Impact Damage Localisation with Piezoelectric Sensors under Operational and Environmental Conditions.

Mohammad Salmanpour,M Aliabadi,Zahra Sharif Khodaei

doi:10.3390/s17051178

Mohammad Salmanpour, M Aliabadi + Show 1 more

Open Access

https://doi.org/10.3390/s17051178

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Journal: Sensors (Basel, Switzerland)	Publication Date: May 22, 2017
Citations: 61	License type: CC BY 4.0

Affiliation: Imperial College London

Abstract

Guided-wave structural health monitoring (SHM) systems with piezoelectric sensors are investigated for localisation of barely visible impact damage in CFRP plates under vibration and different thermal conditions. A single baseline set is used in a delay-and-sum algorithm with temperature correction for damage localisation in a large temperature range. Damage localisation is also demonstrated under transient thermal conditions, with signals recorded while the temperature is rapidly decreased. Damage severity due to successive impact events is studied under constant temperature. Damage is also localised when the plate is subjected to random vibration.

Highlights

Permanently-attached transducer networks are an important part of structural health monitoring (SHM) systems
These systems can be used for damage detection in carbon fibre-reinforced polymer (CFRP) composite materials commonly used in aircraft structures
Visible impact damage was localised on a CFRP plate with a single pristine baseline recorded at 25 ◦ C in a temperatures range of −50 ◦ C to 60 ◦ C by applying temperature compensation

Summary

Introduction

Permanently-attached transducer networks are an important part of structural health monitoring (SHM) systems. These systems can be used for damage detection in carbon fibre-reinforced polymer (CFRP) composite materials commonly used in aircraft structures. SHM covers a wide range of approaches; this work is focused on active ultrasonic guided wave methods. In sparse array guided wave SHM, a network of attached ultrasonic transducers, typically piezoelectric lead zirconate titanate (PZT), generate and sense diagnostics signals, which are influenced by the material and geometric properties of the host structure. Lamb wave propagation can be used in delay-and-sum baseline comparison methods to detect and localise damage [1,2]. Typical airliners operate in a range of conditions; airborne SHM components (see Figure 1)

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Conclusion