发明名称 METHOD FOR PRODUCING PARTS MADE OF A THERMOSTRUCTURAL COMPOSITE MATERIAL
摘要 A method of fabricating a thermostructural composite material part includes making a fiber preform formed of yarns or tows and impregnated by a consolidating composition containing a carbon- or ceramic-precursor, transforming the carbon- or ceramic-precursor by pyrolysis, and then densifying the preform by chemical vapor infiltration. A consolidating composition is used that additionally contains refractory solid fillers in the powder form presenting mean grain size less than 200 nanometers and leaving, after pyrolysis, a consolidated solid phase in which the carbon or the ceramic derived from the precursor occupies a volume representing 3% to 10% of the apparent volume of the preform, and the solid fillers occupy a volume representing 0.5% to 5% of the apparent volume of the preform.
申请公布号 US2011200748(A1) 申请公布日期 2011.08.18
申请号 US200913121278 申请日期 2009.09.23
申请人 SNECMA PROPULSION SOLIDE 发明人 EBERLING-FUX NICOLAS;BOUILLON ERIC;PHILIPPE ERIC;TAWIL HENRI
分类号 C23C16/26;C23C16/22 主分类号 C23C16/26
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