Radiation Curing: Coatings and Composites
Radiation Curing: Coatings and Composites Radiation Curing: Coatings and Composites
Heat Deflection Test Six ply composite X-ray Heat cured in mold at 24 kGy Deflection bis-phenol-A diacrylate >180°C matrix system – no impact additive bis-phenol-A diacrylate >180°C matrix system – with impact additive Test ended at 180°C = maximum temperature of heating bath
X-ray Curing Studies Initial X-ray curing carbon fiber composite in the mold
- 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 and 22: Toughness Testing 123 cm Falling tu
- Page 23 and 24: Properties Six Ply Carbon Fiber Rei
- 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: Heat Deflection Test 1.82 MPa 100 m
- 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
Heat Deflection Test<br />
Six ply composite X-ray Heat<br />
cured in mold at 24 kGy Deflection<br />
bis-phenol-A diacrylate >180°C<br />
matrix system – no impact additive<br />
bis-phenol-A diacrylate >180°C<br />
matrix system – with impact additive<br />
Test ended at 180°C = maximum temperature of heating bath
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