发明名称 Método para o reparo de um segmento de bocal de turbina
摘要 <p>A method for repairing a turbine nozzle segment having at least one vane disposed between outer and inner bands includes separating the inner band from the nozzle segment, and joining the inner band to a newly manufactured replacement casting (30) having an outer band (32) and at least one vane (34). The replacement casting (30) includes a mounting platform (44) formed on one end of the vane (34) and a boss (46) formed on the mounting platform (44). A collar is joined to the inner band and has a slot formed therein. The boss (46) is then inserted into the slot, and the mounting platform (44) is received in a recess formed in the inner band. Joining is completed by joining the boss (46) to the collar and the mounting platform (44) to the inner band. The thickness of the collar is tapered in an axial direction, and a relief is formed in the collar to provide assembly clearance with adjacent components. <IMAGE></p>
申请公布号 BRPI0305595(B1) 申请公布日期 2015.05.12
申请号 BR2003PI05595 申请日期 2003.11.14
申请人 GENERAL ELECTRIC COMPANY 发明人 JAMES WALTER CADDELL;MATTHEW NICKLUS MILLER;BRIAN ALAN NORTON
分类号 B23P15/04;F01D9/04;B23P6/00;F01D5/00;F01D25/00;F02C7/00 主分类号 B23P15/04
代理机构 代理人
主权项
地址