An airflow control system for controlling airflow flowing on the upper surface of an aircraft, the airflow control system being provided with: a blow-out opening which is provided on the front side of the upper surface of the aircraft and which blows out airflow; a suction port that is provided further toward the front side than the discharge port and that sucks in outside air; a fan which is provided on the rear side of the discharge port, sucks air from the front side, and discharges air to the rear side; and a compressor that is provided in the flow path from the suction port to the discharge port, and that pressurizes the outside air sucked from the suction port and delivers the outside air to the discharge port.

    一种气流控制系统,对在飞机的上表面流动的气流进行控制,所述气流控制系统具备:吹出口,所述吹出口设置在飞机的上表面的前方侧,吹出气流;吸入口,所述吸入口设置在比吹出口靠前方侧的位置,吸入外部空气;风扇,所述风扇设置在吹出口的后方侧,从前方侧吸气并且向后方侧排气;以及压缩机,所述压缩机设置于从吸入口至吹出口的流路,对从吸入口吸入的外部空气进行升压并向吹出口压送。


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    Title :

    Airflow control system and aircraft


    Additional title:

    气流控制系统以及飞机


    Contributors:

    Publication date :

    2022-05-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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