发明名称 Cooled rotor-blade for gas-turbine
摘要 A passage in the body of the rotor blade (1) runs between an inlet (4a) and an outlet (4b) in the blade root (2). The steam passing through is collected, and a bypass (7) is provided in one at least of the partitions (31) between the sections of the passage. This bypass is situated near the blade root. At the rear side of the blade a reinforcing rib (8) can be provided, dividing the passage into two or more sections.
申请公布号 DE19814680(A1) 申请公布日期 1998.10.15
申请号 DE1998114680 申请日期 1998.04.01
申请人 MITSUBISHI HEAVY INDUSTRIES, LTD., TOKIO/TOKYO, JP 发明人 TOMITA, YASUOKI, TAKASAGO, HYOGO, JP;FUKUNO, HIROKI, TAKASAGO, HYOGO, JP;SUENAGA, KIYOSHI, TAKASAGO, HYOGO, JP
分类号 F01D5/18;F02C7/18;(IPC1-7):F01D5/18 主分类号 F01D5/18
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