An aircraft assembly is disclosed including a longitudinal spar and an aerofoil cover integrally formed from a composite laminate material to form a spar-cover such that the composite material of the spar extends continuously into the cover through a fold region created between the spar and the cover. The spar and cover are separated by a recess at a longitudinal end of the fold region to define a spar end region and a cover end region, and a reinforcement element extends between the spar end region and the cover end region to couple the spar end region with the cover end region.


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    Title :

    AIRCRAFT ASSEMBLY HAVING AN INTEGRAL SPAR-COVER


    Additional title:

    FLUGZEUGANORDNUNG MIT INTEGRIERTER HOLMABDECKUNG
    ENSEMBLE D'AÉRONEF AYANT UN COUVERCLE DE LONGERON INTÉGRÉ


    Contributors:

    Publication date :

    2023-05-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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