轻质可展开阵列天线及其抗风性能研究

    Research on the Lightweight Deployable Array Antenna and its Wind Resistance Performance

    • 摘要: 针对地面高机动雷达天线阵面折叠展收与结构轻量化需求,在串联四连杆机构构型基础上研制出可展开阵列天线样机,折展比达到9.6: 1。可展开天线以柔性聚酰亚胺覆铝膜作为反射面,天线面密度低至0.88kg/m2,相比常规刚性天线具有显著的轻量化优势。仿真结果表明,可展开天线可满足20m/s风速下的结构刚强度要求。为进一步验证可展开天线的实际抗风性能,提出气压模拟风压的等效风载试验方法,并搭建气压加载与DIC测量试验系统。由于可展开天线样机各铰点存在间隙,在20m/s风速等效压力作用下,天线样机实测变形量较仿真值偏大0.4-1.2mm,但天线整体平面度误差为0.64mm(RMS),可满足天线正常工作形面精度指标要求。

       

      Abstract: In order to meet the requirements for foldable stowage and structural lightweighting of the ground highly mobile radar array antenna, a deployable array antenna prototype was developed based on the serial four-bar linkage configuration, achieving a deployment ratio of 9.6:1. The deployable antenna uses flexible polyimide film coated with aluminum as its reflective surface, resulting in an areal density as low as 0.88kg/m2, which demonstrates significant lightweight advantage over the conventional rigid array antennas. The simulation results indicate that the deployable antenna meets the structural stiffness and strength requirements under a wind speed of 20m/s. To further verify the actual wind resistance performance of the deployable antenna, an equivalent wind load test method using air pressure to simulate wind pressure was proposed, and an air pressure loading and DIC measurement test system was established. Due to the clearances at hinge points of the deployable antenna prototype, the measured deformation of the antenna prototype under the equivalent pressure of 20m/s wind speed was 0.4–1.2mm larger than the simulation value. However, the overall flatness error of the antenna was 0.64 mm (RMS), satisfying the surface accuracy requirements for the normal operation.

       

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