2014
DOI: 10.1177/0021998314531031
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Mechanical evaluation of repair resins for fiber-glass wind turbine blades

Abstract: This paper contains details of mechanical testing of double cantilever beam composite specimens comprising a vacuum-assisted resin transfer molding–infused parent plate and a hand laid-up upper plate simulating a typical blade repair. The testing was carried out as part of an effort to optimize a new repair resin for a wind turbine blade manufacturing company. A number of commercial suppliers were contacted and nine resins with different formulations were selected for screening. Out of these, six were shortlis… Show more

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Cited by 3 publications
(3 citation statements)
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“…In aeroelastic vibration analysis, blades can be simplified or equivalent to beam models, including the cantilever beam 24 and the thin-wall beam, 25 since they have similar mechanical action frame and main structure. In this section, based on the structural characteristics of the blade, we develop the equivalent model to obtain the frequency characteristics of the main body of the blade, instead of the previous method of directly giving the natural frequency value.…”
Section: Solution Of Blade Natural Frequencies Based On Green's Function Methodsmentioning
confidence: 99%
See 1 more Smart Citation
“…In aeroelastic vibration analysis, blades can be simplified or equivalent to beam models, including the cantilever beam 24 and the thin-wall beam, 25 since they have similar mechanical action frame and main structure. In this section, based on the structural characteristics of the blade, we develop the equivalent model to obtain the frequency characteristics of the main body of the blade, instead of the previous method of directly giving the natural frequency value.…”
Section: Solution Of Blade Natural Frequencies Based On Green's Function Methodsmentioning
confidence: 99%
“…To analyze the thin-walled rotor blade better, frequency terms are added in the solution of the above motion equation. Add frequency term, x 2 mz to the motion equation of flap direction, and add frequency term x 2 K 2 m mu in torsion direction, which can be calculated by equations (24) to (26).…”
Section: Eimentioning
confidence: 99%
“…As the service year increases, the hidden defects gradually show up [2,3]. Being affected by environmental corrosion, manufacturing defects, insufficient design, aging of materials, and overload [4,5], the hidden defects eventually appear as different failure modes [6] (such as fiber fracture, matrix failure, delamination, etc.) and damage types [7] (such as adhesive joint failure between skins, sandwich panel face/core debonding, gelcoat cracks, etc.).…”
Section: Introductionmentioning
confidence: 99%