An aircraft thrust control system includes a central power unit and a peripheral power unit. The central power unit includes an upper propeller and a lower propeller arranged one above the other and adapted to rotate in opposite directions, while the propellers of the peripheral power units are located outside the aerodynamic operating range of the propellers of the central power unit.

    一种飞行器推力控制系统包括中央动力单元和外围动力单元。该中央动力单元包括上螺旋桨和下螺旋桨,该上螺旋桨和该下螺旋桨上下布置并且适于沿相反的方向旋转,而该外围动力单元的螺旋桨位于该中央动力单元的螺旋桨的空气动力运行范围之外。


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    Titel :

    Aircraft thrust control system


    Weitere Titelangaben:

    飞行器推力控制系统


    Beteiligte:

    Erscheinungsdatum :

    31.01.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U



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