An aircraft structure (10) and its method of construction avoids the inefficiencies involved in current methods of constructing the aircraft structure, reduces the manufacturing time required for constructing the aircraft structure and reduces the cost involved in constructing the aircraft structure. The aircraft structure and its method of construction is comprised of a geodesic or multi-grid framework of intersecting thermoplastic composite strips (22) that are joined to an interior surface of a thermoplastic composite fuselage skin panel (18) through overmolding/co-consolidation of the grid framework and the skin panel.


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    Titel :

    МНОГОСЕТОЧНАЯ КОНСТРУКЦИЯ ФЮЗЕЛЯЖА ЛЕТАТЕЛЬНОГО АППАРАТА ИЗ ТЕРМОПЛАСТИКА, ПОЛУЧЕННАЯ ПУТЕМ МНОГОКОМПОНЕНТНОГО ФОРМОВАНИЯ/ СОВМЕСТНОЙ КОНСОЛИДАЦИИ


    Erscheinungsdatum :

    2021-01-18


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Russisch


    Klassifikation :

    IPC:    B61L Leiten des Eisenbahnverkehrs , GUIDING RAILWAY TRAFFIC