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

doi:10.1016/j.ast.2021.106952

CORC > 力学研究所 > 中国科学院力学研究所 > 高温气体动力学国家重点实验室

	Advances in plasma-assisted ignition and combustion for combustors of aerospace engines
	Li, Mengzhe 5; Wang, Zhikai 4; Xu, Rongguang 3; Zhang, Xiaoliang 3; Chen, Zhitong 2,3; Wang Q(汪球)1
刊名	AEROSPACE SCIENCE AND TECHNOLOGY
	2021-10-01
卷号	117 页码:27
关键词	Non-equilibrium plasma Plasma-assisted ignition Plasma-assisted combustion Aerospace engine Combustor Extreme condition
ISSN号	1270-9638
DOI	10.1016/j.ast.2021.106952
通讯作者	Chen, Zhitong(zt.chen@nmed.org.cn) ; Wang, Qiu(wangqiu@imech.ac.cn)
英文摘要	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.
分类号	一类
资助项目	National Natural Science Foun-dation of China[11972331] ; National Natural Science Foun-dation of China[12072352]
WOS关键词	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
语种	英语
WOS记录号	WOS:000687270600002
资助机构	National Natural Science Foun-dation of China
其他责任者	Chen, Zhitong ; Wang, Qiu
内容类型	期刊论文
源URL	[http://dspace.imech.ac.cn/handle/311007/87368]
专题	力学研究所_高温气体动力学国家重点实验室
作者单位	1.Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China 2.Natl Innovat Ctr Adv Med Devices, Shenzhen 518000, Peoples R China; 3.George Washington Univ, Dept Mech & Aerosp Engn, Washington, DC 20052 USA; 4.AECC Hunan Aviat Powerplant Res Inst, Zhuzhou 412002, Peoples R China; 5.Northwestern Polytech Univ, Sci & Technol Combust Internal Flow & Thermostruc, Xian 710072, 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.