The present invention provides a method for landing a flying body, which can improve landing performance while achieving both vertical take-off and landing and improvement of fuel economy. A flying body is provided with at least a plurality of rotor parts for generating lift force, a thrust drive device for generating thrust force on the opposite side from the horizontal flight when landing, and fixed wings. In addition, the thrust driving device is provided with a propeller, and the propeller rotates in the reverse direction when the aircraft lands and when the aircraft flies horizontally. In addition, the thrust driving device generates a larger thrust force towards the opposite side during emergency fall than during fall.

    本发明提供一种能够在兼顾垂直起降的实现和燃料经济性的提高的基础上实现降落性能的提高的飞行体的降落方法。一种飞行体,其至少具备产生升力的多个旋翼部、推力驱动装置和固定翼,所述推力驱动装置在降落时,向与水平飞行时相反一侧产生推力。另外,所述推力驱动装置具备螺旋桨,所述螺旋桨在降落时,与水平飞行时反向旋转。另外,所述推力驱动装置在紧急坠落时,与降落时相比产生更大的向相反一侧的推力。


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    Title :

    Flying object, landing method, and program


    Additional title:

    飞行体、降落方法和程序


    Contributors:

    Publication date :

    2023-12-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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