The invention belongs to the technical field of electrostatic protection and electromagnetic compatibility, and particularly relates to a simulation evaluation method for the discharge effect of an airplane electrostatic discharger. According to the simulation evaluation method for the discharge effect of the aircraft electrostatic discharger, evaluation of the effect of the aircraft electrostatic discharger is carried out by using electromagnetic modeling and simulation means, the method is not limited by the development progress of the electrostatic discharger and manufacturing of test pieces, and a design scheme of the electrostatic discharger can be subjected to massive iterative optimization at extremely low cost; the method is suitable for all fixed-wing aircraft platforms, belongs to the verification of the discharge effect of the whole aircraft after the electrostatic discharger is installed, and can be used as a basis for the evaluation of the electrostatic protection design of the whole aircraft.

    本申请属于静电防护及电磁兼容技术领域,特别涉及一种飞机静电放电器放电效果仿真评估方法。本申请的飞机静电放电器放电效果仿真评估方法,利用电磁建模及仿真手段展开飞机静电放电器效果评估,不受静电放电器研制进度以及试验件制作的限制,可以以极低成本对静电放电器设计方案进行大量迭代优化;该方法适用于所有固定翼飞机平台,属于静电放电器装机后的飞机整机放电效果验证,可以作为飞机整机静电防护设计评估的依据。


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    Title :

    Simulation evaluation method for discharge effect of airplane electrostatic discharger


    Additional title:

    一种飞机静电放电器放电效果仿真评估方法


    Contributors:
    ZHEN GUOSHUAI (author) / QI XUEFENG (author) / ZHANG TAO (author) / WANG YAN (author) / MAO YU (author) / ZANG JIAZUO (author)

    Publication date :

    2022-07-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen




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