Obsidian
Aerospace
- Mar 29, 2006
- 9
Evening Forum ,
Can anyone suggest processing factors that may yield lower than expected ILSS test scores for CFRP laminates . The laminates are usually aproximately 8 plies thick with a nominal thickness of 2mm . The fabric is usually woven with the 0 Deg direction aligned in the same orientation for all 8 plies . The resin is an epoxy . The material is laid up as a pre-impregante and autoclave cured at 360 F and 90 psi . The Vf is typically 60 % and Vv is < 2% .
Any thoughts would be appreciated .
Cheers
Can anyone suggest processing factors that may yield lower than expected ILSS test scores for CFRP laminates . The laminates are usually aproximately 8 plies thick with a nominal thickness of 2mm . The fabric is usually woven with the 0 Deg direction aligned in the same orientation for all 8 plies . The resin is an epoxy . The material is laid up as a pre-impregante and autoclave cured at 360 F and 90 psi . The Vf is typically 60 % and Vv is < 2% .
Any thoughts would be appreciated .
Cheers