中国航空学报(英文版)2024,Vol.37Issue(4) :243-255.DOI:10.1016/j.cja.2024.01.015

Experimental and numerical study of combustion characteristics of ammonia-hydrogen-air swirling flame with/without secondary air injection

Chunyu LIU Chenhu GAO Yue HUANG Hua JIN Dan ZHAO Wenjiang XU Yancheng YOU
中国航空学报(英文版)2024,Vol.37Issue(4) :243-255.DOI:10.1016/j.cja.2024.01.015

Experimental and numerical study of combustion characteristics of ammonia-hydrogen-air swirling flame with/without secondary air injection

Chunyu LIU 1Chenhu GAO 2Yue HUANG 2Hua JIN 2Dan ZHAO 3Wenjiang XU 2Yancheng YOU2
扫码查看

作者信息

  • 1. School of Aerospace Engineering,Xiamen University,Xiamen 361005,China;School of Mechanical Engineering,Shanghai Jiao Tong University,Shanghai 200240,China
  • 2. School of Aerospace Engineering,Xiamen University,Xiamen 361005,China
  • 3. Department of Mechanical Engineering,University of Canterbury,Christchurch 8041,New Zealand
  • 折叠

Abstract

Ammonia(NH3)is currently considered to be a potential carbon-free alternative fuel,and its large-scale use as such would certainly decrease greenhouse gas emissions and meet increas-ingly stringent emission requirements.Although the low flame propagation speed and high NO pro-duction of NH3 hinder its direct application as a renewable fuel,co-combustion of NH3-H2 is an effective way to overcome these challenges.In this study,the combustion characteristics of NH3-H2 swirling flames under different equivalence ratios and H2 blending ratios conditions are both numerically and experimentally investigated.Numerically,the One-Dimensional(1D)laminar flame computation presents a comparison base and the Three-Dimensional(3D)numerical simula-tion yields detailed flame property distributions.Experimentally,the high-speed camera takes instantaneous swirl flame images and the gas analyzer measures the NO emission at the exit plane of the flame chamber.Qualitative and quantitative analysis is performed on the flame structure and NO emission for a series of NH3-H2 swirl flames.The variation trends of the NO emission calcu-lated using different techniques agree very well.The quantitative results show that the NO emissions are much higher at lean equivalence ratios than those at rich equivalence ratios,and such difference is closely related to the combustion flame structure.Moreover,it is shown that the utilization of secondary air injection can achieve a significant reduction in NO emissions at the exit of the combustion chamber at equivalence ratios less than or equal to 0.9.

Key words

Ammonia combustion/Swirling flow/NO emission characteristics/Secondary combustion/Chemical reaction mechanism

引用本文复制引用

基金项目

国家自然科学基金(51876182)

国家自然科学基金(52006184)

中央高校基本科研业务费专项(20720180058)

Fundamental Research Funds,China(2020-JJ-118)

出版年

2024
中国航空学报(英文版)
中国航空学会

中国航空学报(英文版)

CSTPCDEI
影响因子:0.847
ISSN:1000-9361
参考文献量34
段落导航相关论文