发明名称 Turbine disk component composed of a composite material and corresponding manufacturing process
摘要 A process for manufacturing a disk shaped component (40) comprising fabricating a disk shaped component using a composite material having at least a first material (42) and a second material (52), wherein the first material (42) is disposed at and proximate to a center portion (44) of the disk shaped component (40) and the second material (52) is disposed at and proximate to a rim of the disk shaped component (40). The first material (42) comprises a first coefficient of thermal expansion, a first stress value and a first oxidation resistance, and the second material (52) comprises a second coefficient of thermal expansion, a second stress value and a second oxidation resistance. The first coefficient of thermal expansion is greater than the second coefficient of thermal expansion, the first stress value is greater than the second stress value and the first oxidation resistance is less than the second oxidation resistance.
申请公布号 EP2090752(A2) 申请公布日期 2009.08.19
申请号 EP20090250345 申请日期 2009.02.11
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 SHI, JUN
分类号 F01D5/04;B22F5/00;B22F5/10;B23P15/00;F01D5/28;F01D5/34;F04D29/02 主分类号 F01D5/04
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