党涛, 田殷, 王辂, 王光明, 郑宏兴. 非谐振多层级联频率选择表面研究[J]. 电波科学学报, 2018, 33(4): 463-469. doi: 10.13443/j.cjors.2018040801
      引用本文: 党涛, 田殷, 王辂, 王光明, 郑宏兴. 非谐振多层级联频率选择表面研究[J]. 电波科学学报, 2018, 33(4): 463-469. doi: 10.13443/j.cjors.2018040801
      DANG Tao, TIAN Yin, WANG Lu, WANG Guangming, ZHENG Hongxing. Non-resonant multilayer cascading of frequency selective surface[J]. CHINESE JOURNAL OF RADIO SCIENCE, 2018, 33(4): 463-469. doi: 10.13443/j.cjors.2018040801
      Citation: DANG Tao, TIAN Yin, WANG Lu, WANG Guangming, ZHENG Hongxing. Non-resonant multilayer cascading of frequency selective surface[J]. CHINESE JOURNAL OF RADIO SCIENCE, 2018, 33(4): 463-469. doi: 10.13443/j.cjors.2018040801

      非谐振多层级联频率选择表面研究

      Non-resonant multilayer cascading of frequency selective surface

      • 摘要: 为了减少工作在L波段的机载天线对高于其工作频率范围来波的散射,设计了一种非谐振单元组成的多层级联结构阵列.它是在十字网栅电感层基础上,通过螺旋曲折线的形式有效延长电流路径,加大电感层的感性效应,这种折线螺旋能够控制单元尺寸,还能抑制高阶模和栅瓣的出现.采用修改电容层金属图案的方法,将贴片单元变为谐振型的方环单元,并将这种带阻型方环单元的传输极点置于阵列干涉点处,可以有效抑制由阵列干涉造成的窄传输峰,从而减少高频电磁波散射的影响,达到减小电磁散射对飞机雷达散射截面的影响,从而实现表面频率选择.采用高频电磁场仿真软件对上述设计的物理模型和等效电路模型进行了仿真,并对结构尺寸进行了优化设计.通过实验对设计样品进行了测试和分析,结果表明上述设计能够达到频率选择的目的.

         

        Abstract: To reduce the scattering of the airborne antenna working in the L band to the wave which is higher than its working frequency range, a multi-layer cascade structure array composed of non resonant elements is designed. Based on the cross grid inductance layer, it effectively prolongs the current path through the form of spiral curved line and increases the inductive effect of the inductance layer. The line helix can control the size of the unit and suppress the appearance of the high order mode and the gate flap. By modifying the capacitance layer metal pattern, the patch unit is transformed into a resonant square ring unit, and the transmission pole of the banded square ring element is placed at the array interference point, which can effectively suppress the narrow transmission peak caused by the array interference. In order to reduce the influence of the high frequency electromagnetic scattering, the influence of the electromagnetic scattering on the radar cross section of the aircraft is reduced, and the selection of the surface frequency is realized. The simulation of the physical and equivalent circuit models of the above design is carried out by the high frequency electromagnetic simulation software, and the size of the structure is optimized. The design samples are tested and analyzed, and the results show that the above design can achieve the purpose of frequency selection.

         

      /

      返回文章
      返回