The invention relates to the technical field of aircraft power devices, in particular to a combined type rotor wing transmission system and a combined type rotor wing aircraft. The combined type rotor wing transmission system comprises a transmission module, and the transmission module is used for being connected with a first driving mechanism, a second driving mechanism, a main rotor wing system and two propelling propeller systems. The transmission module connects the first driving mechanism with the main rotor system, selectively connects the second driving mechanism with the propulsion propeller system and selectively connects the second driving mechanism with the main rotor system, and when the second driving mechanism is connected with the main rotor system, the main rotor system has at least two rotating speeds. The composite rotor transmission system has multiple driving modes, is simple in structure and relatively multiple in driving modes, and meets the use requirements of the composite rotor aircraft on multiple flight modes.

    本发明涉及飞机动力装置技术领域,特别涉及一种复合式旋翼传动系统及复合式旋翼飞行器。复合式旋翼传动系统包括传动模块,所述传动模块用于与第一驱动机构、第二驱动机构、主旋翼系统和两个推进螺旋桨系统连接;传动模块将第一驱动机构与主旋翼系统连接,选择性地将第二驱动机构与推进螺旋桨系统连接,以及选择性地将第二驱动机构与主旋翼系统连接,第二驱动机构与主旋翼系统连接时,主旋翼系统具有至少两个转速。复合式旋翼传动系统具有多种驱动模式,结构简单且驱动模式相对较多,满足复合式旋翼飞行器对多种飞行模式的使用需求。


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    Titel :

    Combined type rotor wing transmission system and combined type rotor wing aircraft


    Weitere Titelangaben:

    一种复合式旋翼传动系统及复合式旋翼飞行器


    Beteiligte:
    QI ZHIGANG (Autor:in) / ZHANG SHILONG (Autor:in) / ZHANG JIECHAO (Autor:in) / GE HANG (Autor:in) / WANG TIANNING (Autor:in)

    Erscheinungsdatum :

    2023-09-19


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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