The invention relates to a hybrid propulsion chain (1) for an aircraft, comprising a plurality of propulsion rotors (R1-RX) electrically connected by means of electrical connections (E1-E4) to a power distribution module (10), which is connected, on the one hand, to a non-propulsion turbine (T) by means of a power generation system (20) and, on the other hand, to a battery (BAT), each propulsion rotor (R1-R4) comprises a stator and at least one rotating shaft configured to rotate relative to the stator when said stator is powered, said hybrid propulsion chain (1) comprising an auxiliary mechanical drive system (30) mechanically connected to a non-propulsion turbine (T), the auxiliary mechanical drive system (30) comprises a plurality of mechanical connections (M1-M4) for mechanically driving in rotation at least one rotation shaft (32) of the propulsion rotor (R1-RX).

    本发明公开了一种用于飞行器的混合动力推进链(1),混合动力推进链(1)包括多个通过电连接件(E1‑E4)与配电模块(10)电连接的推进转子(R1‑RX),配电模块(10)一方面通过发电系统(20)与非推进涡轮机(T)连接,另一方面与电池(BAT)电连接,每个推进转子(R1‑R4)包括定子和至少一个转轴,转轴被配置为当所述定子被供电时相对定子转动,所述混合动力推进链(1)包括与非推进涡轮机(T)机械连接的辅助机械驱动系统(30),辅助机械驱动系统(30)包括多个用于以机械方式驱动推进转子(R1‑RX)的至少一个转轴(32)转动的机械连接件(M1‑M4)。


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    Title :

    Aircraft hybrid propulsion chain comprising auxiliary mechanical drive system


    Additional title:

    包括辅助机械驱动系统的飞行器混合动力推进链


    Contributors:

    Publication date :

    2022-03-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

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



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