A process simulation model for the manufacture of composite laminates from fiber-reinforced, polyimide matrix prepreg materials

dc.contributor.authorLee, Chun-Shoen
dc.contributor.committeechairLoos, Alfred C.en
dc.contributor.committeememberCramer, Mark S.en
dc.contributor.committeememberDavis, Richey M.en
dc.contributor.committeememberGrant, John W.en
dc.contributor.committeememberKraige, Lutheren
dc.contributor.departmentEngineering Mechanicsen
dc.date.accessioned2014-03-14T21:23:02Zen
dc.date.adate2005-11-10en
dc.date.available2014-03-14T21:23:02Zen
dc.date.issued1993-03-15en
dc.date.rdate2005-11-10en
dc.date.sdate2005-11-10en
dc.description.abstractA numerical simulation model has been developed which describes the manufacture of composite laminates from fiber-reinforced polyimide (PMR-15) matrix prepreg materials. The simulation model is developed in two parts. The first part is the volatile formation model which simulates the production of volatiles and their transport through the composite microstructure during the imidization reaction. The volatile formation model can be used to predict the vapor pressure profile and volatile mass flux. The second part of the simulation model, the consolidation model, can be used to determine the degree of crosslinking, resin melt viscosity, temperature, and the resin pressure inside the composite during the consolidation process. Also, the model is used to predict the total resin flow, thickness change, and total process time. The simulation model was solved by a finite element analysis. Experiments were performed to obtain data for verification of the model. Composite laminates were fabricated from ICI Fiberite HMF2474/66C carbon fabric, PMR-15 prep reg and cured with different cure cycles. The results predicted by the model correlate well with experimental data for the weight loss, thickness, and fiber volume fraction changes of the composite. An optimum processing cycle for the fabrication of PMR-15 polyimide composites was developed by combining the model generated optimal imidization and consolidation cure cycles. The optimal cure cycle was used to manufacture PMR-15 composite laminates and the mechanical and physical properties of the laminates were measured. Results showed that fabrication of PMR-15 composite laminates with the optimal cure cycle results in improved mechanical properties and a significantly reduced the processing time compared with the manufacturer's suggested cure cycle.en
dc.description.degreePh. D.en
dc.format.extentxv, 205 leavesen
dc.format.mediumBTDen
dc.format.mimetypeapplication/pdfen
dc.identifier.otheretd-11102005-141103en
dc.identifier.sourceurlhttp://scholar.lib.vt.edu/theses/available/etd-11102005-141103/en
dc.identifier.urihttp://hdl.handle.net/10919/40298en
dc.language.isoenen
dc.publisherVirginia Techen
dc.relation.haspartLD5655.V856_1993.L44.pdfen
dc.relation.isformatofOCLC# 28013337en
dc.rightsIn Copyrighten
dc.rights.urihttp://rightsstatements.org/vocab/InC/1.0/en
dc.subject.lccLD5655.V856 1993.L44en
dc.subject.lcshFibrous composites -- Design and construction -- Mathematical modelsen
dc.subject.lcshLaminated materials -- Design and construction -- Mathematical modelsen
dc.titleA process simulation model for the manufacture of composite laminates from fiber-reinforced, polyimide matrix prepreg materialsen
dc.typeDissertationen
dc.type.dcmitypeTexten
thesis.degree.disciplineEngineering Mechanicsen
thesis.degree.grantorVirginia Polytechnic Institute and State Universityen
thesis.degree.leveldoctoralen
thesis.degree.namePh. D.en

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