The present invention provides an aircraft fuel tank monitoring system and a method of monitoring an aircraft fuel tank, the aircraft fuel tank monitoring system comprising: at least one first sensor for sensing a pressure of fuel within the fuel tank; the second sensor is used for sensing the pressure of the missing space above the fuel in the fuel tank; and a processor for monitoring a change in the pressure of the fuel within the fuel tank over a period of time and for monitoring a change in the pressure of the missing space within the fuel tank over the period of time, and for determining a fault if the monitored pressure change exceeds a normal operating condition.

    本发明提供了飞行器燃料箱监测系统以及监测飞行器燃料箱的方法,该飞行器燃料箱监测系统包括:至少一个第一传感器,第一传感器用于感测燃料箱内的燃料的压力;至少一个第二传感器,第二传感器用于感测燃料箱内的燃料上方的缺量空间的压力;处理器,该处理器用于监测燃料箱内的燃料的压力在一时间段内的变化,并且用于监测燃料箱内的缺量空间的压力在该时间段内的变化,并且用于在监测到的压力变化超过正常运行状况的情况下确定故障。


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    Titel :

    Aircraft fuel tank monitoring system and method of monitoring aircraft fuel tank


    Weitere Titelangaben:

    飞行器燃料箱监测系统以及监测飞行器燃料箱的方法


    Beteiligte:
    VIGNOLA DYLAN (Autor:in) / FALLON ADAM (Autor:in)

    Erscheinungsdatum :

    26.11.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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