<HashMap><database>biostudies-literature</database><scores/><additional><submitter>Kwon W</submitter><funding>the Institute of Civil Military Technology Cooperation funded by the Defense Acquisition Program Administration and Ministry of Trade, Industry and Energy of Korean government</funding><funding>Defense Acquisition Program Administration and Ministry of Trade, Industry, and Energy of the Korean government</funding><pagination>695</pagination><full_dataset_link>https://www.ebi.ac.uk/biostudies/studies/S-EPMC11902468</full_dataset_link><repository>biostudies-literature</repository><omics_type>Unknown</omics_type><volume>17(5)</volume><pubmed_abstract>Fracture toughness is a key property of epoxy resins with a high glass transition temperature (T&lt;sub>g&lt;/sub>), used in carbon fiber/epoxy composites for aerospace applications. Conventional toughening methods rely on adding toughening agents, often compromising the processibility and thermal stability. This study introduces a simple self-toughening approach that enhances the fracture toughness without sacrificing other properties by controlling the cured epoxy network structure. Tetraglycidyl 4,4'-diaminodiphenylmethane (TGDDM) epoxy resin was cured using mixtures of structural isomeric curing agents, 3,3'- and 4,4'-diaminodiphenyl sulfone (3,3'- and 4,4'-DDS), at ratios of 7:3, 5:5, and 3:7. The optimal 7:3 ratio produced a resin with 30% higher fracture toughness compared to TGDDM/3,3'-DDS and 100% higher than the TGDDM/4,4'-DDS system. The T&lt;sub>g&lt;/sub> of the self-toughened resin ranged from 241 to 266 °C, which was intermediate between the T&lt;sub>g&lt;/sub> values of the TGDDM/3,3'-DDS and TGDDM/4,4'-DDS systems. This improvement is attributed to the higher crosslink density and reduced free volume of the epoxy network. These findings demonstrate that simply mixing isomeric curing agents enables self-toughening, providing a practical and efficient strategy to enhance the performance of high-T&lt;sub>g&lt;/sub> epoxy resins in advanced composite applications.</pubmed_abstract><journal>Polymers</journal><pubmed_title>Self-Toughened Epoxy Resin via Hybridization of Structural Isomeric Curing Agents.</pubmed_title><pmcid>PMC11902468</pmcid><funding_grant_id>22-CM-CO-19</funding_grant_id><funding_grant_id>No. 22-CM-19</funding_grant_id><pubmed_authors>Jeong E</pubmed_authors><pubmed_authors>Cheon J</pubmed_authors><pubmed_authors>Jeong HJ</pubmed_authors><pubmed_authors>Lee SG</pubmed_authors><pubmed_authors>Won JS</pubmed_authors><pubmed_authors>Kim BJ</pubmed_authors><pubmed_authors>Kwon W</pubmed_authors><pubmed_authors>Lee MY</pubmed_authors></additional><is_claimable>false</is_claimable><name>Self-Toughened Epoxy Resin via Hybridization of Structural Isomeric Curing Agents.</name><description>Fracture toughness is a key property of epoxy resins with a high glass transition temperature (T&lt;sub>g&lt;/sub>), used in carbon fiber/epoxy composites for aerospace applications. Conventional toughening methods rely on adding toughening agents, often compromising the processibility and thermal stability. This study introduces a simple self-toughening approach that enhances the fracture toughness without sacrificing other properties by controlling the cured epoxy network structure. Tetraglycidyl 4,4'-diaminodiphenylmethane (TGDDM) epoxy resin was cured using mixtures of structural isomeric curing agents, 3,3'- and 4,4'-diaminodiphenyl sulfone (3,3'- and 4,4'-DDS), at ratios of 7:3, 5:5, and 3:7. The optimal 7:3 ratio produced a resin with 30% higher fracture toughness compared to TGDDM/3,3'-DDS and 100% higher than the TGDDM/4,4'-DDS system. The T&lt;sub>g&lt;/sub> of the self-toughened resin ranged from 241 to 266 °C, which was intermediate between the T&lt;sub>g&lt;/sub> values of the TGDDM/3,3'-DDS and TGDDM/4,4'-DDS systems. This improvement is attributed to the higher crosslink density and reduced free volume of the epoxy network. These findings demonstrate that simply mixing isomeric curing agents enables self-toughening, providing a practical and efficient strategy to enhance the performance of high-T&lt;sub>g&lt;/sub> epoxy resins in advanced composite applications.</description><dates><release>2025-01-01T00:00:00Z</release><publication>2025 Mar</publication><modification>2025-04-04T01:28:25.521Z</modification><creation>2025-04-04T01:28:25.521Z</creation></dates><accession>S-EPMC11902468</accession><cross_references><pubmed>40076187</pubmed><doi>10.3390/polym17050695</doi></cross_references></HashMap>