Technologies and studies of gas exchange in two-stroke aircraft piston engine: A review

被引:13
|
作者
Zhou, Yu [1 ,2 ]
Li, Xueyu [2 ,3 ]
Ding, Shuiting [1 ,4 ]
Zhao, Shuai [1 ,2 ]
Zhu, Kun [5 ]
Shao, Longtao [2 ,6 ]
Du, Farong [1 ,2 ]
Wang, Gerui [1 ,2 ]
Xu, Zheng [7 ]
机构
[1] Beihang Univ, Res Inst Aeroengine, Beijing 100191, Peoples R China
[2] Aircraft Engine Integrated Syst Safety Beijing Key, Beijing 100191, Peoples R China
[3] Beihang Univ, Sch Transportat Sci & Engn, Beijing 100191, Peoples R China
[4] Civil Aviat Univ China, Tianjin 300300, Peoples R China
[5] Aero Engine Acad China, Beijing 101304, Peoples R China
[6] Beihang Univ, Sch Energy & Power Engn, Beijing 100191, Peoples R China
[7] Beihang Hangzhou Innovat Inst Yuhang, Hangzhou 310052, Peoples R China
基金
中国国家自然科学基金; 国家重点研发计划;
关键词
Aircraft piston engine; Aircraft power systems; Gas exchange; High-altitude performance; In-cylinder flow; Unmanned Aerial Vehicles; Two-stroke; (UAVs); LARGE-EDDY SIMULATION; SCAVENGE PORT ANGLES; COMBUSTION PROCESS; OPPOSED-PISTON; HEAVY FUEL; PERFORMANCE; DESIGN; MODEL; EFFICIENCY; GASOLINE;
D O I
10.1016/j.cja.2022.08.012
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The in-cylinder gas exchange process is crucial to the power performance of two-stroke aircraft piston engines, which is easily influenced by complex factors such as high-altitude performance variation and in-cylinder flow characteristics. This paper reviews the development history and characteristics of gas exchange types, as well as the current state of theory and the validation methods of gas exchange technology, while also discusses the trends of cutting-edge technologies in the field. This paper provides a theoretical foundation for the optimization and engineering design of gas exchange systems and, more importantly, points out that the innovation of gas exchange types, the modification of theoretical models, and the technology of variable airflow organization are the key future research directions in this field. (c) 2022 Production and hosting by Elsevier Ltd. on behalf of Chinese Society of Aeronautics and Astronautics. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/ licenses/by-nc-nd/4.0/).
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页码:24 / 50
页数:27
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