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高温强余旋来流条件下一体化加力燃烧室流场特性的数值研究

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为发展高温强余旋进气条件下一体化加力燃烧室性能优化方法,开展了不同结构参数变化对一体化加力燃烧室流场特性影响规律的数值模拟研究.结果表明:①扩压器长度过短容易导致流动分离,使总压恢复系数和燃烧效率降低,扩压器长度过长则会影响强余旋来流与整流支板的匹配性;②增加扩压器面积比,可以有效提升支板后回流区稳火性能、燃烧效率及总压恢复系数;③支板长度过短或过长,均会降低总压恢复系数和凹腔-中心锥一体化回流区的稳火性能;④增加支板宽度,可以有效提高燃烧效率与稳火性能;⑤增加支板尾缘扩张角,可以有效提高支板后回流区的稳火性能.
Numerical study on flow field characteristics of an integrated afterburner under high temperature and strong swirling inflow conditions
In order to develop the performance optimization method of the integrated afterburner under the condition of high temperature and strong swirling inflow,the numerical simulation of the influence of different structural parameters on the combustion flow field characteristics of the integrated afterburner was carried out.The results show that:1)If the length of the diffuser is too short,it is easy to cause flow separation and reduce the total pressure recovery coefficient and combustion efficiency.If it is too long,it will affect the matching of the strong after-swirl flow and strut.2)Increasing the diffuser area ratio can effectively improve the flame stabilization performance,combustion efficiency,and total pressure recovery coefficient of the strut.3)If the strut is too short or too long,both the total pressure recovery coefficient and the flame stabilization performance of the cavity-central cone integrated recirculation zone will be reduced.4)Increasing the width of the strut can effectively improve the combustion efficiency and flame stabilization performance.5)Increasing the expansion angle of the trailing edge of the strut can improve the flame stabilization performance of recirculation zone after the strut.

high temperature and strong swirling inflowintegrated afterburnerstructural parametertotal pressure recovery coefficientquantity of refluxflame stabilizationaero-engine

孙维斗、王一搏、黄晓锋、邓远灏、颜应文

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南京航空航天大学能源与动力学院,南京 210016

中国航发四川燃气涡轮研究院,成都 610500

高温强余旋进气 一体化加力燃烧室 结构参数 总压恢复系数 回流量 稳火 航空发动机

2024

燃气涡轮试验与研究
中国燃气涡轮研究院

燃气涡轮试验与研究

影响因子:0.146
ISSN:1672-2620
年,卷(期):2024.37(5)