The invention provides a fused wing body wing and a manufacturing method, the fused wing body wing comprises a main wing, an aileron and a steering engine fairing, the main wing is of a symmetrical structure integrally formed by a left wing and a right wing and comprises a left wing section, a connecting middle section and a right wing section which are sequentially connected, and the connecting middle section is matched with a fuselage in shape and used for being connected with the fuselage; the two ailerons are movably mounted at the rear edges of the left wing section and the right wing section and can swing within a certain range; steering engine fairings are mounted on the sides, close to the fuselage, of the two ailerons. The left and right wing integrated design forming structure is adopted, the wing structure is simple, the number of parts is small, and disassembly and assembly are easy.

    本发明提供了一种翼身融合机翼及制造方法,该翼身融合机翼包括主翼、副翼和舵机整流罩,主翼为左右翼一体成型的对称结构,包括依次连接的左翼段、连接中段、右翼段,连接中段形状与机身匹配,用于与机身连接;两个副翼活动安装在左翼段、右翼段后缘处,副翼能够在一定范围内摆动;两个副翼靠近机身的一侧安装有舵机整流罩。本发明采用左右翼一体设计成型结构,机翼结构简单,零件数量少,拆装容易。


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    Titel :

    Wing with fused wing body and manufacturing method


    Weitere Titelangaben:

    一种翼身融合机翼及制造方法


    Beteiligte:
    HE LIJUN (Autor:in) / ZHOU YING (Autor:in) / CHANG MINGHE (Autor:in) / CHANG HAO (Autor:in) / LI JIANHUI (Autor:in) / ZHANG FAN (Autor:in) / GAO SHUO (Autor:in) / CHEN MINGJUN (Autor:in) / LIU YAOGUO (Autor:in)

    Erscheinungsdatum :

    24.12.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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