In a hybrid flight vehicle, having four rotors attached to a frame and configured to produce propelling force to propel the frame, a gas turbine engine attached to the frame and configured to rotate when fuel is supplied, a generator connected to an output shaft of the engine and configured to generate electric power when driven by the engine, a battery configured to store the electrical power generated by the generator, and four first electric motors each connected to the rotors to drive associated one of the rotors when the electric power is supplied from the battery, and an electronic control unit configured to control flight by regulating driving of the four rotors by the first electric motors. In the vehicle, the output shaft of the engine is attached parallel to at least one among yaw axis, pitch axis and roll axis of the frame.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Hybrid flight vehicle using engine gyro effect for stabilization


    Beteiligte:
    KAWAI KEISUKE (Autor:in)

    Erscheinungsdatum :

    25.04.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    GYRO-STABILIZATION VEHICLE

    DANIEL KEE YOUNG KIM / KEVIN BRETNEY / ANDEREW L TSANG | Europäisches Patentamt | 2016

    Freier Zugriff

    Control moment gyro gravity stabilization

    Scott, E.D. | Engineering Index Backfile | 1964


    Control Moment Gyro Gravity Stabilization

    Langford, Robert C. / Mundo, Charles J. | AIAA | 1964



    Hybrid drive mode spherical robot based on gyro stabilization principle

    HAN YANFEI / SHENG LI / XU TIANZE et al. | Europäisches Patentamt | 2022

    Freier Zugriff