The invention discloses a high-maneuverability aircraft fuel tank, a fuel supply system and a fuel supply method, and belongs to the technical field of aircraft fuel supply. A high-maneuverability aircraft oil tank comprises a shell, a partition plate is arranged in the shell and divides the interior of the shell into an independent electric cavity in the middle and oil cavities on the two sides, an oil bag is arranged in each oil cavity, the two ends of each oil bag are fixed to a front end plate and a rear end plate at the two ends of the corresponding oil cavity respectively, and a porous oil taking pipe is arranged in each oil bag. The two ends of the porous oil taking pipe are fixed to the front end plate and the rear end plate respectively, the porous oil taking pipe is an anti-flattening hose, and the porous oil taking pipe is immersed in fuel oil. By the adoption of the high-maneuverability aircraft fuel tank, the fuel supply system and the fuel supply method, the problems that an existing fuel supply flow is unstable, and the space utilization rate is low can be solved; the device has the advantages of simple structure and light weight.

    本发明公开了一种高机动性飞行器油箱、燃油供应系统及燃油供应方法,属于飞行器燃料供应技术领域。高机动性飞行器油箱,包括外壳,外壳的内部设置有隔板,隔板将外壳的内部分隔成独立的中部的电气腔和两侧的油腔,油腔内设置有油囊,油囊的两端分别固定在油腔两端的前端板、后端板上,油囊的内部设置有多孔取油管,多孔取油管的两端分别固定在前端板、后端板上,多孔取油管为防压扁的软管,多孔取油管浸没在燃油中。采用本发明所述的高机动性飞行器油箱、燃油供应系统及燃油供应方法,能够解决现有的燃油供应流量不稳定、空间利用率低的问题;具有结构简单、质量轻的优点。


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    Title :

    High-maneuverability aircraft fuel tank, fuel supply system and fuel supply method


    Additional title:

    一种高机动性飞行器油箱、燃油供应系统及燃油供应方法


    Contributors:
    BAO WEN (author) / ZHANG JUNLONG (author) / WANG YOUYIN (author) / QIU HONGCHAO (author) / SONG YONG (author)

    Publication date :

    2025-04-15


    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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