The invention discloses a composite multifunctional delta wing aircraft which comprises an aircraft body, a manned assembly is installed at the bottom of the aircraft body, an angle adjusting assembly is installed on the outer side of the manned assembly, and an inclination angle adjusting assembly is installed between the angle adjusting assembly and the manned assembly. A flight person can enter the manned assembly before taking off, then the aircraft body can drive the manned assembly to take off together, when the flight person needs to adjust the shooting angle, adjustment can be conducted through the angle adjusting assembly, the orientation angle of the aircraft does not need to be adjusted at the moment, and therefore the flight person can capture important lenses at the first time; and the adaptability is higher. In the flying and angle adjusting process of the aircraft, extra power is not needed, and the aircraft is more energy-saving and environment-friendly.

    本发明公开了一种复合型多功能三角翼飞行器,包括飞行器主体,所述飞行器主体的底部安装有载人组件,所述载人组件的外侧安装有角度调节组件,所述角度调节组件与载人组件之间安装有倾角调节组件,飞行人员在起飞前可进入载人组件中,随后飞行器主体可带动载人组件一同起飞,在飞行人员需要调整拍摄角度时,可通过角度调节组件进行调节,此时无需调整飞行器的朝向角度,这样可以让飞行人员能够在第一时间抓拍重要镜头,适应性更强。并且该飞行器在飞行以及角度调节的过程中,无需额外的动力提供,更加节能环保。


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    Titel :

    Composite multifunctional delta wing aircraft


    Weitere Titelangaben:

    一种复合型多功能三角翼飞行器


    Beteiligte:
    SUN LIANG (Autor:in)

    Erscheinungsdatum :

    2022-07-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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