Radiation Curing: Coatings and Composites

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Toughness/Impact Testing Four ply carbon fiber composite <strong>and</strong> aluminum test panel of comparable thickness: impacted at 13.6 N-m
Properties Six Ply Carbon Fiber Reinforced <strong>Composites</strong> X-ray cured Initial fracture Izod in mold at 24 kGy of matrix Impact bis-phenol-A diacrylate 6.8 N-m 901 J/m matrix system – no impact additive bis-phenol-A diacrylate 15.8 N-m 1043 J/m matrix system – with impact additive
Page 1 and 2: Radiation Curing: Coatings and Comp
Page 3 and 4: Electron Beam Parameters Voltage =
Page 5 and 6: 80 - 120 keV Development Unit 1.5 m
Page 7 and 8: Low-voltage EB Equipment 300 keV se
Page 9 and 10: X-ray Conversion
Page 11 and 12: Unipolis 10 MeV EB/X-ray Facility
Page 13 and 14: Brenner-Campbell Conclusions
Page 15 and 16: Surface Tension Tests 55 Contact An
Page 17 and 18: VARTM with PC/HDPE Platens Wetted c
Page 19 and 20: Solubility EB/X-ray Cured Samples G
Page 21: Toughness Testing 123 cm Falling tu
Page 25 and 26: Developing Molecular Structures Con
Page 27 and 28: Microphase Understanding Intra-mole
Page 29 and 30: Thermal Analysis Resin Systems X-ra
Page 31 and 32: Dynamic Mechanical Analysis Used by
Page 33 and 34: Dynamic Mechanical Analysis tan δ
Page 35 and 36: Pragmatic Tests: TMA TMA in compres
Page 37 and 38: Heat Deflection Test 1.82 MPa 100 m
Page 39 and 40: X-ray Curing Studies Initial X-ray
Page 41 and 42: X-ray Curing Composites in the Mold
Page 43 and 44: X-ray Cured Sports Car Fender
Page 45: Conclusions + Some properties devel

Radiation Curing: Coatings and Composites

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