The present invention refers to a method for manufacturing a leading edge (1) of an aircraft lifting surface, the leading edge having a leading edge skin (2) and a supporting structure (3) including at least two spars span-wise arranged and fixed internally to the leading edge skin. In the method of the invention, the supporting structure (3) is obtained from a single laminate (4) of plies of composite material, which is conformed in such a manner that in a cross-sectional view of the same, the laminate includes a trapezoidal configuration which forms a front spar (5) and a rear spar (6) of the supporting structure. The invention also refers to a leading edge obtained by the above-described method. Since the supporting structure of the leading edge is obtained from a single component, namely the laminate (4), the manufacturing method is simplified and production costs are significantly reduced.


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    Titel :

    A leading edge for an aircraft lifting surface and manufacturing method thereof


    Weitere Titelangaben:

    Nasenleiste für eine Tragfläche und Verfahren zu ihrer Herstellung
    Bord d'attaque pour surface portante d'aéronef et son procédé de fabrication



    Erscheinungsdatum :

    2016-01-06


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B29D PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE , Herstellen besonderer Gegenstände aus Kunststoff oder aus Stoffen in plastischem Zustand / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B64C AEROPLANES , Flugzeuge



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