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Effect of unidirectional prepreg size on punching of pseudo-ductile CFRP laminates and CFRP/metal hybrid composites
- Source :
- Composite Structures. 186:246-255
- Publication Year :
- 2018
- Publisher :
- Elsevier BV, 2018.
-
Abstract
- Punching is an efficient and economical process for producing a hole in structures for functional requirements, repair, maintenance, and so forth. Toward extending the use of punching to new materials, the punching of multilayer CFRP laminates and CFRP/metal hybrid composites was investigated. In this paper, the effect of the unidirectional (UD) prepreg size on the shear behavior of pseudo-ductile CFRP laminates and CFRP/metal hybrid composites is discussed on the basis of experimental observations. CFRP laminates were individually fabricated using standard (149 g/m 2 ) and thin-ply (62 g/m 2 ) prepregs, and were bonded with three metals (aluminum alloy A6061, magnesium alloy AZ31, and advanced high-strength steel SPFC980) by utilizing an autoclave (co-curing) and adhesive glue for hybrid composite application , then punched by a circular die and punch tool at room temperature. The effects of the UD prepreg size on the punch force, punching resistance (Ks), quality, and sheared surfaces of the through-holes are discussed. The shear behavior for punching in different composites was also studied by microscopic examination. Our results are expected to enable quantitative design for the development of punched CFRP laminates and CFRP/metal hybrid composites.
- Subjects :
- 0209 industrial biotechnology
business.product_category
Materials science
Alloy
chemistry.chemical_element
02 engineering and technology
engineering.material
021001 nanoscience & nanotechnology
Metal
Shear (sheet metal)
020901 industrial engineering & automation
chemistry
Aluminium
visual_art
Autoclave (industrial)
Ceramics and Composites
visual_art.visual_art_medium
engineering
Die (manufacturing)
Magnesium alloy
Composite material
0210 nano-technology
business
Punching
Civil and Structural Engineering
Subjects
Details
- ISSN :
- 02638223
- Volume :
- 186
- Database :
- OpenAIRE
- Journal :
- Composite Structures
- Accession number :
- edsair.doi...........fc0f334147ac7bbf24118cbb39e74772
- Full Text :
- https://doi.org/10.1016/j.compstruct.2017.11.042