The invention concerns a spar structure (11) for connecting a moveable component (4) to an aircraft. The structure is formed from a single continuous body of material defining a plurality of attachment/actuation brackets (10A-10F) and a pair of continuous hinge lines (6, 7) extending through the body.

    L'invention concerne une structure de longeron (11) destinée à relier un élément mobile (4) à un aéronef. La structure est formée à partir d'un seul corps continu de matériau définissant une pluralité de supports de fixation/actionnement (10A-10F) et une paire de lignes continues d'articulation (6, 7) s'étendant à travers le corps.


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    Title :

    HINGE STRUCTURE


    Additional title:

    STRUCTURE D'ARTICULATION


    Contributors:
    DE GRAFF THEO (author) / THOOLEN JOS (author)

    Publication date :

    2020-10-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    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



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