A propeller locking mechanism (100) for an aircraft includes a mounting ring having a locking extension with an aperture. A solenoid (112) is configured with a solenoid pin (113) which interacts with a first arm (110A) of a lever (110). The lever includes a pivotable second arm (110B) configured with a spring (108) and locking pin (106). The second arm is able to pivot and insert the locking pin into the aperture (118) of the locking extension on the mounting ring. The spring biases the locking pin in the locked orientation. Upon sufficient motor torque, the spring force is overcome allowing the locking pin to be removed from the aperture and the mounting ring to be unlocked.


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    Titel :

    PROPELLER LOCKING MECHANISM


    Weitere Titelangaben:

    PROPELLERVERRIEGELUNGSMECHANISMUS
    MÉCANISME DE VERROUILLAGE D'HÉLICE


    Beteiligte:
    KOSEL TADEJ (Autor:in)

    Erscheinungsdatum :

    11.06.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen / B64C AEROPLANES , Flugzeuge



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