Example systems and methods for using a multi-directional baffle in a cryogenic fuel tank are provided. An example cryogenic fuel tank includes an inner surface defining an interior of the cryogenic fuel tank to contain fuel and a plurality of baffles including a first baffle, the first baffle including a first member extending along a first plane and a second member extending along a second plane, the first plane being different than the second plane, the second member connected to the first member, a plurality of baffles are connected to the inner surface.

    提供了用于在低温燃料罐中使用多方向挡板的示例系统和方法。一种示例低温燃料罐包括限定低温燃料罐的内部以容纳燃料的内表面和包括第一挡板的多个挡板,第一挡板包括沿着第一平面延伸的第一构件和沿着第二平面延伸的第二构件,第一平面不同于第二平面,第二构件连接到第一构件,多个挡板连接到内表面。


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    Title :

    Multi-directional baffle for aircraft fuel tank


    Additional title:

    用于飞行器燃料罐的多向挡板



    Publication date :

    2024-10-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F15D FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS , Strömungsdynamik, d.h. Verfahren oder Vorrichtungen zum Beeinflussen der Strömung von Gasen oder Flüssigkeiten



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