发明名称 Internally cooled airfoil
摘要 The flow of cooling fluid through a core tie hole (142) formed between a pair of internal cooling passageways (124,132) of an airfoil component (110) is reduced by providing a restriction that meters coolant flow through the inlet passage (150) of one of the passageways (132) so that the pressures in the two passageways (124,132) are equalized, thereby minimizing the flow of cooling fluid through the hole (142). The restriction can be a metering plate (152) disposed at the entrance of the inlet passage (150) or a restriction integrally formed in the inlet passage . <IMAGE>
申请公布号 EP1070829(A2) 申请公布日期 2001.01.24
申请号 EP20000306185 申请日期 2000.07.20
申请人 GENERAL ELECTRIC COMPANY 发明人 WEBB, ALAN LIONEL;ISBURGH, ANNE MARIE
分类号 F01D5/18 主分类号 F01D5/18
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