The invention provides a rotor support device. The rotor support device (18) includes supports (24, 24b, 24c) that support the rotor (20) and have coupling portions (56, 58) that protrude outward, a connecting member (26b) that forms a protruding portion (64) by forming a notch (62) at an end portion connected to the coupling portions, the protruding portion overlapping an outer peripheral surface of the coupling portions located in a first direction and being detachably connected to the coupling portions, and a reinforcing member (60) that reinforces the rotor (20). Wherein the first direction is orthogonal to the protruding direction of the coupling part, and the reinforcing member overlaps the connecting member and the outer peripheral surface of the coupling part located in a second direction opposite to the first direction and is detachably connected to the coupling part and the connecting member. Therefore, the structure for supporting the rotor wing is easy to assemble, disassemble and maintain.

    本发明提供一种旋翼支承装置。旋翼支承装置(18)具有支承件(24、24b、24c)、连接部件(26b)和加强部件(60),支承件支承旋翼(20)且具有向外侧突出的结合部(56、58),连接部件通过在与结合部连接的端部形成缺口(62)而形成突出部(64),突出部与位于第1方向的结合部的外周面重叠并以可拆装的方式连接于结合部,其中第1方向与结合部的突出方向正交,加强部件与位于第2方向的结合部的外周面和连接部件重叠并以可拆装的方式与结合部和连接部件连接,第2方向是与第1方向相反的方向。据此,关于支承旋翼的结构,易于组装和分解且易于维护。


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    Titel :

    Rotor wing supporting device


    Weitere Titelangaben:

    旋翼支承装置


    Beteiligte:
    ISHITSUKA YUJI (Autor:in)

    Erscheinungsdatum :

    2024-03-05


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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