发明名称 Cooled rotor blade for a gas turbine
摘要 The hollow interior of the blade is lined with a hollow insert and ribs to define a plurality of flow passages of narrow cross-section which connect a cooling-air chamber in the blade root with a cooling-air chamber in the blade tip. The chamber in the blade tip communicates with the interior of the insert and orifices are formed in the insert to exhaust air via a perforated partition through the trailing edge of the blade. The hollow insert is anchored in the blade root in various manners.
申请公布号 US4019831(A) 申请公布日期 1977.04.26
申请号 US19750608754 申请日期 1975.08.28
申请人 BROWN BOVERI SULZER TURBOMACHINERY LTD. 发明人 FRANKLIN, CLIFFORD JOHN;MELLIGER, HANS
分类号 F01D5/18;F02C7/18;(IPC1-7):F01D5/18 主分类号 F01D5/18
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