首页|结构参数对RQL燃烧室燃烧性能影响

结构参数对RQL燃烧室燃烧性能影响

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本文研究了一种以涡流片结构作为火焰筒头部旋流装置的RQL燃烧室的结构参数对燃烧室燃烧性能的影响。采用数值模拟研究了主燃孔、涡流片数、淬熄孔轴向位置、淬熄孔内外环数及淬熄孔类型对燃烧室内的流动、燃烧性能及NOx排放特性的影响。结果表明,燃烧室富油区内的流动是靠涡流片与主燃孔的有效配合来实现的。涡流片的数量是影响富油区内回流区的形状及大小的主要参数,通过优化涡流片数量可以获得所需要的流场;淬熄区通过淬熄孔快速射流完成由富油向贫油的瞬间过渡,且防止接近理想当量比的NOx生成量大的区域;淬熄孔的轴向位置、类型等结构参数是影响燃烧性能的主要结构参数。
Influence of Structural Parameters on Combustion Performance of RQL Combustor
In this paper,the influence of structural parameters on combustion performance of a RQL combustor with vortex plate structure as a swirling device at the head of flame cylinder is studied.The influences of the main combustion hole,the number of vortex plates,the axial position of the quenched hole,the number of inner and outer rings of the quenched hole and the type of quenched hole on the flow,combustion performance and NOx emission characteristics in the combustion chamber were studied by numerical simulation.The results show that the flow in the oil-rich area of the combustion chamber is realized by the effective coordination between the vortex plate and the main combustion hole.The number of eddies is the main parameter that affects the shape and size of the reflux area in the oil-rich region.The desired flow field can be obtained by optimizing the number of eddies.The quenching zone can complete the instantaneous transition from rich oil to poor oil through the quenching hole rapid jet flow,and prevent the area with large NOx generation close to the ideal equivalent ratio.Structural parameters such as axial position and type of quenched hole are the main structural parameters that affect combustion performance.

rich-burn/quench/lean-burn(RQL)combustion chambervortex platequenched holenitrogen oxides(NOx)

惠蕾、刘爱虢、吴小取、张云杰、王鹏

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沈阳航空航天大学航空发动机学院辽宁省航空推进系统先进测试技术重点实验室,沈阳 110136

富油/淬熄/贫油(RQL)燃烧室 涡流片 淬熄孔 氮氧化物(NOx)

沈阳市科技计划项目中航产学研合作项目

22-322-3-30HFZL2023CXY004

2024

工程热物理学报
中国工程热物理学会 中国科学院工程热物理研究所

工程热物理学报

CSTPCD北大核心
影响因子:0.4
ISSN:0253-231X
年,卷(期):2024.45(10)