ASSESSMENT OF SPARK, CORONA, AND PLASMA IGNITION SYSTEMS FOR GASOLINE COMBUSTION

被引:0
作者
Biswas, Sayan [1 ]
Ekoto, Isaac [1 ]
Singleton, Dan [2 ]
Mixell, Kristapher [3 ]
Ford, Patrick [4 ]
机构
[1] Sandia Natl Labs, Livermore, CA 94550 USA
[2] Transient Plasma Syst Inc, Torrance, CA USA
[3] Tenneco Powertrain, Plymouth, MI USA
[4] Ford Motor Co, Dearborn, MI 48121 USA
来源
PROCEEDINGS OF THE ASME 2020 THE INTERNAL COMBUSTION ENGINE DIVISION FALL TECHNICAL CONFERENCE (ICEF2020) | 2020年
关键词
Corona ignition; plasma ignition; nanosecond repetitive pulsed ignition; spark ignition; advanced ignition system; NONEQUILIBRIUM PLASMA; TRANSIENT PLASMA; OXIDATION; MECHANISM;
D O I
暂无
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
In the present study, the performance and emissions characteristics of three low-temperature plasma (LTP) ignition systems were compared to a more conventional strategy that utilized a high-energy coil (93 mJ) inductive spark igniter. All experiments were performed in a single-cylinder, optically accessible, research engine. In total, three different ignition systems were evaluated: (1) an Advanced Corona Ignition System (ACIS) that used radiofrequency (RF) discharges (0.5 - 2.0 ms) to create corona streamer emission into the bulk gas via four-prong electrodes, (2) a Barrier Discharge Igniter (BDI) that used the same RF discharge waveform to produce surface LTP along an electrode encapsulated completely by the insulator, and (3) a Nanosecond Repetitive Pulse Discharge (NRPD) ignition system that used a non-resistor spark plug and positive DC pulses (similar to 10 nanoseconds width) for a fixed frequency of 100 kHz, with the operating voltage-controlled to avoid LTP transition to breakdown. For the LTP ignition systems, pulse energy and duration (or number) were varied to optimize efficiency. A single 1300 revolutions per minute (rpm), 3.5 bar indicated mean effective pressure (IMEP) homogeneous operating point was evaluated. Equivalence ratio (phi) sweeps were performed that started at stoichiometric conditions and progressed toward the lean limit. Both the ACIS and NRPD ignition systems extended the lean limit (where the variation of IMEP < 3%) limit (phi = 0.65) compared to the inductive spark (phi = 0.73). The improvement was attributed to two related factors. For the ACIS, less spark retard was required as compared to spark ignition due to larger initial kernel volumes produced by four distinct plasma streamers that emanate into the bulk gas. For the NRPD ignition system, additional pulses were thought to add expansion energy to the initial kernel. As a result, initial flame propagation was accelerated, which accordingly shortens early burn rates.
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页数:10
相关论文
共 29 条
[1]  
Biswas S., 2019, SAE Technical Paper 2019-01-0966
[2]  
Biswas S., 2019, 20199089 JSAE
[3]   OH production by transient plasma and mechanism of flame ignition and propagation in quiescent methane-air mixtures [J].
Cathey, Charles ;
Cain, Jeremy ;
Wang, Hai ;
Gundersen, Martin A. ;
Carter, Campbell ;
Ryan, Michael .
COMBUSTION AND FLAME, 2008, 154 (04) :715-727
[4]  
Chang J., 2004, NEW HEAT TRANSFER CO
[5]   Measurements of combustion efficiency in nonequilibrium RF plasma-ignited flows [J].
Chintala, N ;
Bao, AN ;
Lou, GF ;
Adamovich, IV .
COMBUSTION AND FLAME, 2006, 144 (04) :744-756
[6]  
Cruccolini V., 2020, Comparative Analysis Between a Barrier Discharge Igniter and a Streamer-Type Radio-Frequency Corona Igniter in an Optically Accessible Engine in Lean Operating Conditions
[7]   Advanced compression-ignition engines-understanding the in-cylinder processes [J].
Dec, John E. .
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2009, 32 :2727-2742
[8]  
Gheorghiu V., 2012, SUSTAINABLE AUTOMOTI
[9]  
Golloch R., 2005, MTZ WORLDWIDE, V66, P20, DOI [10.1007/BF03227737, DOI 10.1007/BF03227737]
[10]   A Computational Study of the Thermodynamic Conditions Leading to Autoignition in Nanosecond Pulsed Discharges [J].
Gururajan, Vyaas ;
Scarcelli, Riccardo ;
Karpatne, Anand ;
Breden, Douglas ;
Raja, Laxminarayan ;
Biswas, Sayan ;
Ekoto, Isaac .
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2021, 143 (11)