发明名称 METHOD AND SUBSTRATE FOR MAKING COMPOSITE MATERIAL PARTS BY CHEMICAL VAPOUR INFILTRATION DENSIFICATION AND RESULTING PARTS
摘要 <p>A composite material part is made by forming a fiber preform (20), forming holes (22) extending within the preform from at least one face thereof, and densifying the preform with a matrix formed at least in part by a chemical vapor infiltration (CVI) type process. The holes (22) are formed by removing material from the preform with fibers being ruptured, for example by machining using a jet of water under pressure, the arrangement of the fibers in the preform with the holes being substantially unchanged compared with the initial arrangement before the holes were formed. This enables the densification gradient to be greatly reduced, and it is possible in a single densification cycle to obtain a density that, in the prior art, required a plurality of cycles separated by intermediate scalping.</p>
申请公布号 EP1886046(B1) 申请公布日期 2011.04.27
申请号 EP20060778912 申请日期 2006.06.01
申请人 SNECMA PROPULSION SOLIDE 发明人 BERNARD, BRUNO;GOUJARD, STEPHANE;BERTRAND, SEBASTIEN;THEBAULT, JACQUES
分类号 F16D69/02;B23K26/28;B26F1/26;C04B35/80;C04B35/83 主分类号 F16D69/02
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