Method for heating components
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.
1. A method of processing a structural component, comprising:
a) providing a structural component that has a processing area which is to be processed;
b) producing plural energy beams respectively individually from plural laser sources;
c) heating the processing area of the structural component by directing the plural energy beams respectively from the plural laser sources onto the processing area while the laser sources remain stationary relative to the processing area of the structural component, whereby the plural energy beams respectively individually form plural energy spots at respective locations on the processing area and the energy spots heat the processing area of the structural component, and wherein during the heating each respective one of the energy spots respectively remains stationary relative to the processing area;
d) respectively individually measuring the heating that is respectively caused by each respective one of the energy spots at the respective locations on the processing area by respectively individually measuring respective actual measured temperature values at the respective locations on the processing area using plural temperature measuring devices that are respectively individually allocated to the plural laser sources;
e) respectively individually controlling the plural laser sources in response to the respective actual measured temperature values; and
f) performing a mechanical processing, distinct from and in addition to the heating, on the processing area of the structural component, at a time that is at least one of before or during or after the heating.
2. The method according to claim 1 , wherein the mechanical processing comprises mechanically machining the processing area.
3. The method according to claim 1 , wherein the mechanical processing comprises deposit welding on the processing area, which is performed during or after the heating when the processing area has thereby been heated to and is at a process temperature required by the deposit welding.
4. The method according to claim 1 , wherein the energy spots do not overlap one another.
5. The method according to claim 4 , wherein the energy spots are respectively spaced apart from one another with spacing distances therebetween.
6. The method according to claim 1 , further comprising providing rated temperature values that are respectively individually allocated to the locations on the processing area, and respectively individually comparing the actual measured temperature values with the rated temperature values to produce respective individual comparison results that are respectively allocated to the laser sources, and wherein the controlling of the laser sources comprises respectively individually controlling the respective output power of the laser sources respectively individually in response to the comparison results that are respectively allocated to the laser sources.
7. The method according to claim 6 , wherein the controlling of the output power comprises individually controlling individual output power values of the energy beams dependent on the comparison results so as to respectively individually adjust the actual measured temperature value toward or to the rated temperature value respectively individually for each respective one of the energy spots.
8. The method according to claim 6 , further comprising producing a varying profile of the output power values allocated to the respective locations on the processing area dependent on a varying cross-sectional profile of the structural component along the processing area.
9. The method of claim 1 , wherein the locations are sufficiently close to one another and the controlling is performed so that the heating of the processing area by the plural energy spots produces a homogeneous heating over an entirety of the processing area.
10. The method of claim 1 , wherein the mechanical processing is performed before the heating.
11. The method of claim 1 , wherein the mechanical processing is performed after the heating.
12. The method of claim 1 , wherein the mechanical processing is performed during the heating.
13. The method of claim 1 , wherein the structural component is a structural component of a gas turbine.