AIRCRAFT LANDING GEAR MONITORING AND ALERTING SYSTEM A landing gear monitoring and alerting system (300) 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 (308). 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 (308) 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 (128) being disposed within the aperture (106). '117 oCD U a o o C a co


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    Title :

    Aircraft landing gear monitoring and alerting system and method


    Contributors:

    Publication date :

    2021-11-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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