作者: A. Theuer , F. J. Arendts
DOI: 10.1007/978-94-009-0787-4_67
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摘要: Carbon fibre reinforced carbon (C/C) as a structural composite material is well known for its good thermomechanical properties above 2000 °C. Main applications in current aeronautical and space programmes are predicted heatshields propulsion systems. Many efforts have to be done protect the from oxidation 500 °C (SiC-matrix). Nevertheless basic mechanical characteristics of this coated C/C depend mainly on skeleton. Some principal effects stress-concentration bolt bearing strength shown here.