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Upscaling the Data-driven Prognostic Methodologies Towards a Condition-based Structural Health Management of Composite Structures

机译:升高数据驱动的预后方法,朝向复合结构的条件的结构健康管理

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We present a conceptual methodology built in the framework of the ongoing EU H2020 Real-time Condition-based Maintenance for Adaptive Aircraft Maintenance Planning project, that leverages structural health monitoring data from different sensing technologies that goes a step beyond damage detection and diagnosis towards the probabilistic remaining useful life estimation in the presence of adverse conditions during flight. The methodology relies in several parallel activities from damage detection and localization to damage identification and severity assessment, sensitive-to-damage feature extraction processes, training methodologies, data fusion and remaining useful life predictions. Various sensing technologies i.e. static and dynamic strain sensing with FBGs, guided waves and acoustic emission are employed. An extensive hierarchical test campaign on test articles of increased complexity based on the building block approach is discussed with details as to the types of damage that are going to be targeted. Single and multi-stringer composite stiffened panels are subjected to realistic loading conditions. Emphasis on impact damage and skin/stringer fatigue disbonding/delamination is given. Last but not least, sophisticated mathematical algorithms are proposed e.g., multi-state degradation models such as Non-Homogeneous Hidden Semi Markov Model in order to deal with the data-driven RUL prediction with uncertainty quantification.
机译:我们提出了一种在适应性飞机维护计划项目的持续基于欧盟H2020实时条件维护的框架内建立的概念方法,该项目利用不同传感技术的结构健康监测数据,这些数据远远超出损坏检测和诊断对概率的验证和诊断在飞行期间存在不利条件的存在,剩余使用寿命估计。该方法依赖于损坏检测和定位的若干并行活动,以损坏识别和严重性评估,敏感的损坏特征提取过程,培训方法,数据融合和剩余的使用寿命预测。各种传感技术,采用了与FBG,引导波和声发射的静态和动态应变感测。基于建筑块方法的复杂性增加的大量分层测试运动是讨论的,详细讨论了要瞄准的损坏类型。单架和多桁条复合材料加强面板经受现实的装载条件。给出了强调冲击损伤和皮肤/纵梁疲劳脱粘/分层。最后但并非最不重要的是,提出了复杂的数学算法,例如,多状态劣化模型,例如非均匀隐藏的半马尔可夫模型,以便处理数据驱动的RUL预测,以不确定量化。

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