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Massachusetts Institute of Technology

Investigation of integrally-heated tooling and thermal modeling methodologies for the rapid cure of aerospace composites

Abstract

dc:description.abstract

Carbon Fiber Reinforced Polymer (CFRP) composite manufacturing requires the CFRP part on the associated tool to be heated, cured, and cooled via a prescribed thermal profile. Current methods use large fixed structures such as ovens and autoclaves to perform this process step; however heating these large structures takes significant amounts of energy and time. Further, these methods cannot control for different thermal requirements across a more complex or integrated composite structure. This project focused on the below objectives and approaches: - Gather baseline energy and performance data on ovens and autoclaves to compare with estimations of new technologies; - Determine feasibility, applicability, and preliminary thermal performance of proposed heated tooling technologies on certain part families via heat transfer analyses. The project yielded the below results and conclusions: - Proved the capability of the modeling software to mimic an oven cure with less than 3% error in maximum exothermic temperature prediction; - Provided guidelines on when to use 1D, 2D, and 3D heat transfer analyses based on part thickness; - Concluded which size/shape of parts would work best for the single sided integral heating technologies; - Calculated energy intensity of incumbent technologies for comparison of future experiments on integrally heated tooling. Overall, this project helped steer the team into the next phase of their research of the technology and its applications. It provided recommendations on what type of parts the technology can be used as well as quantified the energy intensity of incumbents for comparison.

Degree

thesis:*
Department dc:contributor.department
Leaders for Global Operations Program at MIT
Grantor dc:publisher
Massachusetts Institute of Technology
Year dc:date.issued
2015

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Bromley, Harrison Scott
Advisor dc:contributor.advisor
  • Timothy G. Gutowski and Thomas Roemer.

Subjects

dc:subject × 3

Rights

dc:rights
Statement dc:rights
  • M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission.
Language dc:language.iso
eng

Identifiers

dc:identifier.*
Handle dc:identifier.uri
http://hdl.handle.net/1721.1/100149
OAI identifier oai:identifier
oai:dspace.mit.edu:1721.1/100149

Chain of custody

source
Harvested from
MIT
Base URL
dspace.mit.edu/oai/request
Last updated
2026-07-22
Source record
OAI-PMH GetRecord
citation

Bromley, Harrison Scott. Investigation of integrally-heated tooling and thermal modeling methodologies for the rapid cure of aerospace composites. Massachusetts Institute of Technology, 2015. http://hdl.handle.net/1721.1/100149