Plasma-Assisted Active Combustion Control as an Enabling Technology for N+3 Combustors

This proposal will develop a plasma-assisted modification to a lean direct injected(LDI)combustor to control combustion instabilities and enable clean, compact combustion. Controlling combustion dynamics in jet engine combustors continues to be a major challenge especially in advanced engine designs where, due to leaner flames, less cooling air and more turbulent injectors, there is a higher potential for damaging combustion dynamics.turbine. Various active combustion control methods have been demonstrated for improving combustion stability injet engines but they have not found wide-spread commercial use.Moreover, plasma has been shown to be a promising tool for improving flame stabilization. The rapid actuation time and authority of plasma discharges also make plasma an attractive actuator for active combustion control. Plasma can both improve both static stability via kinetic enhancement of reaction pathways and dynamic stability, especially if configured in a closed-loop configuration. Plasmas have already been demonstrated in literature to have positive effects on combustion dynamics. However, further work is necessary to understand the dynamics of flame response to plasma’s, particularly at realistic conditions.To this end, this proposal will use explore a novel method of using plasma as an active control actuator in an LDI combustor to enable reduced emissions and operation at conditions which would have otherwise been unstable. This combustor and its control system will be characterized both at atmospheric pressure as well as at high pressure and high temperature conditions representative of idle and sub idle in a modern jet engine.Various optical and acoustic diagnostics will be used to quantify the effectiveness of the plasma-assisted control system.If this work is successful, it will significantly de-risk the technology and enable partnerships with major engine manufacturers to bring this technology to market.