Manufacture and thermomechanical characterization of wet filament wound C/C-SiC composites |
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Authors: | Martin Frieß Muhammed Böyükbas Felix Vogel Daniel Cepli Oliver Schatz Fabia Süß Yuan Shi |
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Affiliation: | 1. Institute of Structures and Design, German Aerospace Center (DLR), Stuttgart, Germany;2. Institute of Space Systems, University of Stuttgart, Stuttgart, Germany |
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Abstract: | The paper presents manufacture of C/C-SiC composite materials by wet filament winding of C fibers with a water-based phenolic resin with subsequent curing via autoclave as well as pyrolysis and liquid silicon infiltration (LSI). Almost dense C/C-SiC composite materials with different winding angles ranging from ±15° to ±75° could be obtained with porosities lower than 3% and densities in the range of 2 g/cm3. Thermomechanical characterization via tensile testing at room temperature and at 1300°C revealed higher tensile strength at elevated temperature than at room temperature. Thus, C/C-SiC material obtained by wet filament winding and LSI-processing has excellent high-temperature strength for high-temperature applications. Crack patterns during pyrolysis, microstructure after siliconization, and tensile strength strongly depend on the fiber/matrix interface strength and winding angle. Moreover, calculation tools for composites, such as classical laminate and inverse laminate theory, can be applied for structural evaluation and prediction of mechanical performance of C/C-SiC structures. |
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Keywords: | C/C-SiC filament winding fracture surfaces microstructure pyrolysis siliconisation tensile testing thermomechanical characterization winding angle |
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