Strain response analysis of adhesively bonded extended composite wind turbine blade suffering unsteady aerodynamic loads. (March 2018)

• Record Type: Journal Article
• Authors: Wu, Guangxing; Qin, Zhiwen; Zhang, Lei; Yang, Ke
• Is Part Of: Engineering failure analysis. Volume 85(2018)
• Page Start: 36
• Page End: 49
• Publication Date: 2018-03
• Subjects: Adhesively bonding technology -- Extended wind turbine blade -- Strain response -- Fatigue damage -- Unsteady aerodynamic loads; System failures (Engineering) -- Periodicals; Fracture mechanics -- Periodicals; Reliability (Engineering) -- Periodicals; Pannes -- Périodiques; Rupture, Mécanique de la -- Périodiques; Fiabilité -- Périodiques; Fracture mechanics; Reliability (Engineering); System failures (Engineering); Periodicals; Electronic journals; 620.112
• DOI: 10.1016/j.engfailanal.2017.12.009
• Languages: English
• ISSNs: 1350-6307

Abstract

Abstract: Extending blades of wind turbine in service is the most effective method for increasing energy production. Adhesively bonding technology increases less mass and has simpler operation process, which is more suitable for extending blades in service. But unsteady aerodynamic loads on the blades due to stochastic turbulent inflow may lead to fatigue damage and even failure. This paper presented a study on strain response and fatigue life of adhesively bonded extended composite wind turbine blade suffering unsteady aerodynamic loads. Firstly, a loading method that applies periodic distributed aerodynamic loads on the blade was proposed to accurately simulate the unsteady distributed loads on the real extended blades in service. Secondly, strain response behaviors to unsteady aerodynamic loads and strain distribution behaviors in the adhesively bonded area were revealed. Finally, fatigue damage was predicted with unsteady aerodynamic load spectrums, rainflow cycle-counting algorithm, Goodman diagram and Miner's linear superposition principle. Based on the findings obtained from this study, the feasibility of adhesively bonding technology for extending blade was affirmed and a few potential future directions of study were addressed to reduce the risk of adhesively bonded structures. Highlights: A new loading method that applies periodic distributed aerodynamic loads on the blade was proposed. Strain response behaviors to unsteady aerodynamic loads and strain distribution behaviors were studied. Fatigue damage on an adhesively bonded extended composite blade was predicted with unsteady aerodynamic load spectrums.