Fatigue in Fiber-Metal Laminates for Small Wind Turbine Blades Application

A methodology to study the fatigue of a wind turbine blade in a 10KW small wind turbine is proposed in this paper. Two working conditions (namely normal fatigue operation condition and extreme wind condition) are considered based on IEC61400-2. The maximum load calculated from both cases were used a...

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Main Authors: Sai Wei, Chai Gin Boay
Format: Article
Language:English
Published: EDP Sciences 2018-01-01
Series:MATEC Web of Conferences
Online Access:https://doi.org/10.1051/matecconf/201816507005
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author Sai Wei
Chai Gin Boay
author_facet Sai Wei
Chai Gin Boay
author_sort Sai Wei
collection DOAJ
description A methodology to study the fatigue of a wind turbine blade in a 10KW small wind turbine is proposed in this paper. Two working conditions (namely normal fatigue operation condition and extreme wind condition) are considered based on IEC61400-2. The maximum load calculated from both cases were used as a reference to perform material sample fatigue study. Fiber-metal laminate – GLARE 3/2 with a centre 1mm notch on the external aluminium layers was modelled based on fracture mechanics approach to calculate the stress intensity factor and fatigue crack growth rate at maximum applied stress of 240Mpa. GLARE panel fabrication and tensile tests were included. The fatigue tests were performed on unnotched samples with stress range from 80Mpa to 300Mpa and plotted into S-N curve.
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spelling doaj.art-eef5cfcd3d934e85bdc5097f275ce3672022-12-21T21:33:43ZengEDP SciencesMATEC Web of Conferences2261-236X2018-01-011650700510.1051/matecconf/201816507005matecconf_fatigue2018_07005Fatigue in Fiber-Metal Laminates for Small Wind Turbine Blades ApplicationSai WeiChai Gin BoayA methodology to study the fatigue of a wind turbine blade in a 10KW small wind turbine is proposed in this paper. Two working conditions (namely normal fatigue operation condition and extreme wind condition) are considered based on IEC61400-2. The maximum load calculated from both cases were used as a reference to perform material sample fatigue study. Fiber-metal laminate – GLARE 3/2 with a centre 1mm notch on the external aluminium layers was modelled based on fracture mechanics approach to calculate the stress intensity factor and fatigue crack growth rate at maximum applied stress of 240Mpa. GLARE panel fabrication and tensile tests were included. The fatigue tests were performed on unnotched samples with stress range from 80Mpa to 300Mpa and plotted into S-N curve.https://doi.org/10.1051/matecconf/201816507005
spellingShingle Sai Wei
Chai Gin Boay
Fatigue in Fiber-Metal Laminates for Small Wind Turbine Blades Application
MATEC Web of Conferences
title Fatigue in Fiber-Metal Laminates for Small Wind Turbine Blades Application
title_full Fatigue in Fiber-Metal Laminates for Small Wind Turbine Blades Application
title_fullStr Fatigue in Fiber-Metal Laminates for Small Wind Turbine Blades Application
title_full_unstemmed Fatigue in Fiber-Metal Laminates for Small Wind Turbine Blades Application
title_short Fatigue in Fiber-Metal Laminates for Small Wind Turbine Blades Application
title_sort fatigue in fiber metal laminates for small wind turbine blades application
url https://doi.org/10.1051/matecconf/201816507005
work_keys_str_mv AT saiwei fatigueinfibermetallaminatesforsmallwindturbinebladesapplication
AT chaiginboay fatigueinfibermetallaminatesforsmallwindturbinebladesapplication