The invention relates to a vertical take-off and landing aircraft with a tiltable power system and a control method of the vertical take-off and landing aircraft. The vertical take-off and landing aircraft comprises a fuselage, wings and an empennage and further comprises a combined tilting power system and a combined fixed power system. The wings are fixedly arranged on two sides of the middle of the fuselage; the empennage is arranged at the tail of the fuselage; the combined tilting power and the combined fixing power are correspondingly arranged on the front and rear sides of the wings; the front power system is a combined tilting power system, the rear power system is a combined fixed power system, and the combined tilting power system is further provided with a variable pitch propeller. The problems that in the flying process of an existing composite wing aircraft, part of power systems do not work, so that the resistance is too large, the total weight of the aircraft is large in the flying process, and the problems that the flat flying speed and the voyage performance of the aircraft with the composite wing layout are poor are solved. The vertical take-off and landing aircraft with the tiltable power system is relatively simple in structure, relatively low in maintenance cost, more reliable in use performance, safer, capable of meeting various use requirements and convenient to popularize and use.

    本公开涉及一种可倾转动力系统的垂直起降飞行器及其控制方法,包括机身、机翼和尾翼,还包括组合倾转动力系统和组合固定动力系统;机翼固定设置于机身中部的两侧,尾翼设置于机身的尾部;组合倾转动力与组合固定动力对应设置于机翼的前后两侧;前动力系统为组合倾转动力系统,后动力系统为组合固定动力系统,组合倾转动力系统还设置有可变距螺旋桨。本公开解决了现有复合翼飞行器飞行过程中部分动力系统不工作导致飞行时阻力过大飞行器总重大等问题,以及还会出现复合翼布局的飞行器平飞速度和航程性能均较弱的问题。本公开的可倾转动力系统的垂直起降飞行器的结构相对简单,维护成本较低,使用性能更加可靠,更具有安全性,可以满足多种使用需求,便于推广使用。


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    Titel :

    Vertical take-off and landing aircraft with tiltable power system and control method of vertical take-off and landing aircraft


    Weitere Titelangaben:

    一种可倾转动力系统的垂直起降飞行器及其控制方法


    Beteiligte:
    ZHU JIE (Autor:in) / CHEN ENSHI (Autor:in)

    Erscheinungsdatum :

    2023-10-31


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen