PZL-130TCII的在线多路原位无损检测方法

Q4 Engineering
K. Dragan, M. Dziendzikowski, A. Kurnyta, Adam Latoszek, A. Leski, S. Kłysz
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引用次数: 1

摘要

提供一个可靠和通用的结构健康监测(SHM)系统,允许远程飞机检查和降低维护成本是当今航空航天工业面临的主要挑战。基于导向兰姆波的SHM是一种能够在满足所有相关要求的情况下解决这一问题的方法。提出了一种飞机结构连续实时损伤生长监测和早期损伤检测的整体方法。该系统的主要组成部分是压电换能器(PZT)网络。此外,还有其他SHM方法:在选定的飞机热点进行比较真空监测(CVMTM)和电阻计。本文提供了损伤检测能力的描述,包括从PZL-130 Orlik飞机全尺寸疲劳试验中收集的数据分析。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
An On-Line Multiway Approach to In-Situ NDI Looking at the PZL-130TCII
Abstract Providing a reliable and universal Structural Health Monitoring (SHM) system allowing for remote aircraft inspections and a reduction of maintenance costs is a major challenge confronting the aerospace industry today. SHM based on guided Lamb waves is one of the approaches capable of addressing the issue while satisfying all the associated requirements. This paper presents a holistic approach to the continuous real time damage growth monitoring and early damage detection in aircraft structure. The main component of the system is a piezoelectric transducers (PZT) network. It is complemented by other SHM methods: Comparative Vacuum Monitoring (CVMTM) and Resistance Gauges at selected aircraft hot spots. The paper offers the description of damage detection capabilities including the analysis of data collected from the PZL-130 Orlik aircraft full-scale fatigue test.
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来源期刊
Fatigue of Aircraft Structures
Fatigue of Aircraft Structures Engineering-Safety, Risk, Reliability and Quality
CiteScore
0.40
自引率
0.00%
发文量
0
期刊介绍: The publication focuses on problems of aeronautical fatigue and structural integrity. The preferred topics include: full-scale fatigue testing of aircraft and aircraft structural components, fatigue of materials and structures, advanced materials and innovative structural concepts, damage tolerant design of aircraft structure, life extension and management of ageing fleets, structural health monitoring and loads, fatigue crack growth and life prediction methods, NDT inspections, airworthiness considerations.
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