An aircraft transmission mechanism and power system relates to the field of aircraft power systems, and comprises a first belt transmission assembly and a second belt transmission assembly, the first belt transmission assembly is connected with a first propeller rotating shaft to drive the first propeller rotating shaft to rotate; the second belt transmission assembly is connected with the second propeller rotating shaft to drive the first propeller rotating shaft to rotate; the first belt transmission assembly and the second belt transmission assembly transmit power in opposite directions, so that the first propeller rotating shaft and the second propeller rotating shaft rotate in opposite directions. The structure is light in weight, stable in transmission and low in transmission noise, daily maintenance is not needed, and the maintenance cost is effectively reduced. The aircraft power system is realized based on the transmission mechanism. The structure weight is light, power output is stable, power distribution of the aircraft can be effectively carried out, daily maintenance is not needed, and the output stability of the aircraft power unit is further improved.

    一种飞行器传动机构及动力系统,涉及飞行器动力系统领域,包括:第一皮带传动组件和第二皮带传动组件,第一皮带传动组件同第一螺旋桨转轴连接,以带动第一螺旋桨转轴转动;第二皮带传动组件同第二螺旋桨转轴连接,以带动第一螺旋桨转轴转动;第一皮带传动组件和第二皮带传动组件所传递动力方向相反,以使第一螺旋桨转轴和第二螺旋桨转轴反向转动。其结构重量轻、传动平稳、传动噪声小,并且无需进行日常的维护,有效降低了维护成本。一种飞行器动力系统,基于上述传动机构实现。其结构重量轻、动力输出平稳,能够有效进行飞行器的动力分配,不需要进行日常维护,进一步提升飞行器动力单元的输出稳定性。


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    Titel :

    Aircraft transmission mechanism and power system


    Weitere Titelangaben:

    一种飞行器传动机构及动力系统


    Beteiligte:
    TAO FEI (Autor:in)

    Erscheinungsdatum :

    04.06.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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