TY - GEN
T1 - Experimental studies of n-pentane/air ignition by using a multi-channel spark
AU - Zhao, Hao
AU - Zhao, Ningbo
AU - Wu, Shuqun
AU - Ma, Guoming
AU - Yan, Chao
AU - Ju, Yiguang
N1 - Funding Information:
This work was supported by NSF CBET-1507358 research grant and Army Research Office with grant number W911NF-16-1-0076 and W911NF-19-20127.
Publisher Copyright:
© 2020, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
Copyright:
Copyright 2020 Elsevier B.V., All rights reserved.
PY - 2020/1
Y1 - 2020/1
N2 - A three-channel spark igni tion techni que was developed to i ncrease the fuel lean ignition probability i n the present study. By fi xi ng the total igni tion energy, a spati all y separated and temporall y synchroni zed di scharge was performed i n thi s ignition system to i ncrease the igni tion vol ume. The di scharge performance between the mul ti-channel and si ngle-channel igni tion systems was i nvestigated i n a spheri cal bomb with di fferent pressures, discharge gaps. It shows that the igni tion probability is i ncreased and the fuel-lean igni tion limit is extend i n the mul ti-channel spark system at di fferent discharge gaps. And under conditions of smaller discharge di stances the enhancement due to the mul ti-channel spark is more signi ficant.
AB - A three-channel spark igni tion techni que was developed to i ncrease the fuel lean ignition probability i n the present study. By fi xi ng the total igni tion energy, a spati all y separated and temporall y synchroni zed di scharge was performed i n thi s ignition system to i ncrease the igni tion vol ume. The di scharge performance between the mul ti-channel and si ngle-channel igni tion systems was i nvestigated i n a spheri cal bomb with di fferent pressures, discharge gaps. It shows that the igni tion probability is i ncreased and the fuel-lean igni tion limit is extend i n the mul ti-channel spark system at di fferent discharge gaps. And under conditions of smaller discharge di stances the enhancement due to the mul ti-channel spark is more signi ficant.
UR - http://www.scopus.com/inward/record.url?scp=85092410989&partnerID=8YFLogxK
U2 - 10.2514/6.2020-0429
DO - 10.2514/6.2020-0429
M3 - Conference article published in proceeding or book
AN - SCOPUS:85092410989
SN - 9781624105951
T3 - AIAA Scitech 2020 Forum
BT - AIAA Scitech 2020 Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Scitech Forum, 2020
Y2 - 6 January 2020 through 10 January 2020
ER -