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Direct Injection Hydrogen Combustion under Leaner Conditions in an Optical Engine using Optical/Laser Diagnostics

Abstract

Hydrogen’s increasing potential as an alternative fuel for heavy-duty transport has led to the conversion of conventional diesel compression-ignition engines to spark-ignition hydrogen operation. Hydrogen’s broad flammability range enables leaner operation achieving both higher engine efficiency and near-zero emissions. In particular, direct injection hydrogen combustion improves volumetric efficiency and reduces problems including pre-ignition and knock related to hydrogen port-fuel injection. In the present work, we performed an optical investigation of direct injection (DI) hydrogen combustion under leaner mixture conditions. The study was conducted using a heavy-duty optical diesel engine modified for spark-ignition operation. Bottom-view natural flame luminosity and OH-PLIF imaging were conducted along with in-cylinder pressure measurements. Experiments were conducted at three air-excess ratios (3, 3.4, and 3.8) with spark timings (ST) varied from − 15 ◦CA aTDC to − 30 ◦CA aTDC. Hydrogen injection ended at − 30 ◦CA aTDC, with the start of injection adjusted accordingly to achieve the desired lambda conditions. The maximum IMEPg corresponded to the lowest COV of the IMEPg, indicating optimal spark timing for lean DI hydrogen combustion. The optimized spark timing for λ = 3, λ = 3.4, and λ = 3.8 were occurred at − 25 ◦CA aTDC, − 25 ◦CA aTDC, and − 30 ◦CA aTDC, respectively. The corresponding COV of IMEPg values were below 5 % indicating stable combustion. The flame kernel first initiates at the spark plug and then propagates toward the piston’s outer boundary, however, the flame propagation does not remain as a continuous front unlike port-fuel injected hydrogen combustion. The effect of fuel stratification is evident in combustion luminosity and OH-PLIF images, showing pockets of varying intensity within the combustion chamber. Natural flame luminosity images reveal incomplete flame coverage and asymmetric combustion, emphasizing the need for metal engine experiments to further quantify the unburned hydrogen and associated combustion losses.

Funding source: This work was supported by the Saudi Aramco FUELCOM program under Master Research Agreement 6600024505/01.
Related subjects: Applications & Pathways
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/content/journal8288
2025-11-12
2026-02-24
/content/journal8288
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