发明名称 Tip seal and anti-contamination arrangement for air-cooled turbine blades
摘要 A cavity 36 judiciously dimensioned and located adjacent a blade tip's surface discharge port 30 of an internal cooling passage of the blade airfoil extends from the pressure surface (18) (Figs. 1 and 2) to the back wall of the discharge port and guards against the contamination and plugging of the discharge port. A plurality of cavities may be associated with a plurality of ports (Fig. 2) and the cavities may vary in depth (Fig. 4). <IMAGE>
申请公布号 GB2291935(A) 申请公布日期 1996.02.07
申请号 GB19940015591 申请日期 1994.08.02
申请人 * UNITED TECHNOLOGIES CORPORATION 发明人 ROBERT J * KILDEA
分类号 F01D5/18;F01D5/20;F01D11/10;(IPC1-7):F01D5/18;B23P15/02 主分类号 F01D5/18
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