The invention discloses a fixed-wing aircraft-oriented variant wing with a continuously variable wing shape, which comprises rotary wing systems distributed on two sides of an axis of a fuselage, the rotary wing systems are mounted on the fixed wing of the fuselage, a driving motor is mounted on the fuselage, and the driving motor controls the rotary wing systems to work through a transmission system. According to the variant wing with the continuously variable wing shape for the fixed-wing aircraft, the flight performance of the fixed-wing aircraft can be improved so as to adapt to different flight environments and meet the task requirements of high-speed, low-speed and short-distance take-off and landing, and therefore large-speed-range and full-time maneuvering flight of the aircraft is achieved.

    本发明公开了面向固定翼飞机的连续可变翼形的变体机翼,包括分布在机身轴线两侧的转翼系统,转翼系统安装在机身的固定式机翼上,机身上安装有驱动电机,驱动电机通过传动系统控制转翼系统工作。本发明所提供的面向固定翼飞机的连续可变翼形的变体机翼,能提升固定翼飞机的飞行性能,以适应不同的飞行环境,满足高速、低速、短距起降的任务需求,从而实现飞行器的大速域、全时段的机动飞行。


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    Titel :

    Variable wing of continuous variable wing shape facing fixed wing aircraft


    Weitere Titelangaben:

    面向固定翼飞机的连续可变翼形的变体机翼


    Beteiligte:
    WANG ZHENWEI (Autor:in) / ZHAO HAN (Autor:in) / ZHANG ZIYU (Autor:in)

    Erscheinungsdatum :

    2023-08-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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