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基于驻涡稳定的无焰燃烧室实验研究
Experimental Study of Flameless Combustor based On Trapped-Vortex
【摘要】 本文通过将凹腔驻涡技术和无焰燃烧技术相结合,设计了一种基于凹腔驻涡的燃油无焰燃烧室,并对其进行了实验研究。重点关注了空气温度、空气流量、凹腔当量比和主当量比对无焰燃烧的形成和燃烧室污染物排放特性的影响。在实验基础上总结了航空发动机凹腔驻涡燃烧室形成无焰燃烧的条件,为该种燃烧室的设计提供依据。
【Abstract】 In this paper,experimental study is carried out on a liquid flameless combustor,which is designed based on the idea of making use of both trapped-vortex technology and flameless combustion technology. During the experiment,emphasis is placed on the influence of inlet air temperature,air flow rate,equivalence radio of reentrant and main equivalence,aiming to study the condition under which flameless combustion will take place and the combustion characteristic of the combustor. The conclusion may be useful for designing a flameless combustor.
【关键词】 无焰燃烧;
凹腔驻涡;
燃烧特性;
航空发动机;
低排放;
【Key words】 flameless combustion; trapped-vortex; combustion characteristic; aircraft engine; low emission;
【Key words】 flameless combustion; trapped-vortex; combustion characteristic; aircraft engine; low emission;
【基金】 国家自然科学基金项目“燃气轮机燃烧室中低热值富氢燃料无焰燃烧特性研究”(资助号:50706054)
- 【文献出处】 燃气轮机技术 ,Gas Turbine Technology , 编辑部邮箱 ,2014年03期
- 【分类号】V231.2
- 【被引频次】8
- 【下载频次】188