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 in | Polymers & polymer composites Vol. 16; no. 1; pp. 19 - 26 |
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Main Authors | , , , |
Format | Journal Article |
Language | English |
Published |
Shrewsbury
Rapra Technology
01.01.2008
Sage Publications Ltd. (UK) Sage Publications Ltd |
Subjects | |
Online Access | Get full text |
ISSN | 0967-3911 1478-2391 |
DOI | 10.1177/096739110801600103 |
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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. |
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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 |
Author_xml | – sequence: 1 givenname: Sohaib surname: Akbar fullname: Akbar, Sohaib organization: Université Claude Bernard-Lyon1, 43 Bd du 11 Novembre 1918,69622 Villeurbanne Cedex, France – sequence: 2 givenname: Chen Yan surname: Ding fullname: Ding, Chen Yan organization: Université Claude Bernard-Lyon1, 43 Bd du 11 Novembre 1918,69622 Villeurbanne Cedex, France – sequence: 3 givenname: Irfan surname: Yousaf fullname: Yousaf, Irfan organization: Institute of Space Technology, Islamabad highway, Islamabad, Pakistan – sequence: 4 givenname: Hayat M. surname: Khan fullname: Khan, Hayat M. organization: Université Paul Sabatier-Toulouse III, 118 route de Narbonne, Toulouse Cedex 9, France |
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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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References | (bibr12-096739110801600103) 1950 bibr1-096739110801600103 bibr26-096739110801600103 Li Min-Chung (bibr23-096739110801600103) 1992; 11 bibr7-096739110801600103 bibr10-096739110801600103 bibr11-096739110801600103 Hull D. (bibr17-096739110801600103) 1981 bibr5-096739110801600103 bibr4-096739110801600103 Ahn K. J. (bibr6-096739110801600103) 1992; 23 bibr9-096739110801600103 bibr8-096739110801600103 Maji A. K. (bibr14-096739110801600103) 1999; 31 bibr16-096739110801600103 bibr19-096739110801600103 bibr13-096739110801600103 Seferis J. C. (bibr2-096739110801600103) 1989 bibr18-096739110801600103 bibr15-096739110801600103 Hoisington M. A. (bibr3-096739110801600103) 1992 bibr22-096739110801600103 bibr25-096739110801600103 bibr24-096739110801600103 bibr20-096739110801600103 bibr21-096739110801600103 |
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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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