高级检索

    星载可展开螺旋天线螺旋振子的结构设计

    Structural Design of Helicon for Deployable Helix Antenna on Satellite

    • 摘要: 星载通信系统对天线的 “小型化−高可靠性”需求日益严苛,传统固定尺寸四臂螺旋天线(QHA)因展开高度大,超包络,不满足装星要求。本文以星载可展开螺旋天线螺旋振子为研究对象,围绕“收拢压缩无屈服、展开状态保刚度”的核心目标展开设计:首先,基于螺旋弹簧力学理论,建立“工作状态−自由状态”参数映射模型,以展开长度不变为约束,推导自由状态下中径、节距、螺旋角的计算方法;其次,针对大旋绕比导致的稳定性变差的问题,提出“保形拉索预紧+非完全展开”方案,通过预紧载荷平衡刚度与屈服风险;最后,创新采用“模具法成形+随炉热处理+强压处理”工艺组合,解决螺旋振子尺寸精度问题。试验结果表明:采用铍青铜制作的螺旋振子,收拢状态阵子不发生屈服变形,展开重复精度≤1 mm,天线展开基频>1 Hz,满足使用要求。

       

      Abstract: The demand for "miniaturization and high reliability" of antennas in on-board communication systems is increasingly stringent. Traditional fixed-size quadrifilar helical antennas (QHA) fail to meet the on-board requirements due to their large deployment height and excessive envelope. This paper takes the helicon of the on-board deployable helical antenna as the research object, and carries out the design around the core goal of "no yielding in retraction and compression, and stiffness maintenance in the deployed state". First, based on the mechanical theory of helical spring structures, a parameter mapping model of "working state - free state" is established. With the constant deployed length as the constraint, the calculation methods for the mean diameter, pitch and helix angle in the free state are derived. Second, focus on the problem of reduced stability caused by the large helix ratio, a scheme of "conformal cable pre-tightening + incomplete deployment" is proposed, which balances the stiffness and yield risk through pre-tightening load. Finally, an innovative process combination of "mold forming + furnace heat treatment + heavy pressure treatment" is adopted to solve the problem of dimensional precision. Experimental verification shows that the four helicon made of beryllium bronze do not undergo yield deformation in the retracted state, the deployment repeat accuracy is less than or equal to 1 mm, and its fundamental frequency in the expanded state is greater than 1 Hz, the product meets the application requirements.

       

    /

    返回文章
    返回