Effect of the interfacial adhesion on the tensile and impact properties of carbon fiber reinforced polypropylene matrices

Thermoplastic composites have been applied in a wide variety of industrial products, showing recently a great potential to be used in aeronautical field. The objectives of this work were to evaluate the fiber/matrix interface of carbon fiber reinforced polypropylene-based matrices after tensile and...

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Published inMaterials research (São Carlos, São Paulo, Brazil) Vol. 8; no. 1; pp. 81 - 89
Main Authors Nogueira, Clara Leal, Paiva, Jane Maria Faulstich de, Rezende, Mirabel Cerqueira
Format Journal Article
LanguageEnglish
Portuguese
Published ABM, ABC, ABPol 01.03.2005
Associação Brasileira de Metalurgia e Materiais (ABM); Associação Brasileira de Cerâmica (ABC); Associação Brasileira de Polímeros (ABPol)
Subjects
carbon fiber
composites
ENGINEERING, CHEMICAL
MATERIALS SCIENCE, MULTIDISCIPLINARY
mechanical properties
METALLURGY & METALLURGICAL ENGINEERING
polypropylene
composites
carbon fiber
polypropylene
mechanical properties
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Abstract Thermoplastic composites have been applied in a wide variety of industrial products, showing recently a great potential to be used in aeronautical field. The objectives of this work were to evaluate the fiber/matrix interface of carbon fiber reinforced polypropylene-based matrices after tensile and impact tests and also to compare the mechanical test results of the manufactured laminates. The laminates were prepared by stacking carbon fiber fabric style Plain Weave (CF) and films of four different polypropylene matrices, described as (a) polypropylene-PP, (b) polypropylene-polyethylene copolymer-PP-PE, (c) PP-PE with an interfacial compatibilizer-AM1 and (d) PP-PE containing an elastomeric modifier-AM2. The composites were processed using hot compression molding. The mechanical testing results showed that the CF-AM1 laminate family presented the lowest impact strength and the highest tensile strength values when compared to the other laminates. SEM analysis observations of both tensile and impact fractured specimens of the CF-PP/PE-AM1 specimens revealed a stronger fiber/matrix interface. The CF-PP/PE-AM2 laminate showed a lower tensile strength and higher impact strength values when compared to the CF-PP/PE-AM1 one. PP-PE and PP laminates presented the lowest impact strength values.
AbstractList Thermoplastic composites have been applied in a wide variety of industrial products, showing recently a great potential to be used in aeronautical field. The objectives of this work were to evaluate the fiber/matrix interface of carbon fiber reinforced polypropylene-based matrices after tensile and impact tests and also to compare the mechanical test results of the manufactured laminates. The laminates were prepared by stacking carbon fiber fabric style Plain Weave (CF) and films of four different polypropylene matrices, described as (a) polypropylene-PP, (b) polypropylene-polyethylene copolymer-PP-PE, (c) PP-PE with an interfacial compatibilizer-AM1 and (d) PP-PE containing an elastomeric modifier-AM2. The composites were processed using hot compression molding. The mechanical testing results showed that the CF-AM1 laminate family presented the lowest impact strength and the highest tensile strength values when compared to the other laminates. SEM analysis observations of both tensile and impact fractured specimens of the CF-PP/PE-AM1 specimens revealed a stronger fiber/matrix interface. The CF-PP/PE-AM2 laminate showed a lower tensile strength and higher impact strength values when compared to the CF-PP/PE-AM1 one. PP-PE and PP laminates presented the lowest impact strength values.
Author Rezende, Mirabel Cerqueira
Paiva, Jane Maria Faulstich de
Nogueira, Clara Leal
AuthorAffiliation Centro Técnico Aeroespacial
Instituto Tecnológico da Aeronáutica
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  givenname: Clara Leal
  surname: Nogueira
  fullname: Nogueira, Clara Leal
  organization: Instituto Tecnológico da Aeronáutica, Brazil; Centro Técnico Aeroespacial, Brazil
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  surname: Paiva
  fullname: Paiva, Jane Maria Faulstich de
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  givenname: Mirabel Cerqueira
  surname: Rezende
  fullname: Rezende, Mirabel Cerqueira
  organization: Centro Técnico Aeroespacial, Brazil
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10.1016/S0079-6700(99)00015-5
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Issue 1
Keywords composites
carbon fiber
polypropylene
mechanical properties
Language English
Portuguese
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Snippet Thermoplastic composites have been applied in a wide variety of industrial products, showing recently a great potential to be used in aeronautical field. The...
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SubjectTerms carbon fiber
composites
ENGINEERING, CHEMICAL
MATERIALS SCIENCE, MULTIDISCIPLINARY
mechanical properties
METALLURGY & METALLURGICAL ENGINEERING
polypropylene
Title Effect of the interfacial adhesion on the tensile and impact properties of carbon fiber reinforced polypropylene matrices
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