Study on Ignition Characteristics of Microwave Radiation Ignitor

This study explored methods used to improve the ignition efficiency of a microwave radiation igniter; experimental analyses were conducted to characterize the device’s performance in a model combustion chamber. High-speed imaging combined with an image intensifier tracked flame kernel formation and propagation dynamics under varying airflow rates, residual gas coefficients, and microwave pulse parameters. The results demonstrate that increased airflow rates reduced the relative decline in ignition delay time under microwave application, with the flame area growth curve exhibiting a steeper slope compared to non-microwave conditions. Elevated residual gas coefficients enhanced the microwave-induced reduction in ignition delay time, though this effect weakened significantly in fuel-rich environments. Additionally, higher microwave pulse frequencies and peak power levels both contributed to shorter ignition delay times; the delay decreased linearly with the rising pulse frequency and followed a power-dependent reduction trend. These findings systematically quantify the synergistic effects of flow dynamics, residual gases, and microwave parameters on ignition performance.

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Publication Details

Journal
Aerospace
Published
2025-03-04
DOI
https://doi.org/10.3390/aerospace12030208
Primary Topic
Advanced Combustion Engine Technologies
Type
article
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article

Study on Ignition Characteristics of Microwave Radiation Ignitor

Zhiyu Zhao, Changqin Fu, Hao Zeng
Aerospace
Advanced Combustion Engine Technologies
article

Study on Ignition Characteristics of Microwave Radiation Ignitor

Zhiyu Zhao, Changqin Fu, Hao Zeng
article en

Abstract

This study explored methods used to improve the ignition efficiency of a microwave radiation igniter; experimental analyses were conducted to characterize the device’s performance in a model combustion chamber. High-speed imaging combined with an image intensifier tracked flame kernel formation and propagation dynamics under varying airflow rates, residual gas coefficients, and microwave pulse parameters. The results demonstrate that increased airflow rates reduced the relative decline in ignition delay time under microwave application, with the flame area growth curve exhibiting a steeper slope compared to non-microwave conditions. Elevated residual gas coefficients enhanced the microwave-induced reduction in ignition delay time, though this effect weakened significantly in fuel-rich environments. Additionally, higher microwave pulse frequencies and peak power levels both contributed to shorter ignition delay times; the delay decreased linearly with the rising pulse frequency and followed a power-dependent reduction trend. These findings systematically quantify the synergistic effects of flow dynamics, residual gases, and microwave parameters on ignition performance.

AerospaceVol. 12(3)
Air Force Engineering University (CN), Xi'an Jiaotong University (CN)
Openalex Percentile: Top 97%
Advanced Combustion Engine Technologies
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Study on Ignition Characteristics of Microwave Radiation Ignitor — Zhiyu Zhao, Changqin Fu, et al. · Aerospace (2025) | TGRS Research Map | TGRS