Benefits of Non-Destructive Evaluation and Probabilistic Damage Tolerance Cosimulation for Fracture Risk Reduction

Fabrice Foucher, Sébastien Lonné, Philippe Dubois, Stéphane Leberre, Pierre Calmon, Michael Enright, Yasin Zaman
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Abstract

In the context of the damage tolerance approach used to drive aircraft maintenance operations, it is essential to demonstrate the reliability of NDE inspections in detecting structural damage especially for additively manufactured components since this process produces components that may introduce material anomalies at any location within a component. The Probability Of Detection curve (POD) that links the probability to detect a detrimental flaw to its size is generally used as a key indicator for that purpose by giving the maximum flaw size that a NDE process can miss with a given level of probability and confidence. This information can then be used along with other inputs such as component geometries, mechanical properties, constraints, service and residual stresses and damage evolution speed to assess fracture risk and then adapt maintenance scenarios to optimize safety and component service life. NDE reliability and risk assessment are based on statistical indicators that need a large amount of data to provide reliable metrics. It is difficult to obtain such indicators using a purely empirical approach that is based on physical trials and measurements as it may involve many mock-ups and costly processes. Simulation tools can achieve this goal via their ability to include and precisely monitor many parameters as well as high computing capacities that are now available. The work presented in this paper involved cosimulations performed between the DARWIN® probabilistic damage tolerance software and the CIVA NDE simulation software. DARWIN computes fracture risk levels throughout a component, while CIVA can efficiently provide Probability Of Detection curves at different locations in a component and for various NDE methods. The presented application deals with a titanium gas turbine engine impeller disk and involves an Ultrasonic NDE inspection technique. It appears to be a very interesting approach to connect together NDE and Fracture mechanics simulations, two disciplines that generally work on their own. Indeed, DARWIN helps the user to determine detrimental flaw types, locations and sizes which are key inputs to develop an effective NDE inspection method. CIVA can provide location-specific POD curves that enable DARWIN to quantity the effect of dedicated NDE on potential risk reduction. This highlights the importance of NDE simulation for safety and helps to identify potential changes in the physical NDE process and the maintenance cycle that provide the best compromise between detection performance and cost.
无损评估和概率损伤容限联合模拟对降低断裂风险的好处
在用于驱动飞机维修操作的损伤容限方法的背景下,必须证明无损检测检测在检测结构损伤方面的可靠性,特别是对于增材制造的部件,因为该过程产生的部件可能在组件内的任何位置引入材料异常。检测概率曲线(POD)将检测到有害缺陷的概率与其大小联系起来,通过给出NDE过程在给定的概率和置信度水平下可能错过的最大缺陷尺寸,通常用作该目的的关键指标。然后,这些信息可以与部件几何形状、机械性能、约束、使用和残余应力以及损伤演变速度等其他输入一起使用,以评估断裂风险,然后调整维护方案,以优化安全性和部件的使用寿命。NDE可靠性和风险评估基于统计指标,需要大量的数据来提供可靠的度量。使用基于物理试验和测量的纯经验方法很难获得这些指标,因为它可能涉及许多模型和昂贵的过程。仿真工具可以通过包含和精确监控许多参数以及现在可用的高计算能力来实现这一目标。本文中介绍的工作涉及在DARWIN®概率损伤容限软件和CIVA NDE仿真软件之间进行的共同模拟。DARWIN计算整个组件的断裂风险等级,而CIVA可以有效地提供组件不同位置和各种无损检测方法的检测概率曲线。介绍了一种钛合金燃气涡轮发动机叶轮盘的超声无损检测技术。将濒死体验和断裂力学模拟结合起来似乎是一种非常有趣的方法,这两个学科通常是相互独立的。实际上,DARWIN可以帮助用户确定有害缺陷的类型、位置和尺寸,这些都是开发有效无损检测方法的关键输入。CIVA可以提供特定地点的POD曲线,使DARWIN能够量化专用NDE对潜在风险降低的影响。这突出了NDE模拟对安全的重要性,并有助于识别物理NDE过程和维护周期中的潜在变化,从而在检测性能和成本之间提供最佳折衷。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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