Inlet temperatures effect on combustion instabilitycharacteristics of stratified swirl flame

王志超; 林宇震; 韩啸; 吕丽君

doi:10.13224/j.cnki.jasp.2018.10.015

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Inlet temperatures effect on combustion instabilitycharacteristics of stratified swirl flame

更新时间：2026-07-07

- Inlet temperatures effect on combustion instabilitycharacteristics of stratified swirl flame
- Vol. 33, Issue 10, Pages: 2434-2441(2018)
- 作者机构：
  
  1. 北京航空航天大学能源与动力工程学院航空发动机气动热力国家级重点实验室,北京,100191
  2. 先进航空发动机协同创新中心,北京,100191
- 作者简介：
- 基金信息：
- DOI：10.13224/j.cnki.jasp.2018.10.015
  CLC：
- Published：2018
- 稿件说明：
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王志超, 林宇震, 韩啸, 吕丽君. 进口温度对分层旋流火焰燃烧不稳定性的影响[J]. 航空动力学报, 2018, 33(10): 2434-2441.

doi: 10.13224/j.cnki.jasp.2018.10.015
王志超, 林宇震, 韩啸, 吕丽君. 进口温度对分层旋流火焰燃烧不稳定性的影响[J]. 航空动力学报, 2018, 33(10): 2434-2441. DOI： 10.13224/j.cnki.jasp.2018.10.015.

doi: 10.13224/j.cnki.jasp.2018.10.015 DOI：

摘要

为了研究进口温度对分层旋流火焰燃烧不稳定性的影响，实验在单头部燃烧室上测量了不同进口温度下的动态压力，并采用理论分析了进口温度对压力振荡的影响。实验结果显示：该燃烧室出现的燃烧不稳定性呈现的是Helmholtz模态，并且随着进口温度从530K增加至650K时，压力脉动主频增加，幅值减小。分析表明：进口温度的增加会增强燃油的雾化和蒸发，进而加强其与空气的掺混均匀性，减小了当量比脉动，从而抑制了燃烧不稳定性，压力振荡幅值减小。

Abstract

In order to investigate the effects of inlet temperature on the combustion instability in stratified swirl combustor

the dynamic pressure under various inlet temperatures was tested using a single doom combustor

and the effects of inlet temperature on pressure oscillation were analyzed using a theory. The experimental results showed that the mode of combustion instability in this combustor was Helmholtz mode. With the increase of inlet temperature from 530K to 650K

the amplitude of pressure oscillation decreased. Analysis showed that the increase of inlet temperature can enhance fuel atomization and evaporation and then strengthen its mixing with air

making equivalence-ratio oscillation less impossible. Therefore combustion instability was less prone to occur and the dynamic pressure amplitude was smaller.

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