The turbulence friction resistance reduction device based on array type corona micro-blowing comprises a corona discharge cavity plate (1) and a discharge electrode (2). A plurality of cylindrical inclined micro holes are formed in the front face of the corona discharge cavity plate (1) and serve as corona discharge anodes, the cylindrical inclined micro holes are distributed in the front face of the corona discharge cavity plate (1) in an array mode, and the inclined directions of the cylindrical inclined micro holes are changed in a staggered mode. The high-voltage direct-current power supply (4) generates direct-current high voltage and applies the direct-current high voltage to the discharge electrode (2), plasma (6) is generated between the discharge electrode (2) and the corona discharge cavity plate (1), two oblique jet flows of each discharge group are coupled to form spirally-rising jet flows, a normal blowing effect is generated in a flow field, and turbulent friction resistance reduction is achieved. The invention further provides a turbulence friction resistance reduction device and method based on array type corona discharge. The sensor is arranged in a flow field to collect flow field data, the flow field state is sensed in real time, the corona discharge mode is controlled, the optimal resistance reduction effect is kept in the rapidly-changed flow field state, and the resistance reduction adaptability is further improved.

    基于阵列式电晕微吹气的湍流摩擦减阻装置包括电晕放电腔体板(1)、放电电极(2)。电晕放电腔体板(1)正面开有多个圆柱形斜微孔,作为电晕放电的阳极,这些圆柱形斜微孔在电晕放电腔体板(1)正面呈现阵列分布,圆柱形斜微孔的倾斜方向交错改变。高压直流电源(4)产生直流高压,施加到放电电极(2)上,在放电电极(2)与电晕放电腔体板(1)间产生等离子体(6),每个放电组的两个斜射流耦合形成螺旋上升的射流,在流场中产生法向吹气效果,实现湍流摩擦减阻。还提供一种基于阵列式电晕放电的湍流摩擦减阻装置与方法。本发明将传感器布置在流场采集流场数据,实时感知流场状态,控制电晕放电模式,在迅速变化的流场状态下保持最佳的减阻效果,进一步提高减阻适应性。


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    Title :

    Turbulence friction resistance reduction device and method based on array type corona discharge


    Additional title:

    基于阵列式电晕放电的湍流摩擦减阻装置与方法


    Contributors:
    SU ZHI (author) / LIU HONGRUI (author) / ZONG HAOHUA (author) / LIANG HUA (author) / WEI BIAO (author) / WU YUN (author) / YANG HESEN (author) / FANG ZIQI (author)

    Publication date :

    2025-01-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / H05H Plasmatechnik , PLASMA TECHNIQUE



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