An experimental study on the influence of nozzle hole numbers and patterns of a passive pre-chamber spark ignition system

Pre-chamber spark ignition system enhances the combustion stability and efficiency of lean burn engines . Pre-chamber spark ignition system performance directly relies on the characteristics of the turbulent flame jet, which are governed by the pre-chamber geometrical parameters and nozzle hole configurations. Based on the existing literatures, limited research on nozzle hole numbers and patterns is noted with passive pre-chamber, and thus, the impact of these nozzle hole configurations on the combustion and flame development characteristics for hydrogen-methane-air mixtures is investigated in a constant volume combustion chamber . In the current study, single-layer nozzle hole configurations with three, four, six, and eight nozzle holes and double-layer nozzle hole configurations with six and eight nozzle holes are designed and tested in an optically accessible combustion chamber under various equivalence ratio conditions. The results indicated that the combustion characteristics deteriorated with an increase in nozzle holes, except with the single-layer four nozzle hole configuration. Compared to the single-layer eight nozzle hole configuration, the ignition delay and combustion duration for hydrogen-methane-air mixtures with single-layer four nozzle hole configuration was reduced by 31.9% and 30.7% under lean conditions. A reduction in flame jet penetration length, area and velocity and increased adjacent flame jet interaction was noticed for the single-layer configuration with more nozzle holes, and thus, a different nozzle hole pattern was studied in the current study. The double-layer configurations with more nozzle holes showed better combustion and flame development characteristics than single-layer configurations due to their unique flame structure, uniform and faster flame jet distribution, and reduced adjacent flame jet interaction. The ignition delay and combustion duration for hydrogen-methane-air mixtures with the double layer eight nozzle hole configuration were reduced by 30.5% and 40.7% compared to the single-layer eight nozzle hole configuration. • Combustion characteristics deteriorated with an increase in pre-chamber nozzle holes. • SL-H4 configuration exhibited better combustion and flame development characteristics. • Increased jet interaction and reduced jet penetration was noted for more nozzle holes. • DL-H8 configuration improved the combustion process with a unique flame structure.

Authors

Institutions

Publication Details

Journal
International Journal of Hydrogen Energy
Published
2024-10-20
DOI
https://doi.org/10.1016/j.ijhydene.2024.10.226
Citations
9
Primary Topic
Combustion and Detonation Processes
Type
article
Field-Weighted Citation Impact
11.69

Funders

Controls
|||
ALL TIME
JAN
FEB
MAR
APR
MAY
JUN
JUL
AUG
SEP
OCT
article

An experimental study on the influence of nozzle hole numbers and patterns of a passive pre-chamber spark ignition system

Kalil basha Jeelan basha, Vedharaj Sivasankaralingam, Sathishkumar Balasubramani
9 citations
International Journal of Hydrogen Energy
Combustion and Detonation Processes
11.69
article

An experimental study on the influence of nozzle hole numbers and patterns of a passive pre-chamber spark ignition system

Kalil basha Jeelan basha, Vedharaj Sivasankaralingam, Sathishkumar Balasubramani
article en
9 citations

Abstract

Pre-chamber spark ignition system enhances the combustion stability and efficiency of lean burn engines . Pre-chamber spark ignition system performance directly relies on the characteristics of the turbulent flame jet, which are governed by the pre-chamber geometrical parameters and nozzle hole configurations. Based on the existing literatures, limited research on nozzle hole numbers and patterns is noted with passive pre-chamber, and thus, the impact of these nozzle hole configurations on the combustion and flame development characteristics for hydrogen-methane-air mixtures is investigated in a constant volume combustion chamber . In the current study, single-layer nozzle hole configurations with three, four, six, and eight nozzle holes and double-layer nozzle hole configurations with six and eight nozzle holes are designed and tested in an optically accessible combustion chamber under various equivalence ratio conditions. The results indicated that the combustion characteristics deteriorated with an increase in nozzle holes, except with the single-layer four nozzle hole configuration. Compared to the single-layer eight nozzle hole configuration, the ignition delay and combustion duration for hydrogen-methane-air mixtures with single-layer four nozzle hole configuration was reduced by 31.9% and 30.7% under lean conditions. A reduction in flame jet penetration length, area and velocity and increased adjacent flame jet interaction was noticed for the single-layer configuration with more nozzle holes, and thus, a different nozzle hole pattern was studied in the current study. The double-layer configurations with more nozzle holes showed better combustion and flame development characteristics than single-layer configurations due to their unique flame structure, uniform and faster flame jet distribution, and reduced adjacent flame jet interaction. The ignition delay and combustion duration for hydrogen-methane-air mixtures with the double layer eight nozzle hole configuration were reduced by 30.5% and 40.7% compared to the single-layer eight nozzle hole configuration. • Combustion characteristics deteriorated with an increase in pre-chamber nozzle holes. • SL-H4 configuration exhibited better combustion and flame development characteristics. • Increased jet interaction and reduced jet penetration was noted for more nozzle holes. • DL-H8 configuration improved the combustion process with a unique flame structure.

International Journal of Hydrogen EnergyVol. 91
National Institute of Technology Tiruchirappalli (IN)
Department of Science and Technology, Ministry of Science and Technology, India, Science and Engineering Research Board
Climate action
Openalex Percentile: Top 2%
Combustion and Detonation Processes
11.69
AI Navigator

Ask Laika to Summarize, Analyze, and Connect papers live on the map.

Summarize Papers & Methodologies

Extract key findings, datasets, and comparative methods across publications.

Benchmark Rankings & Visual Analytics

Rank top research institutions, authors, funders, topics, and journals by Field-Weighted Citation Impact (FWCI) and paper volume with instant charts.

Connect Distant Disciplines

Bridge topological clusters on the map to find hidden collaborative intersections.