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.

    本发明涉及一种用于将可移动部件(4)连接到飞机的翼梁结构(11)。该结构由单个连续材料形体以及延伸穿过该形体的一对连续铰链线(6、7)形成,该形体限定多个附接/致动支架(10A至10F)。


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    Title :

    HINGE STRUCTURE


    Additional title:

    铰链结构


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

    Publication date :

    2022-02-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    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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