The invention provides a landing assist device. The aerial carrier platform (14) has a rising and falling surface (14a). An opening (16) is formed in the landing and landing surface (14a), said opening (16) being for loading and unloading cargo between the landing and landing surface (14a) and the flying body (12). A plurality of marks such as a mark (36A) are formed on the rising and falling surface (14a). Each mark is a graph or the like for determining the relative position between the flying body (12) and the aerial carrier platform (14). The opening (16) is formed on the rising and falling surface (14a) so that the edge (16a) of the opening (16) does not cross the mark.

    本发明提供一种起落辅助装置。载机平台(14)具有起落面(14a)。在起落面(14a)上,形成有用于在与飞行体(12)之间实施货物装卸的开口部(16)。在起落面(14a)上形成有标志(36A)等多个标志。各个标志为用于对飞行体(12)与载机平台(14)之间的相对位置进行确定的图形等。开口部(16)以开口部(16)的边缘(16a)不会横穿过标志的方式而被形成在起落面(14a)上。


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    Titel :

    Landing and landing assistance device


    Weitere Titelangaben:

    起落辅助装置


    Beteiligte:
    KIYOKAMI HIROAKI (Autor:in) / TAJIMA MASAO (Autor:in)

    Erscheinungsdatum :

    01.03.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U



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