1. 电子科技大学长三角研究院(湖州),湖州,313000
2. 电子科技大学,成都,611731
3. 西华大学,成都,610039
纸质出版:2025
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智鹏鹏, 刘瀚儒, 官毅, 等. 基于主动学习Kriging的航空发动机机构可靠性分析方法[J]. 航空制造技术, 2025,68(20).
ZHI Pengpeng, LIU Hanru, GUAN Yi, et al. Active Learning Kriging-Based Mechanism Reliability Analysis for Aero-Engine[J]. Aeronautical Manufacturing Technology, 2025, 68(20).
智鹏鹏, 刘瀚儒, 官毅, 等. 基于主动学习Kriging的航空发动机机构可靠性分析方法[J]. 航空制造技术, 2025,68(20). DOI: 10.16080/j.issn1671-833x.2025.20.014.
ZHI Pengpeng, LIU Hanru, GUAN Yi, et al. Active Learning Kriging-Based Mechanism Reliability Analysis for Aero-Engine[J]. Aeronautical Manufacturing Technology, 2025, 68(20). DOI: 10.16080/j.issn1671-833x.2025.20.014.
针对复杂航空机构可靠性分析过程中建模难度大、精度差、计算效率低等问题,提出一种数据增强拉丁超立方抽样(Data augmentation Latin hypercube sampling,DALHS)、自适应分区拒绝权重采样(Adaptive partitioned threshold rejection sampling,APTRS)和主动学习Kriging 相结合的机构可靠性分析方法。首先,利用数据增强技术改进拉丁超立方抽样,获取初始样本点,提高初始样本点的多样性和代表性;其次,采用自适应分区策略划分设计空间,并在子空间内执行拒绝权重采样,提升样本局部和全局搜索能力;再次,提出主动学习NU(Normalize U)函数筛选高质量样本,结合准随机分形算法(Quasi-random fractal algorithm,QRFA)动态优化Kriging 模型,构建DALHS– APTRS-Kriging 模型;最后,利用变异系数收敛准则,实现航空机构可靠度的高效计算。结果表明,通航活塞发动机机构的可靠度为0.987,模型调用次数仅为72,相比传统方法,计算误差仅为5.7%,说明所提方法不仅能在少量样本下获得高质量的Kriging 模型,而且在兼具局部和全局搜索下提升了可靠度计算的效率和精度。
In order to address the problems of high modeling difficulty
poor accuracy and low computational efficiency in the process of reliability analysis of complex aerospace agencies
a method combining data augmentation Latin hypercube sampling (DALHS)
adaptive partitioned threshold rejection sampling (APTRS) and active learning Kriging is proposed for agency reliability analysis. First
the data enhancement technique is used to improve Latin hypercube sampling to obtain initial sample points and improve the diversity and representativeness of the initial sample points; second
an adaptive partitioning strategy is used to divide the design space and perform rejection weight sampling within the subspace to improve the local and global search capability of the samples; third
the active learning NU (Normalize U) function is proposed to screen high-quality samples
combined with the quasi-random fractal algorithm (QRFA) to dynamically optimize the Kriging model
and construct the DALHS – APTRS – Kriging model; finally
we use the convergence criterion of the coefficient of variation to realize the efficient calculation of the reliability of the aviation mechanism. The results show that the mechanism reliability of the general aviation piston engine is 0.987
with only 72 model calls
and a calculation error of only 5.7% compared to traditional methods. This indicates that the proposed method can not only obtain high-quality Kriging models with a small number of samples but also improve the efficiency and accuracy of reliability calculation by combining local and global search.
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