Damping mechanism model for fatigue testing of a full-scale composite wind turbine blade, Part 1: Modeling

2018 ◽  
Vol 202 ◽  
pp. 1216-1228 ◽  
Author(s):  
Hak Gu Lee ◽  
Jungwan Lee
Keyword(s):  
Wind Turbine ◽  
Turbine Blade ◽  
Fatigue Testing ◽  
Full Scale ◽  
Wind Turbine Blade ◽  
Mechanism Model

scholarly journals Full-Scale Fatigue Testing of a Wind Turbine Blade in Flapwise Direction and Examining the Effect of Crack Propagation on the Blade Performance

Materials ◽  
2017 ◽  
Vol 10 (10) ◽  
pp. 1152 ◽  
Author(s):  
Othman Al-Khudairi ◽  
Homayoun Hadavinia ◽  
Christian Little ◽  
Gavin Gillmore ◽  
Peter Greaves ◽  
...  
Keyword(s):  
Crack Propagation ◽  
Wind Turbine ◽  
Turbine Blade ◽  
Fatigue Testing ◽  
Full Scale ◽  
Wind Turbine Blade

Finite Element Modeling of a Dual Axis Resonant Test System for Wind Turbine Blades

2009 ◽  
Author(s):  
Michael Desmond ◽  
Darris White ◽  
William Barott
Keyword(s):  
Wind Turbine ◽  
Turbine Blade ◽  
Fatigue Testing ◽  
Turbine Blades ◽  
Test System ◽  
Full Scale ◽  
Wind Turbine Blade ◽  
Test Method ◽  
Wind Turbine Blades ◽  
Design Assessment

Structural testing of wind turbine blades is required for designing reliable, structurally efficient blades. Full-scale blade fatigue testing conducted at the National Renewable Energy Laboratory’s (NREL) National Wind Technology Center (NWTC) provides blade manufacturers quantitative information on design details including design assessment, manufacturing quality, and design durability. Blade tests can be conducted as a single axis test (flapwise or lead-lag) or a dual-axis test (flapwise and lead-lag simultaneously). Dual-axis testing is generally the preferred full-scale test method as it simulates to a greater extent the characteristic loading the blade is subjected to in the field. Historically, wind turbine blade fatigue testing has been performed through forced displacement methods using hydraulic systems which directly apply load to the blade. More efficient methods of fatigue testing are being developed at the NWTC that employ resonant excitation systems to reduce hydraulic supply requirements, increase the test speed, and improve distributed load matching. In the case of a dual-axis resonant test, the blade is excited through multiple actuators at two distinct frequencies corresponding to the flapwise and lead-lag frequencies. A primary objective of a dual-axis test is to test the blade to equivalent damage moments in multiple axes. A code was developed to simulate the performance of the dual-axis resonant test system, comparing the predictions to actual test results. Modeling of this test system was performed using a MATLAB script that integrates the NREL FAST code with a commercial dynamic simulator package ADAMS. This code has the advantage over existing methods to more accurately simulate the coupled response between the flapwise and lead-lag directions. In summary, this paper will provide information on the modeling of wind turbine blade dual-axis resonant test systems.

A method of determining test load for full-scale wind turbine blade fatigue tests

2018 ◽  
Vol 32 (11) ◽  
pp. 5097-5104 ◽  
Author(s):  
Qiang Ma ◽  
Zong-Wen An ◽  
Jian-Xiong Gao ◽  
Hai-Xia Kou ◽  
Xue-Zong Bai
Keyword(s):  
Wind Turbine ◽  
Turbine Blade ◽  
Fatigue Tests ◽  
Full Scale ◽  
Wind Turbine Blade ◽  
Test Load

Fatigue Failure of a Composite Wind Turbine Blade at the Trailing Edge

2018 ◽  
Vol 382 ◽  
pp. 191-195 ◽  
Author(s):  
Zu Jin Pan ◽  
Jian Zhong Wu ◽  
Jian Liu ◽  
Xin Hua Zhao
Keyword(s):  
Wind Turbine ◽  
Turbine Blade ◽  
Failure Modes ◽  
Fatigue Testing ◽  
Turbine Blades ◽  
Local Stress ◽  
Wind Turbine Blade ◽  
Trailing Edge ◽  
Balsa Wood ◽  
Abnormal Sound

The downtime problem of wind turbine increases due to fatigue damage of wind turbine blades, which is even more crucial in the larger blades. One of the critical failure modes is the blade trailing edge failure, which can result in the trailing edge joint cracked. In this paper, we experienced that abnormal sound was happened in the trailing edge at the cross-section in the max chord during fatigue testing of a 2 MW full-scale wind turbine blade according to IEC61400-23. Through the conditional monitoring of the trailing edge, the delamination between GFRP and balsa wood is caused by stress concentration. The abnormal sound is happened due to GFRP beat the balsa wood when the blade vibrates in the edgewise direction. Moreover, the sound is amplified because the introduction of air due to the delamination. The local stress distribution and stability factors are computed through FEM methods, the program that increasing the core materials in the trailing edge is proposed. Therefore the structure reliability in the trailing edge is improved.

scholarly journals Virtual full-scale testing for investigating strength characteristics of a composite wind turbine blade

2020 ◽  
Author(s):  
Can Muyan ◽  
Demirkan Coker
Keyword(s):  
Wind Turbine ◽  
Turbine Blade ◽  
Mechanical Response ◽  
Leading Edge ◽  
Full Scale ◽  
Wind Turbine Blade ◽  
Combined Loading ◽  
Strength Analysis ◽  
Damage Development ◽  
Extreme Load

Abstract. Full-scale structural tests enable us to monitor mechanical response of the blades under various loading scenarios. Yet these tests must be accompanied with numerical simulations, so that the physical basis of the progressive damage development can be captured and interpreted correctly. Within the scope of this paper the previous work of the authors concerning the strength analysis of an existing 5-m GFRP wind turbine blade using Puck failure criteria is revisited. An important outcome of the previous study was that nonlinear Puck material model was found to be necessary for a more realistic simulation of failure mechanisms. In the current work, under extreme load cases internal flange at the leading edge, trailing edge of the blade are identified as the mainly damaged regions. Moreover, dominant failure mechanism is expected to be the de-bonding at the trailing and leading edges. When extreme load case is applied as a combination of edge-wise and flap-wise loading cases, less damage is observed compared to the pure flap-wise loading case. This damage evolution is attributed to the stiffer structural behavior of the blade under combined loading condition.

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