Methods and systems useful during assembly of aircraft are disclosed. One such method comprises loading a fuselage of the aircraft that is unassembled with a wing of the aircraft to obtain a configuration of the fuselage corresponding to when the fuselage is assembled with the wing. The method also comprises calibrating a device of a navigation system of the aircraft when the fuselage is unassembled with the wing and is being loaded to obtain the loaded configuration and, after calibrating the device of the navigation system, assembling the fuselage with the wing.


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    Title :

    SIMULATION OF LOADS ON AEROSTRUCTURES DURING AIRCRAFT ASSEMBLY


    Additional title:

    SIMULIEREN DER BELASTUNG VON FLUGZEUGSTRUKTUREN WÄHREND EINER FLUGZEUGMONTAGE
    SIMULATION DE CHARGES SUR DES AÉROSTRUCTURES PENDANT L'ASSEMBLAGE D'AÉRONEF


    Contributors:

    Publication date :

    2019-05-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    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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