发明名称 Method for manufacturing a ceramic composite material
摘要 The present method of manufacturing a ceramic composite material, composed of matrix and reinforcing materials and an intermediate weak interfice material, creates a composite material particuarly intended for use at temperatures above 1400° C. and in an oxidizing environment. The matrix and reinforcing materials consist of the same or different ceramic oxides having a melting point above 1600° C. The interface material provides in combination with the matrix and reinforcing materials a stress field liable to micro aciding. The reinforcing material is immersed into a powder slurry containing carbon (C) and ZrO2 so as to be coated thereby and then dried. After which, the thus created composite material is subjected to green forming and densifying steps. Finally, the composite material undergoes a heat-treatment in air leaving a porous structure of the interface material.
申请公布号 US6251317(B1) 申请公布日期 2001.06.26
申请号 US20000284221 申请日期 2000.01.13
申请人 VOLVO AERO CORPORATION;ROLLS ROYCE PLC;SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION;OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES 发明人 LUNDBERG ROBERT;HOLMQUIST MAGNUS;RAZZELL ANTHONY G.;MOLLIEX LUDOVIC;SUDRE OLIVIER;PARLIER MICHEL;ROSSIGNOL FABRICE;PARMENTIER JULIEN
分类号 C04B35/628;C04B35/80;(IPC1-7):B29C65/00 主分类号 C04B35/628
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