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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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