An aircraft fuel system comprising: a first fuel storage tank arranged to store a first fuel; a second fuel storage tank arranged to store oxygen-reduced fuel; and a fuel tank inerting system arranged to provide an oxygen-reduced gas from the fuel contained within the second fuel storage tank to generate an oxygen-reduced fuel within the second fuel storage tank. The fuel tank inerting system may include a fuel tank injection system to inject an oxygen-reduced gas directly into the fuel contained in the second fuel storage tank to generate an oxygen-reduced fuel.

    一种飞行器燃料系统,包括:第一燃料存储罐,第一燃料存储罐布置成存储第一燃料;第二燃料存储罐,第二燃料存储罐布置成存储减氧燃料;以及燃料罐惰化系统,燃料罐惰化系统布置成通过包含在第二燃料存储罐内的燃料提供减氧气体,以在第二燃料存储罐内生成减氧燃料。燃料罐惰化系统可以包括燃料罐喷射系统,以将减氧气体直接注入到包含在第二燃料存储罐内的燃料中,从而生成减氧燃料。


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    Titel :

    Aircraft fuel system


    Weitere Titelangaben:

    飞行器燃料系统


    Beteiligte:

    Erscheinungsdatum :

    12.11.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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