发明名称 TURBINE NOZZLE SEGMENT
摘要 PROBLEM TO BE SOLVED: To improve the mounting operation efficiency of a turbine nozzle 5 by suppressing the shaking of turbine nozzle segments 1 with respect to a fixture 31 even if outer channel members 19 are made substantially parallel to the blade spans. SOLUTION: A turbine nozzle segment comprises a plurality of stationary blades 7, an arcuate inner band 9 integrally formed with the blades 7 inside the same, and an arcuate outer band 11 integrally formed with the blades 7 outside the same. The outer band 11 comprises an outer channel member 19, a front outer rim 21, a rear outer rim 23, and a hooking member 29 formed at the center of the arcuate rear end of the outer channel member 19. COPYRIGHT: (C)2005,JPO&NCIPI
申请公布号 JP2004324614(A) 申请公布日期 2004.11.18
申请号 JP20030123923 申请日期 2003.04.28
申请人 ISHIKAWAJIMA HARIMA HEAVY IND CO LTD 发明人 TSURU ATSUSHI;NISHIMURA KEIJI
分类号 F01D9/02;B63H1/20;F01D9/00;F01D25/24;F01D25/28;(IPC1-7):F01D9/02 主分类号 F01D9/02
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