Air evacuation and resin impregnation in semi-pregs: effects of feature dimensions

Prepregs with discontinuous resin (semi-pregs) impart robustness to vacuum-bag-only processing of composites. Limited guidance exists for evaluating advantageous resin patterns (i.e. dry space dimensions required to achieve both efficient air evacuation and full resin infiltration during cure). A fl...

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Main Authors: Sarah G. K. Schechter, Lessa K. Grunenfelder, Steven R. Nutt
Format: Article
Language:English
Published: Taylor & Francis Group 2020-04-01
Series:Advanced Manufacturing: Polymer & Composites Science
Subjects:
Online Access:http://dx.doi.org/10.1080/20550340.2020.1768348
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spelling doaj-eaa183bae6b946328aeefb0ae221e0082020-11-25T03:41:19ZengTaylor & Francis GroupAdvanced Manufacturing: Polymer & Composites Science2055-03592020-04-016210111410.1080/20550340.2020.17683481768348Air evacuation and resin impregnation in semi-pregs: effects of feature dimensionsSarah G. K. Schechter0Lessa K. Grunenfelder1Steven R. Nutt2University of Southern CaliforniaUniversity of Southern CaliforniaUniversity of Southern CaliforniaPrepregs with discontinuous resin (semi-pregs) impart robustness to vacuum-bag-only processing of composites. Limited guidance exists for evaluating advantageous resin patterns (i.e. dry space dimensions required to achieve both efficient air evacuation and full resin infiltration during cure). A flow front model was developed based on resin cure kinetics and rheological behavior, and then determined maximum dry space dimensions for semi-pregs under a range of realistic manufacturing conditions. Model predictions were validated in situ. Under controlled laboratory cure conditions, small surface openings (≤3.7 mm) resulted in full resin infiltration. Under adverse conditions (resin with accrued out-time), the maximum opening size dropped 40% (to ≤2.2 mm). Using a mathematical model, air evacuation time was calculated for various feature sizes using permeability measurements. Model predictions were tested and verified via fabrication of laminates. This methodology can be applied to other resin systems to guide vacuum-bag-only prepreg design and support robust production of composites.http://dx.doi.org/10.1080/20550340.2020.1768348prepregpolymer matrix compositesporositydefectscarbon fiberepoxyout of autoclave processingvacuum bag only
collection DOAJ
language English
format Article
sources DOAJ
author Sarah G. K. Schechter
Lessa K. Grunenfelder
Steven R. Nutt
spellingShingle Sarah G. K. Schechter
Lessa K. Grunenfelder
Steven R. Nutt
Air evacuation and resin impregnation in semi-pregs: effects of feature dimensions
Advanced Manufacturing: Polymer & Composites Science
prepreg
polymer matrix composites
porosity
defects
carbon fiber
epoxy
out of autoclave processing
vacuum bag only
author_facet Sarah G. K. Schechter
Lessa K. Grunenfelder
Steven R. Nutt
author_sort Sarah G. K. Schechter
title Air evacuation and resin impregnation in semi-pregs: effects of feature dimensions
title_short Air evacuation and resin impregnation in semi-pregs: effects of feature dimensions
title_full Air evacuation and resin impregnation in semi-pregs: effects of feature dimensions
title_fullStr Air evacuation and resin impregnation in semi-pregs: effects of feature dimensions
title_full_unstemmed Air evacuation and resin impregnation in semi-pregs: effects of feature dimensions
title_sort air evacuation and resin impregnation in semi-pregs: effects of feature dimensions
publisher Taylor & Francis Group
series Advanced Manufacturing: Polymer & Composites Science
issn 2055-0359
publishDate 2020-04-01
description Prepregs with discontinuous resin (semi-pregs) impart robustness to vacuum-bag-only processing of composites. Limited guidance exists for evaluating advantageous resin patterns (i.e. dry space dimensions required to achieve both efficient air evacuation and full resin infiltration during cure). A flow front model was developed based on resin cure kinetics and rheological behavior, and then determined maximum dry space dimensions for semi-pregs under a range of realistic manufacturing conditions. Model predictions were validated in situ. Under controlled laboratory cure conditions, small surface openings (≤3.7 mm) resulted in full resin infiltration. Under adverse conditions (resin with accrued out-time), the maximum opening size dropped 40% (to ≤2.2 mm). Using a mathematical model, air evacuation time was calculated for various feature sizes using permeability measurements. Model predictions were tested and verified via fabrication of laminates. This methodology can be applied to other resin systems to guide vacuum-bag-only prepreg design and support robust production of composites.
topic prepreg
polymer matrix composites
porosity
defects
carbon fiber
epoxy
out of autoclave processing
vacuum bag only
url http://dx.doi.org/10.1080/20550340.2020.1768348
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