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    Post-Curing Effects on Marine VARTM FRP Composite Material Properties for Test and Implementation

    Source: Journal of Engineering Materials and Technology:;2006:;volume( 128 ):;issue: 001::page 34
    Author:
    Jason J. Cain
    ,
    Yin-Nian Lin
    ,
    Paul E. Hess
    ,
    Judy S. Riffle
    ,
    Nathan L. Post
    ,
    John J. Lesko
    ,
    Scott W. Case
    DOI: 10.1115/1.2128425
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Structural composites are increasingly being utilized in many large naval and civil structures where it is vital that their long-term performance be predictable and their variability definable over the life of the structure. However, these properties may be influenced by the degree of cure of the resin, particularly for room-temperature-cured systems. Thus, this investigation defines the postcure effects on E-glass/vinyl-ester fiber-reinforced polymer (FRP) composites manufactured using the vacuum-assisted resin transfer molding (VARTM) method, which are typical of those used by the US Navy for ship structures. The composites are differentiated by varying levels of postcure temperature and duration, and examined for the effects of advancing cure at various points in the time after postcure. Pseudo-quasi-isotropic [0/+45/90/−45/0]s and angle ply laminate [±45]2s samples from each level of postcure are examined at 1, 10, 30, 100, and 300 days after postcure in order to track strength, stiffness, failure strain, creep, and fatigue performance as functions of time. In parallel, the matrix polymer is inspected using FTIR (Fourier transform infrared spectroscopy) to directly assess the degree of conversion. Dynamic mechanical analysis and shrinkage measurements are also undertaken to assess the Tg and the amount of shrinkage undergone during post-curing, as well as the advancing of the level of cure during the prescribed aging time. Results suggest that the degree of conversion is limited to 80% for the vinyl-ester oligomer and 90–95% for styrene following a postcure of 93°C. It is observed that after 300 days of ambient storage the nonpostcured samples approach the degree of conversion exhibited by those postcured at 93°C, as measured by FTIR. Resin dominated quasi-static properties are greatly affected by the degree of cure, whereas fiber dominated properties are not. Where the degree of cure is comparatively low, viscoelastic properties cause greater changes in creep response as well as influencing fatigue performance.
    keyword(s): Fatigue , Temperature , Composite materials , Laminates , Fourier transform infrared spectroscopy , Curing , Ester , Fiber reinforced plastics , Resins , Storage , Measurement , Testing , Glass , Creep AND Stiffness ,
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      Post-Curing Effects on Marine VARTM FRP Composite Material Properties for Test and Implementation

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    http://yetl.yabesh.ir/yetl1/handle/yetl/133816
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    • Journal of Engineering Materials and Technology

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    contributor authorJason J. Cain
    contributor authorYin-Nian Lin
    contributor authorPaul E. Hess
    contributor authorJudy S. Riffle
    contributor authorNathan L. Post
    contributor authorJohn J. Lesko
    contributor authorScott W. Case
    date accessioned2017-05-09T00:20:06Z
    date available2017-05-09T00:20:06Z
    date copyrightJanuary, 2006
    date issued2006
    identifier issn0094-4289
    identifier otherJEMTA8-27078#34_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/133816
    description abstractStructural composites are increasingly being utilized in many large naval and civil structures where it is vital that their long-term performance be predictable and their variability definable over the life of the structure. However, these properties may be influenced by the degree of cure of the resin, particularly for room-temperature-cured systems. Thus, this investigation defines the postcure effects on E-glass/vinyl-ester fiber-reinforced polymer (FRP) composites manufactured using the vacuum-assisted resin transfer molding (VARTM) method, which are typical of those used by the US Navy for ship structures. The composites are differentiated by varying levels of postcure temperature and duration, and examined for the effects of advancing cure at various points in the time after postcure. Pseudo-quasi-isotropic [0/+45/90/−45/0]s and angle ply laminate [±45]2s samples from each level of postcure are examined at 1, 10, 30, 100, and 300 days after postcure in order to track strength, stiffness, failure strain, creep, and fatigue performance as functions of time. In parallel, the matrix polymer is inspected using FTIR (Fourier transform infrared spectroscopy) to directly assess the degree of conversion. Dynamic mechanical analysis and shrinkage measurements are also undertaken to assess the Tg and the amount of shrinkage undergone during post-curing, as well as the advancing of the level of cure during the prescribed aging time. Results suggest that the degree of conversion is limited to 80% for the vinyl-ester oligomer and 90–95% for styrene following a postcure of 93°C. It is observed that after 300 days of ambient storage the nonpostcured samples approach the degree of conversion exhibited by those postcured at 93°C, as measured by FTIR. Resin dominated quasi-static properties are greatly affected by the degree of cure, whereas fiber dominated properties are not. Where the degree of cure is comparatively low, viscoelastic properties cause greater changes in creep response as well as influencing fatigue performance.
    publisherThe American Society of Mechanical Engineers (ASME)
    titlePost-Curing Effects on Marine VARTM FRP Composite Material Properties for Test and Implementation
    typeJournal Paper
    journal volume128
    journal issue1
    journal titleJournal of Engineering Materials and Technology
    identifier doi10.1115/1.2128425
    journal fristpage34
    journal lastpage40
    identifier eissn1528-8889
    keywordsFatigue
    keywordsTemperature
    keywordsComposite materials
    keywordsLaminates
    keywordsFourier transform infrared spectroscopy
    keywordsCuring
    keywordsEster
    keywordsFiber reinforced plastics
    keywordsResins
    keywordsStorage
    keywordsMeasurement
    keywordsTesting
    keywordsGlass
    keywordsCreep AND Stiffness
    treeJournal of Engineering Materials and Technology:;2006:;volume( 128 ):;issue: 001
    contenttypeFulltext
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