发明名称 |
A method of manufacturing a hollow silicon carbide fibre reinforced silicon carbide matrix component |
摘要 |
Carbon coated carbide fibres (30) are arranged in a predetermined pattern and shape around a silicon carbide coated (36) graphite insert (34). Silicon carbide is infiltrated into the silicon carbide fibres (30) to produce a SiC/SiC composite component (40). The SiC/SiC composite component (40) is coated with glass (42) and is then heated in air to burn out the graphite insert (34) to form a hollow glass coated SiC/SiC composite component. Suitable for producing hollow SiC/SiC composite turbine blades or vanes. <IMAGE>
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申请公布号 |
GB2270310(A) |
申请公布日期 |
1994.03.09 |
申请号 |
GB19920018578 |
申请日期 |
1992.09.02 |
申请人 |
* ROLLS-ROYCE PLC |
发明人 |
STEPHEN * MASON |
分类号 |
C04B35/80;C04B38/00;C23C16/04;C23C16/32;C23C16/44;(IPC1-7):C23D13/00;F01D5/14 |
主分类号 |
C04B35/80 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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