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基于扩展期望改善策略的自适应Kriging可靠性分析方法

李嘉,  余仕龙,  张伟,  石磊,  何聿

李嘉, 余仕龙, 张伟, 等. 基于扩展期望改善策略的自适应Kriging可靠性分析方法[J]. 航空动力学报, 2026, 42(X):20250275 doi: 10.13224/j.cnki.jasp.20250275
引用本文: 李嘉, 余仕龙, 张伟, 等. 基于扩展期望改善策略的自适应Kriging可靠性分析方法[J]. 航空动力学报, 2026, 42(X):20250275 doi: 10.13224/j.cnki.jasp.20250275
Li Jia, Yu Shilong, Zhang Wei, et al. Adaptive Kriging reliability analysis method based on extended expectation improvement strategy[J]. Journal of Aerospace Power, 2026, 42(X):20250275 doi: 10.13224/j.cnki.jasp.20250275
Citation: Li Jia, Yu Shilong, Zhang Wei, et al. Adaptive Kriging reliability analysis method based on extended expectation improvement strategy[J]. Journal of Aerospace Power, 2026, 42(X):20250275 doi: 10.13224/j.cnki.jasp.20250275

基于扩展期望改善策略的自适应Kriging可靠性分析方法

doi: 10.13224/j.cnki.jasp.20250275
基金项目: 陕西省自然科学基金中央引导地方科技发展资金课题(2024ZY-JCYJ-01-10)
详细信息
    作者简介:

    李嘉(1989-),男,副教授、博士生导师,博士,主要从事离心旋转机械性能及可靠性研究。E-mail:lijia@chd.edu.cn

  • 中图分类号: V233.91

Adaptive Kriging reliability analysis method based on extended expectation improvement strategy

  • 摘要:

    为了提高隐式、强非线性结构在可靠性求解时的计算效率与精度,发展一种改进的自适应Kriging可靠性分析方法。在Kriging模型加点策略中引入符号函数与距离权重函数以构建扩展期望改善学习函数,确保在极限状态曲面附近完成样本点更新。结合蒙特卡洛模拟构建自适应可靠性求解框架,确保计算稳定性并降低新增样本数量。通过经典数学算例与经典工程问题表明:所提方法相比蒙特卡洛模拟,失效概率相对误差不超过0.5%,新增样本数量较现有可靠性求解方法实现大幅降低。最后,某航空燃油离心泵汽蚀可靠性有限元算例表明:相对蒙特卡洛模拟,所提方法求解失效概率误差仅为1.06%;相较现有可靠性求解方法,所提方法实现计算成本降低51.06%。上述成果,验证了所提方法在隐式非线性结构可靠性分析中兼顾高精度与高效率的显著优势。

     

  • 图 1  AK-EEI-MCS算法流程

    Figure 1.  Algorithm process of AK-EEI-MCS

    图 2  主动学习函数拟合算例1结果

    Figure 2.  Results of Example 1 of active learning function fitting

    图 3  主动学习函数拟合算例2结果

    Figure 3.  Results of Example 2 of active learning function fitting

    图 4  某屋顶桁架结构示意图

    Figure 4.  Schematic diagram of a certain roof truss structure

    图 5  Non-linear Oscillator系统

    Figure 5.  Non-linear Oscillator system

    图 6  离心泵结构及汽蚀分布云图

    Figure 6.  Structure and cavitation distribution cloud diagram of centrifugal pump

    图 7  离心泵可靠性求解结果

    Figure 7.  Reliability solution results of the centrifugal pump

    表  1  算例1可靠性分析结果

    Table  1.   Reliability analysis results for Example 1

    方法 Ncall Pf /10−3 Cov(Pf)/% $ \varepsilon /\% $
    MCS 106 2.1971 4.6090
    AK-MCS 12+96 2.2172 2.1214 0.91
    AK-EFF-MCS 12+153 2.2901 2.0872 4.23
    AK-EI-MCS 12+95 2.1664 2.1048 1.40
    AK-EEI-MCS 12+79 2.2002 2.1463 0.14
    下载: 导出CSV

    表  2  算例2可靠性分析结果

    Table  2.   Reliability analysis results of Example 2

    方法 Ncall Pf/10−2 Cov(Pf)/% $ \varepsilon /{\text{%}} $
    MCS 106 7.3912 2.0863 -
    AK-MCS 15+771 7.2111 1.1344 2.44
    AK-EFF-MCS 15+776 7.3813 1.1201 0.13
    AK-EI-MCS 15+686 7.2324 1.1193 2.15
    AK-EEI-MCS 15+676 7.3933 1.1431 0.03
    下载: 导出CSV

    表  3  屋顶桁架结构输入参数分布

    Table  3.   Distribution of input parameters for roof truss structures

    变量分布类型均值标准差
    q/(N/m)正态分布200002000
    l/m正态分布13.50.50
    $ {A}_{\mathrm{s}} $/m2正态分布9.82×10−46×10−5
    $ {A}_{\mathrm{c}} $/m2正态分布0.040.008
    下载: 导出CSV

    表  4  某屋顶桁架结构可靠性分析结果

    Table  4.   Reliability analysis results of a certain roof truss structure

    方法 Ncall Pf /10−2 Cov(Pf)/% $ \varepsilon /{\text{%}} $
    MCS 106 4.1092 1.1529
    AK-MCS 8+252 4.1446 1.5347 0.86
    AK-EFF-MCS 8+384 4.1181 1.4786 0.22
    AK-EI-MCS 8+119 4.1125 1.5270 0.08
    AK-EEI-MCS 8+75 4.1072 1.5178 0.05
    下载: 导出CSV

    表  5  Non-linear Oscillator系统参数分布

    Table  5.   Distribution of parameters of non-linear oscillator system

    变量分布类型均值标准差
    m正态分布10.05
    c1正态分布10.1
    c2正态分布0.10.01
    F1正态分布10.2
    r正态分布0.50.05
    t1正态分布10.2
    下载: 导出CSV

    表  6  Non-linear Oscillator可靠性分析结果

    Table  6.   Reliability analysis results of non-linear oscillator

    方法 Ncall Pf /10−2 Cov(Pf)/% $ \varepsilon /{\text{%}} $
    MCS 106 2.7761 1.8714
    AK-MCS 50+221 2.8670 1.8407 3.27
    AK-EFF-MCS 50+384 2.6901 2.0148 3.10
    AK-EI-MCS 50+288 2.8210 1.8560 1.62
    AK-EEI-MCS 50+45 2.7862 1.8680 0.36
    下载: 导出CSV

    表  7  离心泵随机不确定性参数描述

    Table  7.   Description of random uncertainty parameters of centrifugal Pumps

    变量名称分布类型均值标准差
    叶轮入口直径$ {D}_{\mathrm{j}} $/mm正态分布40.6620.3
    叶轮出口直径$ {D}_{2} $/mm正态分布116.3300.3
    叶轮出口宽度$ {b}_{2} $/mm正态分布4.0040.3
    叶片出口角度$ {\beta }_{2} $/°正态分布15.800.03
    下载: 导出CSV

    表  8  离心泵汽蚀可靠性分析结果

    Table  8.   Cavitation reliability analysis results of centrifugal pump

    方法 Ncall Pf /10−4 Cov(Pf)/% $ \varepsilon /{\text{%}} $
    MCS 106 6.6516 4.0051
    AK-MCS 50+128 6.8323 3.8251 2.72
    AK-EFF-MCS 50+129 7.0102 3.6973 5.39
    AK-EI-MCS 50+94 6.3440 3.7463 4.62
    AK-EEI-MCS 50+46 6.5811 4.0019 1.06
    下载: 导出CSV
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  • 收稿日期:  2025-06-09
  • 网络出版日期:  2026-10-14

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