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    • 2. 发明公开
    • Method of repairing turbine blades
    • Verfahren zum Reparieren von Turbinenschaufeln。
    • EP0303433A2
    • 1989-02-15
    • EP88307333.0
    • 1988-08-08
    • REFURBISHED TURBINE COMPONENTS LIMITED
    • Fraser, Michael James
    • B23P6/00
    • B23P6/005B23P15/04F01D5/005Y10T29/49318Y10T29/4973Y10T29/49737Y10T29/49742
    • A method of repairing a turbine blade (11) of the type forming part of an array of turbine blades (10) which are provided with tennons (15) at their outer ends, which tennons engage with a circumferential shroud (23). The repair steps involve the removal of the old damaged tennon and end of the blade, which may or may not be damaged, and replacement by a new part (27) which includes a new tennon (28) and a blade part (29) and locating the new part relative to at least one adjacent blade (12) and securing the new tennon and blade part to the blade being repaired while it is in its located position. The repair ensures that any area of weakness, i.e. where the joint has been made, is removed from the area most prone to damage, the root of the tennon, and the location means (35) ensures that the new part can be properly located.
    • 一种修复涡轮机叶片(10)阵列的类型的涡轮机叶片(11)的方法,涡轮机叶片(10)在其外端处设有天线(15),其与天线罩(23)接合。 修理步骤涉及去除可能损坏的或可能不会损坏的旧损坏的天on杆和刀片末端,以及由新的部件(28)和刀片部件(29)的新部件(27)的更换,以及 将新部件相对于至少一个相邻的刀片(12)定位,并且将新的定影器和刀片部件固定在被修复的刀片上,同时处于其定位位置。 修理确保了任何弱点区域,即关节已被制造的地方,从最容易损坏的区域,地铁的根部和位置装置(35)被移除,确保了新部件能够正确定位。