首页> 外国专利> Connecting metallic structural elements such as turbine blade and turbine blade head of gas turbine, comprises inserting filling material or mass into cavity of the elements, and then connecting by inductive high-frequency pressure welding

Connecting metallic structural elements such as turbine blade and turbine blade head of gas turbine, comprises inserting filling material or mass into cavity of the elements, and then connecting by inductive high-frequency pressure welding

机译:连接诸如燃气轮机的涡轮叶片和涡轮叶片头之类的金属结构元件,包括将填充材料或团块插入元件的腔中,然后通过感应高频压力焊接进行连接

摘要

The process for connecting metallic structural elements (12, 14) such as turbine blade and turbine blade head for a component of a gas turbine, comprises inserting or filling a preformed filling material (18) or a filling mass into a cavity (16) of the elements, connecting corresponding connecting surfaces (20, 22) of the elements by inductive high-frequency pressure welding, and mechanically removing the filling material or the filling mass by ultrasonic or chemical. The material of the filling material or the filling mass is temperature stable for the period of connection of the elements. The process for connecting metallic structural elements (12, 14) such as turbine blade and turbine blade head for a component of a gas turbine, comprises inserting or filling a preformed filling material (18) or a filling mass into a cavity (16) of the elements, connecting corresponding connecting surfaces (20, 22) of the elements by inductive high-frequency pressure welding, and mechanically removing the filling material or the filling mass by ultrasonic or chemical. The material of the filling material or the filling mass is temperature stable for the period of connection of the elements. The filling material or the filling mass projects over the connecting surface of the first or second element. The connecting surfaces of the respective element are beveled before the connecting process. The filling material or the filling mass consists of ceramic, glass, metal, a metal alloy or polystyrene. An independent claim is included for a filling material or filling mass useful for connecting metallic elements.
机译:连接诸如燃气轮机部件的涡轮叶片和涡轮叶片头之类的金属结构元件(12、14)的过程,包括将预制的填充材料(18)或填充物料插入或填充到容器的空腔(16)中。元件,通过感应高频压力焊接连接元件的相应连接表面(20、22),并通过超声或化学方法机械地去除填充材料或填充物。填充材料的材料或填充物质在元件的连接期间是温度稳定的。连接诸如燃气轮机部件的涡轮叶片和涡轮叶片头之类的金属结构元件(12、14)的过程,包括将预制的填充材料(18)或填充物料插入或填充到容器的空腔(16)中。元件,通过感应高频压力焊接连接元件的相应连接表面(20、22),并通过超声或化学方法机械地去除填充材料或填充物。填充材料的材料或填充物质在元件的连接期间是温度稳定的。填充材料或填充物突出在第一或第二元件的连接表面上。在连接过程之前,将各个元件的连接表面切成斜面。填充材料或填充物由陶瓷,玻璃,金属,金属合金或聚苯乙烯组成。对于用于连接金属元件的填充材料或填充物料包括独立权利要求。

著录项

  • 公开/公告号DE102007023150A1

    专利类型

  • 公开/公告日2008-11-27

    原文格式PDF

  • 申请/专利权人 MTU AERO ENGINES GMBH;

    申请/专利号DE20071023150

  • 发明设计人 NENOV CHRIS;KRIEGL BERND;MEIER REINHOLD;

    申请日2007-05-16

  • 分类号B23K13/01;B23P15/04;F01D5/12;

  • 国家 DE

  • 入库时间 2022-08-21 19:09:51

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