Verification of Probabilistic Risk Assessment Method AMETA for Aircraft Fatigue Life Management

被引:0
|
作者
Chen, Tzikang John [1 ]
Shiao, Michael [1 ]
Haile, Mulugeta [1 ]
机构
[1] Army Res Lab, Vehicle Technol Directorate, Adelphi, MD 20783 USA
关键词
Aircraft Maintenance Event Tree Analysis; AMETA; Fatigue Life Management; Monte Carlo; Importance Sampling; probability of detection; inspection scheduling; repair/replacement/retirement strategies;
D O I
10.1117/12.2513592
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
A probabilistic risk assessment method to assess the failure possibilities of aircraft fatigue critical components due to fatigue damage initiation and propagation, as well as the effect of complex maintenance scenarios throughout the aircraft's service life (including multiple repair types and various nondestructive inspection (NDI) techniques), needs to be developed for aircraft fatigue life management. The traditional Monte Carlo simulation (MCS) offers the most robust and reliable solution; however, MCS is time consuming and unable to support prompt risk decisions. To relieve the computational burden, a novel probabilistic method-AMETA (Aircraft Maintenance Event Tree Analysis)-was developed, which combines the generality of random simulations with the efficiency of analytical probabilistic methods. AMETA consists of a fatigue maintenance event tree and a probabilistic algorithm comprising a set of probabilistic equations. AMETA systematically transforms a complex random maintenance pattern requiring a large number (in the order of billions) of MCSs to more logical and manageable fatigue paths represented by a finite set of probabilistic events to achieve the required computational accuracy and efficiency. Furthermore, the Importance Sampling Method (ISM) can be used for efficiency improvement. In this paper, the accuracy, efficiency and robustness of AMETA are verified and demonstrated. A procedure was provided to select the most suitable sampling functions for ISM. It is found that AMETA is several orders of magnitude more efficient than MCS for the same level of accuracy.
引用
收藏
页数:15
相关论文
共 50 条
  • [31] Prediction approach for corrosion fatigue life of aircraft structure based on probabilistic fracture mechanics
    Tan, Xiaoming
    Chen, Yueliang
    Jin, Ping
    FRACTURE AND DAMAGE MECHANICS V, PTS 1 AND 2, 2006, 324-325 : 943 - +
  • [32] Probabilistic Risk Assessment of Accidental Damage to Civil Aircraft Composite Structures
    Jia, Baohui
    Fang, Jiachen
    Lu, Xiang
    Xiong, Yijie
    SAE INTERNATIONAL JOURNAL OF AEROSPACE, 2023, 16 (02): : 221 - 230
  • [33] Fatigue life evaluation and test verification for civil aircraft structure under corrosive environment
    Yang, Hongyuan
    Liu, Wenting
    Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2007, 33 (05): : 514 - 517
  • [34] Fuzzy probabilistic assessment of aging aircraft structures subjected to multiple site fatigue damage
    Akpan, UO
    Rushton, PA
    Dunbar, TE
    Koko, TS
    Fatigue Testing and Analysis Under Variable Amplitude Loading Conditions, 2005, 1439 : 521 - 534
  • [35] Vibration Fatigue Probabilistic Life Prediction Model and Method for Blade
    Lou Guokang
    Wen Weidong
    Wu Fuxian
    Zhang Hongjian
    TransactionsofNanjingUniversityofAeronauticsandAstronautics, 2018, 35 (03) : 494 - 506
  • [36] Vibration Fatigue Probabilistic Life Prediction Model and Method for Blade
    Lou G.
    Wen W.
    Wu F.
    Zhang H.
    Transactions of Nanjing University of Aeronautics and Astronautics, 2018, 35 (03) : 494 - 506
  • [37] A METHOD FOR PROPAGATING UNCERTAINTY IN PROBABILISTIC RISK ASSESSMENT
    AHMED, S
    CLARK, RE
    METCALF, DR
    NUCLEAR TECHNOLOGY, 1982, 59 (02) : 238 - 245
  • [38] A Configuration Management Assessment Method for SON Verification
    Tsvetkov, Tsvetko
    Novaczki, Szabolcs
    Sanneck, Henning
    Carle, Georg
    2014 11TH INTERNATIONAL SYMPOSIUM ON WIRELESS COMMUNICATIONS SYSTEMS (ISWCS), 2014, : 380 - 384
  • [39] Numerical method for fatigue life of aircraft lugs under thermal stress
    You, Ziyun
    Liu, Xintian
    Jiang, Zhao
    Wang, Xu
    Wang, Yansong
    Wang, Xiaolan
    Journal of Aircraft, 2020, 57 (04): : 597 - 602
  • [40] Numerical Method for Fatigue Life of Aircraft Lugs Under Thermal Stress
    You, Ziyun
    Liu, Xintian
    Jiang, Zhao
    Wang, Xu
    Wang, Yansong
    Wang, Xiaolan
    JOURNAL OF AIRCRAFT, 2020, 57 (04): : 597 - 602