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- Publisher Website: 10.1002/1527-2648(200104)3:4<223::AID-ADEM223>3.0.CO;2-H
- Scopus: eid_2-s2.0-0035532237
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Article: A novel powder coated fibre pre-processing route to metal matrix composites
Title | A novel powder coated fibre pre-processing route to metal matrix composites |
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Authors | |
Issue Date | 2001 |
Citation | Advanced Engineering Materials, 2001, v. 3, n. 4, p. 223-226 How to Cite? |
Abstract | Since the dawn of the transport, and in particular, the aerospace engineering industry, there has been an ever-growing need for high performance and high temperature materials. Materials such as titanium/ silicon carbide fibre metal matrix composites (Ti/ SiC MMCs) provide high strength, low density and operate at high temperature to their particular applications. Unfortunately, the maturing technology of Ti/SiC MMCs still suffers from extremely high fabrication costs. Reducing this and increasing component processing flexibility remain the priorities of current research. This article presents a Powder Coated Fibre pre-processing technique to meet such industrial requirements. The technique is based on slurry powder metallurgy and presents itself as a cost-effective alternative to current Ti/SiC MMCs processing methods. It involves firstly, mixing matrix powder particles with an appropriate organic binder and solvent to form a slurry, drawing a continuous silicon carbide fibre through the slurry onto a winding drum, drying the coated-fibre and finally laying up the coated fibre into a composite pre-form for subsequent consolidation. The organic component is removed from the pre-form matrix via a binder burnout phase prior to composite consolidation. |
Persistent Identifier | http://hdl.handle.net/10722/263026 |
ISSN | 2023 Impact Factor: 3.4 2023 SCImago Journal Rankings: 0.808 |
DC Field | Value | Language |
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dc.contributor.author | Guo, Z. Xiao | - |
dc.contributor.author | Beeley, Nathan R.F. | - |
dc.date.accessioned | 2018-10-08T09:29:07Z | - |
dc.date.available | 2018-10-08T09:29:07Z | - |
dc.date.issued | 2001 | - |
dc.identifier.citation | Advanced Engineering Materials, 2001, v. 3, n. 4, p. 223-226 | - |
dc.identifier.issn | 1438-1656 | - |
dc.identifier.uri | http://hdl.handle.net/10722/263026 | - |
dc.description.abstract | Since the dawn of the transport, and in particular, the aerospace engineering industry, there has been an ever-growing need for high performance and high temperature materials. Materials such as titanium/ silicon carbide fibre metal matrix composites (Ti/ SiC MMCs) provide high strength, low density and operate at high temperature to their particular applications. Unfortunately, the maturing technology of Ti/SiC MMCs still suffers from extremely high fabrication costs. Reducing this and increasing component processing flexibility remain the priorities of current research. This article presents a Powder Coated Fibre pre-processing technique to meet such industrial requirements. The technique is based on slurry powder metallurgy and presents itself as a cost-effective alternative to current Ti/SiC MMCs processing methods. It involves firstly, mixing matrix powder particles with an appropriate organic binder and solvent to form a slurry, drawing a continuous silicon carbide fibre through the slurry onto a winding drum, drying the coated-fibre and finally laying up the coated fibre into a composite pre-form for subsequent consolidation. The organic component is removed from the pre-form matrix via a binder burnout phase prior to composite consolidation. | - |
dc.language | eng | - |
dc.relation.ispartof | Advanced Engineering Materials | - |
dc.title | A novel powder coated fibre pre-processing route to metal matrix composites | - |
dc.type | Article | - |
dc.description.nature | link_to_subscribed_fulltext | - |
dc.identifier.doi | 10.1002/1527-2648(200104)3:4<223::AID-ADEM223>3.0.CO;2-H | - |
dc.identifier.scopus | eid_2-s2.0-0035532237 | - |
dc.identifier.volume | 3 | - |
dc.identifier.issue | 4 | - |
dc.identifier.spage | 223 | - |
dc.identifier.epage | 226 | - |
dc.identifier.issnl | 1438-1656 | - |