The invention refers to a trailing edge (2) for a composite lifting surface (1), comprising: a spar (22); upper and lower panels (9) comprising a free edge (23); a seal (5); and an elongated profile (7) located on the panels (9) following the spanwise direction of the trailing edge (2) and comprising: a web (71) extended along the spanwise direction of the trailing edge (2), and first and second flange portions (72, 73) having a transition zone (74) in between to extend at different heights with respect to each other, the first flange portion (72) configured to hold at least a part of the seal (5) underneath, and the second flange portion (73) configured to contact the panel (9), the first flange portion (72) fixing the seal (5) to the panel (9), and the second flange portion (73) fixing the elongated profile (7) to the panel (9).


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    Title :

    TRAILING EDGE FOR A COMPOSITE LIFTING SURFACE


    Additional title:

    HINTERKANTE FÜR EINE ZUSAMMENGESETZTE HUBFLÄCHE
    BORD DE FUITE POUR SURFACE PORTANTE COMPOSITE


    Contributors:

    Publication date :

    2021-11-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F16J Kolben , PISTONS



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