Time-Lapse Helical X-ray Computed Tomography (CT) Study of Tensile Fatigue Damage Formation in Composites for Wind Turbine Blades

Understanding the fatigue damage mechanisms in composite materials is of great importance in the wind turbine industry because of the very large number of loading cycles rotor blades undergo during their service life. In this paper, the fatigue damage mechanisms of a non-crimp unidirectional (UD) gl...

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Main Authors: Ying Wang, Lars P. Mikkelsen, Grzegorz Pyka, Philip J. Withers
Format: Article
Language:English
Published: MDPI AG 2018-11-01
Series:Materials
Subjects:
Online Access:https://www.mdpi.com/1996-1944/11/11/2340
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spelling doaj-24c3d0c99f7a44fda9c26a289fd293c62020-11-24T21:41:36ZengMDPI AGMaterials1996-19442018-11-011111234010.3390/ma11112340ma11112340Time-Lapse Helical X-ray Computed Tomography (CT) Study of Tensile Fatigue Damage Formation in Composites for Wind Turbine BladesYing Wang0Lars P. Mikkelsen1Grzegorz Pyka2Philip J. Withers3Henry Moseley X-ray Imaging Facility, Henry Royce Institute for Advanced Materials, School of Materials, University of Manchester, M13 9PL Manchester, UKComposite Mechanics and Structures, Department of Wind Energy, Technical University of Denmark, DK-4000 Roskilde, DenmarkThermo Fisher Scientific Czech Republic, 67200 Brno, Czech RepublicHenry Moseley X-ray Imaging Facility, Henry Royce Institute for Advanced Materials, School of Materials, University of Manchester, M13 9PL Manchester, UKUnderstanding the fatigue damage mechanisms in composite materials is of great importance in the wind turbine industry because of the very large number of loading cycles rotor blades undergo during their service life. In this paper, the fatigue damage mechanisms of a non-crimp unidirectional (UD) glass fibre reinforced polymer (GFRP) used in wind turbine blades are characterised by time-lapse ex-situ helical X-ray computed tomography (CT) at different stages through its fatigue life. Our observations validate the hypothesis that off-axis cracking in secondary oriented fibre bundles, the so-called backing bundles, are directly related to fibre fractures in the UD bundles. Using helical X-ray CT we are able to follow the fatigue damage evolution in the composite over a length of 20 mm in the UD fibre direction using a voxel size of (2.75 &#181;m)<sup>3</sup>. A staining approach was used to enhance the detectability of the narrow off-axis matrix and interface cracks, partly closed fibre fractures and thin longitudinal splits. Instead of being evenly distributed, fibre fractures in the UD bundles nucleate and propagate locally where backing bundles cross-over, or where stitching threads cross-over. In addition, UD fibre fractures can also be initiated by the presence of extensive debonding and longitudinal splitting, which were found to develop from debonding of the stitching threads near surface. The splits lower the lateral constraint of the originally closely packed UD fibres, which could potentially make the composite susceptible to compressive loads as well as the environment in service. The results here indicate that further research into the better design of the positioning of stitching threads, and backing fibre cross-over regions is required, as well as new approaches to control the positions of UD fibres.https://www.mdpi.com/1996-1944/11/11/2340helical CTcontrast agenthigh cycle fatigue (HCF)fibre breakfibre tows
collection DOAJ
language English
format Article
sources DOAJ
author Ying Wang
Lars P. Mikkelsen
Grzegorz Pyka
Philip J. Withers
spellingShingle Ying Wang
Lars P. Mikkelsen
Grzegorz Pyka
Philip J. Withers
Time-Lapse Helical X-ray Computed Tomography (CT) Study of Tensile Fatigue Damage Formation in Composites for Wind Turbine Blades
Materials
helical CT
contrast agent
high cycle fatigue (HCF)
fibre break
fibre tows
author_facet Ying Wang
Lars P. Mikkelsen
Grzegorz Pyka
Philip J. Withers
author_sort Ying Wang
title Time-Lapse Helical X-ray Computed Tomography (CT) Study of Tensile Fatigue Damage Formation in Composites for Wind Turbine Blades
title_short Time-Lapse Helical X-ray Computed Tomography (CT) Study of Tensile Fatigue Damage Formation in Composites for Wind Turbine Blades
title_full Time-Lapse Helical X-ray Computed Tomography (CT) Study of Tensile Fatigue Damage Formation in Composites for Wind Turbine Blades
title_fullStr Time-Lapse Helical X-ray Computed Tomography (CT) Study of Tensile Fatigue Damage Formation in Composites for Wind Turbine Blades
title_full_unstemmed Time-Lapse Helical X-ray Computed Tomography (CT) Study of Tensile Fatigue Damage Formation in Composites for Wind Turbine Blades
title_sort time-lapse helical x-ray computed tomography (ct) study of tensile fatigue damage formation in composites for wind turbine blades
publisher MDPI AG
series Materials
issn 1996-1944
publishDate 2018-11-01
description Understanding the fatigue damage mechanisms in composite materials is of great importance in the wind turbine industry because of the very large number of loading cycles rotor blades undergo during their service life. In this paper, the fatigue damage mechanisms of a non-crimp unidirectional (UD) glass fibre reinforced polymer (GFRP) used in wind turbine blades are characterised by time-lapse ex-situ helical X-ray computed tomography (CT) at different stages through its fatigue life. Our observations validate the hypothesis that off-axis cracking in secondary oriented fibre bundles, the so-called backing bundles, are directly related to fibre fractures in the UD bundles. Using helical X-ray CT we are able to follow the fatigue damage evolution in the composite over a length of 20 mm in the UD fibre direction using a voxel size of (2.75 &#181;m)<sup>3</sup>. A staining approach was used to enhance the detectability of the narrow off-axis matrix and interface cracks, partly closed fibre fractures and thin longitudinal splits. Instead of being evenly distributed, fibre fractures in the UD bundles nucleate and propagate locally where backing bundles cross-over, or where stitching threads cross-over. In addition, UD fibre fractures can also be initiated by the presence of extensive debonding and longitudinal splitting, which were found to develop from debonding of the stitching threads near surface. The splits lower the lateral constraint of the originally closely packed UD fibres, which could potentially make the composite susceptible to compressive loads as well as the environment in service. The results here indicate that further research into the better design of the positioning of stitching threads, and backing fibre cross-over regions is required, as well as new approaches to control the positions of UD fibres.
topic helical CT
contrast agent
high cycle fatigue (HCF)
fibre break
fibre tows
url https://www.mdpi.com/1996-1944/11/11/2340
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