2020
DOI: 10.1177/0021998320908631
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Cure-induced residual stresses for warpage reduction in thermoset laminates

Abstract: The paper addresses the role played by the cure stage of a vacuum assisted resin transfer molding process in residual stresses generation. The Airstone 780E epoxy resin and Hardener 785H system broadly used in the wind turbine blade industry has been used in this study. The viscous–elastic properties of the resin have been characterized and implemented in a thermo-mechanical FE model. The model has been validated against manufactured [0/90]4 asymmetric laminates. Analysis of residual stresses generation highli… Show more

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Cited by 14 publications
(8 citation statements)
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“…There are still other extrinsic parameters that were studied for the plate warpage, although not for the angle deviation. For example, the heating rate, cure temperature, cure time, and cooling rate are some parameters [36][37][38]. the spring-back deformation under the one-stage cure cycle was about 5% lesser than that under the two-stage cure cycle for parabolic antenna reflectors.…”
Section: Parameter Effects From Experimentsmentioning
confidence: 99%
“…There are still other extrinsic parameters that were studied for the plate warpage, although not for the angle deviation. For example, the heating rate, cure temperature, cure time, and cooling rate are some parameters [36][37][38]. the spring-back deformation under the one-stage cure cycle was about 5% lesser than that under the two-stage cure cycle for parabolic antenna reflectors.…”
Section: Parameter Effects From Experimentsmentioning
confidence: 99%
“…As a result, the tensile properties declined with increasing postcuring time and temperature. 35,36 The presence of paper allowed homogenous flow of the resin, and the presence of randomly oriented cellulose fibers (paper) resulted in a notable improvement in tensile properties of the composite loaded in transverse direction (Figure 3d). Tensile properties of FREC-0, FREC-28, and FREC-68 postcured at 80 C for 16 h are summarized in Table 1.…”
Section: Tensile Propertiesmentioning
confidence: 99%
“…There have been many techniques to reduce the generated thermal residual stress within a composite, including heat treatment after the curing process [ 12 ]; regulating curing cycles [ 13 , 14 ]; addition of various types of nanoscale particles to reduce any mismatch in mechanical properties of the constituents [ 15 , 16 ]; physical and chemical modifications of the constituents [ 17 ]; exploiting partial relaxation of residual stresses due to viscoelasticity [ 18 ]; developing low temperature curing resins [ 19 ], as well as fibre prestressing techniques [ 20 , 21 ]. Among these, fibre prestressing was first developed in the 1960s, which is able to reduce or eliminate residual stresses from the manufacturing of composites, without changing their composition, increasing mass or product dimensions [ 22 ].…”
Section: Introductionmentioning
confidence: 99%