A landing gear monitoring and alerting system includes a locking pin (128) configured to be inserted into an aperture (126) extending through a linkage (118) of an extended landing gear assembly (106). When inserted into the aperture (126), the locking pin (128) inhibits movement of the linkage (118) to establish a locked state of the extended landing gear assembly (106). This system further includes a magnetic sensor (302) and a communication module (306). The magnetic sensor (302) is disposed proximate the aperture (126) and is configured to sense a magnetic response indicative of the locking pin (128) being disposed within the aperture (126). The magnetic sensor (302) is configured to generate a sensor output indicative of the locking pin (128) being disposed within the aperture (126). The communication module (306) has a transmitter (310) coupled to the magnetic sensor (302) so as to receive the sensor output and is configured to responsively transmit a signal indicative of the locking pin being disposed within the aperture.


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    Titel :

    AIRCRAFT LANDING GEAR MONITORING AND ALERTING SYSTEM AND METHOD


    Weitere Titelangaben:

    FLUGZEUGFAHRWERKÜBERWACHUNGS- UND -WARNUNGSSYSTEM UND -VERFAHREN
    SYSTÈME ET PROCÉDÉ DE SURVEILLANCE ET D'ALERTE DE TRAIN D'ATTERRISSAGE D'AÉRONEF


    Beteiligte:

    Erscheinungsdatum :

    2023-08-09


    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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