| Advances in plasma-assisted ignition and combustion for combustors of aerospace engines | |
Li, Mengzhe1; Wang, Zhikai2; Xu, Rongguang3; Zhang, Xiaoliang3; Chen, Zhitong3,4 ; Wang Q(汪球)5
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| Corresponding Author | Chen, Zhitong([email protected]) ; Wang, Qiu([email protected]) |
| Source Publication | AEROSPACE SCIENCE AND TECHNOLOGY
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| 2021-10-01 | |
| Volume | 117Pages:27 |
| ISSN | 1270-9638 |
| Abstract | 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. |
| Keyword | Non-equilibrium plasma Plasma-assisted ignition Plasma-assisted combustion Aerospace engine Combustor Extreme condition |
| DOI | 10.1016/j.ast.2021.106952 |
| Indexed By | SCI ; EI |
| Language | 英语 |
| WOS ID | WOS:000687270600002 |
| WOS Keyword | HYBRID REPETITIVE NANOSECOND ; SWIRL-STABILIZED FLAME ; DISCHARGE PLASMA ; TRAPPED-VORTEX ; AIR MIXTURES ; EMISSION CHARACTERISTICS ; FLOW CHARACTERISTICS ; ANNULAR COMBUSTOR ; NONTHERMAL PLASMA ; NOX REDUCTION |
| WOS Research Area | Engineering |
| WOS Subject | Engineering, Aerospace |
| Funding Project | National Natural Science Foun-dation of China[11972331] ; National Natural Science Foun-dation of China[12072352] |
| Funding Organization | National Natural Science Foun-dation of China |
| Classification | 一类 |
| Ranking | 1 |
| Contributor | Chen, Zhitong ; Wang, Qiu |
| Citation statistics | |
| Document Type | 期刊论文 |
| Identifier | http://dspace.imech.ac.cn/handle/311007/87369 |
| Collection | 高温气体动力学国家重点实验室 |
| Affiliation | 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 |
| Recommended Citation 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.Rp_Au:Chen, Zhitong, Wang, Qiu |
| 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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| File Name/Size | DocType | Version | Access | License | ||
| Jp2021F427.pdf（8841KB） | 期刊论文 | 出版稿 | 开放获取 | CC BY-NC-SA | View Download | |
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