An electric power generation controller for use in an aircraft is a controller of an electric power generating apparatus including a manual transmission configured to change speed of rotational power of an aircraft engine, transmit the rotational power to an electric power generator, and switch a gear stage by a friction clutch pressed by an actuator. The electric power generation controller includes a manual transmission control section configured to control the manual transmission. The manual transmission control section includes: a shift command section configured to output a shift signal which switches the gear stage of the manual transmission; and a clutch control section configured to, when switching the gear stage of the manual transmission, control clutch pressure of the actuator such that the friction clutch becomes a half-engaged state.
ELECTRIC POWER GENERATION CONTROLLER FOR USE IN AIRCRAFT AND ELECTRIC POWER GENERATING APPARATUS INCLUDING SAME
STEUERGERÄT FÜR EINE ERZEUGUNGSVORRICHTUNG FÜR ELEKTRISCHEN STROM FÜR FLUGZEUG UND DAMIT AUSGESTATTETE ERZEUGUNGSVORRICHTUNG
DISPOSITIF DE COMMANDE POUR DISPOSITIF DE GÉNÉRATION DE PUISSANCE ÉLECTRIQUE POUR AÉRONEF ET DISPOSITIF DE GÉNÉRATION DE PUISSANCE ÉQUIPÉ DE CELUI-CI
28.08.2024
Patent
Elektronische Ressource
Englisch
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