Ammonia and hydrogen are promising zero-carbon fuels that can help combustion engines achieve the zero-carbon emissions target. However, ammonia features high ignition energy demand and slow flame propagation speed. Pre-chamber turbulent jet ignition, with high ignition energy and enhanced in-cylinder turbulence, shows potential for achieving efficient and stable engine combustion with low-reactivity fuels. The optical constant volume combustion chamber simulates the process of pressure environment in the engine cylinder during the compression stroke to push the unburned gas into the pre-chamber, and simulates the process of jet ignition during the pressure environment in the main combustion chamber at the end of the compression stroke. The effects of different parameters such as ambient pressure, hydrogen fraction, and orifice diameter on the turbulent jet ignition combustion were investigated. The results indicate that jet ignition is a more effective means than spark ignition to accelerate the ammonia-hydrogen mixture combustion. A hot jet carrying heat and active radicals is injected into the main chamber due to the pressure difference, and then ignites the ammonia-hydrogen mixture. With increased hydrogen volume fraction, the ignition process is advanced due to the earlier formation and higher reactivity of the hot jet. Meanwhile, the enhanced fuel reactivity and turbulent disturbance accelerate turbulent flame propagation with increased hydrogen addition. The ignition delay time and jet flame axial development are accelerated with increase in equivalence ratio from 0.6 to 1.0. With increased orifice diameter, the pre-chamber jet flame is observed due to the weakened quenching effect, leading to shortened ignition delay and extended combustion duration.
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