The invention discloses a special-shaped fuel tank for an aircraft and the aircraft, and relates to the technical field of aircraft part manufacturing, the special-shaped fuel tank comprises a fuel tank shell, the fuel tank shell comprises a first cavity section and a second cavity section, the shapes of the first cavity section and the second cavity section are similar to cylinders, and the cross section area of the second cavity section is larger than that of the first cavity section; the second cavity section extends out of the first cavity section in the radial direction, a partition plate is arranged in the second cavity section, the partition plate is in smooth connection with the end of the first cavity section, the partition plate divides the second cavity section into an oil storage cavity and a bearing cavity, and the oil storage cavity communicates with the first cavity section and is used for storing and providing fuel oil for the aircraft; the bearing cavity is used for bearing aircraft stand-alone equipment. Due to the fact that the bearing cavity, the oil storage cavity and the first cavity section are integrally arranged, a connecting structure does not need to be used for connecting the bearing cavity, the oil storage cavity and the first cavity section, the space occupied by the connecting structure is reduced, and then the oil storage amount of the oil storage cavity and the first cavity section in the oil tank shell can be increased.

    本发明公开了一种用于飞行器的异型油箱及飞行器,涉及飞行器零部件制造技术领域,包括油箱外壳,其包括第一腔段和第二腔段,第一腔段和第二腔段的形状均为类圆柱,且第二腔段的横截面积大于第一腔段的横截面积,第二腔段沿径向方向伸出第一腔段,第二腔段中设有一分隔板,且分隔板与第一腔段的端部平滑连接,分隔板将第二腔段划分为储油腔体和承载腔体,储油腔体与第一腔段连通,用于贮存并向飞行器提供燃油,承载腔体用于承载飞行器单机设备。由于将承载腔体、储油腔体与第一腔段集成布置,无需使用连接结构连接承载腔体、储油腔体和第一腔段,减少了连接结构占用的空间,进而可以提高油箱外壳中储油腔体与第一腔段的储油量。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Special-shaped oil tank for aircraft and aircraft


    Weitere Titelangaben:

    一种用于飞行器的异型油箱及飞行器


    Beteiligte:
    TAN YOUDE (Autor:in) / JIAO YAN (Autor:in) / ZHU XUAN (Autor:in) / LIU QING (Autor:in) / DONG SHIBO (Autor:in) / GAO XU (Autor:in) / XU GAOPING (Autor:in) / UMAJI (Autor:in) / ZHOU MINGXING (Autor:in) / HU SHANGANG (Autor:in)

    Erscheinungsdatum :

    2023-12-22


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



    Aircraft Water Tank

    MASUDA MITSUTAKA | Europäisches Patentamt | 2016

    Freier Zugriff

    Aircraft Water Tank

    MASUDA MITSUTAKA | Europäisches Patentamt | 2016

    Freier Zugriff

    Aircraft fuel tank access cover and an aircraft fuel tank

    KORYA CHETAN / SANDERSON TIMOTHY J | Europäisches Patentamt | 2015

    Freier Zugriff

    AIRCRAFT WATER TANK

    TAGUCHI YUJI / HAGIWARA HIROSHI | Europäisches Patentamt | 2019

    Freier Zugriff

    AIRCRAFT WATER TANK

    MASUDA MITSUTAKA | Europäisches Patentamt | 2019

    Freier Zugriff