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Optimizing Brake Performance of a Heavy-Duty, Compression Ignition Engine using Methanol Erik Svensson, Lund University 2018-05-03

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Page 1: Optimizing Brake Performance of a Heavy-Duty, Compression ...logesoft.com/loge-16/wp-content/uploads/2018/05/...May 03, 2018  · Optimizing Brake Performance of a Heavy-Duty, Compression

Optimizing Brake Performance of a Heavy-Duty, Compression Ignition Engine

using Methanol

Erik Svensson, Lund University

2018-05-03

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Agenda

• Motivation and Introduction of the work

• Methodology

• Results

• Discussion and Conclusions

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Motivation

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MotivationOptimizing the ICE!

Objectives

Efficiency• Gross• Brake

Emissions• Local• Global

Noise

Control

Optimize What?

Means

Metal Experiments

Optical Experiments

3D CFD Simulations

System Simulations

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MotivationOptimizing the ICE!

Objectives

Efficiency• Gross• Brake

Emissions• Local• Global

Noise

Control

Optimize What?

Means

Metal Experiments

Optical Experiments

3D CFD Simulations

System Simulations

This Work

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In This Work

Objectives

Efficiency• Gross• Brake

Emissions• Local• Global

Control

Optimize What?

Means

(Metal Experiments)

Optical Experiments

3D CFD Simulations

System Simulations

This Work

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Motivation

Fuel• Gasoline or Diesel

• Alternative fuels (Alcohols, Low RON Gasoline, H2? etc.)

Design of ExperimentsWhat should we look at?

Impossible to sweep every conditionTime consuming

What about Post Processing?

Methanol

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Optimization

• Parameters• One Parameter?• Two? • All?

• Approach• DoE• Local Optimization• Global Optimization

• Objectives• Maximize Efficiency

• Gross• Brake

• Constraints• Peak Cylinder Pressure (PCP)• Peak Pressure Rise Rate (PPRR)

Parameter 1

Parameter 2

Parameter i,…,N

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Methodology

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Modelling ApproachAn Overview

Experiments

GTise SCE

Loge DI-SRMValidation

GTise + SRM

• Collect and post process experimental data from SCE for model calibration + validation

• Use existing GT model for B.C. to DI-SRM • Tivc, Pivc, IGR, Wall Temps

• Calibrate and validate turbulence model• Six constants

• Couple SRM with MCE model and optimize ηbrake

GTise TPA • Extract burn rate from GT TPA• RoHR != Burn Rate

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Modelling Approach

Experiments

GTise SCE

Loge DI-SRMValidation

GTise + SRM

• Collect and post process experimental data from SCE for model calibration + validation

• Use existing GT model for B.C. to DI-SRM • Tivc, Pivc, IGR, Wall Temps

• Calibrate and validate turbulence model• Six constants

• Couple SRM with MCE model and optimize ηbrake

GTise TPA • Extract burn rate from GT TPA• RoHR != Burn Rate

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Single Cylinder Engine Experiments

Engine Scania Single Cylinder

Displacement 2.12 l

Bore × Stroke 130 mm × 160 mm

Connecting rod length 255 mm

Number of valves 4 per cylinder

Fuel Methanol (100 %Vol)

SCE

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• 72 experiments were chosen

• 3 different piston geometries

• 3 different injectors

• Large variety in operating conditions

Experimental Data

CR (-) Noz_d (μm) Noz_h (#)

15, 17, 27 175, 195, 230 8, 10, 12

N (rpm) imepG (bar) λ (-) EGR (%) Tin (K) #Inj

800 - 1600 5.1 – 15.5 0.9 – 4.1 0 – 55 322 - 455 1-2

Operating Conditions

Geometry

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Modelling Approach

Experiments

GTise SCE

Loge DI-SRMValidation

GTise + SRM

• Collect and post process experimental data from SCE for model calibration + validation

• Use existing GT model for B.C. to DI-SRM • Tivc, Pivc, IGR, Wall Temps

• Calibrate and validate turbulence model• Six constants

• Couple SRM with MCE model and optimize ηbrake

GTise TPA • Extract burn rate from GT TPA• RoHR != Burn Rate

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Transfer experimental data to DI-SRM input

• 𝑷in• 𝑻in• ሶ𝒎fuel• 𝑷ex• EGR

• 𝑷ivc• 𝑻ivc• 𝟑 × 𝑻wall• IGR• 𝝀• imepG• 𝑻exh• 𝜼volumetric• 𝒙𝒊 ∈ 𝑿mole

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Modelling Approach

Experiments

GTise SCE

Loge DI-SRMValidation

GTise + SRM

• Collect and post process experimental data from SCE for model calibration + validation

• Use existing GT model for B.C. to DI-SRM • Tivc, Pivc, IGR, Wall Temps

• Calibrate and validate turbulence model• Six constants

• Couple SRM with MCE model and optimize ηbrake

GTise TPA • Extract burn rate from GT TPA• RoHR != Burn Rate

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LOGE DI-SRM Setup

• PDF Data• Mixing model – EMST1

• Mixing time – 𝑘 − 𝜖1

• Chemistry• Saudi Aramco mechanism 2.02

• 493 Species and >2700 reactions

• Tabulated3

• Heat transfer• Classic Woschni formula with 𝐶1, 𝐶2 based on PPC experiments4

1Franken, T., Sommerhoff, A., Willems, W., Matrisciano, A. et al., "Advanced Predictive Diesel Combustion Simulation Using Turbulence Model and Stochastic Reactor Model," SAE Technical Paper 2017-01-0516, 2017, https://doi.org/10.4271/2017-01-0516.

2http://www.nuigalway.ie/c3/aramco2/frontmatter.html

3Matrisciano, A., Franken, T., Perlman, C., Borg, A. et al., "Development of a Computationally Efficient Progress Variable Approach for a Direct Injection Stochastic Reactor Model," SAE Technical Paper 2017-01-0512, 2017, https://doi.org/10.4271/2017-01-0512.

4Broekaert, S. “A Study of the Heat Transfer in Low Temperature Combustion Engines.” Doctoral Thesis, 2018, https://biblio.ugent.be/publication/8547486

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Calibration of DI-SRM

• 8 of 72 cases were chosen for calibration

• Only the mixing time parameters were tuned

𝜕𝑘

𝜕𝜃= −𝐶𝑑𝑒𝑛 ⋅

2

3⋅𝑘

𝑉𝑐𝑦𝑙⋅𝑑𝑉𝑐𝑦𝑙

𝑑𝜃− 𝐶𝑑𝑖𝑠 ⋅

𝑘32

𝑙+ 𝐶𝑠𝑞 ⋅

𝑘𝑠𝑞

32

𝑙 𝜃 > 𝑇𝐷𝐶+ 𝐶𝑖𝑛𝑗 ⋅

𝑑𝑘𝑖𝑛𝑗

𝑑𝜃+ 𝐶𝑠𝑤𝑖𝑟𝑙 ⋅

𝑐𝑚3

𝑙

𝜏 = 𝐶𝜏 ⋅𝑘

𝜖

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Calibration of DI-SRM

• 8 of 72 cases were chosen for calibration

• Only the mixing time parameters were tuned

𝜕𝑘

𝜕𝜃= −𝐶𝑑𝑒𝑛 ⋅

2

3⋅𝑘

𝑉𝑐𝑦𝑙⋅𝑑𝑉𝑐𝑦𝑙

𝑑𝜃− 𝐶𝑑𝑖𝑠 ⋅

𝑘32

𝑙+ 𝐶𝑠𝑞 ⋅

𝑘𝑠𝑞

32

𝑙 𝜃 > 𝑇𝐷𝐶+ 𝐶𝑖𝑛𝑗 ⋅

𝑑𝑘𝑖𝑛𝑗

𝑑𝜃+ 𝐶𝑠𝑤𝑖𝑟𝑙 ⋅

𝑐𝑚3

𝑙

𝜏 = 𝐶𝜏 ⋅𝑘

𝜖

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Model Validation

Results

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GTP model validationR

el.

diffe

rence

inim

ep

G

min

- +

max

Rel.

diffe

rence

in

min

- +

max

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SRM model validationR

el.

diffe

rence

inim

ep

G,c

min

- +

max

Abs.

diffe

rence

inC

A50

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Modelling Approach

Experiments

GTise SCE

Loge DI-SRMValidation

GTise + SRM

• Collect and post process experimental data from SCE for model calibration + validation

• Use existing GT model for B.C. to DI-SRM • Tivc, Pivc, IGR, Wall Temps

• Calibrate and validate turbulence model• Six constants

• Couple SRM with MCE model and optimize ηbrake

GTise TPA • Extract burn rate from GT TPA• RoHR != Burn Rate

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Multi Cylinder Engine – Scania D13, inline 6

• Turbocharger from BorgWarner

• FMEP = 𝛼 ⋅ IMEP + 𝛽 ⋅ N + 𝛾 ⋅ 𝑝max

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SRM

Burn Rate

GT-ISE

Update B.C.

The MethodologyHow to simulate the engine

Estimate B.C.

Converge?

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Operating Points

Fuel

MEP

Engine Speed

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Optimization using a Genetic Algorithm (GA)

• Single objective – Brake Efficiency

max 𝜂𝐵(𝑥𝑖 , … , 𝑥𝑁)

subject to𝜕𝑝

𝜕𝜃 𝑚𝑎𝑥< 𝑙𝑖𝑚𝑖𝑡 And 𝑝(𝜃)𝑚𝑎𝑥 < 𝑙𝑖𝑚𝑖𝑡

• Which algorithm?

• Particle Swarm

• Artificial Bee Colony

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Optimization using a Genetic Algorithm (GA)

• Single objective – Brake Efficiency

max 𝜂𝐵(𝑥𝑖 , … , 𝑥𝑁)

subject to𝜕𝑝

𝜕𝜃 𝑚𝑎𝑥< 𝑙𝑖𝑚𝑖𝑡 bar And 𝑝(𝜃)𝑚𝑎𝑥 < 𝑙𝑖𝑚𝑖𝑡 bar

• Which algorithm?

• Particle Swarm – Significantly Faster

• Artificial Bee Colony

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Particle Swarm Sensitivity

25 50 75 100

Number of particles in one generation

750 particles

1000 particles

0.5 %0.8 %

0.2 %

0.3 %

1.93 1.95

0.85 0.73

0.61

0.62

0.52 0.55

Gro

ss In

dic

ated

Eff

icie

ncy

(%

)

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Particle Swarm Sensitivity

25 50 75 100

Number of particles in one generation

750 particles

1000 particles

0.5 %0.8 %

0.2 %

0.3 %

1.93 1.95

0.85 0.73

0.61

0.62

0.52 0.55

Gro

ss In

dic

ated

Eff

icie

ncy

(%

)

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Constraint handling

• Single objective – Brake Efficiency

max 𝜂𝐵(𝑥𝑖 , … , 𝑥𝑁)

subject to𝜕𝑝

𝜕𝜃 𝑚𝑎𝑥< 𝑙𝑖𝑚𝑖𝑡 bar And 𝑝(𝜃)𝑚𝑎𝑥 < 𝑙𝑖𝑚𝑖𝑡

• If constraint is violated

𝜂𝐵 = 𝜂𝐵 × 1 −𝑔𝑖 − lim𝑖

lim𝑖𝛽

𝛼

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𝜂𝐵 = 𝜂𝐵 × 1 −𝑔𝑖 − lim𝑖

lim𝑖𝛽

𝛼

Limit 2 × Limit

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Summary

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Summary

• Data from 72 experiments were collected

• B.C. for the DI-SRM were obtain with GT Power

• The turbulence model of the DI-SRM was calibrated

• Finally the DI-SRM was coupled with a MSE model to optimize the brake efficiency of a HD engine running on methanol

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Optimizing Brake Performance of a Heavy-Duty, Compression Ignition Engine

using Methanol

Erik Svensson, Lund University

2018-05-03