The invention relates to the technical field of an airplane seat, and particularly relates to a carbon fiber airplane seat bearing fixing structure, which is mainly used for solving the technical problems that the stress when the carbon fiber airplane seat is assembled and fixed is non-uniform. According to the technical solution, the carbon fiber airplane seat bearing fixing structure consists of a seat base, a seat cross bar, a base chuck and a locked screw, wherein a seat base main body is a pair of right-angled triangular supporting frames, an arc fixed bracket is arranged on an acute-angle end of a bottom right-angled edge, the acute-angle end of a vertical angle edge and the upper end of the arc fixed bracket are provided with the base chuck, the base cross bar is fixed in the base chuck, and two base cross bars are parallel to each other. Under the situation that the overall design of the existing product is not changed, by adjusting the design of the assembled fixed structure, the strength and stability of the product can be improved.


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    Titel :

    Carbon fiber airplane seat bearing fixing structure


    Beteiligte:
    XIONG DAOWU (Autor:in) / CAI JIE (Autor:in)

    Erscheinungsdatum :

    2016-02-03


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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