The invention relates to the technical field of aircraft design, in particular to a liquid fuel storage tank and an aircraft. The liquid fuel storage tank comprises a tank body and an outer shell, the tank body is arranged in an aircraft fuselage, the tank body is arranged in the outer shell, the outer shell is a fuselage shell of an aircraft, and a connecting shell matched with the tank body in structure is arranged on the inner side of the outer shell. According to the liquid fuel storage tank, the fuselage shell of the aircraft is directly used as the outer shell, a shell of the tank body is not independently arranged any more, and the weight of the aircraft can be effectively reduced. Meanwhile, due to the arrangement, the tank body can be placed in a large space, namely the volume of the tank body can be effectively increased, and the cruising ability of the aircraft is further improved. The aircraft provided by the invention comprises the liquid fuel storage tank, so that the weight of the aircraft can be effectively reduced; and meanwhile, the cruising ability of the aircraft is improved.

    本申请涉及飞行器设计技术领域,尤其涉及一种液体燃料储罐及飞行器。本申请提供的液体燃料储罐,包括罐体以及外层壳体,罐体设置于飞行器机身内,罐体设置于外层壳体内,外层壳体为飞行器的机身壳体,外层壳体内侧设置有与罐体结构相适应的连接壳。本申请提供的液体燃料储罐直接将飞行器的机身壳体作为外层壳体,不再单独设置罐体的外壳,可有效地降低飞行器的重量。同时,如此设置可使得具有较大的空间来放置罐体,也就是可以有效地增大罐体的容积,进而增加飞行器的续航能力。本申请提供的飞行器,由于包括上述的液体燃料储罐,因此也具有上述的可有效地降低飞行器的重量;同时,增加飞行器的续航能力的技术效果。


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    Title :

    Liquid fuel storage tank and aircraft


    Additional title:

    液体燃料储罐及飞行器


    Contributors:
    SHI JINGWEI (author) / ZHANG XINTAN (author) / ZHU WENDU (author) / WANG JIANLI (author) / GAO YUNFEI (author) / ZHANG JIONG (author)

    Publication date :

    2024-10-01


    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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