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
20.01.2022
Patent
Elektronische Ressource
Englisch
Europäisches Patentamt | 2022
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