Properties of Vacuum Formed Carbon /Epoxy Matrix Composites
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Affiliation:

1.Composite Technology Center of China Academy of Aeronautical Manufacturing Technology,Beijing 101300;2.AVIC Composite Corporation Ltd.,Beijing 101300

Clc Number:

TB332

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    Abstract:

    The effects of cured temperature, insulation platform and isolation material on the porosity and mechanical properties of vacuum formed CCF300/BA9913 resin matrix carbon composites were studied. The results show that CCF300/BA9913 get better mechanical properties and heat resistance after curing at 125 ℃ for 2 h.The porosity decreases and mechanical properties of the cured CCF300/BA9913 increases by adding 0.5 h insulation platform near the temperature (85 ℃) for lowest viscosity.The porous polytetrafluoroethylene film and semi permeable film are used to improve the air permeability during curing process and increase the mechanical properties of cured CCF300/BA9913 composite.The 0°tensile strength,0°compressive strength,0°flexural strength and interlaminar shear strength are 1 896 MPa,1 387 MPa,1 668 MPa,89.0 MPa.

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History
  • Received:January 12,2021
  • Revised:March 17,2021
  • Adopted:February 24,2021
  • Online: June 03,2021
  • Published: