Abstract
Low Temperature Combustion of Jet Propellant-8 Fuel in Compression Ignition Engine with the Low Compression Ratio
Highlights
Jet Propellant 8 (JP-8) is a military kerosenetype aviation turbine fuel with Fuel System Icing Inhibitor (FSII)
Indicated Mean Effective Pressure (IMEP) for the homogeneous charge compression ignition (HCCI) engine operation was close to 0.5 MPa, which is reported as the maximum achieved in a naturally aspirated HCCI engine using well mixed fuel– air mixture [18]
The Particulate Matter (PM) emission for the HCCI engine operation was higher than for the PPCI operation, Partially Premixed Combustion (PPC) was realised without EGR (Fig. 9b, 9d)
Summary
Jet Propellant 8 (JP-8) is a military kerosenetype aviation turbine fuel with Fuel System Icing Inhibitor (FSII). The results of the HCCI operation were compared to the Partially Premixed Combustion (PPC) mode without EGR, tested on the same engine with a low CR. The experiment aimed to test of possibilities of Low Temperature Combustion (LTC) in a CI engine fueled with JP-8 with a low compression ratio (CR).
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