首页> 外文会议>Symposium of the International Committee On Aeronautical Fatigue >U.S. AIR FORCE EFFORTS IN UNDERSTANDING AND MITIGATING THE EFFECTS OF 'NDI MISSES'
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U.S. AIR FORCE EFFORTS IN UNDERSTANDING AND MITIGATING THE EFFECTS OF 'NDI MISSES'

机译:美国空军在理解和减轻“NDI错过”的影响下的努力

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Recent events within the U.S. Air Force (USAF) have highlighted the reality that cracks large enough to be readily detected by non-destructive inspection (NDI) can be missed during in-service NDI actions. These so-called "missed crack" or "NDI miss" events may pose serious risks to the safety and integrity of aircraft structures. This paper will review USAF actions: 1) to understand the severity and ramifications of the NDI miss problem, 2) to minimize the probability that cracks will be missed, and 3) to mitigate the effects of undetected cracks. Under the current USAF inspection philosophy, missed cracks that are larger than a crack that can grow to a critical size before the next scheduled inspection pose the greatest risk to structural safety. Significant challenges exist in understanding what causes cracks to be missed, in quantifying how many and how frequently cracks are missed based upon available maintenance data, in calculating the risk to flight safety of missed cracks, and, finally, in developing technologies that will minimize the future probability that cracks greater than a specified size will be missed. The probability that a structural component will be inspected as required and that a detectable crack will, indeed, be found, are both key factors affecting NDI misses. In this paper, the probability of detection (POD) concept will be described from the standpoint of the variables that govern the detectable crack size associated with a given POD. Special attention will be given to the utility of the "90/95" crack size (the size of a crack that can be found 90% of the time with 95% confidence). The discussion of the POD idea will be augmented to include the concept of a probability of miss (POM). POM, though computed simply by subtracting POD from unity, focuses attention on the size of a crack that can go undetected and, therefore threaten safety and structural integrity. Examples will be presented that illustrate the ramifications missed cracks have on aircraft structural safety. A technique for estimating the probability distribution of missed cracks based on NDI findings (i.e. "found cracks") and on the knowledge of a specific NDI technique's POD capability will be described. In addition, a brief review of recent advances in NDI technologies and techniques designed to minimize NDI misses will be presented.
机译:美国空军(USAF)内的最近事件强调了在役的非破坏性检查(NDI)中可能错过足够大的裂缝的现实,以便在役的NDI行动中错过。这些所谓的“错过裂缝”或“NDI Miss”事件可能会对飞机结构的安全性和完整性构成严重风险。本文将审查USAF行动:1)了解NDI错过问题的严重程度和后果,2)以最大限度地减少裂缝将错过的概率和3)减轻未检测到的裂缝的影响。在目前的USAF检查哲学下,错过的裂缝大于裂缝,在下一个预定检查之前可能会增加到临界大小的临界大小构成了结构安全的最大风险。在了解裂缝的情况下,在量化基于可用维护数据的情况下,在计算出飞行裂缝的飞行安全风险时,仍然存在裂缝的裂缝,以及最终,在开发最小化的技术未来概率将遗漏大于指定尺寸的裂缝。根据需要检查结构部件的概率,并且确实可以发现可检测的裂缝是影响NDI未命中的关键因素。在本文中,将从控制与给定窗口相关联的可检测的裂缝大小的变量的观点来描述检测(POD)概念的概率。将特别注意“90/95”裂缝尺寸的效用(可以在95%置信度的90%的时间内找到90%的裂缝的大小)。对POD思想的讨论将被增强,以包括小姐(POM)的概率。 POM,虽然只需从Unity中减去豆荚来计算,请注意可以在无法被发现的裂缝的大小,因此威胁到安全性和结构完整性。将提出示例,说明未错过的裂缝对飞机结构安全的影响。基于NDI发现的错失裂缝概率分布(即“发现裂缝”)及对特定NDI技术的知识进行估计的技术将描述。此外,还将介绍对最近的NDI技术和技术旨在最大限度地减少NDI未命中的技术的进步。

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