The invention relates to an aircraft comprising a supply system (200) comprising a hydrogen tank (202), a receiving device (204) consuming hydrogen, a feed line (206) between the tank (202) and the receiving device (204), a first enclosure (222) in which first means for heating hydrogen are mounted, wherein a second enclosure (226) arranged to drive hydrogen towards a second means of the receiving device (204), a safety tank (258) for a pressurized inert fluid and a purge line (262) between the free section (206a) of the feed line (206) and the distribution system (260) are mounted wherein, if a leak is detected, the pressurized inert fluid is pushed into the purge line (262) to expel hydrogen from the free section (206a). With such a supply system, hydrogen present in the free section is discharged in the event of a leak.

    本发明涉及一种飞行器,该飞行器包括供应系统(200),供应系统包括氢气罐(202)、消耗氢气的接收设备(204)、罐(202)与接收设备(204)之间的馈送管线(206)、其中安装有用于加热氢气的第一装置的第一封壳(222),其中安装有布置成将氢气驱动向接收设备(204)的第二装置的第二封壳(226)、用于加压惰性流体的安全罐(258)以及在馈送管线(206)的自由区段(206a)与分配系统(260)之间的吹扫管线(262),其中,如果检测到泄漏,加压惰性流体被推入吹扫管线(262)以从自由区段(206a)排出氢气。利用这样的供应系统,在泄漏的情况下,存在于自由区段中的氢气被排出。


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    Title :

    Aircraft comprising hydrogen supply system


    Additional title:

    包括氢气供应系统的飞行器


    Contributors:

    Publication date :

    2024-05-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    F17D Rohrleitungssysteme , PIPE-LINE SYSTEMS / B08B Reinigen allgemein , CLEANING IN GENERAL / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F17C Behälter zum Aufnehmen oder Speichern verdichteter, verflüssigter oder verfestigter Gase , VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES



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