The invention discloses a module combined type manufacturing method for a four-axis aircraft. The module combined type manufacturing method includes the following steps: (1) a battery module is arranged and is in a cuboid shape, a first contact type female socket is arranged at the back position, and a first buckle is arranged at the bottom; (2) a camera shooting module is arranged and is in a cuboid shape, a camera is arranged on the front portion, a second contact type female socket is arranged at the back position, and a second buckle is arranged at the bottom; (3) a height determining and infrared anti-collision module is arranged, and a third buckle and a third contact type female socket are arranged at the bottom of the height determining and infrared anti-collision module; (4) an aircraft rack module is arranged, and the four-axis aircraft rack module comprises a body part, a flight shaft outwards extending from the body part and propeller power sets arranged at the four ends of the X-shaped flight shaft respectively; and (5) all the modules are assembled in a combined manner through detachable plug-in or buckling mechanisms. The invention further discloses the module combined type four-axis aircraft for implementing the method.


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    Titel :

    Module combined type manufacturing method for four-axis aircraft and four-axis aircraft


    Beteiligte:
    CAI QIANG (Autor:in)

    Erscheinungsdatum :

    16.12.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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