Design of a pulsed eddy current sensor for detection of defects in aircraft lap-joints

This paper presents a new type of pulsed eddy current (PEC) sensor that has been designed for defect detection in aircraft lap-joint structures. The sensor employs a new excitation circuit that requires no additional signal amplification and the paper also reports compensation techniques that improv...

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Veröffentlicht in:Sensors and actuators. A. Physical. 2002-09, Vol.101 (1), p.92-98
Hauptverfasser: Sophian, Ali, Tian, Gui Yun, Taylor, David, Rudlin, John
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container_title Sensors and actuators. A. Physical.
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creator Sophian, Ali
Tian, Gui Yun
Taylor, David
Rudlin, John
description This paper presents a new type of pulsed eddy current (PEC) sensor that has been designed for defect detection in aircraft lap-joint structures. The sensor employs a new excitation circuit that requires no additional signal amplification and the paper also reports compensation techniques that improve the sensing resolution and stability. A new hybrid feature of the peak value in time domain and the maximum frequency magnitude in frequency domain has been investigated. A test rig has been built and some results from aircraft samples are presented.
doi_str_mv 10.1016/S0924-4247(02)00195-4
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source Elsevier ScienceDirect Journals
subjects Aircraft NDT
Cross-disciplinary physics: materials science
rheology
Digital compensation
Exact sciences and technology
Feature extraction
Instruments, apparatus, components and techniques common to several branches of physics and astronomy
Magnetic components, instruments and techniques
Magnetic sensor
Materials science
Materials testing
Nondestructive testing: electromagnetic testing, eddy-current testing
Physics
Pulsed eddy current (PEC) sensor
Transient response
title Design of a pulsed eddy current sensor for detection of defects in aircraft lap-joints
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