空军工程大学学报2024,Vol.25Issue(5) :53-59.DOI:10.3969/j.issn.2097-1915.2024.05.007

一体化加力燃烧室燃油自燃特性研究

An Investigation on Spontaneous Combustion Characteristics of Fuel in Integrated Afterburner

费力 赵兵兵 王壮壮 何立明
空军工程大学学报2024,Vol.25Issue(5) :53-59.DOI:10.3969/j.issn.2097-1915.2024.05.007

一体化加力燃烧室燃油自燃特性研究

An Investigation on Spontaneous Combustion Characteristics of Fuel in Integrated Afterburner

费力 1赵兵兵 2王壮壮 1何立明3
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作者信息

  • 1. 空军工程大学航空机务士官学校,河南信阳,464099
  • 2. 空军工程大学航空工程学院,西安,710038
  • 3. 西北工业大学动力与能源学院,西安,710129
  • 折叠

摘要

为探索一体化加力燃烧室内发生自燃现象的规律,以一体化支板中的燃油喷射系统为研究对象,采用高速摄影法拍摄了燃油在高温来流条件下的自燃火焰,重点分析了一体化加力燃烧室来流温度、来流速度、余气系数、燃油喷嘴类型等因素对于燃油自燃特性的影响规律.结果表明:提高加力燃烧室来流温度使得燃油更容易发生自燃,当来流温度超过1 200 K时所有工况下燃油都可以发生自燃;提高加力燃烧室来流速度有利于抑制自燃,使得燃油自燃延迟距离增大;贫油情况下燃油颗粒可以从环境中吸收更多的热量,自燃延迟距离减小;雾化效果好的锥形雾化喷嘴容易发生自燃,雾化效果差的直射式喷嘴相对稳定.研究结果为一体化加力燃烧室的供油系统和点火系统的设计提供初步的参考价值.

Abstract

In order to investigate the law of spontaneous combustion in the integrated afterburner,taking the fuel injection system in the integrated strut as a research object and adopting the spontaneous combus-tion flame of the fuel under the condition of high temperature inflow recorded by high-speed photography,the effects of input temperature,inlet velocity,residual gas coefficient and fuel nozzle type on the sponta-neous combustion properties of the integrated afterburner are investigated.The results show that the incre-ment of afterburner inlet temperature makes spontaneous combustion easy,and spontaneous combustion can occur under all conditions when the inlet temperature exceeds 1200 K.The increment of afterburner flow velocity is advantageous to the suppression of spontaneous combustion,making the spontaneous com-bustion delay distance of fuel increase.In the case of lean oil,fuel particles can absorb more heat from the environment,and the delay distance of spontaneous combustion is reduced.Conical atomizing nozzles with good atomization effect are prone to spontaneous combustion,while direct atomizing nozzles with poor at-omization effect are relatively stab.The research results provide a preliminary reference value for the de-sign of oil supply system and ignition system of integrated afterburner.

关键词

航空发动机/加力燃烧室/航空燃油/自燃/自燃延迟距离

Key words

aeroengine/afterburner/aviation kerosene/spontaneous combustion/spontaneous combustion delay distance

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基金项目

国家自然科学基金(52276142)

出版年

2024
空军工程大学学报
空军工程大学科研部

空军工程大学学报

CSTPCDCSCD北大核心
影响因子:0.55
ISSN:2097-1915
参考文献量5
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