The invention discloses an aircraft propeller composite material flexible propeller hub and a propeller applying the same, the flexible propeller hub comprises a first butterfly-shaped connecting piece, an outer propeller hub body and an inner supporting bone, the outer side wall of the first butterfly-shaped connecting piece is provided with a first butterfly-shaped ring groove, the inner supporting bone is arranged outside the first butterfly-shaped connecting piece in a sleeving mode, and the outer side wall of the first butterfly-shaped connecting piece is provided with a second butterfly-shaped ring groove; the inner side face of the inner supporting bone is matched with the first annular groove. The inner supporting bone and the first annular connecting piece are installed on the outer propeller hub body, a connecting hole is formed in the outer propeller hub body, the inner supporting bone is provided with an outer extending rod extending out of the connecting hole, and the outer extending rod extends outwards in the radial direction of the inner supporting bone. According to the composite material flexible propeller hub of the aircraft propeller and the propeller applying the composite material flexible propeller hub, the technical effects of being simple in structure, high in reliability, low in cost and long in service life are achieved, and the structure of the flexible propeller hub improves the centrifugal tensile strength of the propeller hub and reduces torsional resistance at the same time.

    本发明公开了一种飞机螺旋桨复合材料柔性桨毂及其应用的螺旋桨,柔性桨毂包括第一蝶形连接件、外桨毂本体和内支撑骨,其中:所述第一蝶形连接件的外侧壁开有第一蝶形环槽,所述内支撑骨套设在所述第一蝶形连接件外,所述内支撑骨的内侧面与所述第一环形槽匹配;所述内支撑骨和所述第一环形连接件安装在所述外桨毂本体上,所述外桨毂本体开有连接连接孔,所述内支撑骨具有延伸出连接孔外的外延伸杆,所述外延伸杆沿所述内支撑骨的径向向外延伸。本发明中,所提出的飞机螺旋桨复合材料柔性桨毂及其应用的螺旋桨,具有结构简单、可靠性高和成本低且寿命长的技术效果,柔性桨毂的结构提高桨毂的离心抗拉强度同时减小扭转阻力。


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    Titel :

    Composite material flexible propeller hub of aircraft propeller and propeller applying composite material flexible propeller hub


    Weitere Titelangaben:

    一种飞机螺旋桨复合材料柔性桨毂及其应用的螺旋桨


    Beteiligte:
    HONG JUN (Autor:in) / SHI LI (Autor:in) / HU HUIJUN (Autor:in)

    Erscheinungsdatum :

    23.05.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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