The invention relates to a system for monitoring a payload of an aircraft, wherein the system has at least one storage surface (26, 28, 30, 32, 36, 38, 42) for a payload and at least one pressure sensor (10), wherein the at least one sensor (10) is designed to sense a weight and its centre of gravity of a payload resting on the storage surface (26, 28, 30, 32, 36, 38, 42). The invention further relates to an aircraft and to a method for operating an aircraft.

    L'invention concerne un système de surveillance d'une charge utile d'un aéronef, le système présentant au moins une surface de stockage (26, 28, 30, 32, 36, 38, 42) pour une charge utile et au moins un capteur de pression (10), le ou les capteurs (10) étant conçus pour détecter un poids et son centre de gravité d'une charge utile reposant sur la surface de stockage (26, 28 30, 32, 38, 42). L'invention concerne également un aéronef et un procédé pour faire fonctionner un aéronef.


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    Title :

    PAYLOAD MONITORING SYSTEM, AIRCRAFT AND METHOD


    Additional title:

    SYSTEME DE SURVEILLANCE D'UNE CHARGE UTILE, AERONEF ET PROCEDE


    Contributors:

    Publication date :

    2021-04-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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