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dc.contributor.advisorBrian L. Wardle.en_US
dc.contributor.authorDaso, Frederick O.(Frederick Odien)en_US
dc.contributor.otherMassachusetts Institute of Technology. Department of Aeronautics and Astronautics.en_US
dc.date.accessioned2019-10-04T21:32:51Z
dc.date.available2019-10-04T21:32:51Z
dc.date.copyright2019en_US
dc.date.issued2019en_US
dc.identifier.urihttps://hdl.handle.net/1721.1/122408
dc.descriptionThesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 2019en_US
dc.descriptionCataloged from PDF version of thesis.en_US
dc.descriptionIncludes bibliographical references (pages 138-149).en_US
dc.description.abstractAerospace manufacturers continue to rely on composite materials to make aerovehicles lighter and stronger, particularly employing carbon fiber reinforced plastics (CFRP) using carbon microfiber reinforcement with thermoset and thermoplastic polymer matrices. With the increasing use of such composites, the need for energy-efficient, cost-effective methods to produce composite structures is desired. Traditional curing processes such as autoclaves and ovens rely on convective heat transfer, which has fundamental inefficiencies and several limitations including infrastructure cost and throughput bottlenecks. Similarly, hot presses (usually for thermoplastic matrices) for processing composites through conductive heat transfer are limited to a narrow range of part geometries. Direct Joule heating with carbon nanotube (CNT) film network heaters has shown significant promise to overcome these key manufacturing challenges of composites in the aerospace industry.en_US
dc.description.abstractThis Out-of-Oven (000) conductive curing technique has been shown to cure aerospace-grade out-of-autoclave (OoA) CFRP prepreg laminates with equivalent quality to that achieved with the manufacturer's recommend cure cycle (MRCC) in an oven. Herein are introduced three new advances utilizing OoO heating: i) the first application of OoO heating to processing aerospace-grade thermoplastic (polyetheretherketone, PEEK) CFRP prepreg, ii) a new method to accelerate the cure cycle of OoA CFRP prepreg, and iii) a novel strategy towards eliminating cure-driven deformations within composites with curved geometries via spatially-tailored OoO 'zonal curing'. OoO is found to produce PEEK CFRP plate specimens comparable or better than MRCC autoclave and hot press-produced laminates, both in terms of quality and strength, with advantages in spatial and temporal control noted.en_US
dc.description.abstractCure cycle duration for the thermoset OoA CFRP can be shortened by more than 60% while still producing flat laminates with similar quality and (short beam shear, SBS) strength compared to MRCC-produced specimens. The OoO zonal curing is shown via modeling to reduce the cure-driven deformation in thermoset OoA CFRP L-shape cuved parts by at least 11%. By demonstrating OoO curing's several advantages due to the CNT film's ability to maintain thermal stability at high temperatures, the near-instantaneous temporal control, the results in this work show that OoO curing can contribute to the next leap in composites manufacturing capability and technology. While the work herein has focused on aerospace-grade CFRP materials with the highest performance and quality, OoO is applicable to other materials in other industries including wind, ground vehicle, and infrastructure applications of a variety of advanced composites, including glass fiber reinforced plastics (GFRP).en_US
dc.description.statementofresponsibilityby Frederick O. Daso.en_US
dc.format.extent149 pagesen_US
dc.language.isoengen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsMIT theses are protected by copyright. They may be viewed, downloaded, or printed from this source but further reproduction or distribution in any format is prohibited without written permission.en_US
dc.rights.urihttp://dspace.mit.edu/handle/1721.1/7582en_US
dc.subjectAeronautics and Astronautics.en_US
dc.titleManufacture of aerospace-grade thermoset and thermoplastic composites via nanoengineered thermal processingen_US
dc.typeThesisen_US
dc.description.degreeS.M.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronauticsen_US
dc.identifier.oclc1119730090en_US
dc.description.collectionS.M. Massachusetts Institute of Technology, Department of Aeronautics and Astronauticsen_US
dspace.imported2019-10-04T21:32:50Zen_US
mit.thesis.degreeMasteren_US
mit.thesis.departmentAeroen_US


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