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
2024-05-01
Patent
Electronic Resource
English
ELECTRIC AIRCRAFT ENGINE AND COMPRESSOR FOR ENGINE RETROFIT
European Patent Office | 2024
|ELECTRIC AIRCRAFT ENGINE AND COMPRESSOR FOR ENGINE RETROFIT
European Patent Office | 2024
|NTRS | 1977
|HYBRID AIRCRAFT ENGINE WITH COMPRESSOR CONTROL FOR ELECTRIC MOTOR FAILURE
European Patent Office | 2025
|