Methods of using laser optical devices
View Patent ↗In a method of spatially detecting the chemical composition of nonmetallic components on a surface which is subsequently to be coated with a metallic and/or ceramic and/or organic layer, a laser optical device is provided. The turbine part is irradiated with monochromatic irradiation at a first wavelength (λ in ) with the laser optical device. Radiation is detected which is emitted by the surface at a second wavelength (λ out ) which is longer than the first wavelength (λ in ).
1. A method of spatially detecting the chemical composition of nonmetallic components on a surface which is subsequently to be coated with a metallic and/or ceramic and/or organic layer, the method comprising:
providing a laser optical device;
irradiating the surface with monochromatic irradiation at a first wavelength (λ in ) with said laser optical device;
detecting radiation emitted by said surface at a second wavelength (λ out ) which is longer than the first wavelength (λ in ) with a detector such that the laser optical device and the detector are maintained at a targeted spatial position; and
determining, based on said detecting, a spatial position of said nonmetallic components relative to at least one of said laser optical device and said detector.
2. The method as claimed in claim 1 , wherein providing comprises providing a Raman spectrometer.
3. The method as claimed in claim 2 , wherein detecting comprises determining organic and/or inorganic contaminations and/or residues on said surface with said Raman spectrometer.
4. The method as claimed in claim 1 , wherein providing comprises providing a fluorescence spectrometer.
5. The method as claimed in claim 4 , wherein detecting comprises determining the presence of aluminum oxide on the surface with said fluorescence spectrometer.
6. The method as claimed in claim 1 , wherein providing comprises providing a Raman spectrometer and a fluorescence spectrometer.
7. The method as claimed in claim 6 , wherein detecting comprises determining the presence of aluminum oxide on the surface with said fluorescence spectrometer.
8. The method as claimed in claim 1 , wherein irradiating comprises systematically guiding the laser optical device over the surface, and further comprising:
processing correspondingly spatially resolved data from said detecting to form a surface image.
9. The method as claimed in claim 8 , wherein processing comprises processing data from a Raman spectrometer and from a fluorescence spectrometer, or from a combined Raman/fluorescence spectrometer, in a combined way to form a surface image.
10. The method as claimed in claim 1 , wherein:
irradiating comprises directing input radiation onto an area having a length in the range of 10-100 μm each spatial direction; and
detecting comprises collimating and analyzing radiation emitted by the surface with respect to the frequencies and/or intensities contained in said radiation, in order to generate a surface image.
11. The method as claimed in claim 1 , wherein:
irradiating comprises defocusing said monochromatic irradiation onto an area having a length in the range of 1-20 mm in each spatial direction; and
detecting comprises collimating and analyzing radiation emitted by the surface with respect to the frequencies and/or intensities contained in said radiation, in order to generate a surface image.
12. The method as claimed in claim 1 , wherein:
said laser optical device comprises at least one optical fiber; and
said irradiating, said detecting, or both are carried out with said least one optical fiber.
13. The method as claimed in claim 12 , wherein the same optical fiber is used for said irradiating and said detecting.
14. The method as claimed in claim 1 , wherein the surface comprises the surface of a turbine part.
15. The method as claimed in claim 1 , wherein the surface comprises the surface of a gas turbine part made of a metallic material.
16. The method as claimed in claim 1 , wherein the surface comprises the surface of a gas turbine part made of a refractory material.
17. The method as claimed in claim 16 , in which said gas turbine part has previously been cast or forged, and wherein the refractory material has previously undergone a surface treatment selected from the group consisting of sandblasting, washing, etching, plasma treatment, coating, and combinations thereof.