A control method is provided for an engine. During this control method, a lambda target parameter indicative of a ratio between a stoichiometric air-to-fuel ratio and an actual air-to-fuel ratio is determined. A control signal is determined using the lambda target parameter. A component of the engine is operated based on the control signal to regulate airflow within a compressor section of the engine.
COMPRESSOR BOOST CONTROL FOR AIRCRAFT ENGINE
COMMANDE DE SURALIMENTATION POUR UN MOTEUR D'AERONEF
01.05.2024
Patent
Elektronische Ressource
Englisch
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