The present invention relates to a new helicopter air plane where a helicopter and a generic air plane can be used. A propeller group is installed inside a pipe to use a method for floating and landing and advancing an air vehicle, and a rudder for rotating the air vehicle toward a left side and a right side and another rudder for enabling the air vehicle to be ascended and descended are installed in the present invention. Therefore, the present invention is capable of freely flying after the air vehicle takes off and safely landing when a defect of the air vehicle is generated since an emergency propeller is installed in an upper portion of the air vehicle and installing the propeller which rotates 360°C toward the right side and the left side in the rear side of the air vehicle to freely switch directions in any spaces.


    Access

    Download


    Export, share and cite



    Title :

    NEW HELICOPTER AIR PLANE


    Contributors:
    O OAN BAY (author)

    Publication date :

    2015-09-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

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



    HYBRID JET PLANE-HELICOPTER

    DUROV DMITRIJ SERGEEVICH | European Patent Office | 2019

    Free access


    Helicopter Rotor Vibration in the Tip Path Plane

    Payne, P.R. | Emerald Group Publishing | 1955


    UNMANNED HIGH-SPEED HELICOPTER, DESANTIFIED FROM PLANE AIRCRAFT

    DUROV DMITRIJ SERGEEVICH | European Patent Office | 2017

    Free access

    Control issues for rigid-in-plane helicopter rotors

    Latz, Amnon / Graham, Kenneth | AIAA | 1996