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Flight Tests Performed by EMBRAER with SHM Systems

机译:EMBRAER与SHM Systems进行的飞行测试

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This paper presents an overview of a set of tests performed by Embraer with two different SHM technologies in an E-Jets flight tests aircraft. Considered as promising technologies for monitoring structural parts, sensors networks including cables and connectors of CVM (Comparative Vacuum Monitoring) and LW (Lamb Waves) were installed in an Embraer-190 aircraft. The two technologies have been investigated by Embraer within the company's effort on Structural Health Monitoring. Scheduled maintenance and inspection activities can take advantage of the SHM technologies by evaluating the structural integrity of an aircraft with on-board sensors and performing less time-consuming procedures - compared to current NDT technologies - which can not only reduce the amount of time and burden of those activities, but also minimize the effects of "human-factors" when compared to current inspection tasks. The tests performed with CVM and LW components (sensors, connectors and cables) installed in a flight tests aircraft focus on the investigation of the technologies' capabilities of withstanding the real aircraft operational conditions. Periodic monitoring of these on-board sensors has been performed using CVM and LW ground equipments. A further phase of this project is currently under development and focus on the demonstration of an on-board in-flight version of the CVM instrumentation system for continuous monitoring of aircraft structures during flight, aiming to demonstrate the ability of the CVM onboard equipment to withstand the aircraft in-flight environmental and operational conditions. Preliminary results on both partially and totally on-board equipments indicate that they can withstand the environmental and operational conditions; however, further tests need to be performed. Performing periodic inspections on ground with SHM systems lead to different qualification requirements when compared to those required for a complete on-board system that performs continuous monitoring. An overview of those two aspects of qualification requirements will also be presented.
机译:本文概述了巴西航空工业公司在E-Jets飞行测试飞机上使用两种不同的SHM技术进行的一系列测试。被认为是监测结构部件的有前途的技术,在Embraer-190飞机上安装了传感器网络,包括CVM(比较真空监测)和LW(Lamb Waves)的电缆和连接器。巴西航空工业公司在公司的结构健康监测工作中对这两种技术进行了研究。与现有的无损检测技术相比,预定的维护和检查活动可以通过评估带有机载传感器的飞机的结构完整性并执行耗时较少的程序来利用SHM技术,这不仅可以减少时间和负担与当前的检查任务相比,还可以最大程度地减少“人为因素”的影响。使用安装在飞行测试飞机上的CVM和LW组件(传感器,连接器和电缆)进行的测试着重于研究技术在承受实际飞机运行条件时的能力。使用CVM和LW地面设备对这些车载传感器进行定期监控。该项目的进一步阶段目前正在开发中,其重点是演示机载飞行中版本的CVM仪器系统,以在飞行过程中连续监视飞机结构,旨在证明CVM机载设备的承受能力飞机在飞行中的环境和运行条件。部分和全部车载设备的初步结果表明它们可以承受环境和操作条件;但是,还需要执行进一步的测试。与执行连续监控的完整车载系统相比,使用SHM系统在地面上进行定期检查会导致不同的资格要求。还将对资格要求的这两个方面进行概述。

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