Experimental investigation of the ignition dynamics in a premixed annular combustor using a pre-chamber ignition system

• The PCC ignition system reduces ignition time in the annular combustor significantly. • PPC accelerates flame propagation over traditional ignition in the annular combustor. • Ignition using PCC is highly reliable in lean conditions in annular combustors. In this paper, the ignition characteristics in a MICCA-type annular combustor are studied for the first time using a pre-chamber combustion (PCC) system. The PCC is proposed to replace the traditional spark electrode ignitor in the annular combustor, aiming to shorten ignition time and prevent misfiring. The PCC system is commonly utilized to initiate the ignition process in internal combustion (IC) engines by generating high-temperature turbulent jets that ignite the fuel/air mixture in the main combustion chamber (MCC). The PCC is integrated into a premixed annular combustor consists of sixteen swirling burners. The ignition characteristics and flame propagation patterns are investigated using a high-speed camera under varying conditions of equivalence ratios, bulk velocities, and thermal power levels. Experimental results demonstrate that the PCC exhibits a high ignition response without misfire. The induced turbulent jet from the PCC is observed to propagate into both sides of the annular combustor with high energy, creating a significant initial flame area along the jet trajectory. This enhances the ignition probability compared to traditional spark electrode ignition systems. Due to the higher burning rate resulting from the jet ignition, the light-round time is reduced by 41 % compared to traditional spark electrode ignition systems operating at the same equivalence ratio of 0.81 and the same bulk velocity of 3.22 m/s. This improvement is particularly advantageous for high-altitude re-ignition scenarios.

Authors

Institutions

Publication Details

Journal
Energy Conversion and Management X
Published
2024-10-01
DOI
https://doi.org/10.1016/j.ecmx.2024.100754
Citations
4
Primary Topic
Combustion and flame dynamics
Type
article
Field-Weighted Citation Impact
1.50

Funders

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

Experimental investigation of the ignition dynamics in a premixed annular combustor using a pre-chamber ignition system

Haiwen Ge, Hui Wang, Elsayed Barakat, Zhixin Zhu et al.
4 citations
Energy Conversion and Management X
Combustion and flame dynamics
1.50
article

Experimental investigation of the ignition dynamics in a premixed annular combustor using a pre-chamber ignition system

Haiwen Ge, Hui Wang, Elsayed Barakat, Zhixin Zhu, Haroun Hassan, Chenghao Qian, Gaofeng Wang
article en
4 citations

Abstract

• The PCC ignition system reduces ignition time in the annular combustor significantly. • PPC accelerates flame propagation over traditional ignition in the annular combustor. • Ignition using PCC is highly reliable in lean conditions in annular combustors. In this paper, the ignition characteristics in a MICCA-type annular combustor are studied for the first time using a pre-chamber combustion (PCC) system. The PCC is proposed to replace the traditional spark electrode ignitor in the annular combustor, aiming to shorten ignition time and prevent misfiring. The PCC system is commonly utilized to initiate the ignition process in internal combustion (IC) engines by generating high-temperature turbulent jets that ignite the fuel/air mixture in the main combustion chamber (MCC). The PCC is integrated into a premixed annular combustor consists of sixteen swirling burners. The ignition characteristics and flame propagation patterns are investigated using a high-speed camera under varying conditions of equivalence ratios, bulk velocities, and thermal power levels. Experimental results demonstrate that the PCC exhibits a high ignition response without misfire. The induced turbulent jet from the PCC is observed to propagate into both sides of the annular combustor with high energy, creating a significant initial flame area along the jet trajectory. This enhances the ignition probability compared to traditional spark electrode ignition systems. Due to the higher burning rate resulting from the jet ignition, the light-round time is reduced by 41 % compared to traditional spark electrode ignition systems operating at the same equivalence ratio of 0.81 and the same bulk velocity of 3.22 m/s. This improvement is particularly advantageous for high-altitude re-ignition scenarios.

Energy Conversion and Management XVol. 24
Shenyang Aerospace University (CN), Mansoura University (EG), Zhejiang Lab (CN), Zhanjiang Experimental Station (CN), Aero Engine Corporation of China (China) (CN), Zhejiang University (CN), Aswan University (EG)
National Natural Science Foundation of China, National Science and Technology Major Project, National Major Science and Technology Projects of China
Openalex Percentile: Top 20%
Combustion and flame dynamics
1.50
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.