等离子体强化燃烧的目前研究进展
发布时间:2019-07-10 21:13
【摘要】:介绍了等离子体强化燃烧的基本原理,总结了等离子体强化燃烧的3种途径,分别是热强化、动力学强化与输运强化;对国际上,特别是国内在等离子体强化燃烧的应用验证、作用机制和数值仿真研究方面的最新代表性成果进行了综述.提出了等离子体强化燃烧的4个研究方向,分别是等离子体强化燃烧机理、多场耦合建模与仿真、测试诊断研究,以及等离子体强化燃烧在航空发动机中应用的其他科学与技术问题,同时提出了开展这4方面研究工作的一些建议,主要是定量研究等离子体点火与助燃的3种效应,分别建立各效应与点火特性、助燃特性之间的关系;建立等离子体强化燃烧的详细动力学模型;应用先进的测试诊断设备,发展等离子体强化燃烧的新型测试技术;考虑等离子体点火与助燃应用到不同类型发动机燃烧室时的匹配问题,特别是等离子体电源的小型化与轻型化问题等.
[Abstract]:This paper introduces the basic principle of plasma enhanced combustion, summarizes three ways of plasma enhanced combustion, namely, thermal enhancement, dynamic enhancement and transport enhancement, and summarizes the latest representative results in the application verification, action mechanism and numerical simulation of plasma enhanced combustion in the world, especially in China. Four research directions of plasma enhanced combustion are put forward, which are plasma enhanced combustion mechanism, multi-field coupling modeling and simulation, test and diagnosis, and other scientific and technical problems in the application of plasma enhanced combustion in aero-engine. At the same time, some suggestions for carrying out the research work in these four aspects are put forward, mainly to quantitatively study the three effects of plasma ignition and combustion. The relationship between each effect and ignition characteristics and combustion characteristics is established respectively. The detailed dynamic model of plasma enhanced combustion is established, the new testing technology of plasma enhanced combustion is developed by using advanced test and diagnosis equipment, and the matching problem of plasma ignition and combustion assistance applied to different types of engine combustion chambers is considered, especially the miniaturization and lightweight of plasma power supply.
【作者单位】: 空军工程大学航空航天工程学院等离子体动力学国家重点实验室;
【基金】:国家自然科学基金(51436008,50776100,51106179) 陕西省自然科学基金(2015jq5124) 空军工程大学航空航天工程学院创新基金(CXJJ201416)
【分类号】:V231.2
本文编号:2512894
[Abstract]:This paper introduces the basic principle of plasma enhanced combustion, summarizes three ways of plasma enhanced combustion, namely, thermal enhancement, dynamic enhancement and transport enhancement, and summarizes the latest representative results in the application verification, action mechanism and numerical simulation of plasma enhanced combustion in the world, especially in China. Four research directions of plasma enhanced combustion are put forward, which are plasma enhanced combustion mechanism, multi-field coupling modeling and simulation, test and diagnosis, and other scientific and technical problems in the application of plasma enhanced combustion in aero-engine. At the same time, some suggestions for carrying out the research work in these four aspects are put forward, mainly to quantitatively study the three effects of plasma ignition and combustion. The relationship between each effect and ignition characteristics and combustion characteristics is established respectively. The detailed dynamic model of plasma enhanced combustion is established, the new testing technology of plasma enhanced combustion is developed by using advanced test and diagnosis equipment, and the matching problem of plasma ignition and combustion assistance applied to different types of engine combustion chambers is considered, especially the miniaturization and lightweight of plasma power supply.
【作者单位】: 空军工程大学航空航天工程学院等离子体动力学国家重点实验室;
【基金】:国家自然科学基金(51436008,50776100,51106179) 陕西省自然科学基金(2015jq5124) 空军工程大学航空航天工程学院创新基金(CXJJ201416)
【分类号】:V231.2
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