In order to improve the attachments of aircraft components (16) to an aircraft wing (14) with regard to simple design and better load distribution, the invention provides an aircraft component support arrangement (46) for connecting the aircraft component (16) to an aircraft wing (14), including a component support (38) and an attachment device (48) for attaching the component support (38) to a wing structure (62), the attachment device (48) comprising:a first to third connection means (60.1, 60.2, 60.3) for connecting the component support (38) to the wing structure (62), the first to third connection means (60.1, 60.2, 60.3) each comprising a floating bearing (66.1, 66.2, 66.3) permitting linear movement in direction of a first to third axis (68.1, 68.2, 68.3), respectively, and angular rotation about a central point in two orthogonal directions, wherein the first to third connection means (60.1, 60.2, 60.3) are spaced apart from each other in two dimensions to connect the component support (38) at three different locations to the wing structure (62) and wherein at least one of the first to third axes (68.1, 68.2, 68.3) has a different orientation to the others of the first to third axes (68.1, 68.2, 68.3).


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    Titel :

    AIRCRAFT COMPONENT SUPPORT ARRANGEMENT, HIGH-LIFT SYSTEM, AIRCRAFT WING AND AIRCRAFT


    Weitere Titelangaben:

    FLUGZEUGKOMPONENTENTRÄGERANORDNUNG, AUFTRIEBSSYSTEM, FLUGZEUGFLÜGEL UND FLUGZEUG
    AGENCEMENT DE SUPPORT DE COMPOSANT D'AÉRONEF, SYSTÈME HYPERSUSTENTATEUR, AILE D'AÉRONEF ET AÉRONEF


    Beteiligte:
    ANDREANI LUC (Autor:in)

    Erscheinungsdatum :

    18.06.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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