A slat for an aircraft wing and a method for assembling said slat, the slat comprising:- a skin wherein an outer surface of the skin forms an aerodynamic surface of the slat body and wherein the skin comprises an upper skin part and a lower skin part extending continuously from a leading edge of the skin such that the upper skin part extends further than the lower skin part seen in a direction along a center line of the slat;- a plurality of stiffeners are assembled to an inner surface of the skin;- a spar extending between the upper skin part and the lower skin part that is connected to the upper skin part and the lower skin part;- wherein the spar is provided with lugs for connection to an actuation system. (Traducción automática con Google Translate, sin valor legal)

    Method for assembling a slat, for an aircraft wing, comprising providing a skin and a plurality of stiffeners; assembling the stiffeners to the skin obtaining a skin sub-assembly; providing a spar and a plurality of lugs; assembling the lugs to the spar obtaining a spar sub-assembly; assembling the spar sub-assembly to the skin sub-assembly to obtain the slat.


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    Titel :

    Hipersustentador para un ala de aeronave, método para fabricar dicho hipersustentador


    Beteiligte:

    Erscheinungsdatum :

    26.01.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Spanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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