发明名称 TURBINE BLADE AND GAS TURBINE
摘要 A turbine blade includes: a base portion fixed to a rotor; a platform that is fixed to the base portion and includes a cooling flow channel; a blade shape portion that extends from the platform to an outer side in a radial direction; and a fillet portion provided in a joint surface between the blade shape portion and the platform, and the turbine blade further includes: a main pipe that is branched off from the cooling flow channel and has an opening at a side end portion of the platform; and a branch pipe that is branched off from the main pipe, extends along the fillet portion so as to be close thereto on an inner side in the radial direction, and includes a film cooling hole opened on a surface of the platform.
申请公布号 US2012263603(A1) 申请公布日期 2012.10.18
申请号 US201113307675 申请日期 2011.11.30
申请人 HADA SATOSHI;MITSUBISHI HEAVY INDUSTRIES, LTD. 发明人 HADA SATOSHI
分类号 F01D5/18 主分类号 F01D5/18
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