The invention relates to a control device for an engine, comprising means (150) for calculating a blade pitch angle setpoint (160) of at least one propeller of the engine, the calculating means (150) using a propeller performance model, taking into account at least one flight speed (115) in order to adapt a blade pitch angle setpoint by taking into account a shaft horsepower setpoint.


    Access

    Download


    Export, share and cite



    Title :

    Control device for an engine


    Contributors:

    Publication date :

    2015-09-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    ENGINE CONTROL DEVICE AND ENGINE CONTROL METHOD

    KIHARA YUSUKE / SUKEGAWA YOSHIHIRO / SHIMADA ATSUSHI et al. | European Patent Office | 2021

    Free access

    ENGINE CONTROL DEVICE AND ENGINE CONTROL METHOD

    YAMAURA TOSHIAKI | European Patent Office | 2019

    Free access

    ENGINE CONTROL DEVICE AND ENGINE CONTROL METHOD

    KIHARA YUUSUKE / SARUWATARI MASAYUKI / KOIKE YUTA | European Patent Office | 2023

    Free access

    ENGINE CONTROL DEVICE AND ENGINE CONTROL METHOD

    YAMOTO SHOKO / OKAHARA AKIO | European Patent Office | 2020

    Free access

    ENGINE CONTROL DEVICE AND ENGINE CONTROL METHOD

    KIHARA YUUSUKE / SARUWATARI MASAYUKI / KOIKE YUTA | European Patent Office | 2022

    Free access