发明名称 COMPOSITE MATERIAL PART STRUCTURE TO BE EXPOSED TO HIGH TEMPERATURE GAS
摘要 PROBLEM TO BE SOLVED: To obtain a composite material (fiber-reinforced ceramic) part structure having excellent erosion resistance and excellent smoothness on the surface to be exposed to high temperature gases, wholly having a proper strength, and capable of being produced at a proper cost by reducing the thickness of each fiber bundle and narrowing the mutual distance of fiber bundles in the surface layers in comparison with those of the lower layer. SOLUTION: This composite material part to be exposed to high temperature gases is formed from a fiber-reinforced ceramic. In the surface layer 1 of the composite material (fiber-reinforced ceramic) part structure, the thickness of each fiber bundle 3 is reduced, and the mutual distance of fiber bundles 3 is narrowed in comparison with those of the lower layer 2. Thereby, the fiber bundles in the matrix 4 of the surface layer 1 are finely distributed, and the dense surface having improved erosion resistance and improved surface smoothness is obtained. The lower layer 2 is controlled to a proper fiber bundle thickness and a proper fiber bundle distance in the consideration of strength and cost. The thickness of the surface layer 1 is desirably 0.2-5 mm. The fiber-reinforced ceramic includes a SiC fiber/SiC matrix, C fiber/SiC matrix, and Al2O3 fiber/Al2O3 matrix.
申请公布号 JP2000143358(A) 申请公布日期 2000.05.23
申请号 JP19980315506 申请日期 1998.11.06
申请人 ISHIKAWAJIMA HARIMA HEAVY IND CO LTD 发明人 NISHIDE SHIGETO;YAMAGUCHI HIROHIDE
分类号 C04B35/565;C04B35/10;C04B35/80;F01D5/28 主分类号 C04B35/565
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