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首页> 外文期刊>Advanced Composite Materials: The Official Journal of the Japan Society of Composite Materials >Design of Composite Multilayer Surface Antenna Structure and Its Bending Fatigue Characteristics
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Design of Composite Multilayer Surface Antenna Structure and Its Bending Fatigue Characteristics

机译:复合多层表面天线结构设计及其弯曲疲劳特性

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摘要

The present study aims to design a multilayer microstrip antenna with composite sandwich construction and investigate fatigue behavior of this multilayer SAS (surface antenna structure) that was asymmetric sandwich structure for the next generation of structural surface technology. This term, SAS, indicates that the structural surface becomes an antenna. Constituent materials were selected considering electrical properties, dielectric constant and tangent loss as well as mechanical properties. For the antenna performance, antenna elements inserted into structural layers were designed for satellite communication at a resonant frequency of 12.2 GHz. From electrical measurements, it was shown that antenna performances were in good agreement with design requirements. In cyclic 4-point bending, flexure behavior was investigated by static and fatigue test. Fatigue life curve of the SAS was obtained. The experimental results of bending fatigue were compared with single load level fatigue life prediction equations and in good agreement. The SAS concept is can be extended to give a useful guide for manufacturers of structural body panels as well as antenna designers.
机译:本研究旨在设计一种具有复合夹层结构的多层微带天线,并研究这种多层SAS(表面天线结构)的疲劳行为,该结构是下一代结构表面技术的非对称夹层结构。 SAS这一术语表示结构表面成为天线。选择材料时要考虑电性能,介电常数和切线损耗以及机械性能。为了提高天线性能,将插入结构层的天线元件设计为以12.2 GHz的谐振频率进行卫星通信。从电气测量中可以看出,天线性能与设计要求非常吻合。在循环四点弯曲中,通过静态和疲劳测试研究了弯曲行为。获得了SAS的疲劳寿命曲线。将弯曲疲劳的实验结果与单载荷水平疲劳寿命预测方程进行了比较,并且吻合良好。可以扩展SAS概念,为结构体面板制造商和天线设计人员提供有用的指导。

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