发明名称 High temperature airfoil
摘要 A high temperature repairable airfoil having a plurality of flow path cover tiles coupled to a single crystal spar member. In one embodiment, the plurality of flow path cover tiles include an attachment portion that is received within a groove formed in the outer surface of the spar. The attachment portion slides into a retaining feature within the groove so as to limit movement of the plurality of flow path cover tiles. Upon rotation of the airfoil, the plurality of flow path cover tiles become centrifugally loaded with a portion of the spar member. In one embodiment, the plurality of flow path cover tiles are formed of a material selected from the group consisting of ceramics, intermetallic, and thermal barrier coated single crystal alloy material.
申请公布号 US6224339(B1) 申请公布日期 2001.05.01
申请号 US19980111651 申请日期 1998.07.08
申请人 ALLISON ADVANCED DEVELOPMENT COMPANY 发明人 RHODES JEFFREY F.;HARVEY JON D.
分类号 F01D5/18;F01D5/28;F01D5/30;(IPC1-7):F01D5/18 主分类号 F01D5/18
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