Model and Igniter Development for Plasma Assisted Combustion

2004 ◽  
Author(s):  
Skip Williams ◽  
S. Popovic ◽  
L. Vuskovic ◽  
C. Carter ◽  
L. Jacobson ◽  
...  
Keyword(s):  
Plasma Assisted Combustion

Plasma-Assisted Combustion Technology for NOx Reduction in Industrial Burners

2013 ◽  
Vol 47 (19) ◽  
pp. 10964-10970 ◽  
Author(s):  
Dae Hoon Lee ◽  
Kwan-Tae Kim ◽  
Hee Seok Kang ◽  
Young-Hoon Song ◽  
Jae Eon Park
Keyword(s):  
Nox Reduction ◽  
Plasma Assisted Combustion ◽  
Combustion Technology

Special Issue on Plasma-Assisted Combustion

2009 ◽  
Vol 37 (12) ◽  
pp. 2273-2274
Author(s):  
Louis A. Rosocha ◽  
Igor Matveev
Keyword(s):  
Special Issue ◽  
Plasma Assisted Combustion

scholarly journals The Influence of Dielectric Barrier Discharge Plasma on the Characteristics of Aero-Engine Combustion Chamber

2019 ◽  
Vol 37 (2) ◽  
pp. 369-377
Author(s):  
Yi Chen ◽  
Li Fei ◽  
Liming He ◽  
Lei Zhang ◽  
Chunchang Zhu ◽  
...  
Keyword(s):  
Dielectric Barrier Discharge ◽  
Barrier Discharge ◽  
Combustion Efficiency ◽  
Future Application ◽  
Outlet Temperature ◽  
Plasma Assisted Combustion ◽  
Dbd Plasma ◽  
Dielectric Barrier ◽  
Rich Condition ◽  
Aero Engine

A test platform was developed to investigate the performance of aero-engine combustor by the dielectric barrier discharge (DBD) plasma assisted combustion (PAC) in the simulated maximum condition. Conventional combustion experiments and plasma-assisted combustion conditions were conducted to study the effect of PAC on the performances including average outlet temperature, combustion efficiency and pattern factor under four different excessive air coefficients five different voltages. The comparative experiment shows that the combustion efficiency is improved after PAC compared with the normal conditions, the combustion efficiency of PAC increases 2.31% in the fuel-rich condition when Up-p is 40 kV. The uniformity of the outlet temperature field is also improved after PAC, the decrease of the pattern factor is more than 5% in the fuel-rich condition. These results offer certain reference value for the future application of PAC in aero-engine combustor and improving its performance.

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