Radiation Curing: Coatings and Composites
Radiation Curing: Coatings and Composites Radiation Curing: Coatings and Composites
from univ.reims.fr
More from this publisher
23.10.2014
Views
Toughness/Impact Testing Four ply carbon fiber composite and aluminum test panel of comparable thickness: impacted at 13.6 N-m
Properties Six Ply Carbon Fiber Reinforced Composites 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
Toughness/Impact Testing<br />
Four ply carbon fiber composite <strong>and</strong> aluminum test panel of<br />
comparable thickness: impacted at 13.6 N-m
Change language