The invention relates to the technical field of aircraft structures, in particular to a truss rib connecting rod and an aircraft. The truss rib connecting rod provided by the embodiment of the invention comprises the first connecting rod, the second connecting rod and the connecting piece, the first connecting rod and the second connecting rod are connected through the connecting piece, and the first connecting rod and the second connecting rod are integrally formed pieces, so that the structures of the first connecting rod and the second connecting rod are more stable, and the overall strength of the truss rib connecting rod is enhanced. The first connecting rod and the second connecting rod are integrally and respectively integrated, so that during assembly, the assembly process is simpler and quicker, and the operation is simple; meanwhile, a connecting mode of the connecting rod and the connector is provided, and the connecting relation is simple and clear. The aircraft provided by the embodiment of the invention also has the technical effects as the aircraft comprises the truss rib connecting rod.

    本发明涉及飞机结构技术领域,尤其涉及一种桁架肋连杆及飞行器。本申请实施例提供的桁架肋连杆包括第一连杆、第二连杆以及连接件第一连杆和第二连杆通过连接件连接,且第一连杆和第二连杆分别都是一体成型件,使得第一连杆和第二连杆的结构更加稳定,进而增强桁架肋连杆的整体强度。将第一连杆和第二连杆整体分别为一体件,在组装时候,使得组装过程中更加简单快捷,操作简单;同时,提供了一种连杆和接头的连接形式,连接关系简单明了。本发明的实施例提供的飞行器,由于包括上述的桁架肋连杆,因此也具有上述的技术效果。


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    Titel :

    Truss rib connecting rod and aircraft


    Weitere Titelangaben:

    桁架肋连杆及飞行器


    Beteiligte:
    MA ZHIYANG (Autor:in) / GUO JIN (Autor:in) / HE TIREN (Autor:in) / XU JIFENG (Autor:in)

    Erscheinungsdatum :

    06.06.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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