Provided is a wing the weight of which can be reduced, with consideration given to stress concentrations in areas around access holes. A wing (1) on which a tensile load is imposed in the longitudinal direction is provided with a center section (3b), a forward section (3a), and an aft section (3c). The center section (3b) is a holed structural member that is a fiber reinforced plastic composite material article which extends in the longitudinal direction and in which access holes (5) are formed. The forward section (3a) and the aft section (3c) are reinforced plastic composite material articles that extend in the longitudinal direction of the wing (1) and are connected to the sides of the center section (3b). The tensile stiffness of the center section (3b) in the longitudinal direction is lower than the tensile stiffness of the forward section (3a) and the aft section (3c) in the longitudinal direction.


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    Titel :

    COMPOSITE MATERIAL STRUCTURE, AS WELL AS AIRCRAFT WING AND FUSELAGE PROVIDED THEREWITH


    Weitere Titelangaben:

    VERBUNDSTOFFMATERIALSTRUKTUR, SOWIE FLUGZEUGTRAGFLÄCHE UND DAMIT AUSGESTATTETER FLUGZEUGRUMPF
    STRUCTURE EN MATÉRIAU COMPOSITE, AINSI QU'AILE ET FUSELAGE D'AÉRONEF COMPORTANT CETTE STRUCTURE


    Beteiligte:
    YOSHIDA SHINICHI (Autor:in) / TANAKA HIDEAKI (Autor:in) / TANAKA YUYA (Autor:in)

    Erscheinungsdatum :

    2018-07-25


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse



    Composite material structure, and aircraft wing and aircraft fuselage provided therewith

    TANAKA YUYA / SUZUKI HIDEYUKI / KANAYAMA YUTAKA et al. | Europäisches Patentamt | 2017

    Freier Zugriff

    COMPOSITE MATERIAL STRUCTURE, AND AIRCRAFT WING AND FUSELAGE PROVIDED THEREWITH

    TANAKA YUYA / YOSHIDA SHINICHI / TANAKA HIDEAKI et al. | Europäisches Patentamt | 2018

    Freier Zugriff

    COMPOSITE MATERIAL STRUCTURE, AND AIRCRAFT WING AND FUSELAGE PROVIDED THEREWITH

    TANAKA YUYA / SUZUKI HIDEYUKI / KANAYAMA YUTAKA et al. | Europäisches Patentamt | 2019

    Freier Zugriff

    COMPOSITE MATERIAL STRUCTURE, AND AIRCRAFT WING AND FUSELAGE PROVIDED THEREWITH

    TANAKA YUYA / YOSHIDA SHINICHI / TANAKA HIDEAKI et al. | Europäisches Patentamt | 2017

    Freier Zugriff

    COMPOSITE MATERIAL STRUCTURE AND AIRCRAFT WING PROVIDED THEREWITH

    TANAKA YUYA / SUZUKI HIDEYUKI / KANAYAMA YUTAKA et al. | Europäisches Patentamt | 2019

    Freier Zugriff