401. Research on knocking characteristics of kerosene spark-ignition engine for unmanned aerial vehicle (UAV) by numerical simulation
- Author
-
Zhenfeng Zhao, Jin Li, Xiaolin Wang, Lei Zhou, and Fujun Zhang
- Subjects
Fluid Flow and Transfer Processes ,Kerosene ,business.industry ,020209 energy ,02 engineering and technology ,Combustion ,Automotive engineering ,020401 chemical engineering ,Spark-ignition engine ,0202 electrical engineering, electronic engineering, information engineering ,Environmental science ,Exhaust gas recirculation ,Ignition timing ,0204 chemical engineering ,Engine knocking ,Gasoline ,business ,Intensity (heat transfer) - Abstract
The favorable physicochemical properties of kerosene have contributed to its widely application in aviation. However, knocking is more prone to take place in kerosene than in gasoline under the same conditions. This paper presents a study on the knock characteristics of a ROTAX914 engine that is fueled by kerosene. The knocking combustion process was simulated under various engine operating conditions. The effect of engine ignition timing, exhaust gas recirculation (EGR), and mixture concentration on the engine knocking combustion were studied based on a three-dimensional simulation. The results showed that engine knock could be effectively suppressed by delayed ignition timing. With increased EGR rates, knocking intensity was greatly suppressed.
- Published
- 2019
- Full Text
- View/download PDF