The present invention discloses an aircraft structural component and a method of manufacturing an aircraft structural component, the aircraft structural component comprising: a flange having a non-planar side; and a web having a first end extending from the non-planar side of the flange and a second end distal from the first end and distal from the non-planar side of the flange, the web has a non-planar shape deviating from a plane perpendicular to the non-planar side of the flange and extending in the longitudinal direction of the aircraft structural component, the web has a non-planar shape such that a deviation of the non-planar shape of the web from the plane increases with a distance along the web in a direction from one of the first and second ends to the other of the first and second ends, and such that the deviation extends over a length of at least 10 cm of the aircraft structural component.

    本发明公开了一种飞行器结构部件及制造飞行器结构部件的方法,该飞行器结构部件包括:凸缘,凸缘具有非平面侧部;以及腹板,腹板具有第一端部和第二端部,该第一端部从凸缘的非平面侧部延伸,该第二端部远离第一端部并且远离凸缘的非平面侧部,其中,腹板具有偏离垂直于凸缘的非平面侧部并且在飞行器结构部件的纵向方向上延伸的平面的非平面形状,使得腹板的非平面形状与所述平面的偏差随着沿着腹板在从第一端部和第二端部中的一者至第一端部和第二端部中的另一者的方向上的距离而增加,并且使得该偏差在飞行器结构部件的至少10cm的长度上延伸。


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    Titel :

    Aircraft structural component and method of manufacturing aircraft structural component


    Weitere Titelangaben:

    飞行器结构部件及制造飞行器结构部件的方法


    Beteiligte:
    BRYANT STEWART (Autor:in) / BARNETT THOMAS (Autor:in)

    Erscheinungsdatum :

    2024-05-21


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    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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