Chemical effects of plasma gases on flame kernel development

A study of the plasma jet ignition of lean methane-air mixtures was conducted to determine the effect of different plasma gases on flame kernel development. A plasma igniter, incorporating a shutter that separated the gases in the igniter from the reactant gases in a combustion chamber before discharge, allowed any combination of gases to be used without mixing. Measurements of the two-dimensional distribution of OH concentration by laser-induced fluorescence in a diametral plane above the igniter yielded information on the ignition process and the subsequent flame kernel development. The methane-air mixtures chosen for study had equivalence ratios, ϕ , near the lean flammability limit of ϕ ═ 0.53. To differentiate OH formation in the initial plasma from that generated during mixing and reaction with gas in the combustion chamber, experiments were conducted using the following combinations of plasma media and reactant gases: H 2 and 2H 2 + O 2 plasmas into air; Ar, N 2 , H 2 and 2H 2 + O 2 plasmas into ϕ ═ 0.50 CH 4 -air; and 2H 2 + O 2 plasma into ϕ ═ 0.65 CH 4 -air. In addition to OH measurements, the pressure in the combustion chamber was measured, and Schlieren photographs were taken. Results indicated relatively small, chemically active regions, generally off-axis and often associated with vortices. Measurements in lean mixtures that are known to discriminate strongly between plasma of different effectiveness confirm the higher incendivity, for the same total energy, of chemically active plasmas and demonstrate the higher concentration and longer persistence of OH during the approach to steady state flame conditions. Such chemically active plasmas promote combustion for hundreds of milliseconds in normally non-flammable sub-limit mixtures.

2018 ◽  
Author(s):  
Mohammadrasool Morovatiyan ◽  
Martia Shahsavan ◽  
Mengyan Shen ◽  
John Hunter Mack

Lean-burn engines are important due to their ability to reduce emissions, increase fuel efficiency, and mitigate engine knock. In this study, the surface roughness of spark plug electrodes is investigated as a potential avenue to extend the lean flammability limit of natural gas. A nano-/micro-morphology modification is applied on surface of the spark plug electrode to increase its surface roughness. High-speed Z-type Schlieren visualization is used to investigate the effect of the electrode surface roughness on the spark ignition process in a premixed methane-air charge at different lean equivalence ratios. In order to observe the onset of ignition and flame kernel behavior, experiments were conducted in an optically accessible constant volume combustion chamber at ambient pressures and temperatures. The results indicate that the lean flammability limit of spark-ignited methane can be lowered by modulating the surface roughness of the spark plug electrode.


Author(s):  
Mohammadrasool Morovatiyan ◽  
Martia Shahsavan ◽  
Mengyan Shen ◽  
J. Hunter Mack

Lean-burn engines are important due to their ability to reduce emissions, increase fuel efficiency, and mitigate engine knock. In this study, the surface roughness of spark plug electrodes is investigated as a potential avenue to extend the lean flammability limit of natural gas. A nano-/micro-morphology modification is applied on surface of the spark plug electrode to increase its surface roughness. High-speed Z-type Schlieren visualization is used to investigate the effect of the electrode surface roughness on the spark ignition process in a premixed methane-air charge at different lean equivalence ratios. In order to observe the onset of ignition and flame kernel behavior, experiments were conducted in an optically accessible constant volume combustion chamber at ambient pressures and temperatures. The results indicate that the lean flammability limit of spark-ignited methane can be lowered by modulating the surface roughness of the spark plug electrode.


Author(s):  
Kelvin Xie ◽  
Shui Yu ◽  
Tongyang Gao ◽  
Xiao Yu ◽  
Ming Zheng ◽  
...  

In order to meet the future carbon dioxide legislation, advanced clean combustion engines are tending to employ low temperature diluted combustion strategies along with intensified cylinder charge motion. The diluted mixtures are made by means of excess air admission or exhaust gas recirculation. A slower combustion speed during the early flame kernel development because of the suppressed mixture reactivity will reduce the reliability of the ignition process and the overall combustion stability. In an effort to address this issue, an ignition strategy using a multi-pole spark igniter is tested in this work. The igniter uses three electrically independent spark gaps to allow three spatially distributed spark discharge. The multi-pole spark strategy, when observed in an optical combustion vessel with lean methane-air mixtures, visually showed increased early flame kernel growth rate. The strategy was tested on an engine using gasoline fuel and low load, lean operation at 1.35 excess air ratio. The results indicated that the combustion phasing parameters were consistently advanced under the multi-pole spark strategy. In conditions where a conventional single spark exhibited stable operation, relatively little additional benefits were seen with the multi-pole strategy. At later spark timings when cycle-to-cycle variations had a greater impact on the engine stability, the multi-pole spark reduced the combustion variability.


Author(s):  
J Song ◽  
M Sunwoo

The purpose of this study is to investigate the relation between ignition systems (or energy) and flame kernel development. In this research, three different kinds of ignition systems and several different kinds of spark plug electrodes are designed and manufactured. The flame propagation velocity in a constant volume combustion chamber is measured by both a laser deflection method using an He-Ne laser and a Schlieren method using a high speed digital camera. In order to control the ignition energy, the dwell time is varied by a spark time controller. The results indicate that, when the ignition energy is increased by extending the dwell time, flame kernel growth accelerates. As the electrode gap width is increased, the breakdown energy is also increased, which stimulates the initial kernel development. The materials, diameter and shape of the electrode affect the discharged energy, the energy transfer efficiency and heat losses and, thus, these also affect the flame kernel development. The average difference in measurement of the flame velocity by the laser deflection method and Schlieren method is only 1.73 per cent. The laser deflection method is found to be preferable because it is more effective and employs simpler means for the analysis of flame kernel development.


2007 ◽  
Vol 73 (732) ◽  
pp. 1745-1752 ◽  
Author(s):  
Shinji NAKAYA ◽  
Kazuo HATORI ◽  
Mitsuhiro TSUE ◽  
Michikata KONO ◽  
Daisuke SEGAWA ◽  
...  

2006 ◽  
Vol 2006.3 (0) ◽  
pp. 297-298
Author(s):  
Shinji NAKAYA ◽  
Kazuo HATORI ◽  
Mitsuhiro TSUE ◽  
Michikata KONO ◽  
Daisuke SEGAWA ◽  
...  

2006 ◽  
Author(s):  
Terry Alger ◽  
Barrett Mangold ◽  
Darius Mehta ◽  
Charles Roberts

Author(s):  
Stefania Falfari ◽  
Gian Marco Bianchi

In SI engines the ignition process strongly affects the combustion process. Its accurate modelling becomes a key issue for a design-oriented CFD simulation of the combustion process. Different approaches to simulate ignition have been proposed. The common base is decoupling the physics related to the very first ignition phase when a plasma is formed from that of the development of the flame kernel. The critical point of ignition models is related to the capability of representing the effect of ignition system characteristics, the criterion used for flame deposit and the initialisation of the combustion model. This paper aims to present and validates extensively an ignition model suited for CFD calculation of premixed combustion. The ignition model implemented in a customized version of the Kiva 3 code is coupled with ECFM Flamelet combustion model. The ignition model simulates the plasma/kernel expansion based on a lump evaluation of main ignition processes (i.e., breakdown, arc-phase and glow phase). A double switch criterion based on physical and numerical consideration is used to switch to the main combustion model. The Herweg and Maly experimental test case has been used to check the model capability. In particular, two different ignition systems having different amount of electrical energy released during spark discharge are considered. Comparisons with experimental results allowed testing the model with respect to its capability to reproduce the effects of mixture equivalence ratio, mean flow, turbulence and spark energy on flame kernel development as never done before in three-dimensional RANS CFD combustion modelling of premixed flames.


Sign in / Sign up

Export Citation Format

Share Document