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Effects of Negative Valve Overlap on the auto-
ignition process of lean ethanol/air mixture in
HCCI–engines
T. Joelsson, R. Yu and X.S. BaiDivision of Fluid Mechanics, Department of Energy Sciences, Faculty of Engineering LTH, Lund University
Fluid Mechanical Seminar Series
2010-03-19 Fluid Mech Seminar NVO combustion study
2
Outline•
Introduction–
Background
–
Experimental Engine Setup
•
Numerical Methods and Setup–
Large Eddy Simulation
–
Multi-Zone Chemistry Model–
Computation Details
•
Results and Discussion•
Conclusion
2010-03-19 Fluid Mech Seminar NVO combustion study
3
Background•
To control HCCI combustion one way is to control the in-cylinder temperature
•
Using and changing Negative Valve Overlap is one way to generate ‘‘optimal’’
in-cylinder temperature and
residual gas amount
•
How does NVO influence temperature and also fuel concentration prior to auto-ignition ?
•
LES is used to resolve the flow patterns and Multi-Zone tools for the chemistry
2010-03-19 Fluid Mech Seminar NVO combustion study
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GoalsUsing Numerical Simulation tools to
investigate –
the mixing process of fresh fuel/air mixture (port-fuel injected) with different amount of residual gas
–
the process of fresh/residual gas heating–
Auto-ignition process of diluted charge with residual gas under different NVO conditions
To develop a better understanding of the phenomenon
2010-03-19 Fluid Mech Seminar NVO combustion study
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Negative Valve Overlap
•
Negative Valve Overlap - (NVO)
–
Trapping residual gas inside cylinder volume
–
An internal EGR system
–
With a time shift of Closing Exhaust Valves and Opening Intake Valves giving that NOT all the exhaust gases can leave the cylinder volume
–
Results of this is that a warmer burned gas amount is kept in the combustion chamber for the next burning cycle
2010-03-19 Fluid Mech Seminar NVO combustion study
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Experimental Engine SetupGeometrical
Data of the Volvo D5
Displacements per cylinder 480 cm3
Valves per cylinder 4
Bore 81 mm
Stroke 93.15 mm
Connection Rod 147 mm
Combustion chamber Pancake
Compression ratio 9.1
Valve timing Fully flexible
Fuel Ethanol
Speed 1200 rpm
Valve
Openings
& Closing
Name EVO EVC IVO IVC
NVO
40 520 700 20 200
NVO
80 520 680 40 200
NVO
160 520 640 80 200
2010-03-19 Fluid Mech Seminar NVO combustion study
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Experimental Results•
HCCI combustion with port-fuel injected Ethanol*
*
H. Persson, J. Sjöholm, E. Kristensson, B. Johansson, M. Richter, M. Aldén, "Study of Fuel Stratification on Spark Assisted Compression Ignition (SACI) Combustion with Ethanol Using High Speed Fuel PLIF"
SAE paper 2008-01-2401. (2008)
2010-03-19 Fluid Mech Seminar NVO combustion study
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Numerical Methods•
LES was used to simulate –
the turbulent flow motion
–
Mixing processes of fresh fuel/air mixture with kept internal residual gas
–
Heat transfer with cylinder walls and compression/expansion
–
Focused on the intake and early compression stages:
0-290 CAD
•
Multi-Zone simulation–
using detailed chemistry for ethanol/air mixture
•
Constant LOAD•
Constant equivalence ratio, Φ–
Based on the LES predicted residual gas and temperature distribution fields
–
Starting from 70 BTDC (290 CAD)
2010-03-19 Fluid Mech Seminar NVO combustion study
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Large Eddy Simulation Approach
2010-03-19 Fluid Mech Seminar NVO combustion study
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LES models•
The governing equations–
Navier-Stokes equations
–
Low Mach number approximation –
Hydrodynamic and thermodynamic pressures
•
Spatial filtering–
Scales larger than the filter scale are resolved
–
Subfilter
scales are modeled (known as SGS)–
Small sub-filter scales are filtered out
•
Subfilter
scale models–
Transport fluxes
–
Chemical reactions
2010-03-19 Fluid Mech Seminar NVO combustion study
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The Navier-Stokes Equations
( )
( )
0
j
j j
j j j j
i
i
i j ijii j i j
j i j j
phuh hD hu hu
t x t x x x
ut x
pu uuu u u u
t x x x x
ρρρ ρ ρ
ρ ρ
ρ τρρ ρ
∂∂∂ ∂ ∂ ∂+ = + + −
∂ ∂ ∂ ∂ ∂ ∂
∂ ∂+ =
∂ ∂∂∂ ∂∂ ∂
+ = − + + −∂ ∂ ∂ ∂ ∂
⎛ ⎞⎟⎜ ⎟⎜ ⎟⎜ ⎟⎜⎝ ⎠
( ) - velocity component in direction 1,2, 3 - pressure
- density
- enthalpy
- viscous stress tensor
- thermal diffusion coefficient
i i
ij
u x i
p
h
D
ρ
τ
=
2010-03-19 Fluid Mech Seminar NVO combustion study
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SGS models for transport fluxes
•
SSM-model is used to take into account the SGS stress
•
Smagorinsky-type model is used to take into account the SGS-flux for scalar transport
•
Spatial and density-weighted filtering is as follow:
( , ; ) ( ; ) ( , )
1( , ; ) ( ; ) ( , ) ( , )
i i i i i
i i i i i i
x t F x x x t dx
h x t F x x x t h x t dx
ρ ρ
ρρ
∞ ∞ ∞
−∞ −∞ −∞∞ ∞ ∞
−∞ −∞ −∞
′ ′ ′Δ = − Δ
′ ′ ′ ′Δ = − Δ
∫ ∫ ∫
∫ ∫ ∫
2010-03-19 Fluid Mech Seminar NVO combustion study
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SGS models for chemical reactions
Reaction progress variable
Tabulation of the chemical source term
( , , )c f c h p=
( )
* **
* *
( ) (0)( ) , ( ) ( ( ), )
( ) (0) i u
jj j
j j j j
h hc h h Y T
h h
u cc cu c u c c
t x x Sc x x
ττ τ τ
τ
ρρ μρ ρ ρ ρ
∞
−= =
−⎛ ⎞∂∂ ∂ ∂ ∂⎟⎜ ⎟⎜+ = + − +⎟⎜ ⎟⎟⎜∂ ∂ ∂ ∂ ∂⎝ ⎠
2010-03-19 Fluid Mech Seminar NVO combustion study
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Mean and Fluctuations from LESStatistical analysis of velocity and temperature
( ) ( ) ( )
1 1 2 2 3 3 1 2 3 1 2 3
12
2 2 2
1 1 2 2 3 3
1 2 3 1 2 3
2
1 2 3 1 2
ˆ ( , , ; ) ( , , )
1ˆ ˆ ˆ
3
1ˆ ( , , ,CAD)
1 ˆ( , , ,CAD)
i i
V
V
V
u G x x x x x x u x x x dx dx dx
u u u u u u u dVV
T T x x x dx dx dxV
T T x x x T dx dx dxV
′ ′ ′ ′ ′ ′ ′ ′ ′= − − − Δ
⎛ ⎞⎟⎜ ⎡ ⎤ ⎟′ ⎜= − + − + − ⎟⎜ ⎢ ⎥ ⎟⎣ ⎦⎜ ⎟⎝ ⎠
′ ′ ′ ′ ′ ′=
⎡ ⎤′ ′ ′ ′ ′ ′ ′= −⎢ ⎥⎣ ⎦
∫∫∫
∫
∫∫∫
∫∫∫12
3
⎛ ⎞⎟⎜ ⎟⎜ ⎟⎜ ⎟⎜ ⎟⎝ ⎠
2010-03-19 Fluid Mech Seminar NVO combustion study
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LES numerical solver•
Staggered deforming grids
•
Predictor/Corrector time integration–
Predictor 2nd
order Adam-Bashforth–
Corrector 2nd
order Crank-Nicolson
•
Spatial discretization–
5th
order WENO scheme for the convective terms
–
4th
order central-difference-scheme for the diffusive terms
2010-03-19 Fluid Mech Seminar NVO combustion study
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Multi-Zone Simulation•
Cantera
solver tool
•
Marinov
Ethanol reaction model•
Two part divide solver–
Chemical Reaction model Constant Volume
–
Non-reaction part Compression of Volume
•
From 290 –
400 CAD
2010-03-19 Fluid Mech Seminar NVO combustion study
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Computational ConditionsInitial conditions of pressure and temperature for residual gas BEFORE EVC and when LES cycle starts and the fuel/air ratio for the multi-zone simulation
Name PINITIAL TINITIAL PRESIDUAL TRESIDUAL PhiCONST PhiLOADNVO
40 1 bar 500 K 1.45 bar 551 K 0.3 0.55
NVO
80 1 bar 500 K 2.9 bar 662 K 0.3 0.61
NVO
160 1 bar 500 K 8.5 bar 863 K 0.3 1.0
11
fuel
airres air res fuel
u b
st
m
mpVMm m m m
FRT xA
φ
⎛ ⎞⎟⎜ ⎟⎜ ⎟⎜⎛ ⎞ ⎟⎜⎝ ⎠⎟⎜ ⎟= = − − =⎜ ⎟⎜ ⎟ ⎛ ⎞⎜⎝ ⎠ ⎟⎜ ⎟⎜ ⎟⎜⎝ ⎠
2010-03-19 Fluid Mech Seminar NVO combustion study
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Residual Gas Distribution
•
Pure residual gas xb
= 1•
Pure fresh fuel/air intake gas xb
= 0
Large Eddy Simulation
Results and Discussionon Flow and Concentration Spatial
and Temporal Distribution
2010-03-19 Fluid Mech Seminar NVO combustion study
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Stratification of mixtures
2 ( )c b bD x xχ = ∇ ∇i
2010-03-19 Fluid Mech Seminar NVO combustion study
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In-cylinder Temperature
2010-03-19 Fluid Mech Seminar NVO combustion study
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Stratification in mixtures and in-cylinder temperature @ 270 CAD
NVO 40 NVO 80
2010-03-19 Fluid Mech Seminar NVO combustion study
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Temperature stratification: Summary•
Temperature stratification develops due to wall heat transfer and the mixing of the fresh charge with the residual gas–
related to wall and exhaust gas temperature
–
related to the ratio between intake and residual gases
•
Decrease of T’
happens due to turbulence mixing and piston expansion–
the slopes are related to the intake -
residual
gas ratio–
Starting point of injection of fresh charge
2010-03-19 Fluid Mech Seminar NVO combustion study
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Charge stratification: Summary•
The value of xb
-mean relates to the amount of intake gas injected into the cylinder–
High NVO gives low amount of intake gas which gives
–
xb
-mean valve starts to decrease when intake valve opens
•
xb
-fluctuations depends on the openings of the valves–
related to the intake/residual gas mass ratio
•
The decrease rate of xb
-fluctuations is related to the amount of intake gas that is in the cylinder and the mixing time–
Scalar dissipation rate
–
Intake valve opening time
Multi-Zone Simulation
Results and Discussionon Detail Chemistry Analysis
2010-03-19 Fluid Mech Seminar NVO combustion study
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Initialization for Multi-Zone Simulation
NVO 40 NVO 80 NVO 160
2010-03-19 Fluid Mech Seminar NVO combustion study
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Initial Conditions & Pressure
Name PhiCONST PhiLOADNVO
40 0.3 0.55
NVO
80 0.3 0.61
NVO
160 0.3 1.0
2010-03-19 Fluid Mech Seminar NVO combustion study
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Constant LOAD Constant Φ
CO2
emission Distribution over Combustion phase
2010-03-19 Fluid Mech Seminar NVO combustion study
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Temperature Distribution over Combustion phase
Constant LOAD Constant Φ
2010-03-19 Fluid Mech Seminar NVO combustion study
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Constant LOAD Constant Φ
CO emission Distribution over Combustion phase
2010-03-19 Fluid Mech Seminar NVO combustion study
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Detailed Chemistry: Summary•
NVO affect the pressure peak and pressure rise-rate–
Large NVO has lower peak and slower pressure-
rise-rate
•
The richest zones are not ignited first–
The rich zones have lower temperature
•
The ignition process is more sensitive to the temperature field than to the charge stratification field, at least for the current cases
2010-03-19 Fluid Mech Seminar NVO combustion study
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Conclusions•
Large eddy simulations coupled with detailed ignition chemistry
•
Different valve timing generates different temperature and mixture compositions
•
Several mechanisms control this mixing and heat transfer process–
Initial temperature difference between colder walls and hot residual gas
•
Influences strongest at early intake stroke–
Inhale of even colder intake gas
–
In-cylinder turbulence enhances diffusion in both temperature and concentration fields
•
Strongest influence at BDC and beyond
2010-03-19 Fluid Mech Seminar NVO combustion study
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Conclusions•
Temperature and concentration fields have strong correlation
•
The detailed chemistry simulations show that the ignition process is mainly correlated to the temperature stratification–
Hot regions ignite first
•
contain higher quantities of residual gas, higher temperature in these zones
•
Overrides at stoichiometric condition
–
NVO 80 give an optimal conditions when its weighted fuel concentration spreads along a longer temperature field than the other cases
–
No radicals were in the residual gas part
Thank you for you attention!
Effects of Negative Valve Overlap on the auto-ignition process of lean ethanol/air mixture in HCCI–enginesOutlineBackgroundGoalsNegative Valve OverlapExperimental Engine SetupExperimental ResultsNumerical MethodsLarge Eddy Simulation ApproachLES modelsThe Navier-Stokes EquationsSGS models for transport fluxesSGS models for chemical reactionsMean and Fluctuations from LESLES numerical solverMulti-Zone SimulationComputational ConditionsResidual Gas DistributionLarge Eddy SimulationStratification of mixturesIn-cylinder TemperatureStratification in mixtures and �in-cylinder temperature @ 270 CADTemperature stratification: SummaryCharge stratification: SummaryMulti-Zone SimulationInitialization for Multi-Zone SimulationInitial Conditions & PressureCO2 emission Distribution �over Combustion phaseTemperature Distribution �over Combustion phaseCO emission Distribution �over Combustion phaseDetailed Chemistry: SummaryConclusionsConclusionsSlide Number 34