Coupling Agents - HME Resin System.

Abstract

Two approaches were taken to improve the SBS strength of HME/AS composites. First, attempts were made to react a number of organo-titanates, epoxides, and modified polybutadiene (PB) epoxides with reactive sites on the graphite fiber surface and then to react, or couple, with the matrix HME resin. Epon 834 (a bisphenol A type epoxy resin), allylglycidyl ether, and a reaction product of C-1000 PB and ERE-1359 epoxy resin produced very slight increases in SBS strengths of HME composites when used as AS fiber sizing. Second, attempts were made to reinforce the HME resin with three finely divided fillers: Vulcan 9A32 carbon black, HiSil 233 hydrated silica, and HR-600 polyimide resin. However, these fillers severely degraded composite strengths. Low profile modifiers, developed to reduce cure shrinkage in polyester resins, were evaluated for this purpose in the HME resin system but were found to be incompatible. It is unlikely that all of the many approaches to form primary chemical bonds between the HME matrix and graphite fiber failed, yet no significant improvement in SBS was achieved over untreated fiber during this program. The possibility that a low cohesive strength in the HME matrix was the problem was briefly explored using fillers, also without success.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1977
Accession Number
ADA054394

Entities

People

  • L. Garry Adams
  • R. E. Hoffman

Tags

Communities of Interest

  • Counter IED

DTIC Thesaurus Topics

  • Air Force
  • Chemical Bonds
  • Chemical Synthesis
  • Chemistry
  • Chlorides
  • Composite Materials
  • Contracts
  • Epoxy Resins
  • Government Procurement
  • Graphitic Materials
  • Laminates
  • Materials
  • Materials Laboratories
  • Materials Science
  • Polyimide Resins
  • Resins
  • Titanium

Fields of Study

  • Materials science

Readers

  • Polymer Science and Engineering.
  • Reinforced Composite Materials
  • Superconducting Magnet Technology