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>
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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 |
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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