A landing gear monitoring and alerting system includes a locking pin configured to be inserted into an aperture extending through a linkage of an extended landing gear assembly. When inserted into the aperture, the locking pin inhibits movement of the linkage to establish a locked state of the extended landing gear assembly. This system further includes a magnetic sensor and a communication module. The magnetic sensor is disposed proximate the aperture and is configured to sense a magnetic response indicative of the locking pin being disposed within the aperture. The magnetic sensor is configured to generate a sensor output indicative of the locking pin being disposed within the aperture. The communication module has a transmitter coupled to the magnetic sensor 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.

    一种起落架监控和警报系统,包括锁定销,该锁定销被配置成插入到延伸穿过伸出的起落架组件的连杆机构的孔隙中。当插入孔隙中时,锁定销抑制连杆机构的运动以建立伸出的起落架组件的锁定状态。该系统还包括磁传感器和通信模块。磁传感器设置在孔隙附近,并且被配置成感测指示锁定销设置在孔隙内的磁响应。磁传感器被配置成产生指示锁定销设置在孔隙内的传感器输出。通信模块具有耦接到磁传感器的发射器,以便接收传感器输出,并且通信模块被配置成响应性地传输指示锁定销设置在孔隙内的信号。


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    Titel :

    AIRCRAFT LANDING GEAR MONITORING AND ALERTING SYSTEM AND METHOD


    Weitere Titelangaben:

    飞机起落架监控和警报系统及方法


    Beteiligte:

    Erscheinungsdatum :

    09.11.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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