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Technologies and studies of gas exchange in two-stroke aircraft piston engine:A review
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作者 Yu ZHOU Xueyu LI +6 位作者 Shuiting DING Shuai ZHAO Kun ZHU Longtao SHAO Farong DU Gerui WANG Zheng XU 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2024年第1期24-50,共27页
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 ... 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. 展开更多
关键词 aircraft piston engine aircraft power systems Gas exchange High-altitude performance In-cylinder flow TWO-STROKE Unmanned Aerial Vehicles(UAVs)
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The Effect of Ignition Parameters on the Combustion Characteristics of an Aviation Piston Engine
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作者 Luda Zhu Wenming Cheng +1 位作者 Eryang Liu Shupeng Wang 《World Journal of Engineering and Technology》 2024年第2期245-257,共13页
A cylinder combustion simulation model was established for a two-stroke aviation piston engine used in a small unmanned aerial vehicle. The influence of different ignition system parameters on the combustion process o... A cylinder combustion simulation model was established for a two-stroke aviation piston engine used in a small unmanned aerial vehicle. The influence of different ignition system parameters on the combustion process of aviation kerosene was studied using this model. The research results showed that under the working conditions of 5500 r/min and 50% throttle opening, as the ignition energy increased, the peak values of average cylinder pressure and average temperature increased, and the combustion duration shortened, The advance of the combustion center of gravity increases the tendency of the engine to knock. Under the same operating conditions, as the ignition timing advances, the peak values of average pressure and average temperature in the cylinder increase, gradually approaching the top dead center, and the tendency of engine detonation increases more significantly. 展开更多
关键词 aircraft piston engines Aviation Kerosene IGNITION Combustion Characteristics KNOCK
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