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空间柔性卷绕式太阳电池阵减振防护技术研究

赵寿根1,高红鑫2,朱佳林3,李一博1,张振1,杨乐天1   

  1. 1. 北京航空航天大学航空科学与工程学院固体力学研究所
    2. 北京航空航天大学航空科学与工程学院
    3. 北京空间飞行器总体设计部
  • 收稿日期:2025-05-07 修回日期:2025-07-09 出版日期:2025-07-15 发布日期:2025-07-15
  • 通讯作者: 赵寿根

Study on vibration reduction method of flexible roll-out solar array

  • Received:2025-05-07 Revised:2025-07-09 Online:2025-07-15 Published:2025-07-15
  • Contact: Shou-Gen ZHANG

摘要: 针对柔性卷绕式空间太阳电池阵在发射阶段振动环境中的结构安全性问题,提出了一种基于卷绕预紧力和聚酰亚胺泡棉的创新性减振防护方案。该方案在无需额外复杂结构的情况下,仅通过调整卷绕预紧力和引入聚酰亚胺泡棉减振层,有效提升了空间电池阵的抗振性。研究首先建立了柔性卷绕式太阳电池阵的精细化仿真分析模型,然后评估了不同振动频率、振幅及预紧力对电池阵结构安全性的影响规律。在此基础上,对样机开展了相应振动试验,验证了论文方案在实际应用中的减振效果,试验实测结果表明该减振防护措施能够显著降低CIC电池的应变响应,减振效率达60%以上,同时,仿真和试验测试结果的一致性,也证明了论文分析模型的准确、可靠。

关键词: 柔性卷绕式太阳电池阵, 卷绕预紧力, 减振防护, 聚酰亚胺泡棉

Abstract: To address the structural safety of flexible roll-out solar array in the vibration environment during the launch phase, an innovative vibration reduction method based on winding preload and polyimide foam is proposed. This solution effectively improves the vibration resistance of the battery array without the need for additional complex structures, simply by adjusting the winding preload and introducing a polyimide foam vibration damping layer. The study first establishes a refined finite element simulation model of a flexible wound solar array, and then evaluates the effects of different vibration frequencies, amplitudes and preload forces on the structural safety of the array. In addition, vibration experiments on a small engineering prototype verified the vibration damping effect of the scheme in practical applications, and the results show that the design can significantly reduce the strain response of the CIC cell, and the vibration damping efficiency reaches more than 60%. The high consistency of the simulation and experimental results indicates that the vibration damping scheme has strong engineering feasibility and practical application potential.

Key words: roll-out solar array, winding preload, vibration reduction design, polyimide foam