Abstract

A computational fluid dynamics study of a large-bore, two-stroke, integral compressor engine is conducted. The engine under study operates on natural gas and uses a prechamber for ignition. The purpose of this work is to ascertain how property variations in the prechamber jet affect NOx formation in the main combustion chamber. Several testing suites were performed using a CFD model of a Cooper-Bessemer GMV four-cylinder engine. The chemical composition and temperature of the prechamber jet were manually modified for each simulation. NO emissions were found to be more sensitive to increases in the jet temperature than decreases in the jet temperature. NO2 emissions were largely insensitive to any jet temperature modification. Jet composition was modified to represent discrete prechamber fuel-air ratios. A non-monotonic relationship exists between jet composition and NOx formation. In general, the optimal balance among NOx, residual CH4, and CO was found for simulations using a prechamber equivalence ratio slightly rich of stoichiometric. NO tended to form relatively early in the cycle in areas surrounding the PCC jet. Later in the cycle, NO collected around the perimeter of the cylinder. The extended Zeldovich and N2O mechanisms were the highest contributors to NO formation. NO2 formed relatively late in the cycle in areas of high NO concentration.

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