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MSU Rapid Compression Machine and Turbulent Jet Ignition Testing
Dr. Elisa ToulsonAssistant Professor Department of Mechanical Engineering, Michigan State University
7/29/2016 2
Turbulent Jet Igniter
Fuel and Air Inlet /Exhaust Gas Outlet
Hydraulic Reservoir
Pneumatic Piston assembly
Hydraulic Piston
RCM Optical Head
Combustion Cylinder Piston
High Speed Camera
A rapid compression machine uses a single mechanical stroke of a piston to compress a charge of fuel and air to an elevated temperature and pressure suitable for combustion
Key FeaturesPneumatically driven and hydraulically stoppedVariable compression ratioControlled Chamber Wall TemperatureOptical Access for combustion visualizationEffective Compression Time: 7 ms Compressed Conditions
• Pressure= 10-30 bar (optical) and up to 50 bar (metal)
• Temperature= 600-1000 K
Rapid Compression Machine
RCM Direct Test Chamber (DTC) Charge Preparation
Compression and ignition of fuel
Introduction of oxidizer/diluent gases @ T0, p0
Metered injection of test fuel
Evaporation of fuel inside the chamber (~2 min)
(4)(1) (2) (3)
Fuel Injector
First stage ignition delay due to low temperature heat release
Overall ignition delay
End of RCM compression stroke
Pressure increase due to RCM compression
JP-8 sampled at t = 2 min after injection
S
S
+ t for evaporation
Samples drawn through septum witha syringe and analyzed in GC/MS
Gas Chromatography/Mass Spectrometry (GC/MS)
0.0
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1.0
1.2 Volatilized JP-8 Samples from RCM JP-8 Reference
145 °C
125 °C
C17
C16C8
C14
C13
C12
C11
C15
C10
Nor
mal
ized
Abu
ndan
ce
105 °C
C9
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2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 180.0
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Time [min]
0.0
0.2
0.4
0.6
0.8
1.0
1.2 Volatilized JP-8 Samples from RCM JP-8 Reference
145 °C
125 °C
C17
C16C
8
C14
C13
C12
C11
C15
C10
Nor
mal
ized
Abu
ndan
ce
105 °C
C9
0.0
0.2
0.4
0.6
0.8
1.0
1.2
Nor
mal
ized
Abu
ndan
ce
2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 180.0
0.2
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0.6
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1.0
1.2
Nor
mal
ized
Abu
ndan
ce
Time [min]
7/29/20164
TJI is a pre-chamber ignition enhancement concept that produces a distributed ignition source through the use of a jet undergoing combustion
1.13 ms 1.25 ms 1.38 ms 1.63 ms 2.00 ms 2.25 ms 4.38 ms 10.00 ms
Advantages•Fast burning rates•Knock mitigation•Facilitates lean combustion and ignition of highly dilute mixtures
Turbulent Jet Ignition
Turbulent Jet Ignition Spark Ignition
7/29/2016 5
No Auxiliary Fueling PW=1.0 ms
No auxiliary fuel injection
Auxiliary fuel injection 1ms pulse
Pre-chamber visualization
6
RANS Modeling of the TJI Process in the RCM
• RCM Schlieren Imaging• RCM testing and optical
imaging of a natural gas TJI system for large bore truck engines
• RANS modeling of TJI system in large bore truck engine
• Autoignition and spray testing of ethanol gasoline blends in RCM
• Construction of Optical Constant Volume Combustion Chamber (CVCC) for laminar flame speed measurements
7
Plans for Future WorkRCM Schlieren Head Spray imaging in RCM
Initial Converge Modeling of Large Bore Truck Engine
Preliminary CVCC Design