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Structural Analysis of Composite Wind Blade Using Finite Element Technique

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초록

This study evaluates the structural safety of wind turbine blades, analyzes the behavior of composite laminate structures with and without defects, and assesses surface erosion wear. The NREL 5 MW standard is applied to assign accurate composite material properties to each blade section. Modeling and analysis of the wind turbine blades reveal stable behavior under individual load conditions (gravity, motor speed, wind speed), with the web bearing most of the load. Surface erosion wear analysis in which microparticle impacts are simulated on the blade coating shows a maximum stress and maximum displacement of 14 MPa and 0.02 mm, respectively, indicating good initial durability, but suggest potential long-term performance issues due to cumulative effects. The study examines defect effects on composite laminate structures to compare the stress distribution, strain, and stiffness characteristics between normal and cracked states. Although normal conditions exhibit stable behavior, crack defects lead to fiber breakage, high-stress concentration in the vulnerable resin layer, and decreased rigidity. This demonstrates that local defects can compromise the safety of the entire structure. The study utilizes finite element analysis to simulate various load scenarios and defect conditions. Results show that even minor defects can significantly alter stress distributions and potentially lead to catastrophic failure if left unaddressed. These findings provide valuable insights for wind turbine blade safety evaluations, surface protection strategies, and composite structure health management. The methodology and results can inform the design improvements, maintenance strategies, and defect detection techniques of the wind energy industry.

Abstract

This study evaluates the structural safety of wind turbine blades, analyzes the behavior of composite laminate structures with and without defects, and assesses surface erosion wear. The NREL 5 MW standard is applied to assign accurate composite material properties to each blade section. Modeling and analysis of the wind turbine blades reveal stable behavior under individual load conditions (gravity, motor speed, wind speed), with the web bearing most of the load. Surface erosion wear analysis in which microparticle impacts are simulated on the blade coating shows a maximum stress and maximum displacement of 14 MPa and 0.02 mm, respectively, indicating good initial durability, but suggest potential long-term performance issues due to cumulative effects. The study examines defect effects on composite laminate structures to compare the stress distribution, strain, and stiffness characteristics between normal and cracked states. Although normal conditions exhibit stable behavior, crack defects lead to fiber breakage, high-stress concentration in the vulnerable resin layer, and decreased rigidity. This demonstrates that local defects can compromise the safety of the entire structure. The study utilizes finite element analysis to simulate various load scenarios and defect conditions. Results show that even minor defects can significantly alter stress distributions and potentially lead to catastrophic failure if left unaddressed. These findings provide valuable insights for wind turbine blade safety evaluations, surface protection strategies, and composite structure health management. The methodology and results can inform the design improvements, maintenance strategies, and defect detection techniques of the wind energy industry.

참고문헌 (8)

  1. Griffith, D. T., "Technology Trends 2012", Presented at the 5th Sandia Wind Turbine Blade Workshop (2012)
  2. Jensen, F. M., "Investigating the impact of non-linear geometrical effects on Wind Turbine Blades—Part 1 : Current status of design and test methods and future challenges in design optimization", Wind Energy, 14, pp.239~254 (2011)
  3. Jensen, F. M., "Change in Failure Type when Wind Turbine Blades Scale-Up", Presented at the 5th Sandia Wind Turbine Blades Workshop (2012)
  4. Moon, S., "Analysis of Tilting Pad Journal Bearing Characteristics and Rotordynamics for Centrifugal Compressors Using Multiphysics Software", Tribol. Lubr, 39(6), pp.268~272 (2023)[DOI]
  5. Mamalis, D., "Effect of fibre straightness and sizing in carbon fibre reinforced powder epoxy composites", Compos A Appl Sci Manuf, 110, pp.93~105 (2018)
  6. Wang, Y., "Modeling ablation of laminated composites : a novel manual mesh moving finite element analysis procedure with ABAQUS", International Journal of Heat and Mass Transfer, 116, pp.306~313 (2018)
  7. Seo, D., "Dynamic Analysis of Tie-rod-fastened Rotor Considering Elastoplastic Deformation", Tribol. Lubr, 40(1), pp.8~16 (2024)[DOI]
  8. Mehdikhani, M., "Voids in fiber-reinforced polymer composites : A review on their formation, characteristics, and effects on mechanical performance", J Compos Mater, 53, pp.1579~1669 (2019)

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