发明名称 Method for heating components
摘要 A processing area of a structural component, such as a gas turbine component, is heated by irradiation with several laser sources prior to and/or during and/or after carrying out a processing such as a deposit welding or machining of the component on the processing area. For the heating, each laser source directs a respective energy beam onto the processing area, which respectively produces an energy spot on the processing area. The respective positions of the energy spots are static or quasi-static on the processing area. The energy spots jointly heat the processing area.
申请公布号 US8124912(B2) 申请公布日期 2012.02.28
申请号 US20040585435 申请日期 2004.12.11
申请人 BAYER ERWIN;BECKER WOLFGANG;STIMPER BERND;MTU AERO ENGINES GMBH 发明人 BAYER ERWIN;BECKER WOLFGANG;STIMPER BERND
分类号 B23K26/00;C21D1/34;H05B3/00 主分类号 B23K26/00
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