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    • 4. 发明公开
    • VERFAHREN ZUM HERSTELLEN ODER REPARIEREN VON INTEGRAL BESCHAUFELTEN GASTURBINENROTOREN
    • EP2352615A1
    • 2011-08-10
    • EP09771683.1
    • 2009-11-05
    • MTU Aero Engines GmbH
    • RICHTER, Karl-Hermann
    • B23K13/01B23K20/12
    • B23K13/015B23K20/1205B23K20/129B23K2201/001Y10T29/49318Y10T29/4932Y10T29/49325
    • The invention relates to a method for producing integrally bladed gas turbine rotors, especially of integrally bladed turbine rotors. According to said method, rotating vanes (10) are joined to a rotor base (11) while interposing an adapter (14) in such a manner that first an adapter is joined to a connecting section (15) of every rotating vane to be connected to the rotor base and then every rotating vane (10) is joined to a connecting section (16) of the rotor base (11) via the adapter (14) connected to said rotating vane. The invention is characterized in that every adapter (14) is connected to the connecting section (15) of the respective rotating vane (10) by welding, every rotating (10) vane being connected to the respective connecting section of the rotor base by inductive HF pressure welding via the adapter (14) connected to said rotating vane.
    • 本发明涉及一种用于制造整体叶片式燃气轮机转子的方法,特别是整体叶片式涡轮转子,其中旋转叶片(10)以这种方式与转子基座(11)接合,中间处理适配器(14) 首先将适配器连接到每个旋转叶片的连接部分(15)以连接到转子基座,并且随后每个旋转叶片(10)经由转子基座(11)的连接部分(16)经由 连接到所述刀片的适配器(14)。 根据本发明,每个适配器14通过焊接连接到相应的旋转叶片10的连接部分15,每个旋转叶片10都通过感应高速连接到转子底座的相应的连接部分, 通过连接到叶片的适配器(14)进行频率压力焊接。