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Final PresentationAthens, October 8, 2003
Introduction and background
• During the design stage of a ship, engine operating parameters are selected / optimised for one operating point (usually close to MCR)
• Engine performance and emissions degrade during the ship’s lifetime
• Emission regulations become more stringent
Final PresentationAthens, October 8, 2003
Introduction and background
X
Y
CONTROLUNIT
Final PresentationAthens, October 8, 2003
• DANAOS Shipping Co. (EL)
• National Technical University of Athens / LME (EL)
• MAN B&W Diesel A/S (DK)
• ABB Service A/S (DK)
• Germanischer Lloyd AG (D)
• Hapag-Lloyd Container Linie AG (D)
• CIMAC - National Members Association Greece (EL)
LOW IN FUEL AND EMISSIONS TWO-STROKEINTELLIGENT MARINE ENGINE
GROWTH Project G3RD-CT-2000-00245 - STARTING DATE: 1.4.2000 - DURATION: 39 months
Final PresentationAthens, October 8, 2003
� To establish correlations between performance,
emissions, and engine operating parameters , applicable to
a wide variety of direct drive marine engines.
Objectives and Methodology
LIFETIME OBJECTIVES:
� To develop control systems including the correlations
above, able to optimise engine performance, based on
standard measurable operating and external parameters, with
emissions level as an optimisation constraint.
Final PresentationAthens, October 8, 2003
Objectives and Methodology
(I) To perform a series of full scale shipboard tests and
testbed experiments of powerplant performance and
emissions for large two stroke marine engines, to compound
the partner’s cumulated experience and information
repository
LIFETIME METHODOLOGY:
Final PresentationAthens, October 8, 2003
(II) To conduct a series of detailed simulations of ship powerplant
operation using comprehensive advanced mathematical
models , calibrated using the results of (I), so as to arrive at
OBJ.1:
Objectives and Methodology
Correlations linking performance, emissions and the
engine parameters.
LIFETIME METHODOLOGY:
Final PresentationAthens, October 8, 2003
(III) To use simulation models, in combination with engine control
systems design procedures and electronic system test bed
trials, so as to arrive at OBJ.2 :
Objectives and Methodology
Engine add-on systems including the optimisation
correlations of OBJ.1.
LIFETIME METHODOLOGY:
Final PresentationAthens, October 8, 2003
(IV) To install prototype systems respectively on:
Objectives and Methodology
- A conventional direct-drive slow-speed engine of a
Danaos containership
- A state-of-the-art ultra-large-bore engine of a newly built
Hapag-Lloyd containership
- The “Intelligent" engine of the MAN B&W research testbed
LIFETIME METHODOLOGY:
Final PresentationAthens, October 8, 2003
- Injection timing- Exhaust valve closing- Injection pulse- Lub oil dosage- T/C system control- Air cooler contol- Starting air system control- Cylinders and turbochargers cut out at part loads
Control System
EmissionsEstimation
Set of Correlations betweenperformance, emissions andengine operating parameters
- Cylinder pressures and temperatures- Receivers pressures and temperatures- Crankshaft speed, torque and position- T/C speed- Fuel index- Lub oil pressure and temperature
- Optimization criterion - Ordered speed
Control schemes algorithm
- Ambient conditions - Fuel quality
2-stroke Marine Diesel Engine
LIFETIME PROTOTYPE CONTROL SYSTEM
Objectives and Methodology
Final PresentationAthens, October 8, 2003
Work Overview
On-boardExperiments
Simulations
Correlations
Control Schedules Full Scale
TestsTestbed
Experiments
Observer
EngineControl
Unit
LIFETIME PROTOTYPESYSTEMS
Analysis of results
Final PresentationAthens, October 8, 2003
Vessels for shipboard measurement campaigns
Hapag-Lloyd’s containership “Antwerpen Express”
Hapag-Lloyd’s containership “Shanghai Express” Odfjell’s chemical carrier “Bow Cecil”
Final PresentationAthens, October 8, 2003
Research Centre and Intelligent Engine Testbed
Exterior view of the MAN B&W facility
Final PresentationAthens, October 8, 2003
Research Centre and Intelligent Engine Testbed
View of the engine testbed with the 4T50MX Research Engine
Final PresentationAthens, October 8, 2003
The two possible configurations of the Intelligent Engine
Installation of the IEFuel Injection and Exhaust Valve
control systemsin parallel to
the conventional camshafton the 6L60MC engine
Final PresentationAthens, October 8, 2003
Exterior view of the ABB facility
Turbocharger test centre
Final PresentationAthens, October 8, 2003
ABB Turbocharger on the test rig
Turbocharger test centre
Final PresentationAthens, October 8, 2003
Intelligent EnginePerformance& Emissions
Investigations
“Bow Cecil” engine roomMAN B&W Testbed
Final PresentationAthens, October 8, 2003
Turbocharger measurement points setup
TurbochargerPerformanceInvestigations
at ABB Testbed
Turbine blades (condition as supplied for tests)
Final PresentationAthens, October 8, 2003
Turbine nozzle ring contamination
Nozzle ring No1(condition as supplied for tests)
Nozzle ring No2(condition as supplied for tests)
Final PresentationAthens, October 8, 2003
Compressor impeller preparation
Compressor wheelcoated with glass fibres
Final PresentationAthens, October 8, 2003
Compressor
Final PresentationAthens, October 8, 2003
Partners onboard “Shanghai Express” for measurements
Final PresentationAthens, October 8, 2003
“Shanghai Express” Propulsion Plant: 9K90MC engine
Final PresentationAthens, October 8, 2003
Measurement of brake power, MS “Shanghai Express”
Final PresentationAthens, October 8, 2003
Comparison of independent power measurement for main engine MS “Shanghai Express”
Final PresentationAthens, October 8, 2003
MS “Shanghai Express” sampling points for gaseous emissions (1), particulate matter (2), opacity (3) and filter smoke number (4)
Final PresentationAthens, October 8, 2003
Sampling probe for gaseous emission Sampling probe for particulate emission
Sampling point for gaseousand particulate emission
Sampling points and analysers for measurement of opacity and filter smoke number
“Shanghai Express”Exhaust gas
measurements
Final PresentationAthens, October 8, 2003
“Shanghai-Express” - ABB DAQ (SeMCa) connected to the 3rd turbocharger
Final PresentationAthens, October 8, 2003
“Antwerpen Express” Propulsion Plant: 7K98MC engine
Final PresentationAthens, October 8, 2003
Compressor outlet measurementsTemperature and pressure
Turbine outlet measurementsTemperature and pressure
Air-filter with thermocouplesTurbocharger speed sensor
“Antwerpen Express”Air management
systemmeasurements
Final PresentationAthens, October 8, 2003
Measuring data acquisition system ZXTFLEX/ABBonboard “Antwerpen Express”
Final PresentationAthens, October 8, 2003
Analysers for exhaust gas measurement, MS “Antwerpen Express”
Final PresentationAthens, October 8, 2003
The ageing process
Analysis of ageing effect
Final PresentationAthens, October 8, 2003
� Collection of performance data and component running hours for 4 ships
(DANAOS, HL, GCA members) out of 12 candidate
� Data pre-processing and selection of key operational parameters to be
investigated
� Statistical analysis of ageing ratios - regression models
� Results assessment - conclusions
Analysis of ageing effect - Methodology
Final PresentationAthens, October 8, 2003
Analysis of ageing effect - Data Summary
Final PresentationAthens, October 8, 2003
Ship: Maersk Livorno (DANAOS)
Analysis of ageing effect - Typical results
Exhaust gas temperature before T/C ageing ratio ε and corresponding ageing models
ε∆Texh_bTC
0%
5%
10%
15%
20%
25%
30%
35000 40000 45000 50000 55000 60000 65000 70000 75000 80000
M/E Hours
0
2000
4000
6000
8000
10000
12000
14000
16000
18000
20000
TC
Hours
TC Hours Period1 Period2 Peiod3 Predict Linear (Period1) Linear (Period2) Linear (Peiod3)
Compression pressure ageing ratio ε and corresponding ageing models
ε∆Pcyl_cmp
0%
5%
10%
15%
20%
25%
30%
35000 40000 45000 50000 55000 60000 65000 70000 75000 80000 85000
M/E Hours Period1 Period2 Period3 EST EST21 Linear (Period1) Linear (Period2) Linear (Period3)
The ageing ratio is defined as a deviation ratio of the operating parameter value, in a specific engine load condition, to the corresponding value of the
sea trial performance curves.
Final PresentationAthens, October 8, 2003
♦ Performance degradation significant after 15000 hours
♦ Newly built ships � no ageing phenomena for 2 years (min)
♦ Established ageing effects (after 15000 – 20000 hrs)
- Exhaust Temperature before T/C
- Cylinder compression pressure
- Turbocharger speed
- Scavenging air pressure.
♦ 5% increase in SFOC AGEING
Analysis of ageing effect - Conclusions
Final PresentationAthens, October 8, 2003
Multi-zone Combustion Model
Maps in fuel spray at one time instant:� Equivalence ratio� Temperature� % fuel mass burnt� NOx
Fuel spray developmentwith time
FUEL JET DEVELOPMENT vs TIMEGREY : 0 deg ATDC PURPLE : 5 deg ATDCBLUE : 10 deg ATDCRED : 20 deg ATDC
1
2
3
2141
6171
0.4
0.5
0.6
0.7
0.8
0.9
1.0
1.1
1.2
1.3
1.4
1.5
EQUIVALENCE RATIO MAP, 10 deg ATDC
1500
1600
1700
1800
1900
2000
2100
2200
2300
2400
2500
TEMPERATURE MAP, 10 deg ATDC
0
10
20
30
40
50
60
70
80
90
100
FUEL BURNT PERCENTAGE MAP, 10 deg ATDC
0250500750100012501500175020002250250027503000
NOx MAP, 10 deg ATDC
Final PresentationAthens, October 8, 2003
01050100250500750100012501500175020002250250027503000NOx MAP, 0 deg ATDC
0
250
500
750
1000
1250
1500
1750
2000
2250
2500
2750
3000
NOx MAP, 10 deg ATDC
0
250
500
750
1000
1250
1500
1750
2000
2250
2500
2750
3000
4000
5000
NOx MAP, 20 deg ATDC
050100200500750100012501500175020002250250027503000
NOx MAP (ppm), 5 deg ATDC
NOx maps in fuel spray at 4 time instants
Multi-zone Combustion Model
Final PresentationAthens, October 8, 2003
“Shanghai Express”Measured engine performance data (7 hours)
Engine Performance Modelling
Final PresentationAthens, October 8, 2003
Comparison between measured data and simulation resultsafter determining the engine governor constants
Engine Performance Modelling
Final PresentationAthens, October 8, 2003
Endurance test with high ash fuel
on a large 4-S engine
T/C Fouling Modelling
Final PresentationAthens, October 8, 2003
PARAMETRIC RUNSMeasured and predicted engine
performance and emissions parametersfor various values of VIT change
Simulations - 7K98MC engine
Final PresentationAthens, October 8, 2003
Simulations - 7K98MC engine
Predicted NOx using MOTHER and comparison with engine shop trials data
NOx model Validation
Final PresentationAthens, October 8, 2003
-5 -4 -3 -2 -1 0 1 2 3 4 5
Fuel Index Change (%)
172
173
174
175
176
177
178
179
180
181
182
183
184
BS
FC
(gr/kWh)
-5 -4 -3 -2 -1 0 1 2 3 4 5
Fuel Index Change (%)
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
NO
x (g
r/kW
h)
VIT Change (deg)
Engine Load @ 75% of MCR
Typical NOx and BSFC maps for 75% load
Simulations - 7K98MC engine
Creation of parameter maps (to be used for control)
Final PresentationAthens, October 8, 2003
Piston ring wear
Simulations of Ageing and Wear
Cylinder liner wear
Empirical models of component wear
Final PresentationAthens, October 8, 2003
Possible Types of Correlation
• Ship-specific look-up table
* Simple but less accurate
* Results based on a few experimental measurements
* Valid only in range close to the measured values
• Process model
* Physical model including in-cylinder processes for NOx formation
* Able to account for out-of-range inputs
* Ageing effect can be incorporated
* Higher execution time
Final PresentationAthens, October 8, 2003
LIFETIME Control System
Ship-specific correlation to be included in “Contro l” system
Control System
Set of Correlations betweenperformance, emissions andengine operating parameters
Control schemes algorithm
INTELLIGENT Engine
Final PresentationAthens, October 8, 2003
where K1, K2 , α engine-specific constants
Oxygen concentration & Maximum temperature from:
* A/F ratio (stoichiometric)
* Scavenging pressure
* Scavenging temperature
* other measured operational parameters
Mathematical functional correlation (MAN B&W) :
LIFETIME Control System
Final PresentationAthens, October 8, 2003
Process modelwas included in “observer”
(NTUA)
LIFETIME observer system (NOx-Box)
Observer System
NOxEstimation
- Receivers pressures and temperatures- Crankshaft speed, and torque- T/C speed- Fuel index
- VIT
2-S Marine Diesel Engine
Mathematical Model
MOTHER
Final PresentationAthens, October 8, 2003
• Process model (MoTher code) embedded in PC platform (NOx-BOX )
• PC connected to onboard Data Acquisition (DAQ) System
• Several engine operating parameters required for input and validation purposes
LIFETIME observer system (NOx-Box)
EXHAUSTRECEIVER
CYLINDERS
INLETVALVES
EXHAUSTVALVES
TURBINE
SCAVENGINGRECEIVER
PLENUM AFTERTURBINE
LOAD Te
RPM
FUELRACK
VITP,T
RPM PP,T
0
250
500
750
1000
1250
1500
1750
2000
2250
2500
2750
3000
NOx MAP, 10 deg ATDC
Monitoringsystem
NOx-Box
Communication Serial link
Embedded
MoTher DAQ
Final PresentationAthens, October 8, 2003
IMPLEMENTATION
• NOx-BOX onboard “Antwerpen Express” (HL) using automatic data input
• NOx-BOX onboard “APL Scotland” (DANAOS) using manually inserted parameter
values
LIFETIME observer system (NOx-Box)
• Initial calibration using on-board measurements and simulation runs
• Validation error (Predicted-Measured)
• Error exceeds limit � re-calibration of MoTher code constants
Calibration of estimated NOx value
Final PresentationAthens, October 8, 2003
LIFETIME observer system (NOx-Box)DANAOS Containership “APL Scotland ”
Hapag-Lloyd’s containership “Antwerpen Express”
Final PresentationAthens, October 8, 2003
Determination of the operating parameters to be controlled
Basic selected controlled parameters
• Injection timing
• Choice of injection profile
• Exhaust valve open timing
• Exhaust valve close timing
• Hydraulic supply pressure (injection pressure)
• Simulation results of the powerplant performance performed in WP5
(Powerplant simulation)
• Engine-specific correlation between operating prameters and emissions
obtained in WP6
• Available control options for the conventional and intelligent engines.
Determination based on:
Final PresentationAthens, October 8, 2003
Development of engine running modes
Validation of control schemes
• Low Emission mode
• Economy Mode
Cylinder Pressure
70
80
90
100
110
120
130
140
150
160
170
50 60 70 80 90 100 110
Engine Load [%]
[bar
abs
.]
Low Emission modeEconomy mode
Pmax
Pcomp
Fuel Injection & Exhaust Valve Timing
50 60 70 80 90 100 110
Engine Load [%]
Tim
ing
Low Emission mode
Economy mode
Injection Timing
Exhaust valve open
Exhaust valve close
Fuel Oil Consumption
-6.0
-4.0
-2.0
0.0
2.0
4.0
50 60 70 80 90 100 110
Engine Load [%]
[g/k
Wh]
Low Emission mode
Economy mode
Final PresentationAthens, October 8, 2003
Testbed implementation of the control schemes
Validation of the control schemes in the MAN B&W te stbedin Copenhagen in order to:
• To expand the knowledge of the engine combustion cycle with regard
to exhaust emissions and efficiency
• To determine the influence of variation in-cylinder compression
pressure and maximum combustion pressure on the engine operational
behaviour
• To make an initial evaluation of the control schemes proposed for the
intelligent engine and to expand the knowledge with regard to
adjustments on the conventional (mechanically actuated) engine
Final PresentationAthens, October 8, 2003
Testbed implementation of the control schemes
Validation of the control schemes in the MAN B&W te stbedin Copenhagen in order to:
• To expand the knowledge of the engine combustion cycle with regard
to exhaust emissions and efficiency
• To determine the influence of variation in-cylinder compression
pressure and maximum combustion pressure on the engine operational
behaviour
• To make an initial evaluation of the control schemes proposed for the
intelligent engine and to expand the knowledge with regard to
adjustments on the conventional (mechanically actuated) engine
• A test series of 42 tests (about 1000 running hours ) was carried out with a
parameter variation of compression pressure and max imum firing pressure
Final PresentationAthens, October 8, 2003
Analysis
• For a fixed Pmax, decreasing Pcomp (or increasing Pmax minus Pcomppressure) results in decreasing NOx. The effect is small at high loads, but
stronger at lower loads
• The HC emission at high loads (75% and 100%) is not affected by either Pmaxor Pcomp variations
• CO emissions decrease with increasing Pcomp, i.e. decreasing with higher
air/fuel ratio caused by larger air amount trapped in the cylinder at the higher
compression pressure
• The effect of Pmax and Pcomp on PM (Particulate matter) emission follows the
same trend as that of HC emission
Observations:
• Use of the compression pressure influence on NOx em issions, in the
MAN B&W NOx function.
Final PresentationAthens, October 8, 2003
Initial calibration of the prototype control system s
Prototype Control Systems
• MAN B&W Prototype for the Intelligent Engine
• On-line NOx-BOX observer system for the ultra-large bore engine
• Off-line NOx-BOX observer system for the conventional engine
Design and implementation of the prototype control systems
• “Antwerpen Express” of HL was replaced by “Tokyo Express” of HL for the measurement campaign.
Managerial decision
Final PresentationAthens, October 8, 2003
On-line NOx-BOX Observer System - General
Ultra-Large Bore Engine
• A portable computer connected to the ship’s engine monitoring system able to calculate continuously the level of NOx emission
• Includes the MOTHER simulation code to calculate the engine NOx level using the values of several measured engine operating parameters
• Input data for the NOx-BOX calculations are provided on-line by the
monitoring system of the ship
EXHAUSTRECEIVER
CYLINDERS
INLETVALVES
EXHAUSTVALVES
TURBINE
SCAVENGINGRECEIVER
PLENUM AFTERTURBINE
LOAD Te
RPM
FUELRACK
VITP,T
RPM PP,T
Final PresentationAthens, October 8, 2003
On-line NOx-BOX Observer System - Development
Ultra-Large Bore Engine
• Development of the User Interface
20 30 40 50 60 70 80 90 100 110Load (%)
68
101214161820
BM
EP
(b
ar)
1.61.8
22.22.42.62.8
Re
l. A
/F R
atio
(-)
160165170175180185
BS
FO
C (
gr/
kWh
)
6080
100120140160
Pm
ax
(ba
r)
100020003000400050006000
Bra
ke P
ower
per
cylin
der
(kW
)
Predicted
Reference data
5
10
15
20
25
30
30 40 50 60 70 80 90 100 110
Load (%)N
Ox
(gr/
kWh)
MOTHER results
Engine Shop Trials• Development of the communication protocol between the NOx-BOX and the
ship’s monitoring system – Testing with STN ATLAS emulator
• Initial calibration using the engine shop trials
Final PresentationAthens, October 8, 2003
Engine Running Mode software has been developed and integrated in the ME Engine Control System (ECS). It includes:
Intelligent Engine
• The generic engine running mode
Fuel Injection & Exhaust Valve Timing
50 60 70 80 90 100 110
Engine Load [%]
Tim
ing
Low Emission mode
Economy mode
Injection Timing
Exhaust valve open
Exhaust valve close
• The engine running mode controller
• The injection and exhaust valve close timing maps
• The user interface on Main Operating Panel of the ECS
Final PresentationAthens, October 8, 2003
Off-line NOx-BOX Observer System - General
Conventional Engine
• A computer able to calculate the level of NOx emission manual data input of measured engine operating parameters
• Includes the MOTHER simulation code to calculate the engine NOx level
using measured engine operating parameters
• Input data for the NOx-BOX calculations are provided off-line by the ship’s operator
VESSEL: ENGINE: MAN B&W 12K90 MC
Date: Date: Date: Engine Operation Data (Fill in the values of the shipboard measurement
instruments; use the units indicated in brackets) Time Time Time Time Time Time Time Time Time
Scav. Air Pressure (receiver) [bar]
Scav. air temp. after cooler [deg C]
Exhaust Receiver Pressure [bar]
Turbine Inlet Temperature [deg C]
Barometric Pressure (engine room) [mbar]
Shaft Torque [kNm]
Engine Speed [rpm]
Engine Power (MID) [BHP]
Engine Power (SEMS) [BHP]
Fuel Pump Index (average) [-]
Pmax adjustment index (V.I.T.) [-]
Turbocharger RPM [rpm]
Pmax [bar] (if available)
Final PresentationAthens, October 8, 2003
Off-line NOx BOX Observer System - Development
Conventional Engine
• Development of the User Interface
• Initial calibration using the engine shop trials
Final PresentationAthens, October 8, 2003
Prototype Control Systems
• MAN B&W Prototype for the Intelligent Engine (MAN B&W Testbed,
Copenhagen)
• On-line NOx-BOX observer system for the ultra-large bore engine (Tokyo
Express)
• Off-line NOx-BOX observer system for the conventional engine (APL Scotland)
Initial installation of the prototype control syste ms
Final PresentationAthens, October 8, 2003
On-line NOx-BOX Observer System
Ultra-Large Bore Engine
• Installed onboard “Tokyo Express” of HL at the port of Bremerhaven
• After the initial functionality tests, full system tests were performed during normal ship operation, while sailing towards Le Havre (France) with an intermediate stop at
Rotterdam
• After the completion of the trip, the prototype NOx-BOX was removed and taken back to NTUA for analysis of results and re-calibration
Final PresentationAthens, October 8, 2003
Engine Running Mode software installation
Intelligent Engine
• New Engine Control System (ECS) hardware & cabling
• New mechanical/hydraulic components for controlling exhaust valve, injection
valve and start air valves
• The injection and exhaust valve close timing maps
• Test setup for providing stimuli from all control stations (Bridge, ECR and Local)
Final PresentationAthens, October 8, 2003
Off-line NOx-BOX Observer System - Installation
Conventional Engine
• A CD with the installation program of the OFF-LINE NOx-BOX prototype was
sent to “APL Scotland” containership of DANAOS for installation
• The program was installed on a ship's computer and worked with manually
entered data
Final PresentationAthens, October 8, 2003
Prototype Control Systems
• Recalibration of the on-line NOx-BOX system sea-trials onboard “Tokyo
Express”
• Latest corrections and final calibration / fine-tuning of the intelligent engine control system (ECS) in the MAN B&W testbed in Copenhagen.
• No recalibration needed for the Off-line version of NOx-BOX onboard APL
Scotland.
Recalibration of the prototype control systems
Final PresentationAthens, October 8, 2003
On-line NOx-BOX Observer System
Ultra-Large Bore Engine
• The analysis of “Tokyo Express” sea trials, led to the necessity of NOx-BOX
prototype recalibration.
• the deviation of “Tokyo Express” propeller curve from “AntwerpenExpress” propeller curve, used in initial calibration.
• the narrow initial calibration range of prototype
• Recalibration was performed with use of the results of the “Tokyo Express”sea trials.
20 40 60 80 100Load %
60
80
100
120
140
Pm
ax
(ba
r)
measuredpredicted
20 40 60 80 100Load %
1000
2000
3000
4000
5000
kW/C
YL
20 40 60 80 100Load %
8
12
16
20
24
NO
x [g
r/kW
h]
50 60 70 80 90 100Engine rpm
10000
20000
30000
40000
Pb
[kW
]
• The severe fluctuations of predicted NOx emissions and brake power at part loads were attributed to:
Final PresentationAthens, October 8, 2003
Off-line NOx_BOX Observer System
Conventional Engine
• The initial calibration of the OFF-LINE NOx-BOX prototype was successful
and good agreement between the recorded and calculated engine
performance parameters has been obtained during the onboard tests
55 60 65 70 75 80 85 90 95rpm
0
1000
2000
3000
4000
5000
Po
we
r (K
W/c
yl)
55 60 65 70 75 80 85 90 95rpm
60
80
100
120
140
160
Ma
xim
um
Pre
ssu
re (b
ar)
55 60 65 70 75 80 85 90 95rpm
18
20
22
24
26
28
NO
x (g
r/KW
h)
K90 Simulation Results
MeasuredPredicted• No re-calibration of the OFF-LINE NOx-BOX prototype was necessary
Final PresentationAthens, October 8, 2003
On-line NOx-BOX Observer System
Ultra-Large Bore Engine
• The ON-LINE NOx-BOX prototype was re-installed onboard “Tokyo Express” at the port of Bremerhaven, for the sea trial campaign to the port of Le Havre, France
• Initial functionality tests and full system tests were performed. During the trip the data acquired were logged in order to be analysed in WP11.
• The prototype used the same protocols and connection equipment as in the previous trials (Sep 2002), since no communication problem was observed
Final PresentationAthens, October 8, 2003
Engine Running Mode software
Intelligent Engine
• The installation of test wall for in-office ‘hardware in the loop’ test of the complete ECS was completed on the Intelligent engine T50ME-X
• Compression ratio as function of engine load
• Maximum cylinder pressure as function of engine load
• Exhaust valve open angle as function of engine load
• Hydraulic supply pressure as function of engine load
• A series of functionality tests, preparing the system for the full-scale trials was also performed.
• The following parameters have been calibrated in order to achieve the desired performance and emission values for the two running modes (optimisation of SFOC or NOx emissions):
Final PresentationAthens, October 8, 2003
Work Overview
On-boardExperiments
Simulations
Correlations
Control Schedules Full Scale
TestsTestbed
Experiments
Observer
EngineControl
Unit
LIFETIME PROTOTYPESYSTEMS
Analysis of results
Final PresentationAthens, October 8, 2003
On-line NOx-BOX Observer System
Ultra-Large Bore Engine
• Full scale measurements of the engine performance and emissions were
performed onboard “Tokyo Express”
• Measurements were conducted with the ship main engine operating on 23 -100% of its rated power.
• Operational parameters of the engine were measured by three independent
sources (GL, MAN B&W and HL).
• The On-line NOx-BOX kept log of the data and NOx estimates, gathered
during the full-scale trials.
Final PresentationAthens, October 8, 2003
GL Measurements
Ultra-Large Bore Engine
• Exhaust gas and fuel samples have been analysed in the laboratory of GL
prior to onboard measurements to find out the particulate matter composition and the influence of fuel quality on emissions.
• Emissions measurements at required operating points specified by IMO for
Test Cycle E3 have been conducted.
63 %80 %91 %100 %speed
25 %50 %75 %100 %power
Test Cycle E3
Final PresentationAthens, October 8, 2003
GL Measurements
Ultra-Large Bore Engine
• The specific emissions were calculated with Method 2 (Carbon Balance)
according to IMO NOX Technical Code.
• The engine operational parameters were recorded by the partners.
-0.150.15-0.5-0.2-weighting factor
151186331330497538537kg/hmeasured NOx in exhaust gas
19.418.518.016.917.917.716.0g/kWhmeasured NOx in exhaust gas
7794100541841619529277253042733575kWmeasured power
55%63%80%81%91%96%98%-speed % of rated speed
19%25%46%49%69%76%84%-power % of rated power
23%30%55%58%83%91%100%-power % of max. actual power
Operating point / PowerUnitParameter
Final PresentationAthens, October 8, 2003
MAN B&W Measurements
Ultra-Large Bore Engine
• MAN B&W conducted measurements of ship operational data (power and rotational speed measurements) onboard “Tokyo Express”
• Results
• The engine speed measurements for all three independent measurements
differed not more than 1% in relation to the speed measured by GL.
• The power measurement by MAN B&W was in a range of +7% to +12% in
relation to the GL power measurement
• The on board measurement system of the ship showed a maximum
difference of 10% (up to 15% for low engine load).
0
5000
10000
15000
20000
25000
30000
35000
40000
0 10 20 30 40 50 60 70 80 90 100
Speed, rpm
Po
wer
, kW
Germanischer Lloyd (GL) HAPAG-Lloyd, ship's system HAPAG-Lloyd / MAN B&W Diesel A/S, indicator system
Test Cycle E3: “Test cycle for Propeller-law-operated main and propeller-law-operated auxiliary engine application “
Final PresentationAthens, October 8, 2003
On-line NOx-BOX Operation
Ultra-Large Bore Engine
• The On-line NOx-BOX kept log of the data and NOx estimates, gathered during the full-scale trials performed in the sea-passage Bremerhaven-Le
Havre.
• Engine operational data were collected along with the estimates generated by the NOx-BOX inference algorithm.
• Comparison of measured NOx by GL and calculated NOx by ON-LINE NOx-BOX has been conducted.
Final PresentationAthens, October 8, 2003
On-line NOx-BOX measurements – Selection of Results
Ultra-Large Bore Engine
Power vs. Time
0
5000
10000
15000
20000
25000
30000
35000
20:0
1:12
20:2
9:15
21:0
6:44
21:3
6:42
22:1
0:07
22:4
1:05
23:1
0:51
23:4
3:32
8:37
:19
8:54
:31
9:13
:10
9:32
:38
9:52
:04
10:1
0:47
10:3
2:50
10:5
2:48
11:1
0:07
11:3
0:18
11:4
9:46
12:0
7:42
13:0
6:57
13:3
8:33
13:5
9:18
14:1
6:53
14:3
4:22
14:5
3:17
Time (hh,mm,ss)
Pow
er, k
W
Predicted
Measured
(Dec 27, 2002) (Dec 28, 2002)No prediction due to “out of range data” error
Laptop PC overheating period
Power vs. RPM
0
5000
10000
15000
20000
25000
30000
35000
40000
50 55 60 65 70 75 80 85 90 95
RPM
Pow
er, k
W
Measured - Dec 27, 2002
Measured - Dec 28, 2002
Calibration curve
Measured - GL0
5
10
15
20
25
0 5000 10000 15000 20000 25000 30000 35000 40000Power, kW
NO
x em
issi
ons,
gr/k
Wh
Measured, GL
Predicted, NTUA
Weighted emissions (IMO, Test Cycle 3) GL: 17.5 gr/kWh NTUA: 17.67 gr/kWh
Final PresentationAthens, October 8, 2003
Ultra-Large Bore Engine
NOxEstimation
On-line NOx-BOX Observer System
Final PresentationAthens, October 8, 2003
Intelligent Engine
• The full-scale tests included variation of the controllable parameters for the two running modes under consideration (emission mode, performance mode)
Intelligent Engine - Results
• A series of functionality tests, preparing the system for the full-scale trials was also performed.
• The full-scale tests demonstrated the flexibility of the system, and the
possibilities with regard to emission and fuel consumption adjustment.
Final PresentationAthens, October 8, 2003
Off-line NOx-BOX Observer System
Conventional Engine
• For 30 days the crew recorded input data as well as some validation data in pre-specified datasheets.
Final PresentationAthens, October 8, 2003
Off-line NOx-BOX Observer System
Conventional Engine
• The output of each NOx estimation cycle has been appropriately post-
processed to estimate the ship’s NOx emissions with regard to the main operational parameters logged onboard ship.
10
12
14
16
18
20
22
24
26
28
28000 30000 32000 34000 36000 38000 40000 42000
Brake Power, kW
NO
x em
issi
ons,
gr/
kWh
-8
-7
-6
-5
-4
-3
-2
-1
0
1
2
Pow
er P
redi
ctio
n E
rror
, %
29
45
3 k
W
29
66
1 k
W
29
69
0 k
W
30
14
9 k
W
30
20
6 k
W
30
27
3 k
W
30
53
3 k
W
30
54
3 k
W
30
65
8 k
W
37
65
7 k
W
37
86
2 k
W
38
02
5 k
W
38
29
3 k
W
38
80
2 k
W
39
03
7 k
W
39
04
1 k
W
39
50
1 k
W
39
69
6 k
W
41
05
2 k
W
41
29
7 k
W
41
70
4 k
W
Engine Power, kW
Final PresentationAthens, October 8, 2003
Analysis of Results
• Effect of control schemes on performance and emissions
• NOx-BOX operation evaluation
• Model-based vs. correlational methods of NOx estimation
• Compressor map line position under different conditions
• Future engine control systems
Final PresentationAthens, October 8, 2003
Effect of control schemes on performance and emissi ons
Findings of the Intelligent Engine measurements
• For the RPM variation it was shown that the same tendency is observed for all loads, with a clear trend that higher RPM results in a lower NOx level.
• For the Pmax variation and the Pcomp/Pscav variation the relation is close to
linear, but with the gradient depending of the engine load.
• Blow back variation did not have a significant influence on NOx emission, but
remains an important factor with regard to scavenge efficiency and cleanness of the scavenge space.
• The hydraulic pressure influenced both the fuel injection pressure and the
opening of the exhaust valve.
Final PresentationAthens, October 8, 2003
NOx-BOX operation evaluation
Analysis of the operation and evaluation of the per formance of NOx-BOX• NOx-BOX software sensor is capable of accurately predicting the engine
operational parameters, provided efficient calibration is done prior to onboard
installation.
• Power calculation accuracy is a valid criterion toward accurate NOx emissions
prediction.
• NOx emissions prediction is accurate in cases where suitable data of the engine performance, as well as measured NOx emissions have been used for
the initial calibration of the NOx-BOX software sensor
Final PresentationAthens, October 8, 2003
NOx-BOX operation evaluation
Further development of NOx-BOX
• Calibration with different parameters
• Proper periodic recalibration
• In fixed intervals
• After scheduled on non-scheduled major engine modifications
• With automatic recalibration methods (using an embedded optimisation
code and adaptation schemes)
Final PresentationAthens, October 8, 2003
Model-based vs. correlational methods of NOx estimat ion
NOx emissions estimation
• MAN B&W correlation function (engine-specific)
• NTUA thermodynamic software (model-based)
An engine-specific formula (correlation) which associates measured operational
parameters in the form of a NOx prediction function
The MOTHER simulation code and the multizone combustion model which calculate the
NOx emissions in several loading and operational conditions.
The NOx emissions measured during the performance and emission tests on the 4T50MX test
engine in Copenhagen by MAN B&W have been predicted using two methods, by MAN B&W and
NTUA.
Final PresentationAthens, October 8, 2003
Load 50%
Model-based vs. correlational methods of NOx estimat ion
MAN B&W NOx function vs. NTUA model-based NOx estim ation (4T50MX engine)
0
5
10
15
20
25
30
40% 60% 80% 100% 120%
Engine Load (%)
NO
x E
mis
sion
(gr
/kW
h)
MAN B&W
NTUA
0
5
10
15
20
25
T02030(Pmax=161.5bar,
Pcomp=136.7)
T02031(Pmax=149.4bar,
Pcomp=135.7)
T02032(Pmax=136.2.5bar,
Pcomp=135.9)
T02033(Pmax=161.9bar,
Pcomp=127.1)
T02036(Pmax=159.8bar,
Pcomp=115.4)
NO
x em
issi
on (g
r/kW
h)
MAN B&W (Measured)
NTUA (Calculated)
MAN B&W (Calculated)
0
2
4
6
8
10
12
14
16
T02040(Pmax=105bar,
Pcomp=85)
T02041(Pmax=95bar,
Pcomp=85)
T02042(Pmax=85bar,
Pcomp=85)
T02043(Pmax=105bar,
Pcomp=75)
T02046(Pmax=105bar,
Pcomp=65)
NO
x em
issi
on (g
r/kW
h)
MAN B&W (Measured)
NTUA (Calculated)
MAN B&W (Calculated)
(*)
Baseline (Load 100%)
Load 75%
Final PresentationAthens, October 8, 2003
0
20
40
60
T02030(Pmax=161.5bar,
Pcomp=136.7)
T02031(Pmax=149.4bar,
Pcomp=135.7)
T02032(Pmax=136.2.5bar,
Pcomp=135.9)
T02033(Pmax=161.9bar,
Pcomp=127.1)
T02036(Pmax=159.8bar,
Pcomp=115.4)
Cal
cula
tion
Err
or (
%)
MAN B&W
NTUA
0
20
40
60
T02040(Pmax=105bar,
Pcomp=85)
T02041 (Pmax=95bar,
Pcomp=85)
T02042 (Pmax=85bar,
Pcomp=85)
T02043 (Pmax=105bar,
Pcomp=75)
T02046(Pmax=105bar,
Pcomp=65)
Cal
cula
tion
Err
or (
%)
MAN B&W
NTUA
(*)
Load 75% Load 50%
Calculation error of the two methods • Maximum error below 20%
• Minimal error in tests with high maximum pressure
• The MAN B&W function provides better calculations in the 75% load. The NTUA model-based method provides better calculations in the 50% load.
• Brake power calculation accuracy estimated using the MOTHER code is a valid criterion toward accurate NOx emissions prediction
Model-based vs. correlational methods of NOx estimat ion
Final PresentationAthens, October 8, 2003
Turbocharger components for surge free operation (A BB)
Objectives
• Development of a mathematical model define the engine operating line on the compressor map under normalised boundary conditions
• Analysis of the turbocharger behavior under various turbocharger and engine
operational conditions
• Determination of turbocharger components for surge free turbocharger operation
Method
• Analysis of data from measurements performed in August 2001 on board the
HL ship “Antwerpen Express” and on December 2002 on board the Hapag
Lloyd ship “Tokyo Express”.
Final PresentationAthens, October 8, 2003
“Antwerpen Express” running with clean and fouled tur bochargers
TCs clean TCs fouled
Pe=32,86 MWn=94 rpm
Pe=30,56 MWn=90 rpm
Pe=25,79 MWn=86 rpm
Pe=19,34 MWn=75 rpm
Ship: Hapag Lloyd "Antwerpen Express"Test Trials: 15.08.2001 and 23.08.2001Engine: MAN B&W 7K98MC with 3xTPL85-B11Engine operating lines with clean and fouled TCs
Pe=32,52 MWn=94 rpm
Pe=25,31 MWn=86 rpm
Pe=20,09 MWn=80 rpm
Pe=16,44 MWn=75 rpm
Final PresentationAthens, October 8, 2003
Turbocharger components for surge free operation
• Engine parameter variations that have been investigated using turbochargers with clean and fouled turbines:• Engine speed variation (Engine speed: 89 to 95 rpm with constant bmep)
• Exhaust valve open variation (Eo=-10 to +10 °CA) f or 100% - and 75%-load
• Exhaust valve close variation (Ec=-20 to +20 °CA) for 100% - and 75%-load.
• Measures in order to achieve optimum turbocharger operation:• Preventive measures like turbine dry cleaning with rice or nut shells or
turbine and compressor washing with water
• Turbocharger and engine manufacturer have to co-operate with the power plant enduser in order to find appropriate turbocharger cleaning intervals.
• For a safe engine and turbocharger operation engine and turbochargingsystem designers have to co-operate in order to produce turbocharger components for surge free turbocharger operation.
Final PresentationAthens, October 8, 2003
Future engine control systems
• Design aspects towards better efficiency – less emiss ions marine diesel engines
• Control of operational parameters and optimization of engine performance with respect to fuel oil consumption and emissions leads to moresophisticated and reliable 2-stroke marine diesel engines
• Use of advanced control schemes leads to improved performance of marine engines.
Final PresentationAthens, October 8, 2003
Future engine control systems
• Advanced control features of the intelligent engine
Exhaust valve movement
0
10
20
30
40
50
60
70
80
90 110 130 150 170 190 210 230 250 270 290
Dg. C. A.
mm
Early closing
Late closing
Early opening
Late opening
Reference
Final PresentationAthens, October 8, 2003
Future engine control systems
• Innovations introduced with the Intelligent Engine
• Hydraulic Power Supply unit
• Hydraulic Cylinder Unit, including:
electronically controlled fuel pump
electronically controlled exhaust valve actuator
• Electronically controlled starting air valves
• Integrated electronic control of auxiliary blowers
• Integrated electronic governor functions
• Crankshaft position sensing and tacho system
• Electronically controlled Alpha Lubricators for cylinder lubrication
• PMI system - off-line cylinder pressure measurement system
• Local Operating Panel
Final PresentationAthens, October 8, 2003
Future engine control systems
• Advanced control features of the intelligent engine
• Optimal control and flexibility of fuel injection in terms of pressure, timing, rate, shaping, main, pre & post injection pressure.
• Optimal adaptation to different fuel.
• Optimal adaptation to different operation modes.
• Optimal combustion at all operation speeds and loads
• Optimal engine acceleration
• Reduced fuel consumption
• Operational safety and flexibility
Final PresentationAthens, October 8, 2003
Future engine control systems
X
Y
ECS
• The intelligent engine implementation
Final PresentationAthens, October 8, 2003
PART 4CONCLUSIONS
Final PresentationAthens, October 8, 2003
CONCLUSIONS
• Conduction of initial onboard and testbed measurements and correlation with simulation models.
• Investigation of the engine ageing and turbocharger fouling effects.
• Determination of the operating parameters values for optimum powerplantoperation in terms of performance and emissions.
• Development of advanced control schemes.
• Design and development of electronic control and observer prototype systems.
• Onboard installation and full-scale tests.
� Work Progress
Final PresentationAthens, October 8, 2003
CONCLUSIONS
Outcome and possible implications of the LIFETIME p roject
• The installation of advanced marine engines is promoting the EU policy concerned with improvement of working conditions
• Adjustment of engine emissions according to regional or local legislation and requirements is promoting cost-effective marine operations
• The development of emissions observer systems may lead to cost-effective real-time evaluation of ship emission legislation conformance
• Environmental benefits can be directly associated with the reduction in exhaust emissions of marine powerplants, through the use of advanced control systems and technologies.
Final PresentationAthens, October 8, 2003
The End