplacementdisplacementdisplacementdisplacement
times as times as times as times asdisplacementdisplacementdisplacementdisplacement
WeightWeightWeightWeight Increase (UreaIncrease (UreaIncrease (UreaIncrease (Ureatank & systems)tank & systems)tank & systems)tank & systems)
PackagingPackagingPackagingPackaging catalyst onlycatalyst onlycatalyst onlycatalyst only catalyst onlycatalyst onlycatalyst onlycatalyst only Urea tank &Urea tank &Urea tank &Urea tank &InjectionInjectionInjectionInjectionsystemsystemsystemsystem
InfrastructureInfrastructureInfrastructureInfrastructure UreaUreaUreaUrea
Engine controlEngine controlEngine controlEngine control Post injectionPost injectionPost injectionPost injection Rich-leanRich-leanRich-leanRich-leancombustioncombustioncombustioncombustioncontrolcontrolcontrolcontrol
No needNo needNo needNo need
combustioncombustioncombustioncombustioncontrolcontrolcontrolcontrol
Total evaluateTotal evaluateTotal evaluateTotal evaluate Low conversionLow conversionLow conversionLow conversion Low conversionLow conversionLow conversionLow conversionHard to controlHard to controlHard to controlHard to control
Rich/LeanRich/LeanRich/LeanRich/Lean
High potentialHigh potentialHigh potentialHigh potentialperformanceperformanceperformanceperformance( Need Urea( Need Urea( Need Urea( Need Urea
systemsystemsystemsystemInstallation andInstallation andInstallation andInstallation and
down sizingdown sizingdown sizingdown sizingcatalystcatalystcatalystcatalyst
HC-SCR catalystHC-SCR catalystHC-SCR catalystHC-SCR catalystLean NO trapLean NO trapLean NO trapLean NO trap
catalystcatalystcatalystcatalystUrea-SCR catalystUrea-SCR catalystUrea-SCR catalystUrea-SCR catalyst
5.2 System selection and basic study (gas model)
Fig. 31 shows an overview of the systems involved in the aftertreatment selection, in which candidateswere first listed up for study. For the reduction of HC, a study using a model gas was conducted toselect a coating material with higher oxidation property because of the high stability of CH4. Fig. 32
shows the sample a coating material with pt/pd series was selected.Table 5 provides the overview of characteristics of the candidate agents for the reduction of NOx.HC-SCR catalyst was eliminated from the selection pool early in the process due to its conversion ratio.Studied were NOx absorber (LNT) and urea-SCR catalysts. In the case of LNT, it was found that a) it
would unlikely produce the target conversion rate; b) the cost would be higher than other options forthe same level of NOx reduction (approximately twice or more of SCR); and, c) it would not reduce
CH4 and therefore require the engine to control injection and combustion for the reduction process to
occur due to the need for unsaturated gas of CO or C3H8 and higher hydrocarbons. These led to thefinal selection of the urea-SCR catalyst. Fig. 33 shows one example of the basic study of LNT
catalyst.
Fig. 31 Possible After Treatment system
(Proposal)
Fig. 32 Selection Test of Catalyst for CH4
Table 5 Comparison of Characteristic of NOx
Catalysts
Fig. 33 Basic Test of NOx Absorbed Catalyst
Fig. 34 describes one example of coating material tests with a model gas for SV ratio (catalyst size)which was conducted to determine the urea-SCR catalyst. When urea-SCR catalyst was chosen, thestudy of coating material properties for ammonia catalyst was initiated using a model gas in
consideration of urea slip.
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0
10
20
30
40
50
60
70
80
90
100
100 150 200 250 300 350 400 450 500 550 600
Catalyst inlet temp.
NO
conversion
%
Low temp. active type
High temp. active type
SV30000O2 10H2O 6NO 200ppmNH3 200ppmTemp rise speed 5/min
Catalyst size Temp.(Prospect)
Pressure loss(Prospect)
Remarks
35.5mm70mm 750 18 (kPa)200cell/cell thickness 60
m Metal honeycomb
5.66"4.84" 700 6.6 (kPa)400cell/cell thickness6mill Ceramic honeycomb
5.66"4.84" 700 5.4 (kPa)300cell/cell thickness8mill Ceramic honeycomb
7.5"7" 650 4.9 (kPa)400cell/cell thickness6mill Ceramic honeycomb
9"12" 600 5.3 (kPa)400cell/cell thickness6mill Ceramic honeycomb
9"4" 600 2.3 (kPa)400cell/cell thickness6mill Ceramic honeycomb
Under floorNO Oxidation catalyst
Under floorUrea-SCR catalyst
Under floorCH3-slip catalyst
Position
Pre-TurboOxidation catalyst
Post-TurboOxidation catalyst
Post-TurboOxidation catalyst
HCOxidationcatalyst
UreaPump
NOOxidationCatalyst
SCRCatalyst
CNG Engine
Ureacontrol PC
EngineECU
Tank
Temp.sensor
Ureainjector
UreaInjectionECU
HCOxidationcatalyst
HCOxidationcatalyst
UreaPump
NOOxidationCatalyst
NOOxidationCatalyst
SCRCatalyst
CNG EngineCNG Engine
Ureacontrol PC
EngineECU
Tank
Temp.sensor
Ureainjector
UreaInjectionECU
Fig. 34 Basic Test of Urea SCR Catalyst
Table 6 Estimation of Exhaust Pressure Drop forEach Catalyst
Fig. 35 Pre-Turbo HC Catalyst
In addition, the target for the total back pressure was set at 20kPa or less from the beginning since
incorporating these catalysts after the engine would increase the back pressure, thus affectingefficiency. Table 6 shows the calculated backpressure of each catalyst. As seen, the
backpressure is high at 18 to 20kPa with these catalysts alone; the use of catalysts at the turbointake for HC reduction was therefore abandoned. Fig. 35 shows a prototype HC catalyst system
for the entrance of the turbo.
5.3 SCR system1. System and rig test results
Fig. 36 shows the system drawing of the SCR catalyst. Isuzu has been engaged in the R&D ofurea-SCR catalysts for heavy-duty engines but only in the air-assisted uniform injection approach ofurea water solution over the exhaust pipes. Since this study was for light-duty vehicles, which have
no high-pressure air sources, there was no choice but to employ the direct injection of urea water.
Fig. 36 Urea SCR Catalyst System
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0
5
10
15
20
25
30
35
40
0 0.1 0.2 0.3 0.4 0.5
Duty ratio A/(A+B)
Massflow(g/m)
Max. Target
Min. Target A B
Duty ratio
+
Exhaust gas flow
Exh. Gas temp.
Low load & rpm
Urea injector position
Impactor
Diameter
SCR
Catalyst
Exhaust gas flow
Exh. Gas temp.
Low load & rpm
Urea injector position
Impactor
Diameter
SCR
Catalyst
In our system, a large amount of urea water is constantly circulated at a certain pressure, and injections
are made through the control of the duty ratio by an electromagnetic valve in its circuit. Fig. 37 is aphoto of the injection device, while Fig. 38, an example of injection characteristics.
Fig. 37 Appearance of Urea SCR Injector Fig. 38 Characteristic of Urea SCR Injector
2. Novel concepts for better efficiency in uniform atomization and vaporization.
As shown in the picture, the urea water injector has one injection hole with a reflector panel set at a45-degree angle. The mounting position and other factors for the injector were studied using CAE in
order to ensure that the resultant spray would enter the catalyst uniformly and fully vaporized. Fig. 39shows one such example. For the reduction of actual emissions, different exhaust pipe configurationswere studied to produce better uniformity of atomization and vaporization. It was finally concluded the
cone-shaped piping produced favorable results. The photos in Fig. 40 are the tested exhaust pipes.
Fig. 39 Urea Flow Simulation with Injection, diffusion and Vaporization by CAE
Fig. 40 Prototype Diffuser Cone and Exhaust Pipe System
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42
33
43
71
83
91
79
56
75
46
64
84
7983 84 84 83
89
98 98
81
99100100
0
10
20
30
40
50
60
70
80
90
100
M2 M3 M5 M6 M7 M8 M9 M10 M11 M12 IDLE TOTALMODE NUMBER in G13Mode
NOxconversion(%)
W/O Oxidation Catalyst
W/ Oxidation Catalyst
Load(Nm)
0
50
100
150
200
250
300
350
400
450
500
Engine Speed (rp m)
800 1000 1200 1400 1600 1800 2000 2200
1100
700
400
250
120
160
120
160
250
400
700
1100
(ppm)
0
10
20
30
40
50
60
70
80
90
100
50 100 150 200 250 300 350 400 450 500 550 600
Catalyst inlet temp.
NOconversion
(%)
Pt/Pd sytem A
NO oxidation catalystPt systemPt/Pd system B
Pt/Pd system C
Measurementpoint
NOx THC CO CO2COVlevel
Initial test resultInitial test resultInitial test resultInitial test result Engine outEngine outEngine outEngine out 8.78.78.78.7 5.825.825.825.82 6.476.476.476.47 626626626626TargetTargetTargetTargetachievemachievemachievemachievementententent
TargetWithout EGR,Catalyst)
Engine out 12 6.5 15 600
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Load(Nm)
0
50
100
150
200
250
300
350
400
450
500
Engine Speed (rp m)
800 1000 1200 1400 1600 1800 2000 2200
30
30
50
100
200
30020
30
50
100
200
300
(ppm)
Load(Nm)
0
50
100
150
200
250
300
350
400
450
500
Engine Speed (rp m)
800 1000 1200 1400 1600 1800 2000 2200
300
2000
2000
1000
900
900
700
700
500
500
500
300
500
700
900
1000
2000
(ppm)
02468
10
0
100
200
0
7500
15000
0
100
200
0
150
300
-5 0 5 10 15 20
CO(g/h)
CO(g/h)
CO(g/h)
CO(g/h)
2(g/h)
2(g/h)
2(g/h)
2(g/h)
THC(g/h)
THC(g/h)
THC(g/h)
THC(g/h)
NOx(g/h)
NOx(g/h)
NOx(g/h)
NOx(g/h)
COV(%)
COV(%)
COV(%)
COV(%)
EGR ratio EGR ratio EGR ratio EGR ratio
0
2
4
6
0
150
300
0
8500
17000
0
25
50
0
250
500
0 2 4 6 8 10 12 14
CO(g/h)
CO(g/h)
CO(g/h)
CO(g/h)
2(g/h)
2(g/h)
2(g/h)
2(g/h)
THC(g/h)
THC(g/h)
THC(g/h)
THC(g/h)
NOx(g/h)
NOx(g/h)
NOx(g/h)
NOx(g/h)
COV(%)
COV(%)
COV(%)
COV(%)
Injection timingBTDC)Injection timingBTDC)Injection timingBTDC)Injection timingBTDC)
0
200
400
600
800
1000
1200
1400
1600
1800
Decrease by EGR
Decrease by timing retard
NOx Con. After the ta il pipe
2 3 5 6 7 8 9 10 11 12
Fig. 44 Characteristic of HC before Fine Tuning Fig. 45 Characteristic of CO before Fine Tuning
Fig. 46 Characteristic of EGR before Fine
Tuning
Fig. 47 Investigation of Contribution of Injection
Timing and EGR to Emission Reduction
One example of the study on the contributing factor for different emission properties by changing,among other things, injection timing and EGR ratio is presented in Fig. 47. Fig. 48 shows oneexample of the studies done for reduction rate and ammonia slip by changing the urea-SCR conditions.
Fig. 49 shows the temperature of engine exhaust gas at different points in the after flow in each of the
G 13 Mode. This figure illustrates the challenges of reaching targeted the thermal efficiency (nonegative influence on CO2) while increasing the exhaust temperature (for utilizing catalyst bymaintaining the temperature at the catalyst activation temperature or higher.)
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Ureapump
Diffusion coneOxidationcatalyst
SCRcatalyst
CNG-DI Engine
UreainjectionECU
Ureacontrol PC
Engine ECU
Tank
Ureapump
Diffusion coneOxidationcatalyst
SCRcatalyst
CNG-DI Engine
Diffusion coneDiffusion coneOxidationcatalyst
Oxidationcatalyst
SCRcatalystSCR
catalyst
CNG-DI EngineCNG-DI Engine
UreainjectionECU
Ureacontrol PC
Engine ECU
Tank
NOx NMHC CO CO2 COV
(g/kWh) (g/kWh) (g/kWh) (g/kWh) (%)
Final resultFinal resultFinal resultFinal result 0.510.510.510.51 0.100.100.100.10
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Load(Nm)
0
50
100
150
200
250
300
350
400
450
500
Engine Speed (rp m)
800 1000 1200 1400 1600 1800 2000 2200
10
102020
20
40
40
60
60
80
100
10
20
40
60
80
100
(ppm)
Load(Nm)
0
50
100
150
200
250
300
350
400
450
500
Engine Speed (rp m)
800 1000 1200 1400 1600 1800 2000 2200
90
60 40
40
10
10
20
20
10
20
40
60
90
(ppm)
Load(Nm)
0
50
100
150
200
250
300
350
400
450
500
Engine Speed (rp m)
800 1000 1200 1400 1600 1800 2000 2200
7500
8600
12000
13000
14000
15000
7500
8600
12000
13000
14000
15000
(kPa)
Load(Nm)
0
50
100
150
200
250
300
350
400
450
500
Engine Speed (rp m)
800 1000 1200 1400 1600 1800 2000 2200
1.5
1.5
2.02.0
.5
2.5
3.0
4.04.0
(lamda)
1.5
2
2.5
3
4
Load(Nm)
0
50
100
150
200
250
300
350
400
450
500
Engine Speed (rp m)
800 1000 1200 1400 1600 1800 2000 2200
ALL AREA 0 ppm
Overall length
Overall width
Overall height
Wheel base
Maximum payload
Occupant
GVW
As seen from this table, all targets were achieved. The engine characteristics are shown in 51 to 55
(emission: NOx, HC, CO, Pmax, , etc.)
Fig. 51 Diagram of NOX with Final Engine
Specifications
Fig. 52 Diagram of HC with Final Engine
Specifications
Fig. 53 Diagram of CO with Final Engine
Specifications
Fig. 54 Diagram of Pmax with Final Engine
Specifications
Fig. 55 Diagram of Excess Air Ratio () with
Final Engine Specifications
Table 9 Summary of Main Vehicle Specifications
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Oxidationcatalyst
Urea catalyst
Silencer Tank
Tank
Fuel compressor
Heatexchanger
Acumulator
Regulator
Urea supplysystem
Aircleaner
7. Vehicle development
7.1 Vehicle specificationThe target performance for the vehicle was, as mentioned earlier, based on the 2-ton ELF-CNGV, avery popular model currently available on the market with fuel economy and driveability that replicate
those of diesel vehicles rather than those of gasoline vehicles. Fig. 56 shows the appearance of thedeveloped vehicle, while Table 9 presents its major specifications.
7.2 Vehicle layout and development
Fig. 57 shows the assembly of the frame and components. Fig. 58 shows simplified schematics ofdifferent systems in the vehicle. Fig. 59 is an electrical plan for coordination and control of these
systems. There is the main engine ECU, CNG-related ECU, and emission-related ECU (for
urea-SCR), all integrated through CAN BUS for control as a vehicle.
Fig. 56 Appearance of Completed Vehicle
Fig. 57 Drawing of Layout Plan for Vehicle Fig. 58 Schematics of Different System Layout
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AP sensor
Idle switch
Switch
A/C switch
Glow relay
Check engine ramp
Injector driver
Glowplugdriver
Main
Engine
Control
Module
Urea
Injector
Control
module
Sub
Engine
Control
Module
Vehicle
Interface
Module
Crank angle sensor
Cam angle sensor
Intake throttleposition sensor
VNT positionsensorVNT control
Intake throttle drive
Injector drive
Glowplugdrive
Inletair temp. sensor
MAP sensor
Common rail pressuresensor
Fuel temp. sensor
Common rail
Injector
EGR cooler
Ignition switch
Starter switch
Battery
EXH. Brake
Solenoid valve
Echo relay
EXH.Brake
EXH. Brake ramp
Glowplug ramp
EXH. Brake ramp switch
Stopramprelay
Clutch switch
Neutral switch
Vehicle speedsensor
Parking swwitch
Idle up volume
Tachometer
Vehicle function
EGR valve driveEGR valve position sensor
IAT sensor
Compressormodule
Mainrelay
Battery
Pressure
sensor
AP sensor
Idle switch
Switch
A/C switch
Glow relay
Check engine ramp
Injector driver
Glowplugdriver
Main
Engine
Control
Module
Urea
Injector
Control
module
Sub
Engine
Control
Module
Vehicle
Interface
Module
Crank angle sensor
Cam angle sensor
Intake throttleposition sensor
VNT positionsensorVNT control
Intake throttle drive
Injector drive
Glowplugdrive
Inletair temp. sensor
MAP sensor
Common rail pressuresensor
Fuel temp. sensor
Common rail
Injector
EGR cooler
Ignition switch
Starter switch
Battery
EXH. Brake
Solenoid valve
Echo relay
EXH.Brake
EXH. Brake ramp
Glowplug ramp
EXH. Brake ramp switch
Stopramprelay
Clutch switch
Neutral switch
Vehicle speedsensor
Parking swwitch
Idle up volume
Tachometer
Vehicle function
EGR valve driveEGR valve position sensor
IAT sensor
Compressormodule
Mainrelay
Battery
Pressure
sensor
0
10
20
30
40
50
60
0 5000 10000 15000 20000 25000
Drive distance
Vehiclespeed
Km/
Fig. 59 Electric Wiring Diagram of Control
System
Fig. 60 Drive Route for Fuel Consumption Test
8. Results of driving test
8.1 Validation of basic performanceThe validation was performed not only for fuel economy and driveability, but also to achieve a
diesel-equivalent level in low-end torque and exhaust braking as well as a practical level in response,vibration and noise.
8.2 Evaluations at Bibendum 2003The study vehicle was entered in Bibendum 2003; a competition organized by Michelin that was heldfrom September 23 to 25, 2003 in California. The participating vehicles went through strict evaluations
based on ISO. Our vehicle earned the following awards in recognition of our achievements:
A) Fuel economy: Gold medal (absolute values not published); a diesel vehicle ran the same course
for comparison; a distance of 14 miles (approx. 22.5 km) including 45 abrupt starts and stops. Fig.60 shows the driving pattern.
B) Emission: application by document; Gold medal (including the validation of J-G13 Mode and SCRfunctionality)
C) Noise (acceleration): 70.4 dB(A); Silver medal;D) Acceleration: 47.1 miles per hour; Bronze (internal test before the event: 56 57 miles per hour)
due to facing wind and slopes;E) General driveability test, including a rally to the Golden Gate Bridge; (approximately 60 km in the
suburb and approximately 40 km of freeway driving). The vehicle successfully completed the run,receiving the checker flag.
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9. Summary and future challenge
9.1 SummaryWe succeeded in the incorporation of an ISUZU and Westport hot surface ignition CNG-direct injectiondiesel cycle engine in a commercial vehicle and its operation as a complete vehicle for the first time in
the world. As seen in the records at the Bibendum, it was demonstrated that the vehicle has satisfiedall the parameters of a vehicle at a high level, indicating the high potential of this technology forcommercialization in the near future. It is a significant milestone.9.2 Future subjects
a) Pursuit of full reliability and durability: Refinement of ISUZU and Westport fuel, ignition andcontrol systems as required for full commercialization.
b) Further improvements in emission and fuel economy: the test mode for emission will be
changed from G-13 to transition mode. Better fuel economy and cleaner emission must bepursued in line with this change. In addition, commercialization without urea-SCR catalyst
should be explored; and,c) Price reduction, lighter weight, and smaller size must be worked at along with the issues in a)
for the eventual commercialization and sophistication of each system.
I would like to take this opportunity to sincerely thank all those involved for their extraordinarydedication and support, without which we could not possibly have completed and operated the vehicle
in such a short time with such demanding targets. I am certain we can deliver even greaterdevelopments of this technology.
REFERENCES
1. G. Zakis, H C. Watson, 2003, "Alternative Ignition System for CNG in Diesel Applications",
IPC12-D32.2. P. Ouellette, Westport, 2000,"High pressure Direct Injection (HPDI) of Natural Gas in Diesel
Engine", NGV2000.3. T. Komada, Mitsui Eng'ng & Ship, 2004"The Large Gas Injection Engine", ENGINE
TECHNOLOGY 30.4. M. Shioji, Kyoto Unv. 2001,"Study & Research for Ignition and Combustion System of High
Performance Natural gas Engine" JGA-Report.5. M. Oguchi, JARI, 2001,"Research & Evaluation of High Efficiency Natural Gas Vehicle"
JGA-Report.6. M. Okada, Isuzu Motors, 2003,"The Commercial Development of High-Efficiency, Ultra-Low
Emission CNG Vehicles" NEDO-Report.