2011
DOI: 10.1002/9781118144442.ch1
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Influence of Fiber Orientation on the Mechanical Properties and Microstructure of C/C‐SiC Composite Plates Produced by Wet Filament Winding Technique

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Cited by 4 publications
(6 citation statements)
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“…A focus of this paper is to utilize the MoC-based models (GMC, MsGMC, and MsHFGMC) to predict the elastic properties of C/C-SiC plates, manufactured by Breede and colleagues using a wet filament winding and LSI technique, where it has been shown that the C/C-SiC microstructure is dependent on the filament winding angle [18]. Unfortunately, significant data on the geometry and volume fraction of the constituents within the filament wound C/C-SiC, needed to create a representative RUC, was not available.…”
Section: Resultsmentioning
confidence: 99%
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“…A focus of this paper is to utilize the MoC-based models (GMC, MsGMC, and MsHFGMC) to predict the elastic properties of C/C-SiC plates, manufactured by Breede and colleagues using a wet filament winding and LSI technique, where it has been shown that the C/C-SiC microstructure is dependent on the filament winding angle [18]. Unfortunately, significant data on the geometry and volume fraction of the constituents within the filament wound C/C-SiC, needed to create a representative RUC, was not available.…”
Section: Resultsmentioning
confidence: 99%
“…It has been demonstrated that filament winding is a promising manufacturing technique, as compared to the use of textile preforms, to attain reinforcement in arbitrary directions within CMC structures [9,17]. A novel manufacturing method utilizing wet filament wind unidirectional carbon fiber perform and liquid silicon infiltration (LSI) has been develop by the German Aerospace Institute (DLR) to manufacture state-of-the-art C/C-SiC structures [18]. The filament winding manufacturing process offers increased flexibility in two ways.…”
Section: Introductionmentioning
confidence: 99%
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“…In this study C/C-SiC composites 1 were tested [14,15]. Two C/C-SiC panels, one with a 0/90å nd one with a ±15˚fiber architecture, were manufactured using the liquid silicon infiltration (LSI) process [16].…”
Section: Materials and Testing Proceduresmentioning
confidence: 99%
“…Thus, there is a huge potential for future rocket propulsion applications. [10][11][12][13][14] State of the art is the use of commercially available fabrics to manufacture complex shaped CMC components with low porosity in one cycle, providing moderate strength materials, or even lower performance materials based on short fibers applied on cost-efficient components where low strength can be accepted. [15][16][17][18] Characterization of C/C-SiC composites with respect to thermal and mechanical properties was investigated under different loads and are summarized in previous studies.…”
Section: Introductionmentioning
confidence: 99%