Frieß, M. und Krenkel, W. und Nestler, K. und Marx, G. (2001) CVD-Coating of Fabric Sheets in Combination with the LSI-Process. In: High Temperature Ceramic Matrix Composites, Seiten 199-204. Wiley- VCH. 4th International Conference on High Temperature Ceramic Matric Composites (HT-CMC 4), München, 1-3. Oktober 2001. ISBN 3-527-30320-0.
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Kurzfassung
Due to short processing times and fairly low manufacturing costs the Liquid Silicon Infiltration Process (LSI) developed at the DLR in Stuttgart is a well established process to produce ceramic matrix composites (CMC) without any fiber coating [1]. The key step is the liquid silicon infiltration of porous carbon/carbon composites (C/C) whose distinct microstructure is formed in the preceding pyrolysis step of carbon fiber reinforced plastics (CFRP). These were produced by resin transfer molding (RTM) in a first step. This process leads to C/C-SiC composites being characterized by high mass-specific properties in combination with an extreme thermal shock stability. By applying special process pa-rameters the microstructure as well as the physical properties can be tailor-designed to match spe-cific requirements. However, compared to CMCs reinforced with coated fibers [2-5], C/C-SiC has a low damage tolerance and tensile strength since the fiber matrix bonding (FMB) is too high. An improvement can be achieved by a fiber pretreatment at about 600 °C prior to composite manufacturing [6]. However, the superior properties of composites manufactured with coated fibers cannot be achieved. Unfortunately, single fiber coating increases CMC costs considerably [7]. In order to overcome this problem, woven C-fabrics have been coated with pyrolytic carbon (pyC) and then submitted to the LSI-process yielding dense C/C-SiC. In a first step, C-fabric sheets (30 mm in width and 300 mm in length) were coated with pyC in both a CVD hot wall and alternatively in a CVD cold wall reactor under static condi-tions at about 900 °C. Toluene was used as a precursor whereas argon served as a carrier gas. Deposition times ranging from 10 to 20 min resulted in an increase in weight of 50 to 250 mg corre-sponding to a mean layer thickness of 39 to 189 nm on each single fiber. The pyC-coated C-fabrics exhibited increased stiffness with increased coating thickness as well as reference samples were submitted to the conventional LSI-process. Besides SEM-investigations on the pyC-coating, this paper reports on the physical and the mechanical properties of the composites manufactured via LSI-processing in all stages CFRP, C/C and especially C/C-SiC.
elib-URL des Eintrags: | https://elib.dlr.de/14840/ | ||||||||||||||||||||
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Dokumentart: | Konferenzbeitrag (Paper) | ||||||||||||||||||||
Zusätzliche Informationen: | LIDO-Berichtsjahr=2002, | ||||||||||||||||||||
Titel: | CVD-Coating of Fabric Sheets in Combination with the LSI-Process | ||||||||||||||||||||
Autoren: |
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Datum: | 2001 | ||||||||||||||||||||
Erschienen in: | High Temperature Ceramic Matrix Composites | ||||||||||||||||||||
Open Access: | Nein | ||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||
In SCOPUS: | Nein | ||||||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||||||
Seitenbereich: | Seiten 199-204 | ||||||||||||||||||||
Herausgeber: |
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Verlag: | Wiley- VCH | ||||||||||||||||||||
ISBN: | 3-527-30320-0 | ||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||
Stichwörter: | CMC, ceramic, manufacture, silicon-based materials, LSI, reentry, coating | ||||||||||||||||||||
Veranstaltungstitel: | 4th International Conference on High Temperature Ceramic Matric Composites (HT-CMC 4), München, 1-3. Oktober 2001 | ||||||||||||||||||||
Veranstalter : | DGM/DLR | ||||||||||||||||||||
HGF - Forschungsbereich: | Verkehr und Weltraum (alt) | ||||||||||||||||||||
HGF - Programm: | Weltraum (alt) | ||||||||||||||||||||
HGF - Programmthema: | W RP - Raumtransport | ||||||||||||||||||||
DLR - Schwerpunkt: | Weltraum | ||||||||||||||||||||
DLR - Forschungsgebiet: | W RP - Raumtransport | ||||||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | NICHT SPEZIFIZIERT | ||||||||||||||||||||
Standort: | Stuttgart | ||||||||||||||||||||
Institute & Einrichtungen: | Institut für Bauweisen- und Konstruktionsforschung | ||||||||||||||||||||
Hinterlegt von: | DLR-Beauftragter, elib | ||||||||||||||||||||
Hinterlegt am: | 16 Sep 2005 | ||||||||||||||||||||
Letzte Änderung: | 14 Jan 2010 22:22 |
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