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Journal ArticleDOI

Detection of bolt loosening in C–C composite thermal protection panels: I. Diagnostic principle

Jinkyu Yang, +1 more
- 01 Apr 2006 - 
- Vol. 15, Iss: 2, pp 581-590
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TLDR
In this article, an attenuation-based diagnostic method was proposed to assess the fastener integrity by observing the attenuation patterns of the resultant sensor signals, which is based on the damping phenomena of ultrasonic waves across the bolted joints.
Abstract
A concept demonstrator of the structural health monitoring (SHM) system was developed to autonomously detect the degradation of the mechanical integrity of the standoff carbon–carbon (C–C) thermal protection system (TPS) panels. This system enables us to identify the location of the loosened bolts, as well as to predict the torque levels of those bolts accordingly. In the process of building the proposed SHM prototype, efforts have been focused primarily on developing a trustworthy diagnostic scheme and a responsive sensor suite. In part I of the study, an attenuation-based diagnostic method was proposed to assess the fastener integrity by observing the attenuation patterns of the resultant sensor signals. The attenuation-based method is based on the damping phenomena of ultrasonic waves across the bolted joints. The major advantage of the attenuation-based method over the conventional diagnostic methods is its local sensing capability of loosened brackets. The method can further discriminate the two major failure modes within a bracket: panel-joint loosening and bracket-joint loosening. The theoretical explanation of the attenuation-based method is performed using micro-contact theory and structural/internal damping principles, followed by parametric model studies and appropriate hypothesis testing.

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Citations
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Journal ArticleDOI

Active health monitoring of an aircraft wing with embedded piezoelectric sensor/actuator network: I. Defect detection, localization and growth monitoring

TL;DR: In this article, an ultrasonic guided wave structural health monitoring (SHM) system was developed for aircraft wing inspection, where small, low-cost and light-weight piezoelectric (PZT) discs were bonded to various parts of the aircraft wing, in a form of relatively sparse arrays, for simulated cracks and corrosion monitoring.
Journal ArticleDOI

Structural health monitoring of bolted joints using linear and nonlinear acoustic/ultrasound methods

TL;DR: In this paper, the authors developed a reliable index able to assess the loosening/tightening health state of a bolted structure based on linear and nonlinear acoustic/ultrasound parameters.
Journal ArticleDOI

Damage localisation in plate-like structures based on PZT sensors

TL;DR: In this article, signal processing algorithms for damage localisation purposes in plate-like structures were proposed, where elastic wave propagation phenomenon was used for damage detection and localisation, and the proposed methods were successfully tested on aluminium alloy specimen and carbon-epoxy specimen.
Journal ArticleDOI

Proof-of-concept study of monitoring bolt connection status using a piezoelectric based active sensing method

TL;DR: In this article, two piezoceramic patches are bonded to the two different parts of a bolted connection, and the received energy depends on the interface fastening pressure which is determined by the bolt torque.
Journal ArticleDOI

A Novel Fractal Contact-Electromechanical Impedance Model for Quantitative Monitoring of Bolted Joint Looseness

TL;DR: This paper attempts to quantify EMI based methods through the integration of fractal contact theory, the result of which is a novel electromechanical impedance model for quantitative monitoring of bolted looseness.
References
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MonographDOI

Contact Mechanics: Frontmatter

K. L. Johnson
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Acoustic Fields and Waves in Solids

Bert A. Auld
TL;DR: In this article, the authors apply the material developed in the Volume One to various boundary value problems (reflection and refraction at plane surfaces, composite media, waveguides and resonators).
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