In some examples, a wing for an aircraft, the wing having a passive variable aeroelastic geometry for accommodating efficient flight at multiple aircraft speeds, comprises a wing skin comprising a composite structure comprising a lamination of multiple layers deposited for the wing skin according to a predetermined lamination profile, at least one of the layers comprising a continuous non-linear deposition of material, the wing skin comprising a stiffness distribution profile defined by the lamination profile.


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    Titel :

    AIRCRAFT WINGS COMPRISING AN AEROELASTICALLY TAILORED COMPOSITE STRUCTURE


    Weitere Titelangaben:

    FLUGZEUGFLÜGEL MIT AEROELASTISCH ANGEPASSTER FASERVERBUNDSTRUKTUR
    AILES D'AVION COMPRENANT UNE STRUCTURE COMPOSITE AEROELASTIQUEMENT CONFECTIONNÉE


    Erscheinungsdatum :

    10.04.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B29D PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE , Herstellen besonderer Gegenstände aus Kunststoff oder aus Stoffen in plastischem Zustand / B64C AEROPLANES , Flugzeuge / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung



    Supersonic flutter of aeroelastically tailored oblique wings

    WEISSHAAR, TERRENCE / BOHLMANN, JONATHAN | AIAA | 1987


    Supersonic flutter of aeroelastically tailored oblique wings

    WEISSHAAR, TERRENCE A. / BOHLMANN, JONATHAN D. | AIAA | 1989


    Aeroelastically Tailored Propellers

    Rogers, J. B. / Dwyer, W. J. | SAE Technical Papers | 1977



    Aeroelastically tailored wing design

    BROWN, JR., L. / PRICE, M. / GINGRICH, P. | AIAA | 1980