Lean Flame Stabilization With Nanosecond Plasma Discharges in a Gas Turbine Model Combustor - Archive ouverte HAL
Communication Dans Un Congrès Année : 2023

Lean Flame Stabilization With Nanosecond Plasma Discharges in a Gas Turbine Model Combustor

Résumé

This paper presents an experimental study of lean flames stabilization with nanosecond repetitively pulsed discharges. The two-stage, swirled-stabilized, multipoint injector BIMER operates at atmospheric pressure with methane-air mixtures in the present study. It is representative in its design of a realistic lean premixed prevaporized injector of gas turbine engines operated at a lab-scale level. The lean blow-off extension with plasma is characterized. The combustion efficiency and the pollutant emissions are quantified near blow-off with and without plasma for 50-kW flames. We show that it is possible to stabilize lean flames down to an equivalence ratio of 0.3, with less than 5 ppm of NOx emitted, thanks to NRP discharges with an electric power that represents less than 0.25% of the flame thermal power. This study also clearly shows that it is necessary to account for the plasma system integration at the early stage of the combustor design to fully benefit from the plasma stabilizing effects on the flame.
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Dates et versions

hal-04311330 , version 1 (11-12-2023)

Identifiants

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Victorien Blanchard, Frédéric Roqué, Philippe Scouflaire, Christophe O Laux, Sébastien Ducruix. Lean Flame Stabilization With Nanosecond Plasma Discharges in a Gas Turbine Model Combustor. ASME Turbo Expo 2023: Turbomachinery Technical Conference and Exposition, Jun 2023, Boston, United States. pp.GT2023-102621, ⟨10.1115/GT2023-102621⟩. ⟨hal-04311330⟩
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