The invention discloses a multi-convex wing, a multi-convex wing engine and a control method of the multi-convex wing engine, the multi-convex wing comprises a multi-convex wing base body and a drainage body, the multi-convex wing base body is provided with a plurality of continuous convex curved surfaces formed by connecting a plurality of single convex wings, and the drainage body is arranged between the two convex curved surfaces of the multi-convex wing base body; the multi-convex-wing engine comprises a plurality of convex wings, a flow channel and a high-speed fluid generator, the plurality of convex wings are arranged on the inner cavity face of the flow channel, and the high-speed fluid generator is a device capable of outputting high-speed fluid. When fluid flows through the multi-convex-wing base body, the drainage body guides the fluid flowing through the previous convex curved surface to the next convex curved surface, the fluid is guided to flow along the convex curved surfaces of the multi-convex-wing base body, the pressure of the fluid on the upper portion of the multi-convex-wing base body is blocked through the combined action of fluid viscosity and fluid inertia, and a negative pressure area is formed on the convex curved surfaces. Accordingly, a plurality of corresponding lift force areas are generated on the multi-convex-wing base body, the lift force and the force effect are greatly improved, and the problem that the efficiency of a vehicle and equipment adopting a traditional engine is low is solved.

    本发明公开了一种多凸翼及多凸翼引擎及其控制方法,多凸翼包括多凸翼基体和引流体,多凸翼基体由多个单凸翼联接而成连续的多个凸起曲面,引流体设置于多凸翼基体的两凸起曲面之间;多凸翼引擎包括多凸翼、流道、高速流体发生器,所述多凸翼设置于所述流道内腔面上,所述高速流体发生器为可输出高速流体的装置。流体流经多凸翼基体时,引流体将流过前一个凸起曲面的流体引向后一个凸起曲面,引导流体沿多凸翼基体的凸起曲面流动,流体粘性和流体惯性共同作用阻隔多凸翼基体上部流体的压力而在凸起曲面上形成负压区,进而在多凸翼基体上产生对应的多个升力区,升力及力效大幅提高,解决了采用传统引擎的交通工具及装备效率较低的问题。


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    Titel :

    Multi-convex-wing engine, multi-convex-wing engine and control method of multi-convex-wing engine


    Weitere Titelangaben:

    一种多凸翼及多凸翼引擎及其控制方法


    Beteiligte:
    TIAN GUICHUAN (Autor:in) / XIONG FANG (Autor:in)

    Erscheinungsdatum :

    24.01.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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