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EXPERIMENTAL STUDY ON PEK-C MODIFIED EPOXIES AND THE CARBON FIBER COMPOSITES FOR AEROSPACE APPLICATION
作者姓名:LI Yang  YI Xiao-Su  TANG Bang-ming
作者单位:National Key Laboratory of Advanced Composites, Beijing Institute of Aeronautical Materials, Beijing 100095, China
基金项目:Key Laboratory Funds,,
摘    要:Epoxy(EP) resins have been widely used astraditional materials in aerospace applications dueto their relatively high stiffness and strength,goodthermal stability,excellent adhesion,and goodprocessabilities,particularly because thatthey havebeen toughened by incorporating rubber particlesand thermoplastic(TP) component into the resinsto form multi- component systems1~ 5] .Comparedwith rubber modifiers,thermoplastics can improvethe epoxy toughness without sacrificing the ther-mal stabilities …

关 键 词:PEK-C  thermoset/thermoplastic  binary  system  phase  behavior

EXPERIMENTAL STUDY ON PEK-C MODIFIED EPOXIES AND THE CARBON FIBER COMPOSITES FOR AEROSPACE APPLICATION
LI Yang,YI Xiao-Su,TANG Bang-ming.EXPERIMENTAL STUDY ON PEK-C MODIFIED EPOXIES AND THE CARBON FIBER COMPOSITES FOR AEROSPACE APPLICATION[J].Chinese Journal of Aeronautics,2000,13(4):242-249.
Authors:LI Yang  YI Xiao-Su  TANG Bang-ming
Abstract:The morphological structure of various epoxies toughened with a special amorphous thermoplastic PEK-C and their carbon fiber composites were studied by using SEM. For both cases, phase separation and inversion took place to form fine epoxy-rich globules dispersing in the PEK-C matrix, in which the epoxy-rich phase had the absolutely higher volume fraction. The phase structure and the interfacial properties were also studied by means of FTIR, DSC, and DMTA as well. An accompanying mechanical determination revealed that an improved toughness was achieved both in the blend casts and in the carbon fiber composites. A composite structural model was hence suggested.
Keywords:interface  toughness  carbon fiber composites
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