Research on Combustion Performance of the Edge Blowing Mixture Curtain Flameholder

YUE Lian-jie; XIONG Jian-qiu; FAN Wei-jun; YANG Mao-lin

Chinese

您当前的位置：

首页 >

文章列表页 >

Research on Combustion Performance of the Edge Blowing Mixture Curtain Flameholder

更新时间：2026-07-07

- Research on Combustion Performance of the Edge Blowing Mixture Curtain Flameholder
- Vol. 16, Issue 4, (2001)
- 作者机构：
  
  北京航空航天大学动力系,北京,100083
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2001
- 稿件说明：
移动端阅览
YUE Lian-jie, XIONG Jian-qiu, FAN Wei-jun, et al. Research on Combustion Performance of the Edge Blowing Mixture Curtain Flameholder[J]. 2001, 16(4).
DOI：

YUE Lian-jie, XIONG Jian-qiu, FAN Wei-jun, et al. Research on Combustion Performance of the Edge Blowing Mixture Curtain Flameholder[J]. 2001, 16(4). DOI：

摘要

在初步试验研究的基础上

对尾缘吹气式稳定器进行了结构改进

并进行了燃烧性能试验研究。探讨了新型稳定器的贫熄特性

分析了尾缘吹气速度与供油量对燃烧性能的影响

比较了稳定器前方供油与稳定器内供油的不同供油方式下的燃烧性能

并和V型稳定器性能进行了对比。研究结果表明

新型稳定器是一种能稳定工作的可控高效低阻稳定器

在未来发动机加力尤其是外涵加力上具有应用前景。尾缘吹气并供油

改善了燃烧区燃油浓度分布。燃烧性能优于槽宽大1倍的V型稳定器。

Abstract

On the basis of elementary research

the geometry structure of the edge blowing mixture curtain (EBMC) flameholder was improved and the experimental study on the combustion performance of the EBMC flameholder was carried out in 2D afterburning test rig.The flame stability

the influence of jet velocity and fuel supply at the trail edge on the combustion performance and the performance difference between fuel supply from the frontal injector and jet curtain were analyzed.At the same time

V-gutter flameholder was used to compare with the new type flameholder.The results show that the new type flameholder is a controllable flameholder

that can work stably with higher efficiency and lower pressure loss.It is expected to be used in future aero-engine

especially its by-pass afterburner.

关键词

Keywords

references

Views

424

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Influence of propellant composition on performance of solid fuel ramjet

Effect of fuel distribution on combustion performance for micro gas turbine combustor,

Experiment on effects of wall cooling with microchannels on performances of swirl combustor

Comparison of combustion performance for different nozzles in gas turbine combustor

Preliminary study on combustion performance of dual-mode scramjet engine

Related Author

QIU Shuang

SU Yingli

YANG Haitao

CHEN Xuanren

LIU Aiguo

HU Jian

林志伟

黄玥

Related Institution

南京机电液压工程研究中心航空机电系统综合航空科技重点实验室

厦门大学航空航天学院

南京航空航天大学能源与动力学院

中国航空发动机集团四川燃气涡轮研究院,四川江油

AI问答

Postal code：100079
Tel：（010）53879206 Email：tmw@bjxintong.com.cn
Technical support is provided by Beijing Founder electronics co., LTD 京ICP备09082226号-64 京公网安备11010602201714号
It is recommended to read the content of this site in Chrome&IE9+. Please switch to extreme mode in browser 360.
Cookies We use cookies to help provide and enhance our service and tailor content. By continuing, you agree to the use of cookies.

⁰