The invention provides a hybrid power double-fuselage tilting propeller vertical take-off and landing high-speed aircraft and a method. The hybrid power double-fuselage tilting propeller vertical take-off and landing high-speed aircraft comprises fuselages, canards, main wings, tilting assemblies, folding and unfolding assemblies, an electric system, an oil drive system and a vertical fin. The canard wings and the main wings are mounted at the head and the tail of the fuselage respectively, and the top wall of the tail of the fuselage is provided with a vertical fin and inclines backwards; the oil-driven system comprises a piston engine with a propeller, is arranged at the center of the canard wing and the main wing through a tilting assembly, and is used for providing tension during vertical take-off and landing and cruising flight of the aircraft; the electric system comprises a plurality of electrically-driven propellers which are arranged at the top of the vertical fin and on the two sides of the head of the fuselage and can provide pulling force and conduct posture adjustment during vertical take-off and landing and low-speed forward flight; the electrically-driven propellers located in the front are connected with the fuselage through folding and unfolding assemblies and can be folded or unfolded along the fuselage. Power is provided in different flight stages through the electrically-driven propellers and the piston engines, the loading capacity is improved, and the endurance time is prolonged.

    本发明提供了一种混合动力双机身倾转螺旋桨垂直起降高速飞行器及方法,包括机身、鸭翼、主机翼、倾转组件、折展组件、电动系统、油动系统和垂尾;机身为双机身设置,鸭翼和主机翼分别安装在机身头部和尾部,机身尾部顶壁设有垂尾且向后倾斜;油动系统包括带有螺旋桨的活塞发动机,通过倾转组件设置在鸭翼和主机翼中心,用于提供飞行器垂直起降和巡航飞行时的拉力;电动系统包括多个电驱动螺旋桨,设置在垂尾顶部和机身头部两侧,能够在垂直起降和低速前飞时提供拉力并进行姿态调整;位于前面的电驱动螺旋桨通过折展组件与机身连接,能够沿机身折叠或展开。本发明通过电驱动螺旋桨和活塞发动机在不同飞行阶段提供动力,提升了载荷能力和续航时间。


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    Titel :

    Hybrid power double-fuselage tilting propeller vertical take-off and landing high-speed aircraft and method


    Weitere Titelangaben:

    一种混合动力双机身倾转螺旋桨垂直起降高速飞行器及方法


    Beteiligte:
    DENG YANGPING (Autor:in) / MI BAIGANG (Autor:in) / ZHAN HAO (Autor:in) / WANG BAN (Autor:in)

    Erscheinungsdatum :

    14.06.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64U / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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