Heidenreich, Bernhard und Jain, Neraj und Postler, Kevin und Koch, Dietmar und Schneck, Tanja, K. und Hermanutz, Frank und Clauß, Bernd und Buchmeiser, Michael, R. und Brück, Bastian und Schulz, Michael und Müller, Wolfgang und Horn, Siegfried, R. (2019) C/C-SiC Materials Based on High Performance C Fibres with Tailored Fibre-Matrix Bonding. 10th International Conference on High Temperature Ceramic Matrix Composites (HTCMC 10), 2019-09-20 - 2019-09-22, Bordeaux, Frankreich.
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Kurzfassung
The Liquid Silicon Infiltration (LSI) process is used to manufacture carbon fiber based C/C-SiC composites. A CFRP-preform (carbon fibre reinforced polymer) is manufactured by infiltrating C fibre rovings with a phenolic resin, wet filament winding and warm pressing. After curing, the polymer matrix is converted to carbon by a high temperature treatment. Due to matrix shrinkage, the resulting C/C preform is characterized by a high amount of porosity. The pore morphology includes fine, closed pores as well as open porosity in form of segmentation microcracks (SMC), fragmenting the fibre tows into discrete C/C bundles and forming a 3D-network of interconnected microchannels. Depending on the fibre matrix bonding (FMB) and interaction, also shrinkage cracks between individual filaments and matrix (FMC) are observed in the C/C bundles all over the composite. During siliconization, the molten silicon is infiltrating the open pores and microcracks and SiC matrix is built up by a chemical reaction of Si and C. In order to obtain damage tolerant C/C-SiC materials, the fibres have to be protected from Si contact and conversion to SiC. Therefore, FMI has to be tailored to form dense C/C bundles and to avoid shrinkage cracks between filaments and matrix. In the current work, the formation of SMC and FMC is studied on CFRP-preforms based on standard high tenacity as well as on intermediate and ultrahigh modulus C fibres and is simulated in a FE-model. The influence of fibre surface treatment on FMB and microstructure development as well as on the material processing and, finally, on the mechanical properties of the resulting C/C-SiC materials is presented.
elib-URL des Eintrags: | https://elib.dlr.de/132914/ | ||||||||||||||||||||||||||||||||||||||||||||||||||||
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Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Titel: | C/C-SiC Materials Based on High Performance C Fibres with Tailored Fibre-Matrix Bonding | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Autoren: |
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Datum: | September 2019 | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Referierte Publikation: | Ja | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Open Access: | Ja | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||||||||||||||||||||||||||||||||||
In SCOPUS: | Nein | ||||||||||||||||||||||||||||||||||||||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Stichwörter: | C/C-SiC, ceramic composite, carbon fibres | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Veranstaltungstitel: | 10th International Conference on High Temperature Ceramic Matrix Composites (HTCMC 10) | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Veranstaltungsort: | Bordeaux, Frankreich | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Veranstaltungsbeginn: | 20 September 2019 | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Veranstaltungsende: | 22 September 2019 | ||||||||||||||||||||||||||||||||||||||||||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||||||||||||||||||||||||||||||||||
HGF - Programm: | Raumfahrt | ||||||||||||||||||||||||||||||||||||||||||||||||||||
HGF - Programmthema: | Raumtransport | ||||||||||||||||||||||||||||||||||||||||||||||||||||
DLR - Schwerpunkt: | Raumfahrt | ||||||||||||||||||||||||||||||||||||||||||||||||||||
DLR - Forschungsgebiet: | R RP - Raumtransport | ||||||||||||||||||||||||||||||||||||||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | R - Wiederverwendbare Raumfahrtsysteme und Antriebstechnologie | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Standort: | Stuttgart | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Institute & Einrichtungen: | Institut für Bauweisen und Strukturtechnologie > Keramische Verbundstrukturen | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Hinterlegt von: | Heidenreich, Bernhard | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Hinterlegt am: | 18 Dez 2019 11:30 | ||||||||||||||||||||||||||||||||||||||||||||||||||||
Letzte Änderung: | 24 Apr 2024 20:36 |
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