The invention relates to a method for monitoring a propulsion system (102) of an aircraft (100), the method comprising:-calculating a margin of a parameter (NG, T4x) of a thermal chain (TH) as a margin (PMD1, PMT1) of the thermal chain (TH); -calculating a margin of the parameter (IBAT) of the electrical chain (ELEC), taking at least a portion of the margin as the margin of the electrical chain (ELEC); adding the margin (PMD1, PMT1) of the thermal chain (TH) to the margin of the electrical chain (ELEC) to obtain a total margin (ePMD) of the propulsion system (102); and-transmitting the total margin to a display device (AF) of the aircraft (100) such that the display device (AF) displays the total margin (ePMD).

    本发明涉及一种用于监测飞行器(100)的推进系统(102)的方法,该方法包括:‑计算热链(TH)的参数(NG,T4x)的裕度,将该裕度作为热链(TH)的裕度(PMD1,PMT1);‑计算电气链(ELEC)的参数(IBAT)的裕度,将该裕度的至少一部分作为电气链(ELEC)的裕度;将热链(TH)的裕度(PMD1,PMT1)与电气链(ELEC)的裕度相加,以获得推进系统(102)的总裕度(ePMD);以及‑将总裕度传输至飞行器(100)的显示设备(AF),以使显示设备(AF)显示总裕度(ePMD)。


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    Titel :

    Monitoring of aircraft propulsion systems


    Weitere Titelangaben:

    飞行器推进系统的监测



    Erscheinungsdatum :

    11.04.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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