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Journal of Composite Materials
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A New Method to Reduce Cure-Induced Stresses in Thermoset Polymer Composites, Part III: Correlating Stress History to Viscosity, Degree of Cure, and Cure Shrinkage

John D. Russell

Air Force Research Laboratory, Materials and Manufacturing Directorate, Wright-Patterson AFB, OH 45433-7750

Madhu S. Madhukar

Dept. of Mech., Aero. & Eng. Sci., 414 Dougherty Eng. Bldg., The University of Tennessee, Knoxville, TN 3 7996-2210

Mohamed S. Genidy

Dept. of Mech., Aero. & Eng. Sci., 414 Dougherty Eng. Bldg., The University of Tennessee, Knoxville, TN 3 7996-2210

Andre Y. Lee

Michigan State University, Dept. of Materials Science & Mechanics, East Lansing, MI 48824-1226

Non-thermoelastic effects such as cure shrinkage of a polymer can play a role in residual stresses in composite parts. Studies have shown that cure shrinkage can place significant stresses on fibers. Therefore, the cure cycle of 3501-6 epoxy resins was modified to change its cure shrinkage characteristics to minimize the stresses. New cure strategies were developed using volumetric dilatometry, differential scanning calorimetry, dielectric cure monitoring, and a unique single fiber stress test method. Cure cycles were modified to balance the resin's thermal expansion with its cure shrinkage. In some cases, a region of constant volume was achieved for a short time. However, the cure shrinkage eventually dominated over thermal expansion in all cycles as the polymer gelled. Changing the cure cycle affected the degree of cure at the point where the fiber/matrix interface developed as well as the amount of cure shrinkage occurring afterwards. A higher degree of cure at this point leads to longer stress relaxation time. Furthermore, less cure shrinkage at this point leads to less stress on the fibers. Also, slow heating rates allow more time for the polymer to relax and relieve stresses caused by cure shrinkage. Finally, a cure cycle that minimizes stresses due to cure shrinkage has been demonstrated.

Journal of Composite Materials, Vol. 34, No. 22, 1926-1947 (2000)
DOI: 10.1106/UY9U-F2QW-2FKK-91KG


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Modeling the Dimensional Variations of Composites Using Effective Coefficients of Thermal Expansion
Journal of Composite Materials, October 1, 2009; 43(22): 2639 - 2652.
[Abstract] [PDF]