Lighthouse scanner with a rotating mirror and a circular ring target

Abstract

The present invention introduces a scanning arrangement and a method suitable for coating processes applying laser ablation. The arrangement is suited to prolonged, industrial processes. The arrangement comprises a target, which has an annular form. The laser beam direction is controlled by a rotating mirror locating along the center axis of the annular target. The scanning line will rotate circularly along the inner target surface when the mirror rotates. The focal point of the laser beams may be arranged to locate on the inner target surface to ensure a constant spot size. A ring-formed, a cylinder-shaped or a cut conical-shaped target may be used. The inner surface of the target may thus be tapered in order to control the release direction of the ablated material towards a substrate to be coated.

Claims

1. A scanning arrangement for a thin film forming apparatus applying laser ablation, wherein the scanning arrangement comprises: a rotatable mirror for redirecting an input laser beam to a substantially circular scanning pattern around a rotation axis of the rotatable mirror, which axis is substantially parallel with the direction of the input laser beam; an annularly formed target, where the center point of the target is positioned along the axis of rotation of the rotatable mirror, and where the reflected laser beam makes contact with the surface of the annular target in order to release target material along the substantially circular scanning pattern; and a chamber having capabilities to control at least the pressure, the temperature and possible additional materials present within the chamber, and wherein the rotatable mirror, the annular target and a substrate locate within the chamber.

2. The arrangement according to claim 1, wherein the arrangement further comprises: a laser source; and optical means for manipulating a laser beam created by the laser source.

3. A thin film forming apparatus comprising the scanning arrangement according to claim 1 wherein the apparatus further comprises: a substrate to be coated with the released target material.

4. The arrangement according to claim 2, wherein the arrangement comprises control means controlling the laser source, the optical means and the rotation of the mirror in a desired manner.

5. The arrangement according to claim 1, wherein the inner surface of the annular target is tapered.

6. The arrangement according to claim 1, wherein the rotating motion is coupled to the mirror with a hollow tube through which the input laser beam can be guided to the mirror.

7. The arrangement according to claim 1, wherein the rotating mirror has multiple facets.

8. The arrangement according to claim 7, wherein the rotating multi-faceted mirror is coupled to a rotating diffractive optical element producing multiple laser beams from a single input laser beam, with the axis of rotation substantially parallel with the direction of the input laser beam.

9. The arrangement according to claim 2, wherein the optical means comprise a rotating optical element configured to change polarization of the input laser beam, where the rotating optical element is synchronized with the rotation of the mirror.

10. The arrangement according to claim 2, wherein the optical means further comprise means configured to manipulate the spatial intensity distribution of the input laser beam.

11. The arrangement according to claim 2, wherein the laser source outputs laser pulses.

12. The arrangement according to claim 11, wherein the laser pulses hitting the target surface are P-polarized, S-polarized or elliptically polarized.

13. The arrangement according to claim 1, wherein the diameter of the annular target and the rotation speed of the mirror are selected such that the speed of the scanned laser spot on the target is at least 1 m/s.

14. The arrangement according to claim 1, wherein the diameter of the annular target and the rotation speed of the mirror are selected such that the speed of the scanned laser spot on the target is at least 10 m/s.

15. The arrangement according to claim 1, wherein the diameter of the annular target and the rotation speed of the mirror are selected such that the speed of the scanned laser spot on the target is at least 100 m/s.

16. The arrangement according to claim 1, wherein the angle of the rotatable mirror changes with respect to the input laser beam during the scan.

17. The arrangement according to claim 11, wherein the energy of the laser pulses can be controlled in synchronization with the rotation of the mirror.

18. The arrangement according to claim 1, wherein the annular target is movable along its central axis.

19. The arrangement according to claim 1, wherein the annular target is rotated around its central axis in the opposite direction compared to the rotation of the mirror.

20. The arrangement according to claim 19, wherein the rotation speed of the annular target is between 0.01 and 100 000 rpm.

21. The arrangement according to claim 2, wherein the optical means is a focusing lens.

22. The arrangement according to claim 21, wherein the focusing lens is moved along the laser beam.

23. The arrangement according to claim 22, wherein the focusing lens is moved along the laser beam in synchronization with a linear movement of the target.

24. The arrangement according to claim 1, wherein the annular target is made of metal, metal compound, glass, stone, ceramics, synthetic polymer, semisynthetic polymer, natural polymer, composite material, inorganic or organic monomeric or oligomeric material.

25. The arrangement according to claim 1, wherein the annular target is composed of annular segments of at least two different materials.

26. The arrangement according to claim 1, wherein the reflectivity of the mirror is preserved throughout the process by: static mechanical shields; and/or moving shields, tubes or apertures; and/or electrical means; and/or magnetic means; and/or heating of the mirror; and/or pressure control around the mirror; and/or gas flow; and/or laser cleaning; and/or ion bombardment; and/or sacrificial layers between the target and the mirror.

27. The arrangement according to claim 1, wherein the annularly formed target has a ring shape, a cylinder shape or a truncated conical shape.

28. A laser ablation and deposition method for coating a substrate with one or more coating materials, the method comprising the steps of: creating a laser beam in a laser source; manipulating the laser beam by optical means, wherein the method also comprises the steps of: directing an input laser beam to a rotatable mirror rotating around an axis substantially parallel with the input laser beam direction, thus producing a substantially circular scanning pattern around the axis of rotation of the mirror; directing the reflected laser beam onto the surface of an annular target, where the center point of the target is positioned along the axis of rotation of the rotatable mirror, and wherein coating material is released from the target along the substantially circular scanning pattern as a material plume; and directing the released material plume onto the substrate to obtain a coated substrate, wherein the laser ablation and deposition of the released target material is performed in a chamber, wherein the rotatable mirror, the annular target and the substrate locate within the chamber, and the chamber has capabilities to control at least the pressure, the temperature and possible additional materials present within the chamber.

29. The method according to claim 28, wherein the method comprises: holding the substrate to be coated at a selected distance and angle from the annular target, the substrate locating on an opposite side of the target compared to the incoming laser beam.

30. The method according to claim 28, wherein the method comprises: moving and/or rotating the substrate in the material plume released from the surface of the annular target.

31. The method according to claim 28, wherein the chamber is provided with a controlled flow of background gas in a controlled pressure during the laser ablation and deposition, wherein the background gas is inert or reactive.

32. The method according to claim 28, wherein the ablated released material is influenced by an electric field or by a magnetic field or by both.

33. The method according to claim 28, wherein the deposition process is influenced by ion bombardment from an ion source.

34. The method according to claim 28, wherein the substrate is electrically biased.

35. The method according to claim 28, wherein a physical mask is placed between the target and the substrate.

36. The method according to claim 35, wherein the physical mask is configured to move during the process.

37. The method according to claim 36, wherein the physical mask is configured to rotate synchronically with the rotation of the mirror.

38. The method according to claim 30, wherein the substrate forms a planar and bendable sheet, and the substrate is further configured to be released to the deposition area from a first roll and collected to a second roll after the deposition.

39. (canceled)

40. The method according to claim 28, wherein the angle between the input and reflected laser beams is α, where 0<α<180°.

41. The method according to claim 28, wherein the angle between the input and reflected laser beams is substantially equal to 90°.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0023] FIG. 1 illustrates the coating process applying the pulsed laser deposition (PLD) in general,

[0024] FIG. 2 illustrates an example of a turbine scanner which may be used in generating desired kinds of laser pulses or laser pulse fronts,

[0025] FIG. 3 illustrates an embodiment of the annular form of the target according to the invention, which target is usable in pulsed laser deposition processes,

[0026] FIG. 4 illustrates a cross-sectional, direct side view of the scanning arrangement according to an embodiment of the invention, and

[0027] FIG. 5 illustrates an example of a protective enclosure around the rotating mirror.

DETAILED DESCRIPTION OF THE INVENTION

[0028] The present invention introduces a laser ablation and deposition arrangement and method comprising a scanning arrangement and method for a thin film forming apparatus comprising a rotating mirror and a circularly shaped target, resulting in a lighthouse-type of a scanning device. The circularly shaped target may be a ring-formed or a cylindrically formed target, i.e. its cross-section on the plane of the scanning beam (output beam) is substantially a circle. The arrangement is formed thus with physical components where a laser source is the energy source, the elements are controlling and interacting with the laser energy, and the released material from the target as a result of the laser beam contact will in the end form e.g. a coating on a substrate. At least the laser beam contact with the target and the material flow into the substrate will preferably be located inside a vacuum chamber, providing a controllable environment for the laser ablation. The device and the corresponding method allow coating a substrate (element, component, small or large surface or another thin film) with one or more coating materials originating from the target.

[0029] At first, we refer to FIG. 1 discussing generally the pulsed laser deposition for creating e.g. a good-quality coating on a desired surface. In this Figure, the target is simplified as a simple rectangular element for illustrative purposes only, and in the actual invention, the target is discussed in a more detailed manner.

[0030] The basic arrangement for realizing the method of the invention consists of a laser source 11, 11′, an optical path 12, 12′ to guide the laser beam (laser pulses), at least one focusing lens 14, and the ablation will take place in a vacuum chamber 18. Within the vacuum chamber 18 there is a laser beam manipulating element such as a rotating scanning mirror 13, an annular target 15 (simplified in the Figure as a rectangular target block for illustrative purposes) with mechanics capable of holding and manipulating (like e.g. moving and/or rotating) the target 15, and a substrate 17 together with the holding means and mechanics enabling the manipulation (like e.g. moving and/or rotating) of the substrate 17. Additional features in the ablation arrangement are control means 11c, 11c′ for the laser pulse control (pulse picking), optical elements for changing the properties of the laser pulses (e.g. polarization, intensity distribution, beam splitting into multiple beamlets), means to protect the rotating scanning mirror 13 from material build-up (static masks and diaphragms, dynamic masks and diaphragms (e.g. rotating with the scanning mirror), electric and/or magnetic fields, heating elements, gas flow arrangements), static and dynamic masks between the target and the substrate to selectively manipulate the flow of the ablated material both spatially and temporally. In one embodiment, the control means 11c, 11c′ may control the laser source 11, 11′ but also the optical elements such as possible movement or focusing of the lenses, and additionally the control means (or a controller) 11c, 11c′ may control the rotation of the rotating mirror 13 for directing the laser pulses towards the target contact point 15c on the annular target 15. In order words, according to an embodiment of the invention, the arrangement comprises control means controlling the laser source 11, 11′, the optical means (lenses and a possible turbine scanner) and the rotation of the mirror 13 in a desired manner. The latter includes selecting the direction and angular velocity and a possible scanning line pattern with the rotatable mirror 13.

[0031] In the context of the description and the claims, the at least one focusing lens 14 and a possible turbine scanner 21, 22 (see the description of FIG. 2) along with the mentioned optical elements from above, together are part the optical means specified in the claims. The optical means comprise one or more such manipulating elements for the laser beams. The focusing lens 14 or several lenses may be arranged so that the lens or lenses may be moved in the direction of the laser beam 12, 12′, i.e. along the propagating laser beam. In one embodiment, the focusing lens 14 is moved along the laser beam 12, 12′ in synchronization with a linear movement of the target 15.

[0032] The rotating mirror 13 may be a simple rectangular two-dimensional piece of plane provided with a reflecting surface facing the incoming laser pulses, and where the rectangular piece of mirror is rotatable around an obliquely locating rotation axis.

[0033] Otherwise, the rotating mirror 13 can be a cross-sectionally triangular element with mirrored outer surfaces, where the element may for instance have a pyramid form, turned around as upside down. The rotation axis of the rotating mirror 13 is substantially parallel with the direction of the input laser beam in the preferred embodiment.

[0034] The focusing lens 14 or lenses may locate anywhere along the laser pulse path 12, 12′. The lens 14 may therefore locate also between the laser source 11 (or 11′) and the mirror arrangement 13. The turbine scanner option is discussed in FIG. 2 in more detail.

[0035] In an embodiment, the optical means (or optical elements as said above) 14, 21, 22 further comprise means configured to manipulate the spatial intensity distribution of the input laser beam 12.

[0036] The laser source 11 can be a pulsed or continuous wave laser, and able to operate with laser properties and parameters suitable to the process. In a preferred embodiment of the invention, the laser source 11 produces laser pulses. In a further embodiment, the laser source 11 is able to produce pulse bursts comprising two or more laser pulses.

[0037] In one embodiment, the laser source 11 and its controller 11c is located outside the vacuum chamber 18. The laser pulses are fed inside the vacuum chamber 18 through a window 18w locating in the wall of the vacuum chamber 18. In another possible embodiment of the invention, also the laser source 11′ and the controller 11c′ are placed inside the ablation chamber 18. In this option, the laser source 11′ creating the laser pulses, the manipulating elements of the pulses, the ablation of the material 16 in the target contact point 15c of the target 15, and the substrate 17 to be coated with the released material are all placed and the method steps will therefore be implemented inside the vacuum chamber 18. The target contact point 15c will move on the inner surface of the target 15 in a desired pattern, in order to avoid steep holes to be formed on the target surface during material release process.

[0038] The arrangement comprises a capability to control at least the pressure and the temperature and possible additional materials (flowing in and/or flowing out) present within the vacuum chamber 18. In other words, the chamber 18 is provided with a controlled flow of background gas in a controlled pressure during the laser ablation and deposition. Background gas may be inert or reactive. The additional material(s) may be in gaseous form but also liquid submersion is possible for the ablation process in some useful embodiments.

[0039] FIG. 2 shows an example of a turbine scanner which can be used as an optical tool (part of the optical means) between the laser source 11, 11′ and the rotating mirror 13 (the latter is not shown in FIG. 2). The turbine scanner manipulates the incoming laser pulses into a laser pulse front which propagates on a single plane. The structure of the turbine scanner includes turning mirror surfaces 21 which can be formed as a polygon and which is rotatable around its axis. The angles between the mirror surfaces can be selected so that the resulting reflected laser pulses form a fan-shaped set of laser beams. The reflected pulses are directed to a telecentric lens 22, which in turn manipulates the incoming reflected pulses into a substantial parallel set of laser beams 23. The manipulated laser pulse front 23 may still be directed into a further lens or several lenses (not shown in FIG. 2), such as to lens 14 shown in FIG. 1, or some other lens locating before the mirror 13. Finally, the manipulated laser pulse front makes contact with the rotatable mirror 13. The operation of the turbine scanner 21, 22 may be controlled by the same controller 11c, 11c′, which has already been discussed above.

[0040] FIG. 3 shows the target 15 in more detail according to the preferred embodiment of the invention. The target is shaped in an annular form, and preferably it forms a complete circle when looked from the above as shown in FIG. 3. Actually the target 15 may form a shape of a ring, meaning a thin segment of a cylindrical wall structure. The center point of the target 15 is positioned along the axis of rotation of the rotatable mirror 13. Thus, the center point of the annular target 15 may be the same as the reflection point of the rotatable mirror 13, but the center point may also locate directly above or beneath the mirror 13, if the annular target plane is located horizontally, as shown in FIG. 3. Therefore, the reflection angle a of the laser beam in the mirror 13 may be substantially equal to 90 degrees, but in other embodiments, the reflection angle a may be freely selected from angle values fulfilling 0<α<180°. When the rotating mirror 13 (meaning its effective reflection point for the laser beams) is placed in the midpoint of the annular ring-shaped target, the distance from the reflection point to the target surface will remain constant all the time (when no wear of the target is taken into account). When the ablation process is turned on, the reflective element 13 is controlled in its first embodiment so that the reflective element is rotated in a constant angular velocity.

[0041] The result is that the laser beams 12′ will affect the inner surface of the annular target in a smooth and uniform manner. In other words, the rotating mirror functions similarly as a lighthouse, and the result is a substantially circular scanning pattern on an inner surface of the annular target.

[0042] FIG. 4 shows another kind of viewpoint of the same arrangement already shown in FIG. 3. FIG. 4 is a cross-sectional direct side view “cut” with a vertical plane locating in the middle of the arrangement. The input laser beam 12 arrives to the arrangement beneath the vacuum chamber 18. The beam 12 will travel into a hollow tube 51 or pipe where it will pass a window 18w, thus arriving into the chamber 18. The rotating mirror 13 is placed obliquely in the propagation path of the beam 12, and the rotation axis of the mirror 13 is in this picture vertically directed. The beam will reflect to a horizontal direction as beam 12′. While the mirror 13 rotates around a total circle, the respective reflected beams 12′ will together form a horizontal scanning plane. The point of contact of the reflected beam 12′ and the tapered inner surface of the annular target 15 is the spot 15c. The result of the ablation is a material plume 16, which as a result of the oblique arrival angle onto the target will point out in a tilted direction upwards. In this direction locates also the substrate 17 which is ready to receive the released particles. When the material plume 16 makes contact with the substrate 17, it will stick onto it and form a coating on it. The result is e.g. a thin film formed from the target material onto the substrate sheet or component where the coating can be produced in an industrially professional manner and speed.

[0043] FIG. 5 illustrates an example of a protective enclosure used for protecting the rotating scanning mirror 13. The upper part of FIG. 5 shows the arrangement from the above as a cross-section, and the lower part is shown as a side-view, and also as a cross-section. Such an arrangement is used to prevent target material build-up on the mirror 13. The input laser beam 12 may travel through a hollow tube 51 towards the mirror 13, wherein the input laser beam 12 direction is parallel to the axis of the hollow tube 51. The reflected beam 12′ will propagate from the mirror 13 towards the target through gaps in the protective shield structure 52. In this example, five protective wall pieces 52 are placed in a protective enclosure. Naturally, there might be some other number of protective walls, depending on the required effectiveness needed in the protection of the mirror 13. The contact point with the target will naturally locate outside the farthermost protective wall piece. The protective walls 52 are preferably formed in a circular shape, locating centrically inside the annular target. The wall pieces 52 may be fixed to the enclosure base in an opposite manner, such as shown in the figure where the first, middle and the last pieces are fixed to the top base plate 53 and the second and fourth pieces are fixed to the bottom base plate 54. The pieces fixed to the top base plate 53 have holes where the reflected laser beams 12′ can propagate through. When the mirror 13 and the hollow tube 51 rotates according to the principle of the invention, the top base plate 53 together with the first, third and fifth wall pieces rotates too. The bottom base plate 54 together with the second and fourth wall pieces will remain stationary in relation to the upper enclosure part. Furthermore, it is possible to feed gas to a selected gap between the protective walls, and correspondingly, to pump out the gas e.g. from some other gap between the protective walls. Such an exemplary rotating shield structure collects effectively the released material pointing directly or almost directly back towards the rotating mirror 13.

[0044] The effect of the scanning on the target 15 may be enhanced by rotating the annular target 15 around its central axis in the opposite direction compared to the rotation of the mirror 13. This is illustrated by the arrows in FIG. 3 and such a target rotation will increase the effective scanning spot speed on the target 15. In one embodiment, the rotation speed of the annular target 15 is selected from values between 0.01 . . . 100 000 rpm.

[0045] In an embodiment, the rotating mirror 13 has multiple facets. In a yet further embodiment, into the rotating multi-faceted mirror 13 is coupled a rotating diffractive optical element producing a rotating bundle of laser beams (beamlets) from a single input laser beam 12, with the axis of rotation along the input laser beam 12.

[0046] In yet another embodiment of the rotatable mirror 13, the mirror 13 is formed in a shape of a pyramid. When such a pyramid-type of mirror is placed upside down, and it is pointed with e.g. a circularly placed bundle of input laser beams 12, the reflecting beams 12′ will form a horizontal beam plane when the pyramid is rotated around a vertical axis. By selecting the amount of laser beams in the bundle, a possible rotation of the created bundle, together with the rotation speed of the pyramid, the resulting scanning pattern is more complex on the inner surface of the annular target 15. The material plume can be created simultaneously in e.g. 4 different locations 15c around the target if the mirror 13 is a square pyramid, if at least one laser beam of the bundle makes contact with each of the pyramid side triangles, irrespective of the mirror rotation angle. Such an embodiment makes the process even more rapid and suitable for coating a larger sheet area in a shorter time.

[0047] In creating the parallel bundle of laser pulses or beams, the earlier discussed diffractive optical element may be used. Another option is to include a turbine scanner between the laser source 11 and the rotating mirror 13. A yet another option is to have several laser sources, or other kinds of optical means which divide the single laser beam into a bundle of beams or beamlets.

[0048] With the substantially circular scanning pattern, we mean the form created together by all the contact spots 15c around the annular target 15 after the mirror arrangement has already rotated for a while at least. If the mirror is a simple 2-dimensional mirror plane rotating in an oblique angle, the reflecting beams 12′ will form a continuous circle. In case we use a pyramid type of mirror 13, together with a bundle of laser pulses incorporating parallel (e.g. a circle-shaped or square-shaped) laser beams where the center of the bundle will point at the pyramid top point now pointing directly downwards, the resulting contact points 15c will simultaneously ablate the material in four segments of the inner surface of the target 15, but the end result will be a 360 degrees coverage of contact points 15c which together form a circular scanning pattern on the cross-section of the horizontal scanning plane with the inner target surface.

[0049] Naturally, the directions of the whole arrangement can be tilted to any other appropriate angle depending on the used application. For instance, the arrangement of FIG. 4 could be turned 90 degrees clockwise, when the ring-shaped target would locate vertically and also the substrate would locate in a vertical direction. In that case the material plume would flow obliquely to the right-hand side and the incoming laser beams would be created by the laser source locating in the left-hand side of the arrangement (in case no additional mirror arrangements are used for beam redirecting).

[0050] Plasma or other material 16 is disengaged from the target when the laser pulses make contact with the target inner surface 15 along the circular scanning pattern, and the removed material will form a material cloud 16 or material plume. The plume may include plasma, particles or other kinds of target material pieces in different sizes. When the laser beams 12′ make contact along the inner circumference of the target as pointed e.g. by the arrow in FIG. 3, the created plasma cloud 16 emerges from different places along the perimeter of the circular target. When the plasma releases to an upwards direction as is shown in FIG. 3, the material flow reaching the substrate 17, will in preferred embodiment coat a much larger area of the substrate without moving the substrate at all. If the substrate 17 is moved in a desired pattern together with the depicted kind of target 15, the result is a highly industrial and scalable coating method of the substrate which coats the surfaces and elements in much higher speed than previously.

[0051] In one embodiment, the ablated released material 16 may be influenced by an electric field or by a magnetic field or by both. In another embodiment, the deposition process can be influenced by ion bombardment from an ion source. In one embodiment relating to the substrate to be coated in the deposition process, the substrate 17 can be electrically biased.

[0052] The inner surface of the annular target 15 may have a tapered shape in order to control the direction of the releasing material plume. The whole inner surface edge of the target thus may have an oblique angle. It is also possible that the inner edge of the target 15 has a zigzag-type of roughened shape, creating a non-smooth surface for the inner edge of the target 15. When the ablation process has taken place for a while, it is notable that the target wear will affect the contact surface smoothness. The present invention however enables a uniform wear pattern on the target because the scanning will happen in a similar way as the lighthouse works.

[0053] Generally regarding the ablation method and the tuning of the optical elements, the spot size of the reflected laser beam 12′ on the inner surface of the annular target 15 may be substantially the same for all rotation angles of the rotatable mirror 13, where the focal point of the reflected laser beam 12′ may locate substantially on the inner surface of the annular target 15, and where coating material 16 is released from the target 15 along the circular scanning pattern as a material plume. As a result, the released material plume 16 is directed onto the substrate 17 to obtain a coated substrate. However, this is not always the desired situation, and the spot size on the target and the focal point may also vary during the scanning process.

[0054] More specifically, the focusing lens 14 has a focal length defined by the diameter of the annular target 15 and the distance between the lens 14 and the target surface 15c. Furthermore, the focal length and positioning of the lens 14 are defined by additional beam manipulation optics, e.g. a beam shaper to change the intensity distribution of the laser spot on the target 15c, and the desired intensity distribution and spot size on the target surface 15c.

[0055] As also mentioned above, the focusing lens 14 or one lens among several applied lenses may well locate on the same plane as the annular target 15, i.e. between the rotating mirror 13 and the target contact point 15c. In such a case, lens 14, target 15 and mirror 13 all locate essentially on the same plane and the reflection angle α=90°.

[0056] In a preferred embodiment of the invention, the focusing lens 14 can be moved along the direction of the laser beams 12, 12′ to change the location of the beam waist with respect to the target surface. This feature allows maintaining the spot size accurately on the target surface 15c during the process as the target 15 wears in the ablation process along material removal 16 from the target.

[0057] In an embodiment, the optical means 14, 21, 22 comprise a rotating optical element configured to change polarization of the input laser beam 12, where the rotating optical element is synchronized to the rotation of the mirror 13.

[0058] In case the incoming laser beam 12 is static with linear polarization and the circular scanning pattern is produced by a rotating oblique mirror 13, the polarization of the scanned laser beam changes continuously throughout the rotation. The polarization affects the reflection properties of the laser on the target surface. Without corrective optics this would lead into different ablation conditions at different rotation angles of the circular scan. In a preferred embodiment of the invention, the polarization of the incoming laser beam 12 is controlled such that the laser beam hitting the surface of the target 15c is P-polarized which yields minimum reflectance, especially at the Brewster's angle. The polarization control can be realized by rotating a half-wave plate synchronized with the scanning mirror 13 rotation and having half of the speed of the scanning mirror 13 rotation speed. The polarization of the target hitting laser beam can also be S-polarized, circularly or elliptically polarized in other embodiments of the invention. An important factor is to maintain the laser-target interaction constant throughout the scanning cycle.

[0059] In an embodiment of the invention, the laser beam 12, 12′ is guided through a hollow motor spindle which produces the rotating motion of the scanning mirror 13 (similarly as described in “Howard”). In other words, the rotating motion is coupled to the mirror 13 with a hollow tube 51 through which the input laser beam 12 can be guided to the mirror 13. This structure enables a compact arrangement of the components inside the vacuum chamber 18 such that the space on the other side of the scanning plane is free for the substrate 17 movement.

[0060] Generally regarding the holding and manipulating features of the target and the substrate, the substrate to be coated may be held at a selected distance and angle from the annular target. Furthermore, the substrate preferably is located on an opposite side of the target compared to the incoming laser beam. In a further embodiment, the ablation and deposition method comprises moving or rotating the substrate in the material plume released from the surface of the annular target.

[0061] In one embodiment, the substrate may be in a form of a relatively thin, planar sheet-like of surface which may be bent and rolled as a roll without damaging the sheet. The uncoated substrate sheet may be stored around a first roll, from where it is released to the deposition area, where the substrate 17 has contact with the arriving released coating material 16. When the coating has attached on the surface of the substrate during the deposition, the coated planar substrate may be post-processed (e.g. cooled down if the processing area has been heated externally), and finally the post-processed coated substrate may be collected and rolled around a second roll for storage of the resulting product.

[0062] In one embodiment regarding the volume where the material plume 16 travels towards the substrate 17 to be coated, a physical mask can be placed between the target 15 and the substrate 17. This can be performed to create desired coating patterns on the substrate. This enables even complicated patterns and fine-tuned distributions of the coated material on the substrate. In a further embodiment of the physical mask, the physical mask is configured to move during the process. In a yet further embodiment, the physical mask is configured to rotate synchronically with the rotation of the mirror 13.

[0063] In an embodiment of the invented arrangement, the rotating obliquely angled mirror surface locates at a 45° angle compared to the input laser beam 12 direction such that the scanning plane is perpendicular to the optical axis of the input laser beam 12. In other embodiments, however, it is possible to place the mirror plane at less than 45° angle (sharp angle) to the input beam direction or at larger than 45° angle (obtuse angle) to the input beam direction. In yet another embodiment, the angle of the rotatable mirror 13 may be changed with respect to the input laser beam 12 during the scan.

[0064] The required rotation speed of the scanning mirror 13 is defined by the diameter of the annular target 15 (circumference of the ablated surface on the target which can be a dynamic value), the laser spot size along the scanning direction, pulse repetition rate of the laser beam 12, 12′ incident on the target, desired overlap or separation between successive laser pulses, and desired energy distribution along the scan. Rotation speeds can have values in a wide range from a fraction of rps to tens of thousands of rpm (0.01 rps-100 000 rpm). The energy of the laser pulses 12, 12′ can be controlled in synchronization with the rotation of the mirror 13.

[0065] In one embodiment regarding the scanning speeds of the laser spots travelling on the target surface, the diameter of the annular target 15 and the rotation speed of the mirror 13 are selected such that the speed of the scanned laser spot on the target 15 is at least 1 m/s. In another embodiment, the corresponding values are selected so that the above scanning speed will be at least 10 m/s. In yet another embodiment, the corresponding values are selected so that the above scanning speed will be at least 100 m/s.

[0066] In addition to scanning the laser beam 12′ on the target surface 15 on the circular path, the relative speed between the target 15 and the scanned beam can be increased by rotating the annular target 15 to the opposite direction compared to the scanning beam.

[0067] As the laser pulses strike the surface of the target material 15, a jet of ablated material 16 will be released practically in all directions from the point of incidence 15c. Although the jet 16 has some directionality and angular distribution, some portion of the material will travel to the direction of the laser beam, towards the scanning mirror 13 (this portion is not shown in FIGS. 1-3). In order to avoid, or at least minimize, the amount of material build-up on the mirror 13 and/or to maintain the laser pulse energy throughout the process, in an embodiment of the invention, the mirror 13 is protected using one or a combination of the following features: [0068] static mechanical shields between the target and the mirror allowing the laser beam to pass unobstructed but limiting the amount of ablated material travelling in the opposite direction in comparison to the laser beam propagation; [0069] an enclosure around the scanning mirror having a higher pressure compared to the rest of the space in the vacuum chamber making the free path shorter for the material ejecting from the target (i.e. pressure control around the mirror); [0070] an enclosure around the scanning mirror with a gas flow obstructing the free movement of the material ejected from the target; [0071] an enclosure having a path (i.e. a tube, a shield or an aperture rotating with the mirror) for the laser beam rotating with the mirror making the time shorter when the mirror will be exposed to the incoming target material. This particular solution is especially enabled by the way the scanning is produced on an annular target, and it is not reasonably applicable in conventional scanning methods. Arranged around the rotating mirror, concentric rotating walls with a hole for the laser separated with static concentric walls short enough not to block the beam, one is able to realize compartments with different pressures and differential pumping to reduce the build-up of the released material on the mirror surface; [0072] a sacrificial layer or several layers on or in front of the mirror to be replaced after significant material build-up (e.g. a replaceable or moveable window between the target and the mirror); [0073] heating of the mirror to reduce the sticking of the material hitting the mirror surface; [0074] electric and/or magnetic means creating electric and/or magnetic fields to change the path of the incoming charged particles; [0075] cleaning the mirror with, e.g., a laser beam (i.e. laser cleaning) or with ion bombardment.

[0076] Using one or several of those options will preserve the reflectivity of the mirror 13 throughout the process.

[0077] In an embodiment of the invention, the annular target is placed with its center point in the axis of rotation of the scanning mirror such that the distance the laser beam travels from the lens to the target surface is the same for all the scanning angles guaranteeing thus a constant spot size throughout the scanning cycle.

[0078] The inner surface of the annular target is the surface where the reflected laser beam hits and from where the material is released in the laser ablation process. The material jet is mainly directed perpendicular to the target surface but it might also have other directions depending on the surface topography on the target. Thus, the plane of the target surface affects the propagation direction for the ablated material. The annular target can have a surface designed to produce a certain kind of material distribution or porousness in the coating resulting on the substrate. In an embodiment of the invention, the ablation surface of the annular target is tapered such that, in the plane of incidence, the laser beam forms an angle with the target surface (like in FIG. 1 if target section 15 is seen as part of an oblique inner surface of the annular target). Furthermore, this angle is determined such that the ablated material is directed away from the plane of scanning. The plane of scanning is a horizontal plane if the reflection angle a of the mirror is 90 degrees. In case the rotation angle α is 0<α<180°, the plane of scanning will be a conical surface.

[0079] The ablation process with a single scanning line on the same circular track on the target surface would eventually lead to a deep trench being formed on the target. In order to enable a stable process, the wear of the target needs to be controlled and homogeneous. That is why the location of the scan line on the target is moved during the process in addition to the circular scanning of the laser beam on the target. This makes the ablation track two-dimensional instead of a one-dimensional track, and as a result, a homogeneous wear of the target can be realized. The movement of the scan line on the target can be realized by: [0080] linear movement of the annular target; and/or [0081] changing the angle of the scanning mirror; and/or [0082] changing the angle of another reflecting optics; and/or [0083] providing refractive optics to change the angle of the laser beam incident on the target surface.

[0084] At the first option of the above, the annular target 15 is movable along its central axis.

[0085] The arrangement with a linear movement of the target provides stable conditions by preserving the angle of incidence of the laser beam on the target surface, and furthermore, is straightforward to realize as an independent movement as opposed to the wobbling of a mirror or other optics rotating at a high speed.

[0086] In the case of a tapered inner surface of the annular target, the movement of the target or the location of the scan line on the target affects the circumference length of the ablation track. This in turn affects the scanning speed on the target surface (spatial spot overlap and separation), the duration of one full scan cycle around the target, and the location of the optimal intensity distribution with respect to the target surface. In yet further embodiments of the invention, these effects need to be compensated by synchronized control of: [0087] the rotation speed of the scanner for the optimal separation between successive pulses; and/or [0088] the movement speed of the target for optimal overlapping between successive scan cycles on the target; and/or [0089] movement of the focusing lens or beam-manipulation optics (intensity distribution shaping optics) for maintaining the optimal and desired intensity distribution on the target surface.

[0090] For a continuous ablation and coating process, a constant feed of the source material is required. The annular target can in such a case be realized as a cylinder (by expanding the ring-shaped target of FIG. 3 vertically) in which case the range of the linear movement of the target changes as the target wears out on the tapered ablation surface. The cylindrical target may be moved slowly in a controlled manner in a vertical direction in order to affect new target surface under the arriving laser pulses. Another option is to e.g. incorporate controllable refractive optics between the reflecting mirror and the cylindrical target, in order to slightly redirect the angle of the laser beams towards a fresh target area. Such arrangements provide a way to have a sufficient amount of the source material available for a prolonged ablation and coating process. Such longer processes comprise industrial coating processes for exceptionally large surface areas.

[0091] Summarizing the possible shapes of the target with an annular cross-section along the scanning line, the annularly formed target 15 may have a ring shape, a cylinder shape or a truncated conical shape. A broader ring-formed segment with a tapered inner surface is an example of the truncated conical shape of an annularly formed target.

[0092] Regarding possible materials of the target 15, the annular target 15 can be made of metal, metal compound, glass, stone, ceramics, synthetic polymer, semisynthetic polymer, natural polymer, composite material, inorganic or organic monomeric or oligomeric material. In a further embodiment, the annular target 15 is composed of annular segments of at least two different materials. With such a target structure, a desired coating structure comprising at least two different coatings is possible.

[0093] Regarding some examples of the possible end products after the deposition according to the invention, the coated substrate may be a component of a lithium-ion battery, a component of a sensor or sensor device, or a cutting-tool component.

[0094] The presented method and arrangement can also be used in a production method of nanoparticles. Such a method may utilize the scanning and ablation arrangement as presented above, but additionally, the chamber which otherwise would be a vacuum or comprise a selected pressure of gas, would in this case be immersed in a liquid.

[0095] In the present invention, it is possible to combine features and/or characteristics of the invention from the above and from the dependent claims in order to achieve new variations of the invention applying at least two of the mentioned features or characteristics.

[0096] The scope of the invention is defined by the following claims.