A skin for an aircraft is configured to be disposed on a first rigid member (182). The first rigid member has at least a portion of a structural frame for the aircraft. The skin is configured to be disposed on a second rigid member (184) that has at least a portion of the structural frame for the aircraft. The second rigid member (184) is moveable with respect to the first rigid member (182) and a distance is defined between the first rigid member and the second rigid member. A morphing member of the skin extends between the first rigid member and the second rigid member. The morphing member compensates for at least one of a change in the distance and a change in an orientation between the first rigid member and the second rigid member.

    L'invention concerne un revêtement pour un aéronef qui est configuré pour être placé sur un premier élément rigide (182). Le premier élément rigide comprend au moins une partie d'une ossature structurale de l'aéronef. Le revêtement est configuré pour être placé sur un second élément rigide (184) qui comporte au moins une partie de l'ossature structurale de l'aéronef. Le second élément rigide (184) est mobile par rapport au premier élément rigide (182), et une distance est définie entre le premier élément rigide et le second élément rigide. Un élément adaptable du revêtement s'étend entre le premier élément rigide et le second élément rigide. L'élément adaptable compense un changement de distance et/ou un changement d'orientation entre le premier élément rigide et le second élément rigide.


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    Title :

    MORPHING SKIN FOR AN AIRCRAFT


    Additional title:

    REVÊTEMENT ADAPTABLE POUR UN AÉRONEF


    Contributors:

    Publication date :

    2016-03-31


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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