一种飞艇载SAR相控阵天线结构设计

    A Structural Design of Phased Array Antenna for Airship-borne SAR

    • 摘要: 飞艇具有可悬停、可机动、驻空时间长、造价低等特点,适合作为合成孔径雷达(SAR)天线的搭载平台进行空间遥感成像。针对某型飞艇承载能力、振动结构等约束及电性需求,提出一种一体化设计与片式组件技术相结合的SAR有源相控阵天线架构,通过机电力热多学科耦合设计,实现天线整机高集成、低剖面与轻量化;基于大尺寸微波基板与连接器精密装焊技术,提出超小型推入式连接器、印制电路板与结构底板一体化焊接方案,提升阵面刚度与平面度;通过综合运用多功能集成芯片、硅铝合金材料和激光封焊等技术,实现有源模块的轻薄化和高导热。样机试验结果表明,天线的机电性能、刚强度及热控设计均满足指标要求,对艇载、机载等有源相控阵天线的多功能一体化设计具有重要借鉴意义。

       

      Abstract: Airships, with their hovering capability, maneuverability, long hovering time, and low cost, are suitable as platforms for carrying synthetic aperture radar (SAR) antennas for space remote sensing imaging. To address the constraints of load-bearing capacity, vibration structure, as well as the electrical requirements of a certain type of airship, an active SAR phased array antenna structure combining integrated design with tile-type module technology is presented in this paper.A high integration, low profile and lightweight antenna system is achieved by means of a multidisciplinary coupled design involving mechanical engineering, electronics, mechanics, and thermodynamics. Based on the precision assembling and welding technology of large-size microwave substrates and connectors, an integrated welding solution for ultra-miniature push-in connectors, printed circuit boards and structural base plates is proposed to improve the rigidity and flatness of the array surface.A lightweight active module with high thermal conductivity is achieved by comprehensively utilizing multi-functional integrated chips, silicon-aluminum alloy materials, and laser sealing technologies. Results of prototype testing show that the electromechanical performance, rigidity and thermal design of the antenna all meet the required specifications, providing important reference for the multi-functional integrated design of active phased array antennas for airship-borne and airborne applications.

       

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