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Turbine nozzle segment, method of repairing a such nozzle segment and replacement casting for use in repairing the turbine nozzle segments

机译:涡轮喷嘴段,修复这种喷嘴段的方法以及用于修复涡轮喷嘴段的替换铸件

摘要

A method for repairing a turbine nozzle segment (10) having at least one vane (34) disposed between outer and inner bands (14,16) includes separating the inner band (16) from the nozzle segment (10), and joining the inner band (16) 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 (38) is joined to the inner band (16) and has a slot (42) formed therein. The boss (46) is then inserted into the slot (42), and the mounting platform (44) is received in a recess (40) formed in the inner band (16). Joining is completed by joining the boss (46) to the collar (38) and the mounting platform (44) to the inner band (16). IMAGE
机译:一种用于修理涡轮喷嘴段(10)的方法,该涡轮喷嘴段(10)具有布置在外带和内带(14,16)之间的至少一个叶片(34),该方法包括将内带(16)与喷嘴段(10)分开,并将内部带(16)连接起来。带(16)到具有外带(32)和至少一个叶片(34)的新制造的替换铸件(30)。替换铸件(30)包括形成在叶片(34)的一端上的安装平台(44)和形成在安装平台(44)上的凸台(46)。轴环(38)连接到内带(16)并具有形成在其中的狭槽(42)。然后将凸台(46)插入狭槽(42)中,并且将安装平台(44)容纳在形成于内带(16)中的凹部(40)中。通过将凸台(46)连接到轴环(38)和将安装平台(44)连接到内带(16)来完成连接。 <图像>

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