TY - GEN
T1 - Numerical simulation of pollutant emission of a turbojet engine with water injection
AU - Sun, Lanxin
AU - Sun, Tao
AU - Wang, Yanmin
AU - Yang, Wen
N1 - Publisher Copyright:
© Copyright 2016 by ASME.
PY - 2016
Y1 - 2016
N2 - Numerical simulation of a turbojet engine with water injection from the compressor inlet has been executed to evaluate the effect of wet compression on the pollutant emission in this paper. Water injection technique has shown the advantage of reducing the compression work and increasing the power output, and can also reduce the gas temperature in the combustion chamber and turbine which can help to reduce the thermal fatigue of the hot parts and extend their service life. Previous studies have indicated that there is a great relationship between pollutant emission of NOx and the combustion temperature, so the decrease of combustion temperature can reduce the amount of pollutant production of aircrafts especially near the airport because of the takeoff and landing of the aircrafts. And this potential of meeting the increasingly stringent pollutant emission target of water injection technique has aroused great interest of the world major engine manufacturers and research institutions. Compared with cases of no water injection, the results of this study show that the inlet temperature of combustion chamber drops obviously because of water injection, the average NO concentration in combustion chamber decreases greatly, but the concentration of CO increases significantly. Analysis of the results shows that based on fuel consumption of per unit mass the relation between the NO production in combustion chamber and the mass water evaporation varies according to the exponential law and CO production in water injection cases is similar to the cases without water injection.
AB - Numerical simulation of a turbojet engine with water injection from the compressor inlet has been executed to evaluate the effect of wet compression on the pollutant emission in this paper. Water injection technique has shown the advantage of reducing the compression work and increasing the power output, and can also reduce the gas temperature in the combustion chamber and turbine which can help to reduce the thermal fatigue of the hot parts and extend their service life. Previous studies have indicated that there is a great relationship between pollutant emission of NOx and the combustion temperature, so the decrease of combustion temperature can reduce the amount of pollutant production of aircrafts especially near the airport because of the takeoff and landing of the aircrafts. And this potential of meeting the increasingly stringent pollutant emission target of water injection technique has aroused great interest of the world major engine manufacturers and research institutions. Compared with cases of no water injection, the results of this study show that the inlet temperature of combustion chamber drops obviously because of water injection, the average NO concentration in combustion chamber decreases greatly, but the concentration of CO increases significantly. Analysis of the results shows that based on fuel consumption of per unit mass the relation between the NO production in combustion chamber and the mass water evaporation varies according to the exponential law and CO production in water injection cases is similar to the cases without water injection.
KW - Full engine simulation
KW - NOx reduction
KW - Numerical simulation
KW - Pollutant emission
KW - Water injection
UR - https://www.scopus.com/pages/publications/84991294585
U2 - 10.1115/GT2016-57074
DO - 10.1115/GT2016-57074
M3 - 会议稿件
AN - SCOPUS:84991294585
T3 - Proceedings of the ASME Turbo Expo
BT - Aircraft Engine; Fans and Blowers; Marine
PB - American Society of Mechanical Engineers (ASME)
T2 - ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition, GT 2016
Y2 - 13 June 2016 through 17 June 2016
ER -