Method for establishing electromagnetic compatibility digital model of all-composite aircraft

The invention discloses a method for establishing an electromagnetic compatibility digital model of an all-composite aircraft. The method comprises the following steps: dividing the electromagnetic compatibility digital model of the all-composite aircraft into an all-composite aircraft shielding eff...

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Hauptverfasser: WANG LEI, ZHANG ZHIQIANG, REN JINGZHI, CUI TONGKAI, PAN MINGJIAN, FANG JIANPING, WU XIAORUI, YAN ZHIQIANG, CAO JUANJUAN, JIANG HUAN, XIAO ZHEN, SU HANSHENG, SUN JIAN, REN LIANG, SUN SHIJIE, HE ZHENGGUANG, LI LIANG
Format: Patent
Sprache:chi ; eng
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Zusammenfassung:The invention discloses a method for establishing an electromagnetic compatibility digital model of an all-composite aircraft. The method comprises the following steps: dividing the electromagnetic compatibility digital model of the all-composite aircraft into an all-composite aircraft shielding effectiveness model and an aircraft cabin electromagnetic interference incidence relation model; establishing an all-composite aircraft shielding effectiveness model by using the reflection loss model of the composite interface, the transmission loss model in the composite and the aircraft geometric model; and establishing an incidence relation model of electromagnetic interference in the aircraft cabin by using the parameterized model of the on-board radiation source equipment, the parameterized model of the on-board sensitive equipment and the interference power matrix of all the radiation source equipment received by the on-board sensitive equipment. According to the method, the shielding effectiveness and the cond