The invention relates to a body and fuel tank integrated aircraft. The body and fuel tank integrated aircraft comprises an aircraft body, a device compartment, wings, an undercarriage and an empennage; the device compartment is arranged at the front end of the aircraft body; the wings are arranged on the top end of the aircraft body; the undercarriage is arranged at the bottom end of the aircraft body; the empennage is arranged at the tail end of the aircraft body; the aircraft body is a pressure-resistant tank. The body and fuel tank integrated aircraft has the advantages that the pressure-resistant bank is used as the aircraft, so that a force transmission line of the aircraft under various loads is simplified, the difficulty at the structural design is reduced, and the structural efficiency is raised; by treating pressure-resistant bank as the aircraft, the weight of the aircraft body structure is greatly saved, and therefore, the whole-aircraft fuel carrying capacity is improved.


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    Titel :

    Body and fuel tank integrated aircraft


    Beteiligte:
    HUANG MINJIE (Autor:in) / XU WEIQIANG (Autor:in) / CHEN YING (Autor:in)

    Erscheinungsdatum :

    01.04.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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