A head propeller of the flying vehicle compresses incoming flow at a vehicle head inside an upper duct to a lower duct through an air suction channel. A portion of airflow is compressed to the lower duct through the air suction channel under an action of a guide plate and a vehicle body propeller. A bottom propeller of the flying vehicle compresses an airflow into pressure bins of the lower duct at a lower portion through the air suction channel. A sealing state of the pressure bins of the lower duct is destroyed. High-pressure airflow inside the lower duct is jetted out from an air outlet channel to the upper duct. A tail propeller guides the airflow to the tail portion of the vehicle body. The upper duct and the lower duct are constructed inside the pipeline, so a running resistance of the flying vehicle is reduced.


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    Titel :

    OPERATION METHOD AND OPERATION SYSTEM FOR UPPER AND LOWER DOUBLE-DUCT JET-PROPELLED PIPELINE ULTRA-HIGH SPEED FLYING VEHICLE


    Beteiligte:
    MA TIEHUA (Autor:in) / ZHANG KUN (Autor:in) / WU YAOYAN (Autor:in) / CHEN CHANGXIN (Autor:in) / FENG LEI (Autor:in)

    Erscheinungsdatum :

    12.12.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B61B RAILWAY SYSTEMS , Eisenbahnanlagen / B60V Luftkissenfahrzeuge , AIR-CUSHION VEHICLES



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