发明名称 Gas turbine moving blade
摘要 A gas turbine moving blade in which the moving blade operating in a high temperature operating gas is cooled from its interior by steam and the steam after being used for the cooling is recovered, by use of a simple structure. A supply side passage (10), through which steam (6) is supplied directly into a cooling passage (51) of a blade leading edge side (11), is provided within a blade root portion (2) and a pocket (19). One end of the pocket is connected to the supply side passage and the other end of which is connected to a cooling passage (52) of a blade trailing edge side (12). The pocket is covered with a plate, which extends in a blade chord direction on an outer peripheral side face of the blade root portion between a blade platform and a rotor plate. Thus, efficiency of the gas turbine can be effectively enhanced.
申请公布号 US5915923(A) 申请公布日期 1999.06.29
申请号 US19970861753 申请日期 1997.05.22
申请人 MITSUBISHI HEAVY INDUSTRIES, LTD. 发明人 TOMITA, YASUOKI;ICHIRYU, TAKU;SUENAGA, KIYOSHI
分类号 F01D5/18;(IPC1-7):F16D5/18 主分类号 F01D5/18
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