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Integrated phased array transducer, system and methodology for structural health monitoring of aerospace structures

机译:集成相控阵换能器,用于航空结构结构健康监测的系统和方法

摘要

Permanently bonded to a structure, an integrated Phased Array (PhA) structural radar transducer that can provide reliable electromechanical connection with corresponding sophisticated miniaturized electronic "all in one" SHM device installed directly above it, without need for any interface cabling, during entire aerospace structure lifecycle and for a huge variety of real harsh service environments of structures to be monitored is presented. The integrated PhA transducer consists of a set of aligned piezo-electric discs with wrap around electrodes for transceiving of elastic ultrasonic waves, plurality of electrical traces and contact pads, several layers of a flexible printed circuit board, electromagnetic shielding between channels and overall, one electromechanical multipinned connector and all that integrated into one small unit easy for surface installation by bonding and final application on real structures. This invention is intentioned to be used for numerous important real time or on demand applications like: structural health monitoring, temperature distribution mapping, deformation distribution mapping, stress distribution mapping, stiffness distribution mapping, vibration distribution mapping, characterization of structure material physical properties, impact detection, leakage detection, etc. and all that during almost all phases of structure life cycle, like manufacturing process, curing, assembly, certification testing, flight testing, maintenance and real service. The invention is an important prerequisite toward future real extensive application of distributed structural health monitoring systems on common aircraft structures with in situ processing, quick reports generation about real structural health, status, condition or performance. This integrated PhA transducer, as a key component of PAMELA SHM (Phased Array Monitoring for Enhanced Life Assessment) system, has two principal tasks at the same time, reliably transceive elastic waves and serves as a reliable sole carrier or support for associated sophisticated SHM electronic device attached above.
机译:集成相控阵(PhA)结构雷达传感器永久性地结合在结构上,可以在整个航空航天结构中与直接安装在其上方的相应的精密小型化电子“多合一” SHM设备提供可靠的机电连接,而无需任何接口电缆提出了生命周期以及要监视的结构的各种实际恶劣服务环境。集成的PhA换能器由一组对齐的压电圆盘组成,带有环绕式电极,用于收发弹性超声波,多条电迹线和接触垫,几层柔性印刷电路板,通道与整体之间的电磁屏蔽,一个机电式多针连接器,所有这些都集成到一个小单元中,通过粘接和最终应用到实际结构上,易于表面安装。本发明旨在用于许多重要的实时或按需应用,例如:结构健康监测,温度分布图,变形分布图,应力分布图,刚度分布图,振动分布图,结构材料物理特性的表征,冲击检测,泄漏检测等,以及结构生命周期几乎所有阶段的所有过程,例如制造过程,固化,组装,认证测试,飞行测试,维护和实际服务。本发明是未来将分布式结构健康监测系统真正地广泛应用到具有现场处理的普通飞机结构上的重要先决条件,能够快速生成有关实际结构健康,状态,状况或性能的报告。作为PAMELA SHM(用于增强寿命评估的相控阵监测)系统的关键组件,该集成式PhA传感器具有两个主要任务,可同时可靠地收发弹性波,并且可作为可靠的唯一载体或对相关的复杂SHM电子设备的支持上面连接的设备。

著录项

  • 公开/公告号EP2489442A1

    专利类型

  • 公开/公告日2012-08-22

    原文格式PDF

  • 申请/专利权人 AERNNOVA ENGINEERING SOLUTIONS IBERICA;

    申请/专利号EP20110382045

  • 发明设计人 COKONAJ VALERIJAN;

    申请日2011-02-18

  • 分类号B06B1/06;

  • 国家 EP

  • 入库时间 2022-08-21 17:12:00

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