Abstract
Composites use in the aerospace industry is expanding, in particular carbon fibre reinforced plastics (CFRP) for structural components. Machinability can however be problematic especially when drilling, due to CFRP's inherent anisotropy/in-homogeneity, limited plastic deformation and abrasive characteristics. Following a brief review on composites development and associated machining, the paper outlines experimental results when twist drilling 1.5 mm diameter holes in 3 mm thick CFRP laminate using tungsten carbide (WC) stepped drills. The control variables considered were prepreg type (3 types) and form (unidirectional (UD) and woven), together with drill feed rate (0.2 and 0.4 mm/rev). A full factorial experimental design was used involving 12 tests. Response variables included the number of drilled holes (wear criterion VB(B)max
Original language | English |
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Pages (from-to) | 1023-1034 |
Number of pages | 12 |
Journal | Journal of Materials Processing Technology |
Volume | 210 |
Issue number | 8 |
DOIs | |
Publication status | Published - 1 Jun 2010 |
Keywords
- CFRP
- Drilling
- Prepreg form
- Delamination
- Composites