The invention relates to an airplane windshield window frame skeleton assembly which comprises a window frame skeleton, the window frame skeleton comprises a main windshield opening frame surrounding a main windshield of an airplane and a side windshield opening frame surrounding a side windshield of the airplane, and the main windshield opening frame, the side windshield opening frame, the corresponding main windshield and the corresponding side windshield are installed and matched into a whole in a tight fit mode. Load transmission of the airplane is achieved. The two main windshield opening frames are in direct contact and are connected in an involution mode, and the main windshield opening frames and the side windshield opening frames are also in direct contact and are connected in an involution mode. Through the folding connection design of the opening frames of the four integral window frame frameworks and the use of the connecting band plates at the butt joint sections of the opening frames, the force transmission route of the window frame frameworks at the connection sections is directly changed, higher load transmission efficiency and higher structure use efficiency are achieved, and on the premise that the bearing design requirement is met, due to the fact that the window frame section form is simple, the structure is simple, and cost is low. And the manufacturing difficulty and the manufacturing cost are greatly reduced.

    本发明涉及一种飞机风挡窗框骨架组件,其包括:窗框骨架,窗框骨架包括围绕飞机的主风挡的主风挡口框和围绕飞机的侧风挡的侧风挡口框,并且主风挡口框和侧风挡口框与对应的主风挡和侧风挡通过紧配合的形式安装配合成形一体,实现飞机的载荷传递。两个主风挡口框直接接触并且对合连接,主风挡口框与侧风挡口框也是直接接触并且对合连接。四个整体式窗框骨架的口框的对合连接设计和在口框对接断面处使用连接带板使得窗框骨架在连接断面处传力路线更改直接,实现了更高的传载效率,更高的结构使用效率,在满足承载设计需求的前提下,由于窗框截面形式简单,大大降低了制造难度和制造成本。


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    Titel :

    Aircraft windshield window frame framework assembly


    Weitere Titelangaben:

    飞机风挡窗框骨架组件


    Beteiligte:
    XU LINA (Autor:in) / LI KUNPENG (Autor:in) / ZHONG WENLIANG (Autor:in) / WANG ZHILONG (Autor:in) / LUO LIN (Autor:in) / WANG YI-FENG (Autor:in)

    Erscheinungsdatum :

    2023-09-05


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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