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复材飞机电气回路网物理-概率耦合可靠性评估

肖女娥,陈琦,汪克念,李勃阳   

  1. 中国民航大学
  • 收稿日期:2026-01-05 修回日期:2026-05-19 出版日期:2026-05-21 发布日期:2026-05-21
  • 通讯作者: 肖女娥
  • 基金资助:
    中央高校基本科研业务费项目;国家重点研发计划

Physics-Probability Coupled Reliability Assessment of Electrical Return Network in Composite Aircraft

  • Received:2026-01-05 Revised:2026-05-19 Online:2026-05-21 Published:2026-05-21
  • Supported by:
    Basic Research Funds for Central Universities;National Key Research and Development Program of China

摘要: 针对复合材料飞机电气回路网(Electrical Return Network, ERN)因节点规模庞大导致的状态空间爆炸与概率资源错配问题,提出一种结合拓扑筛选与概率引导的可靠性评估方法。该方法基于渗流理论与Molloy-Reed准则构建截断边界,通过网络度矩特征识别并剔除物理不可连通状态;进一步结合动态风险权重与后验后果截断机制,构建概率导引模型,从而引导蒙特卡洛采样向高风险失效区域聚焦。82节点主案例和29节点对照网络的结果表明,所提方法在保证评估精度的同时降低了计算开销。其中,在82节点主案例中,评估次数较传统蒙特卡洛方法削减96.25%,计算效率提升18.25倍,并在不同系统规模下保持较好的适用性。此外,异构部件寿命参数敏感性分析表明不同类型组件退化特征对系统连通可靠度衰退过程的影响存在差异。该方法可为复合材料飞机电气回路网全寿命周期连通可靠性分析提供一种可行的评估框架。

关键词: 复合材料飞机, 电气回路网, Survival Signature, 渗流理论, 动态风险权重

Abstract: To address the state-space explosion and probability resource mismatch caused by the large node scale of the composite aircraft electrical return network (ERN), a reliability assessment method combining topological screening and probability guidance is proposed. Based on the percolation theory and the Molloy-Reed criterion, a truncation boundary is constructed to identify and eliminate physically disconnected states through network degree-moment characteristics. Furthermore, a probability-guided model is established by integrating dynamic risk weights and a posterior consequence truncation mechanism, which guides the Monte Carlo sampling to focus on high-risk failure regions. The results of the 82-node primary case and the 29-node comparison network show that the proposed method reduces computational overhead while ensuring assessment accuracy. Specifically, in the 82-node primary case, the number of evaluations is reduced by 96.25% and the computational efficiency is improved by 18.25 times compared with the traditional Monte Carlo method, demonstrating good applicability across different system scales. In addition, the sensitivity analysis of heterogeneous component life parameters indicates that the degradation characteristics of different component types have different effects on the degradation process of system connectivity reliability. The proposed method can provide a feasible assessment framework for the full-life-cycle connectivity reliability analysis of the composite aircraft ERN.

Key words: Composite aircraft, Electrical Return Network, Survival Signature, Percolation Theory, Dynamic Risk Weight

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