TY - JOUR
T1 - Numerical study of effects on combustion characteristics and emissions of an X-type rotary engine by ignition location under wide open throttle conditions
AU - Zou, Run
AU - Li, Liangyu
AU - Yang, Wei
AU - Liu, Jinxiang
AU - Li, Feng
AU - Zhang, Lei
N1 - Publisher Copyright:
© 2024 Elsevier Ltd
PY - 2024/12/15
Y1 - 2024/12/15
N2 - The coupling of ignition position with chamber structure significantly affects combustion performance of an X-rotary engine (XRE). In the work, a three-dimensional simulation model of the XRE was established, and effects of ignition location on combustion characteristics and emissions were numerically investigated. Results showed that at the later stage of compression stroke, a complex vortex was formed in the recess of the XRE at medium to high engine speeds, which significantly affected ignition kernel development and flame propagation. The ignition location situated in the middle of the recess accelerated flame propagation by fully utilizing surrounding space and higher velocity field formed at the transition between the vortex and the vortex-free flow field, thus significantly shortening combustion duration. Meanwhile, this ignition scenario had the largest peak pressure, which increased by more than 30% over the worst scenario. Moreover, this ignition scenario had higher indicated thermal efficiency and indicated mean effective pressure at high-speed conditions, but also higher NOx generation. Peak pressure was reduced with increasing engine speed. The maximum peak pressure at 4500 RPM was 26.2% lower than that at 1500 RPM. Notably, ignition location had a slight effect on formations of Soot and CO in the XRE.
AB - The coupling of ignition position with chamber structure significantly affects combustion performance of an X-rotary engine (XRE). In the work, a three-dimensional simulation model of the XRE was established, and effects of ignition location on combustion characteristics and emissions were numerically investigated. Results showed that at the later stage of compression stroke, a complex vortex was formed in the recess of the XRE at medium to high engine speeds, which significantly affected ignition kernel development and flame propagation. The ignition location situated in the middle of the recess accelerated flame propagation by fully utilizing surrounding space and higher velocity field formed at the transition between the vortex and the vortex-free flow field, thus significantly shortening combustion duration. Meanwhile, this ignition scenario had the largest peak pressure, which increased by more than 30% over the worst scenario. Moreover, this ignition scenario had higher indicated thermal efficiency and indicated mean effective pressure at high-speed conditions, but also higher NOx generation. Peak pressure was reduced with increasing engine speed. The maximum peak pressure at 4500 RPM was 26.2% lower than that at 1500 RPM. Notably, ignition location had a slight effect on formations of Soot and CO in the XRE.
KW - Combustion characteristics
KW - Emissions
KW - Ignition location
KW - Numerical simulation
KW - X-type rotary engine
UR - http://www.scopus.com/inward/record.url?scp=85206918883&partnerID=8YFLogxK
U2 - 10.1016/j.energy.2024.133436
DO - 10.1016/j.energy.2024.133436
M3 - Article
AN - SCOPUS:85206918883
SN - 0360-5442
VL - 312
JO - Energy
JF - Energy
M1 - 133436
ER -