E-Glass/Phenolic Prepreg Processing by Solvent Impregnation

The increased interest in polymer matrix composites is partly due to their vast application in aeronautical and aerospace engineering. The preparation of prepreg is frequently the first move in the manufacture of parts. Although industry has developed reliable and successful processes yet there is a...

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Published inPolymers & polymer composites Vol. 16; no. 1; pp. 19 - 26
Main Authors Akbar, Sohaib, Ding, Chen Yan, Yousaf, Irfan, Khan, Hayat M.
Format Journal Article
LanguageEnglish
Published Shrewsbury Rapra Technology 01.01.2008
Sage Publications Ltd. (UK)
Sage Publications Ltd
Subjects
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ISSN0967-3911
1478-2391
DOI10.1177/096739110801600103

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Abstract The increased interest in polymer matrix composites is partly due to their vast application in aeronautical and aerospace engineering. The preparation of prepreg is frequently the first move in the manufacture of parts. Although industry has developed reliable and successful processes yet there is a need for further scientific investigation because most existing methods have been devised from practices based on trial and error. This paper reports a new approach to the design and operational features of prepregging machines. Our understanding of the subject is then utilized for the production of E-glass/phenolic prepregs. Characterization of manufactured prepregs by resin content, solvent contents, extent of impregnation and tack and drape properties permits comparison of different operational cycles and design parameters. The results have confirmed the success of our approach of successive decreases in the pressure of the squeezing roller in the soaking zone and successive increases in the chamber temperatures in the drying zone. This idea can be utilized in standard engineering operations to describe the operation protocol for the equipment and to give criteria for setting up the impregnation process, along with the design conditions for prepreg manufacturing.
AbstractList The increased interest in polymer matrix composites is partly due to their vast application in aeronautical and aerospace engineering. The preparation of prepreg is frequently the first move in the manufacture of parts. Although industry has developed reliable and successful processes yet there is a need for further scientific investigation because most existing methods have been devised from practices based on trial and error. This paper reports a new approach to the design and operational features of prepregging machines. Our understanding of the subject is then utilized for the production of E-glass/phenolic prepregs. Characterization of manufactured prepregs by resin content, solvent contents, extent of impregnation and tack and drape properties permits comparison of different operational cycles and design parameters. The results have confirmed the success of our approach of successive decreases in the pressure of the squeezing roller in the soaking zone and successive increases in the chamber temperatures in the drying zone. This idea can be utilized in standard engineering operations to describe the operation protocol for the equipment and to give criteria for setting up the impregnation process, along with the design conditions for prepreg manufacturing.
The increased interest in polymer matrix composites is partly due to their vast application in aeronautical and aerospace engineering. The preparation of prepreg is frequently the first move in the manufacture of parts. Although industry has developed reliable and successful processes yet there is a need for further scientific investigation because most existing methods have been devised from practices based on trial and error. This paper reports a new approach to the design and operational features of prepregging machines. Our understanding of the subject is then utilized for the production of E-glass/phenolic prepregs. Characterization of manufactured prepregs by resin content, solvent contents, extent of impregnation and tack and drape properties permits comparison of different operational cycles and design parameters. The results have confirmed the success of our approach of successive decreases in the pressure of the squeezing roller in the soaking zone and successive increases in the chamber temperatures in the drying zone. This idea can be utilized in standard engineering operations to describe the operation protocol for the equipment and to give criteria for setting up the impregnation process, along with the design conditions for prepreg manufacturing. [PUBLICATION ABSTRACT]
Audience Academic
Author Yousaf, Irfan
Khan, Hayat M.
Akbar, Sohaib
Ding, Chen Yan
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Cites_doi 10.1088/0954-0083/9/4/007
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10.1016/S0142-9418(99)00032-X
10.1016/S1359-835X(97)00115-2
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Issue 1
Keywords Laminate
Fiber reinforced material
Experimental study
Mineral fiber
Property processing relationship
Phenolic resin
Composite material
Optimization
Impregnation
Tack
Experimental design
Surface properties
Prepreg
Manufacturing
Glass fiber
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SubjectTerms Aerospace materials
Applied sciences
Composition
Exact sciences and technology
Forms of application and semi-finished materials
Glass fibers
Laminates
Manufacturing
Materials
Materials science
Methods
Phenols
Polymer industry, paints, wood
Polymer matrix composites
Processes
Production processes
Solvents
Technology of polymers
Textile fibers, Synthetic
Title E-Glass/Phenolic Prepreg Processing by Solvent Impregnation
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