发明名称 Stationary blade of integrated segment construction and manufacturing method therefor
摘要 The present invention provides a stationary blade of integrated segment construction, in which a thermal barrier coating can be applied to the whole blade surface and excessive stress can be avoided in a shroud. A plate seat connector is provided at each end face portion of an inside shroud and an outside shroud attached to outside and inside ends of gas turbine stationary blade. Several stationary blades are integrated by joining the plate seat connectors of the adjacent shrouds by means of bolts and nuts to provide a stationary blade of integrated segment construction.
申请公布号 US6261058(B1) 申请公布日期 2001.07.17
申请号 US19990414394 申请日期 1999.10.07
申请人 MITSUBISHI HEAVY INDUSTRIES, LTD. 发明人 KATAOKA MASAHITO;TERAZAKI MASAO;HASHIMOTO YUKIHIRO
分类号 F01D5/28;F01D9/04;(IPC1-7):F01D9/00 主分类号 F01D5/28
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