Advances in plasma-assisted ignition and combustion for combustors of aerospace engines

doi:10.1016/j.ast.2021.106952

	Advances in plasma-assisted ignition and combustion for combustors of aerospace engines
	Li, Mengzhe 1; Wang, Zhikai 2; Xu, Rongguang 3; Zhang, Xiaoliang 3; Chen, Zhitong3,4 ; Wang Q(汪球)5
通讯作者	Chen, Zhitong(zt.chen@nmed.org.cn) ; Wang, Qiu(wangqiu@imech.ac.cn)
发表期刊	AEROSPACE SCIENCE AND TECHNOLOGY
	2021-10-01
卷号	117 页码:27
ISSN	1270-9638
摘要	The improvement of the ignition and combustion performance of aerospace engines under extreme conditions such as high altitude, low temperature, low pressure, and high speed is a research topic of broad and current interest. Plasma technology has attracted increasing attention due to its significant potential in improving ignition and combustion performance. Scientists and engineers have conducted numerous investigations and experiments on the use of plasma technology in aerospace engines, especially in aviation gas turbine engines, driving the research and applications of plasma-assisted ignition (PAI) and plasma-assisted combustion (PAC). The aim of this comprehensive review paper is to summarize and discuss the developments and applications of PAI and PAC in the fields of aerospace engines during the last ten years, including ignition, lean blow-out, combustion efficiency, emission, outlet temperature distribution quality, combustion stability, and fuel distribution. This review paper mainly focuses on experimental research progress. We also introduce new applications of PAI and PAC in novel aerospace engines and discuss the prospects for its practical implementation. (C) 2021 Elsevier Masson SAS. All rights reserved.
关键词	Non-equilibrium plasma Plasma-assisted ignition Plasma-assisted combustion Aerospace engine Combustor Extreme condition
DOI	10.1016/j.ast.2021.106952
收录类别	SCI ; EI
语种	英语
WOS记录号	WOS:000687270600002
关键词[WOS]	HYBRID REPETITIVE NANOSECOND ; SWIRL-STABILIZED FLAME ; DISCHARGE PLASMA ; TRAPPED-VORTEX ; AIR MIXTURES ; EMISSION CHARACTERISTICS ; FLOW CHARACTERISTICS ; ANNULAR COMBUSTOR ; NONTHERMAL PLASMA ; NOX REDUCTION
WOS研究方向	Engineering
WOS类目	Engineering, Aerospace
资助项目	National Natural Science Foun-dation of China[11972331] ; National Natural Science Foun-dation of China[12072352]
项目资助者	National Natural Science Foun-dation of China
论文分区	一类
力学所作者排名	1
RpAuthor	Chen, Zhitong ; Wang, Qiu
引用统计	被引频次：29[WOS] [WOS记录] [WOS相关记录]
文献类型	期刊论文
条目标识符	http://dspace.imech.ac.cn/handle/311007/87369
专题	高温气体动力学国家重点实验室
作者单位	1.Northwestern Polytech Univ, Sci & Technol Combust Internal Flow & Thermostruc, Xian 710072, Peoples R China; 2.AECC Hunan Aviat Powerplant Res Inst, Zhuzhou 412002, Peoples R China; 3.George Washington Univ, Dept Mech & Aerosp Engn, Washington, DC 20052 USA; 4.Natl Innovat Ctr Adv Med Devices, Shenzhen 518000, Peoples R China; 5.Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China
推荐引用方式 GB/T 7714	Li, Mengzhe,Wang, Zhikai,Xu, Rongguang,et al. Advances in plasma-assisted ignition and combustion for combustors of aerospace engines[J]. AEROSPACE SCIENCE AND TECHNOLOGY,2021,117:27.
APA	Li, Mengzhe,Wang, Zhikai,Xu, Rongguang,Zhang, Xiaoliang,Chen, Zhitong,&汪球.(2021).Advances in plasma-assisted ignition and combustion for combustors of aerospace engines.AEROSPACE SCIENCE AND TECHNOLOGY,117,27.
MLA	Li, Mengzhe,et al."Advances in plasma-assisted ignition and combustion for combustors of aerospace engines".AEROSPACE SCIENCE AND TECHNOLOGY 117(2021):27.

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