发明名称 TURBINE BLADE
摘要 The amount of cooling air (cooling medium) can be reduced, and low-temperature cooling air is prevented from being blown out through film cooling holes. Part of a cooling medium impingement-cooling an inner circumferential surface (17) of a blade main body (11) located on a ventral side further impingement-cools the inner circumferential surface (17) of the blade main body (11) located on a dorsal side and is blown out through film cooling holes (13) in the blade main body (11) that are located on the dorsal side.
申请公布号 EP2351909(B1) 申请公布日期 2016.10.19
申请号 EP20080877979 申请日期 2008.11.07
申请人 MITSUBISHI HITACHI POWER SYSTEMS, LTD. 发明人 HADA, SATOSHI;HASHIMOTO, TOMOKO;YURI, MASANORI;KUWABARA, MASAMITSU
分类号 F01D9/02;F01D5/18 主分类号 F01D9/02
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