A tank for an aircraft 1000 is disclosed, the tank comprising two pressure bulkheads 11a, 11b connected to each other by a tank wall 15, the tank wall 15 being at least partially formed by a portion of a skin 101 of a fuselage 100 of the aircraft. The tank 10 further comprises at least one anti-sloshing wall 12a, 12b, 12c, 12d, which (respectively) at least partially closes one or several openings O1, O2, O3, O4 and is at least partially formed by an attachment frame 13a, 13b, 13c, 13d stabilizing the skin 101. A fuselage 100 comprising such a tank and an aircraft 1000 comprising such a fuselage 100 are also disclosed.

    公开了一种用于飞行器1000的罐,该罐包括两个耐压舱壁11a、11b,它们通过罐壁15连接到彼此,罐壁15至少部分地由飞行器的机身100的蒙皮101的一部分形成。罐10还包括至少一个防晃荡壁12a、12b、12c、12d,这些防晃荡壁(分别)至少部分地封闭一个或若干个开口O1、O2、O3、O4,并且至少部分地由稳定所述蒙皮101的附属框架13a、13b、13c、13d形成。还公开了包括这样的罐的机身100和包括这样的机身100的飞行器1000。


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    Title :

    Fuel tank for aircraft, fuselage of aircraft and aircraft


    Additional title:

    用于飞行器的燃料罐、飞行器的机身和飞行器


    Contributors:
    LINDE PETER (author) / TELKAMP MARC (author)

    Publication date :

    2024-10-29


    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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