IGNITION PROCEDURE FOR A TURBINE ENGINE COMBUSTION CHAMBER

摘要

The invention relates to an ignition procedure for a turbine engine combustion chamber (10) supplied with fuel by injectors (26) and comprising means (28) for igniting the fuel injected into the chamber (10). This procedure comprises: an initial phase (36) during which a constant flow of fuel is injected into the chamber (10) at the same time as the ignition means (28) are energized; and, in the event of non-ignition in the chamber (10) at the end of the initial phase (36), a second phase (38) during which the injected-fuel flow rate is increased rapidly by 20 to 30%.