航空学报 > 2025, Vol. 46 Issue (7): 230948-230948   doi: 10.7527/S1000-6893.2024.30948

固体力学与飞行器总体设计

机理与生成对抗代理建模融合的飞机系统可靠性评估

冯蕴雯1,2, 腾达1,2(), 路成1,2, 王锐1,2, 陈俊宇1,2   

  1. 1.西北工业大学 航空学院,西安 710072
    2.飞行器基础布局全国重点实验室,西安 710072
  • 收稿日期:2024-07-15 修回日期:2024-09-09 接受日期:2024-10-08 出版日期:2024-10-16 发布日期:2024-10-15
  • 通讯作者: 腾达 E-mail:tengda@mail.nwpu.edu.cn
  • 基金资助:
    国家自然科学基金(51875465)

Integrated mechanism and generative adversarial surrogate modeling for aircraft systems reliability evaluation

Yunwen FENG1,2, Da TENG1,2(), Cheng LU1,2, Rui WANG1,2, Junyu CHEN1,2   

  1. 1.School of Aeronautics,Northwestern Polytechnical University,Xi’an 710072,China
    2.National Key Laboratory of Aircraft Configuration Design,Xi’an 710072,China
  • Received:2024-07-15 Revised:2024-09-09 Accepted:2024-10-08 Online:2024-10-16 Published:2024-10-15
  • Contact: Da TENG E-mail:tengda@mail.nwpu.edu.cn
  • Supported by:
    National Natural Science Foundation of China(51875465)

摘要:

为有效开展飞机系统可靠性评估,提出了一种机理与数据双驱的可靠性评估(MDRM)理念,在MDRM理念中,基于功能危险性分析(FHA)、故障模式及影响分析(FMEA)和故障树分析(FTA),从正向机理角度构建故障逻辑图,结合运行数据构建贝叶斯网络模型选取重要影响参数,将生成对抗理论引入代理模型,提出了生成对抗代理建模策略,用于建立影响参数与研究对象的关联模型,进而实现可靠性评估。基于MDRM理念,融合神经网络模型和紧支撑域思想,提出了生成对抗回归网络(GARN)方法用于飞机系统的可靠性评估。此外,运用数学案例证明所提出GARN的建模性能,通过某型国产民机1号液压系统低压和起落架刹车温度多失效案例验证所研究方法的工程适用性。通过多种方法对比表明,GARN具有突出的建模性能和仿真性能优势,所提出的理念和方法可为飞机系统可靠性评估提供有力的理论和技术支撑。

关键词: 机理与数据双驱, 飞机系统, 可靠性评估, 生成对抗代理建模, 液压系统低压, 起落架刹车温度多失效

Abstract:

To effectively perform aircraft system reliability evaluation, the Mechanism and Data dual-drive Reliability Monitoring (MDRM) concept has been proposed. In the MDRM concept, the fault logic diagram is constructed from the perspective of forward mechanism based on the Functional Hazard Analysis (FHA), Failure Mode and Effects Analysis (FMEA), and Fault Tree Analysis (FTA). By integrating optional data, a Bayesian network model is built to select important influencing parameters. The generative adversarial theory is introduced into the surrogate model, and a generative adversarial surrogate modeling strategy is presented to establish a correlation model between the influencing parameters and research object, thus enabling the reliability evaluation. The Generative Adversarial Regression Network (GARN) method is proposed for aircraft systems reliability evaluation by integrating the MDRM concept with neural network models and compact support region thought. In addition, the mathematical cases are adopted to demonstrate the modeling performance of proposed GARN, and the engineering applicability of developed method are verified through the No.1 hydraulic system low-pressure and landing gear brake temperature multi-failures of a domestic civil aircraft. The comparison of several methods shows that GARN holds outstanding modeling and simulation performance advantages, and the proposed concept and method can provide strong theoretical and technical support for aircraft system reliability assessment.

Key words: mechanism and data dual-drive, aircraft system, reliability evaluation, generative adversarial surrogate modeling, hydraulic system low-pressure, landing gear brake temperature multi-failures

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