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MULTI-DAMAGES MONITORINGIN CFRP LAMINATED COMPOSITES

机译:CFRP层压复合材料中的多损伤监测

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摘要

Metallic structure monitoring has proved able to reduce both the risks of accident and maintenancecosts. Today monitoring systems designed for composite structures are limited to some kind ofdegradation like ones created by impacts. However, damage mechanisms in composite structures aremultiple and complex, they don’t only come from exceptional loading like impacts; a compositestructure is gradually damaged under a static or a fatigue loading.However we have to control and supervise those damage mechanisms to ensure the safety and themaintenance of systems. Today models able to predict the evolution of damages exist but theirprecision is limited because of the uncertainties linked to loading, initial material state andcharacteristics of the material. To remedy this problem we work on a monitoring system associatingpredictive models with periodic or continuous measurements. The measured variables could be astrain, a level of diffuse damage or characteristics of a delamination or a crack (position, size).In this paper, after the description of an application: a helicopter blade, we present a method based onthe electrical impedance measurement to monitor a delamination zone and the use of the Lamb wavespropagation to detect a crack along a structure edge. To finish we talk about the ways considered tomeasure the level of diffuse damage.
机译:金属结构监测已被证明能够降低事故风险和维护成本。如今,为复合结构设计的监控系统仅限于某种退化,例如由于撞击而造成的退化。但是,复合结构中的损伤机制是多种多样的,而且复杂的不仅是来自像冲击这样的异常载荷。复合材料结构在静态或疲劳载荷作用下会逐渐损坏。但是,我们必须控制和监督这些损坏机制,以确保系统的安全性和维护性。如今,已经存在能够预测损伤演变的模型,但由于与载荷,初始材料状态和材料特性有关的不确定性,其精度受到限制。为了解决这个问题,我们在监视系统上进行工作,将预测模型与定期或连续测量相关联。测得的变量可能是应变,弥散损伤的程度或分层或裂纹的特征(位置,大小)。在对应用进行描述之后:直升机叶片,我们提出了一种基于电阻抗测量的方法监测分层区域并使用兰姆波传播来检测沿结构边缘的裂缝。最后,我们讨论考虑测量弥散损伤程度的方法。

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