发明名称 Trailing edge cooling for gas turbine airfoils
摘要 <p>A hollow airfoil has a pressure side wall 12, a suction side wall 14, a cavity 16 formed between the pressure and suction side walls, a plurality of cooling ports 18 disposed within the pressure side wall 12, and a plurality of passages 42, each extending between the cavity 16 and one of the cooling ports 18. Each passage 42 has a first wall 54 adjacent the suction side wall 14, a pair of passage 58 side walls extending substantially toward the pressure side wall 12, and a second wall 56 adjacent the pressure side wall 12. Each passage further includes a pair of fillets 60,62 extending between the passage side walls 58 and the second wall 56. Alternatively, or in addition, each passage 42 includes a jog adjacent each cooling port 18 so as to extend parallel to the pressure side wall 12. &lt;IMAGE&gt;</p>
申请公布号 EP0916809(A2) 申请公布日期 1999.05.19
申请号 EP19980309323 申请日期 1998.11.13
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 PRZIREMBEL, HANS R.;SOECHTING, FRIEDRICH O.
分类号 F01D5/18;F01D9/02;(IPC1-7):F01D5/18 主分类号 F01D5/18
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