The invention relates to a method for manufacturing an aerodynamic structure (34) comprising a first panel (42) having an aerodynamic surface (F34) and a reinforced second panel (44), characterized in that the manufacturing method comprises: a step of stamping the second panel (44) to obtain at least one concave-convex shape (46), the at least one concave-convex shape part is concavely arranged on the second surface (44.2); and a step of connecting the first and second panels (42, 44) by pressing the first and second panels (42, 44) against each other outside the concave-convex shape portion (46). The invention also relates to an aerodynamic structure obtained using said method.

    本发明涉及一种用于制造空气动力学结构(34)的方法,所述空气动力学结构包括具有空气动力学面(F34)的第一面板(42)以及增强的第二面板(44),其特征在于,所述制造方法包括:冲压所述第二面板(44)以获得至少一个凹凸形状部(46)的步骤,所述至少一道凹凸形状部凹入在第二面(44.2)上;以及通过将所述第一面板和第二面板(42,44)在所述凹凸形状部(46)之外彼此压靠来使所述第一面板和所述第二面板连结的步骤。本发明还涉及一种使用所述方法获得的空气动力学结构。


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    Title :

    Method for manufacturing aircraft aerodynamic structure and aircraft aerodynamic structure obtained thereby


    Additional title:

    用于制造飞行器空气动力学结构的方法和由此获得的飞行器空气动力学结构


    Contributors:

    Publication date :

    2022-09-23


    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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