The Continuous Monitoring of the Health of Composite Structure

Currently nondestructive testing techniques for composite aircraft structures are disadvantaged when compared to instant structural health monitoring (SHM) systems that monitor the structure while being in-service and give real-time data. This paper reports on the use of Polyvinylidene Fluoride (PVD...

Full description

Saved in:
Bibliographic Details
Main Authors: T. P. Masango, O. Philander, V. Msomi
Format: Article
Language:English
Published: Wiley 2018-01-01
Series:Journal of Engineering
Online Access:http://dx.doi.org/10.1155/2018/8260298
Tags: Add Tag
No Tags, Be the first to tag this record!
_version_ 1832548444966748160
author T. P. Masango
O. Philander
V. Msomi
author_facet T. P. Masango
O. Philander
V. Msomi
author_sort T. P. Masango
collection DOAJ
description Currently nondestructive testing techniques for composite aircraft structures are disadvantaged when compared to instant structural health monitoring (SHM) systems that monitor the structure while being in-service and give real-time data. This paper reports on the use of Polyvinylidene Fluoride (PVDF) sensors in sensing (or monitoring) and locating the defect of a flexible composite structure. The samples used for the tests were manufactured through the use of vacuum infusion process. The three-point bending test was performed to determine the material properties. The vertical sample deflection was measured through the use of vertical height Vernier. It should be noted that the samples were analyzed as cantilever beam due to limited availability of test equipment. The sample health was monitored through the use of PVDF sensor. The sensor data was logged and recorded through the use of Fluke-View scopemeter. The 50 g mass pieces were used as a mode of subjecting the structure to the vertical load. The experiment was performed on samples with defects (drilled 3 mm hole) sample and no-defected sample. The deflection and output voltage from the PVDF sensor of all the samples were comparatively studied.
format Article
id doaj-art-00df3a4b29e94abdbbb81e5514db71f9
institution Kabale University
issn 2314-4904
2314-4912
language English
publishDate 2018-01-01
publisher Wiley
record_format Article
series Journal of Engineering
spelling doaj-art-00df3a4b29e94abdbbb81e5514db71f92025-02-03T06:13:55ZengWileyJournal of Engineering2314-49042314-49122018-01-01201810.1155/2018/82602988260298The Continuous Monitoring of the Health of Composite StructureT. P. Masango0O. Philander1V. Msomi2Faculty of Engineering, Department of Mechanical Engineering, Cape Peninsula University of Technology, P.O. Box 1906, Bellville 7535, South AfricaFaculty of Engineering, Department of Mechanical Engineering, Cape Peninsula University of Technology, P.O. Box 1906, Bellville 7535, South AfricaFaculty of Engineering, Department of Mechanical Engineering, Cape Peninsula University of Technology, P.O. Box 1906, Bellville 7535, South AfricaCurrently nondestructive testing techniques for composite aircraft structures are disadvantaged when compared to instant structural health monitoring (SHM) systems that monitor the structure while being in-service and give real-time data. This paper reports on the use of Polyvinylidene Fluoride (PVDF) sensors in sensing (or monitoring) and locating the defect of a flexible composite structure. The samples used for the tests were manufactured through the use of vacuum infusion process. The three-point bending test was performed to determine the material properties. The vertical sample deflection was measured through the use of vertical height Vernier. It should be noted that the samples were analyzed as cantilever beam due to limited availability of test equipment. The sample health was monitored through the use of PVDF sensor. The sensor data was logged and recorded through the use of Fluke-View scopemeter. The 50 g mass pieces were used as a mode of subjecting the structure to the vertical load. The experiment was performed on samples with defects (drilled 3 mm hole) sample and no-defected sample. The deflection and output voltage from the PVDF sensor of all the samples were comparatively studied.http://dx.doi.org/10.1155/2018/8260298
spellingShingle T. P. Masango
O. Philander
V. Msomi
The Continuous Monitoring of the Health of Composite Structure
Journal of Engineering
title The Continuous Monitoring of the Health of Composite Structure
title_full The Continuous Monitoring of the Health of Composite Structure
title_fullStr The Continuous Monitoring of the Health of Composite Structure
title_full_unstemmed The Continuous Monitoring of the Health of Composite Structure
title_short The Continuous Monitoring of the Health of Composite Structure
title_sort continuous monitoring of the health of composite structure
url http://dx.doi.org/10.1155/2018/8260298
work_keys_str_mv AT tpmasango thecontinuousmonitoringofthehealthofcompositestructure
AT ophilander thecontinuousmonitoringofthehealthofcompositestructure
AT vmsomi thecontinuousmonitoringofthehealthofcompositestructure
AT tpmasango continuousmonitoringofthehealthofcompositestructure
AT ophilander continuousmonitoringofthehealthofcompositestructure
AT vmsomi continuousmonitoringofthehealthofcompositestructure