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HCCI – Diagnostics and Control. Prof. Bengt Johansson Div. of Combustion Engines, Dept. of Heat and Power Engineering,. bengt.johansson@vok.lth.se www.vok.lth.se. Outline. Current engines HCCI in general HCCI in Lund, some results Production. Normal SI engine fuel consumption.
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HCCI – Diagnostics and Control Prof. Bengt Johansson Div. of Combustion Engines, Dept. of Heat and Power Engineering, bengt.johansson@vok.lth.se www.vok.lth.se
Outline • Current engines • HCCI in general • HCCI in Lund, some results • Production
Introduction Lean limit 100% Catalyst Efficiency 99% 98% 0.8 1.0 1.5 2.0 2.5 5.0 SI engine - part load improvement Stoichiometric premixed charge SI engine - Low part load efficiency + Low emissions with 3-way catalyst Lean burn premixed charge SI engine + Reduced pumping work improved part load efficiency - Increased HC and NOx Stratified charge SI engine - GDI + Removed pumping work much improved part load efficiency - Large problem with NOx and PM HCCI + Removed pumping work much improved part load efficiency + Shorter combustion period improved overall efficiency - Engine control problem
Diesel Engine (CI) • Large problems with emissions of NOx and PM • High fuel efficiency (low CO2 emission)
HCCI Emissions AutoTechnology Oct. 2002, p 54 HCCI 0,01 USA 2007 * PM 0,00 0,05 0 0,5 NOx
HCCI activities in Lund • Basic engine studies • Laser diagnostics • Combustion modeling - Chemical kinetics • Closed loop combustion control
Experimental facilities – single cylinder engines Scania 2 liter (Volvo 1.6 liter) Volvo/Alvar 0.5 liter VCR Old Hot bulb engine
Multicylinder engines for HCCI control Scania 12 liter 6 cylinder dual fuel Volvo 12 liter 6 cylinder VGT Volvo 3 liter 6 cylinder VVT Saab 1.6 liter 5 cylinder VCR/FTM
HCCI activities in Lund • Basic engine studies • Laser diagnostics • Combustion modeling - Chemical kinetics • Closed loop combustion control
Low NOx from HCCI mode Gasoline & Diesel fuel 0.05 100% Gas l =3.0 0.045 65% Gas n=1000 rpm 40% Gas 0.04 20% Gas 0% Gas 0.035 0.03 Specific NOx emissions [g/kWh] 0.025 0.02 0.015 0.01 0.005 0 10 15 20 25 Compression Ratio
With Variable Compression Ratio, VCR, the HCCI engine can useANYliquid or gaseous fuel!
Turbulence and geometry effects on HCCI Experimental setup Square bowl-in-piston Disc Swirl Ratio=2.8 HS case Swirl Ratio=2.0 LS case
Turbulence and geometry effects on HCCI 4 Disc, LS Head Centre Position Disc, HS Head 3.5 Square, LS Head Square, HS Head 3 2.5 Turbulence [m/s] 2 1.5 1 0.5 0 -50 -40 -30 -20 -10 0 10 20 30 40 50 Crank Angle [CAD] Turbulence
Turbulence and geometry effects on HCCI 8 Disc, LS Head Side Position Disc, HS Head 7 Square, LS Head Square, HS Head 6 5 Turbulence [m/s] 4 3 2 1 0 -50 -40 -30 -20 -10 0 10 20 30 40 50 Crank Angle [CAD] Turbulence Different scale
Turbulence and geometry effects on HCCI 800 Disc, LS Head SOC=-2 CAD Disc, HS Head 700 Square, LS Head Square, HS Head 600 500 Rate of Heat Release [J/CAD] 400 300 200 100 TDC 0 -5 0 5 10 ° Crank Angle [ ATDC] Rate of Heat Release
HCCI activities in Lund • Basic engine studies • Laser diagnostics • Combustion modeling - Chemical kinetics • Closed loop combustion control
The influence of Charge Heterogeneity on the HCCI Combustion Process (?)
Fuel DistributionPrior to Combustion With port-injection With mixing tank
Tracer PLIF after Auto-ignition With port-injection With mixing tank
OH PLIF Imaging With port-injection With mixing tank
Multi YAG-Laser System Ordinary laser t Multiple pulse laser t • Single/Double pulse operation • 4 Pulses:Time separation (0-100ms) • 8 Pulses:Time separation (6-145µs) • Wavelengths:532nm and 266nm • Dye-laser for tuneable operation
High Speed Camera • 8 independent CCD’s, 576x384 pixels 10 ns temporal resolution • Optional image intensifier UV sensitive 1 µs temporal resolution
Cyl. Volume 1951 cm3 Bore 127 mm Stroke 154 mm Comp. Ratio 16:1 Chamber design Pancake Fuel Ethanol Lambda 3.85 Experimental setup(Scania)
2 ATDC 2.5 ATDC 3 ATDC 3.5 ATDC 4 ATDC 4.5 ATDC 5 ATDC 5.5 ATDC • Fuel: ethanol • Tracer: 10% acetone • l3.85 • Rc: 16:1 Fuel Tracer PLIF(resolved single-cycle) W16mars_4
Conceptual model of HCCI Assuming homogeneous distributions of P, l, EGR% and RR: Ignition occurs when I reaches a critical value
Conceptual model of HCCI Effect of heterogeneous air/fuel ratio
Turbulence and geometry effects on HCCI +2 +2.5 +3 +3.5 +4 +4.5 +5 +5.5 Suppression of hot and reactive zones Single cycle fuel tracer LIF sequences
HCCI activities in Lund • Basic engine studies • Laser diagnostics • Combustion modeling - Chemical kinetics • Closed loop combustion control
Closed loop combustion control, CLCC Inlet Conditions (pin,Tin) User Inputs HEATERS PC Status Calculation NI PCI 6054 WaveBook 516 n-heptane i-octane PID Controllers PressureTraces Injector Actuator
Control Parameters 6 x 10 15 Max dp/dCA Max Pressure 10 Cylinder Pressure [Pa] 5 0 -40 -20 0 20 40 60 80 Controlled • CA50 • Net IMEP:s Constraints • Peak pressure • Peak dp/dCA • Net heat release 3000 Heat Release 2000 Heat Release, Q [J] 1000 0 CA50 -1000 -40 -20 0 20 40 60 80 Crank Angle [deg ATDC]
Combustion Timing Ignition Diagram 15 10 5 Combustion phasing [CA 50] 0 40 50 60 70 80 90 100 -5 -10 Octane Number S = d(CA50%) / d(Octane Number)
Unstable Operation 35 Stable Unstable 30 25 20 CA50 [°ATDC] 15 10 5 0 0 100 200 300 400 Cycle Index @ 3 bar IMEP @ 4.5 bar IMEP Closed loop control switched off
Operating range 280 kW (380 hk) • HCCI Diesel • 21 bar • 280 310 kW
Typical high load cycle 200 2 180 1.8 160 1.6 140 1.4 120 1.2 Cylinder Pressure [bar] Rate of Heat Release [kJ/CAD] 100 1 80 0.8 60 0.6 40 0.4 20 0.2 0 0 -30 -30 -20 -20 -10 -10 0 0 10 10 20 20 30 30 Crank angle [CAD] Load limited by Peak Cylinder Pressure at 200 bar and maximum rate of pressure at 30 bar/CAD IMEP net 17.4 bar IMEP gross 20.4 bar Animation Power