发明名称 A method of brazing composite material parts sealed with a silicon-based composition
摘要 In order to prevent brazing composition from coming into contact with the silicon or other elements present in the materials of two parts made of thermostructural composite material that are being assembled together by brazing, a refractory ceramic material layer is formed at least on those surfaces of the parts that are to be united, which material is not reactive with silicon at brazing temperature.
申请公布号 GB0511696(D0) 申请公布日期 2005.07.13
申请号 GB20050011696 申请日期 2005.06.09
申请人 SNECMA PROPULSION SOLIDE 发明人
分类号 B23K1/08;B23K1/20;C04B37/00 主分类号 B23K1/08
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