According to the design method of the novel vertical take-off and landing composite wing aircraft, the advantages of a multi-axis aircraft and a fixed wing aircraft are achieved, the extremely simple and compact design is adopted, the aircraft has the vertical take-off and landing capacity, and the aircraft can hover, accelerate forwards and cruise efficiently through cooperation of the specially-designed power mechanism and the flight controller. According to the design, a control-surface-free control method can be adopted, the problems of delay, instability and the like existing in a traditional control surface control method are solved, the resistance of the aircraft is reduced, and the flight performance of the aircraft is improved. The method is simple in design, high in reliability and low in cost, and has a wide application prospect in the field of aircrafts.

    本发明提供一种新型垂直起降复合翼飞行器的设计方法,具有多轴飞行器和固定翼飞行器的优点,采用极简、紧凑的设计,该飞行器具有垂直起降的能力,而且通过特殊设计的动力机构配合飞行控制器,飞行器可悬停、前加速和高效率巡航。该发明设计还可采用免舵面控制方法,避免了传统舵面控制方法中存在的延迟和不稳定等问题,并减小了飞机的阻力,提高了其飞行性能。本发明设计简单、可靠性高、成本低,在飞行器领域具有广阔的应用前景。


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    Titel :

    Novel vertical take-off and landing composite wing aircraft


    Weitere Titelangaben:

    一种新型垂直起降复合翼飞行器


    Beteiligte:
    WANG HAIFENG (Autor:in)

    Erscheinungsdatum :

    2024-04-16


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U



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