The invention discloses a boundary layer suction type propulsion system and an aircraft. The propelling system comprises an open type rotor engine and a BLI fan. A part of energy of fuel combustion of the open type rotor engine is used for driving a rotor of the open type fan to rotate to serve as propelling power. The other part of fuel chemical energy is converted into electric energy which is transmitted to a BLI fan installed on the rear portion of the fuselage, and the electric energy drives the BLI fan to rotate so as to provide the other part of propelling power.

    一种边界层吸入式推进系统以及飞机。其中,所述推进系统包括:开式转子发动机,以及BLI风扇;其中,所述开式转子发动机的燃料燃烧的一部分能量用以驱动开式风扇的转子旋转作为推进动力;另一部分燃料化学能转化为电能,传递给安装在机身后部的BLI风扇,电能驱动BLI风扇旋转,用以提供另一部分推进动力。


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    Title :

    Boundary layer suction type propulsion system and airplane


    Additional title:

    边界层吸入式推进系统、飞机


    Contributors:
    LUO JU (author) / LIU HUI (author) / GAO YANFEI (author)

    Publication date :

    2025-05-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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