发明名称 METHOD FOR PRODUCING A TURBINE BLADE
摘要 The turbine blade (1) has internal cooling channels (12), each provided with a throttle device (11) for regulating the flow of the cooling gas. The latter is fed between the foot and head regions of each turbine blade, before the cooling gas is discharged via openings (8) in the surface of the blade, with the throttle device positioned at the rear end of the flow path, adjacent the discharge openings. The throttle device may be provided at the last deflection point (13) for the cooling gas flow direction before the discharge openings.
申请公布号 EP1228293(A1) 申请公布日期 2002.08.07
申请号 EP20000969567 申请日期 2000.10.30
申请人 SIEMENS AKTIENGESELLSCHAFT 发明人 ANDING, DIRK;SCHEURLEN, MICHAEL;TIEMANN, PETER
分类号 F01D9/02;F01D5/18;F02C7/00;F02C7/18 主分类号 F01D9/02
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