Transferability of Insights from Fundamental Investigations into Practical Applications of Prechamber Combustion Systems

Efforts to reduce CO2 emissions from spark ignition engines have driven engine development to lean-burn or high-dilution operation, which results in high combustion variability as well as increased unburned hydrocarbon emissions. A widely used technology to reduce these issues are prechamber ignition systems, in which the external ignition source is located in a separate small volume, connected to the main chamber via small orifices. This setup allows for design of favourable ignition conditions near the ignition source, which results in fast and repeatable early flame propagation. The pressure increase resulting from combustion taking place inside the prechamber leads to the ejection of jets containing hot combustion products and possibly active radicals into the main chamber, which ignite the lean or diluted mixture; this process is often dubbed turbulent jet ignition or TJI. The use of TJI systems in engines allows the combustion of very lean/diluted mixtures, resulting in higher efficiencies and lower NOx emissions. In this work we shed light into the importance of quenching for practical applications involving turbulent jet ignition. This is achieved through optical investigations in a generic, constant volume test-rig, combined with zero-dimensional (0-D) model calculations. The 0-D model is applied to the generic setup and in real engine applications under varying operating conditions, in order to highlight the relative importance of quenching under the various thermochemical conditions encountered. The results indicate that thermal quenching in the nozzle should not be expected due to the small flame thickness under high pressure encountered in internal combustion engines. Nevertheless, under the jet mixing conditions expected in engines, hydrodynamic quenching due to mixing of burned products with unburned (cold) main chamber mixture can be expected. In most engine conditions, the re-ignition process of the initially quenched jet after their exit from the prechamber is expected to be so fast, that quenching will not be apparent in most measurements