A system and method for detecting fixed pitch operation of a variable pitch propeller (130) of an engine (110). A command signal for maintaining a rotational speed of the propeller (130) at a reference speed is output. An actual value of at least one of the rotational speed and a blade angle of the propeller (130) is obtained. From the actual value, it is assessed whether an expected change in the at least one of the rotational speed and the blade angle of the propeller (130) has occurred in response to the command signal. Responsive to determining that the expected change in the at least one of the rotational speed and the blade angle of the propeller (130) has not occurred in response to the command signal, operation of the propeller (130) at fixed pitch is detected and an alert output accordingly.


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    Titel :

    SYSTEM AND METHOD FOR DETECTING PROPELLER MALFUNCTION


    Weitere Titelangaben:

    SYSTEM UND VERFAHREN ZUR ERKENNUNG VON PROPELLERFEHLFUNKTIONEN
    SYSTÈME ET PROCÉDÉ DE DÉTECTION DE DYSFONCTIONNEMENT D'HÉLICE


    Beteiligte:
    KRZYWON JAGODA (Autor:in)

    Erscheinungsdatum :

    09.10.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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