A method for assembling two components and method for assembling two portions of an aircraft. A method for assembling first and second components includes, prior to the setting in place of temporary linking elements in the first and second starter holes, producing the first starter holes in the first component, depositing a sealing mastic on at least one of the first and second contact faces of the first and second components, placing the first and second components against one another, and producing second starter holes in the second component using a drilling tool connected to a suction system and equipped with a drill bush including a first part that has an outside diameter less than or equal to that of the first starter holes and a first end bearing against the second contact face of the second component upon production of the second starter holes.


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    Title :

    PROCÉDÉ D'ASSEMBLAGE DE DEUX PIÈCES ET PROCÉDÉ D'ASSEMBLAGE DE DEUX TRONÇONS D'UN AÉRONEF


    Additional title:

    METHOD FOR ASSEMBLING TWO PARTS AND METHOD FOR ASSEMBLING TWO SECTIONS OF AN AIRCRAFT
    VERFAHREN ZUM ZUSAMMENBAU VON ZWEI TEILEN, UND VERFAHREN ZUM ZUSAMMENBAU VON ZWEI ABSCHNITTEN EINES LUFTFAHRZEUGS


    Contributors:
    FARRE ERIC (author)

    Publication date :

    2021-11-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / 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 / E21B EARTH OR ROCK DRILLING , Erd- oder Gesteinsbohren




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