The invention belongs to the technical field of aircraft aerodynamic layout and control strategy design of the aircraft aerodynamic layout, and particularly relates to an aircraft aerodynamic layout structure and a control method of the aircraft aerodynamic layout structure. The two canards are installed on the two sides of the front section of the fuselage, provided with actuating cylinders and capable of driving the two canards to extend out of the fuselage or retract into the fuselage; the two wings are mounted on two sides of the middle section of the fuselage; the two leading edge inner flaps are arranged on the inner sides of the leading edges of the two wings; the two leading edge outer flaps are arranged on the outer sides of the leading edges of the two wings; the two trailing edge flaps are arranged on the inner sides of the two wing trailing edges; the two trailing edge ailerons are arranged on the outer sides of the trailing edges of the two wings; the two V tails are arranged on two sides of the tail part of the fuselage; the two lifting/direction coupling rudders are arranged at the rear edges of the two V tails; the two wing crane engines are hung below the two wings; and the two tail suspension engines are mounted at the tail part of the fuselage and are positioned above the connecting parts of the two V tails and the fuselage.

    本申请属于飞机气动布局及其操纵策略设计技术领域,具体涉及一种飞机气动布局结构及其操纵方法,其中,飞机气动布局结构包括:机身;两个鸭翼,安装在机身前段两侧,设置有作动筒,能够驱动两个鸭翼伸出到机身外侧或缩入机身到内部;两个机翼,安装在机身中段两侧;两个前缘内襟翼,设置在两个机翼前缘内侧;两个前缘外襟翼,设置在两个机翼前缘外侧;两个后缘襟翼,设置在两个机翼后缘内侧;两个后缘副翼,设置在两个机翼后缘外侧;两个V尾,设置在机身尾部两侧;两个升降/方向耦合舵,设置在两个V尾后缘;两个翼吊发动机,吊挂在两个机翼下方;两个尾吊发动机,安装在机身尾部,处在两个V尾与机身连接部位的上方。


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    Titel :

    Aircraft aerodynamic layout structure and control method thereof


    Weitere Titelangaben:

    一种飞机气动布局结构及其操纵方法


    Beteiligte:
    WANG WEI (Autor:in) / LI JUNFU (Autor:in) / TAN YUTING (Autor:in) / ZHAO YAN (Autor:in) / AI JUNQIANG (Autor:in) / GUO JIAHAO (Autor:in)

    Erscheinungsdatum :

    2024-03-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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