Abstract
This paper deals with investigations of gas discharge in a recently developed plasma pilot for ignition and flame control. The characteristic features of this discharge burning mode are extremely low current (about 0.1 A) and low average power (less than 100 W). However, ignition and flame stabilization in a wide range of equivalence ratios for air-hydrocarbon mixtures are demonstrated. The physical mechanism of ignition is associated with the nonsteady-state properties of discharge. At the low current level, discharge burns in a kind of glow mode, and because of the glow-to-spark transition, the high-current nanosecond pulses are superimposed on the glow plasma background. Then spark discharge initiates combustion process, which is efficiently sustained in the glow plasma.
| Original language | English |
|---|---|
| Pages (from-to) | 2507-2513 |
| Number of pages | 7 |
| Journal | IEEE Transactions on Plasma Science |
| Volume | 34 |
| Issue number | 6 |
| DOIs | |
| Publication status | Published - Dec 2006 |
Fingerprint
Keywords
- Combustion stabilization
- Glow-to-spark transition
- Plasma pilot
- Plasma torches
ASJC Scopus subject areas
- Physics and Astronomy(all)
- Condensed Matter Physics
Cite this
Nonsteady-state processes in a plasma pilot for ignition and flame control. / Korolev, Yuri D.; Matveev, Igor B.
In: IEEE Transactions on Plasma Science, Vol. 34, No. 6, 12.2006, p. 2507-2513.Research output: Contribution to journal › Article
}
TY - JOUR
T1 - Nonsteady-state processes in a plasma pilot for ignition and flame control
AU - Korolev, Yuri D.
AU - Matveev, Igor B.
PY - 2006/12
Y1 - 2006/12
N2 - This paper deals with investigations of gas discharge in a recently developed plasma pilot for ignition and flame control. The characteristic features of this discharge burning mode are extremely low current (about 0.1 A) and low average power (less than 100 W). However, ignition and flame stabilization in a wide range of equivalence ratios for air-hydrocarbon mixtures are demonstrated. The physical mechanism of ignition is associated with the nonsteady-state properties of discharge. At the low current level, discharge burns in a kind of glow mode, and because of the glow-to-spark transition, the high-current nanosecond pulses are superimposed on the glow plasma background. Then spark discharge initiates combustion process, which is efficiently sustained in the glow plasma.
AB - This paper deals with investigations of gas discharge in a recently developed plasma pilot for ignition and flame control. The characteristic features of this discharge burning mode are extremely low current (about 0.1 A) and low average power (less than 100 W). However, ignition and flame stabilization in a wide range of equivalence ratios for air-hydrocarbon mixtures are demonstrated. The physical mechanism of ignition is associated with the nonsteady-state properties of discharge. At the low current level, discharge burns in a kind of glow mode, and because of the glow-to-spark transition, the high-current nanosecond pulses are superimposed on the glow plasma background. Then spark discharge initiates combustion process, which is efficiently sustained in the glow plasma.
KW - Combustion stabilization
KW - Glow-to-spark transition
KW - Plasma pilot
KW - Plasma torches
UR - http://www.scopus.com/inward/record.url?scp=33947379172&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=33947379172&partnerID=8YFLogxK
U2 - 10.1109/TPS.2006.884791
DO - 10.1109/TPS.2006.884791
M3 - Article
AN - SCOPUS:33947379172
VL - 34
SP - 2507
EP - 2513
JO - IEEE Transactions on Plasma Science
JF - IEEE Transactions on Plasma Science
SN - 0093-3813
IS - 6
ER -