A drive system (17) of an aircraft provides drive power for takeoff, landing and flight operations after takeoff and before landing, having a fuel cell (18) as a first power source, which fuel cell can be supplied with hydrogen by a hydrogen tank (19) and air by a fan (20), the driving device is designed to provide driving power for flight operation after taking off and before landing according to the hydrogen mass flow provided by the hydrogen tank (19) and according to the air mass flow provided by the fan (20); an electrical energy store (22) as a second power source, which is designed to provide additional drive power for take-off and landing. When the electrical energy store (22) fails, the fuel cell (18) can be supplied with an additional hydrogen mass flow by the additional hydrogen tank (23) and an additional air or oxygen mass flow by the air or oxygen tank (24). The invention also relates to an aircraft and a method for operating an aircraft.

    一种飞行器的驱动系统(17),该驱动系统为起飞、降落以及起飞后和降落前的飞行运行提供驱动功率,其具有:作为第一电源的燃料电池(18),该燃料电池能够由氢气罐(19)供应氢气且能够由风机(20)供应空气,且被设计为用于根据由氢气罐(19)提供的氢气质量流量以及根据由风机(20)提供的空气质量流量来为起飞后和降落前的飞行运行提供驱动功率;作为第二电源的电能量储存器(22),其被设计为用于为起飞和降落提供额外的驱动功率。在电能量储存器(22)失效时,燃料电池(18)能够由附加氢气罐(23)供应额外的氢气质量流量并且能够由空气或氧气罐(24)供应额外的空气或氧气质量流量。本发明还涉及一种飞行器及运行飞行器的方法。


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    Title :

    Drive system for aircraft, aircraft and method for operating aircraft


    Additional title:

    飞行器的驱动系统、飞行器和用于运行飞行器的方法


    Contributors:
    FAORI MARCO (author)

    Publication date :

    2022-10-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

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



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