Title of Invention

MATERIAL-MACHINING DEVICE HAVING A LASER BEAM WHICH IS INJECTED INTO A LIQUID JET

Abstract A process for machining the material of workpieces using a laser beam which is injected into and guided in a liquid jet, characterized in that in this process three requirements have to be satisfied together, namely in a fIrst processing step the laser beam being with a radiation focusing cone onto a channel-entry plane of a nozzle channel which shapes the liquid jet, in a second processing step said liquid which is to be shaped into a jet by the nozzle channel be supplied to the nozzle-channel opening without turbulence, and in a third processing step said liquid being supplied to the chanpel opening without a tangential flow component with respect to the nozzle- channel axis and with a rapid flow velocity and without liquid retention spaces, into the immediate vicinity of the radiation-focusing cone, as a result of the flow of liquid being divided into a plurality of equal partial flows which flow in radially and are spaced apart at uniform angles.
Full Text The invention relates to a method for machining material in accordance with the preamble of patent claim 1 and to a material-machining device in accordance with the preamble of patent claim 4.
Prior art
Material machining using laser radiation is used in a very wide variety of ways for cutting, boring, welding, marking and generally for removing material. To make it possible to commence removal of material, a predetermined intensity of the radiation has to be reached on the material surface which is to be machined. This high radiation intensity used to be achieved by focusing the laser radiation at the focal point. However, a drawback of this technique is the small axial extent of the focal point (beam width) in which this high intensity was reached. If deep cuts or holes are to be made, the location of the focal point had to be maintained with a very high level of accuracy or even tracked. The beam tapers conically toward the focal point, meaning that particularly in the case of deep cuts, starting on the surface it was always necessary to remove sufficient amounts of material for the conical beam to be able to reach the machining location. However, deep cuts or holes always have to be made with inclined side walls.
To avoid having to track the focal point and to be able to make narrow cuts and holes with approximately vertical side walls, it has been proposed in US-A 5 773 791, EP-A 0 515 983, DE-A 36 43 284 and WO 95/32834, to inject laser radiation into a liquid jet, as a light conductor, which is directed on to the workpiece to be machined.
In DE-A 36 43 284, the laser radiation was supplied by means of a glass fiber. The end of this

glass fiber had a water jet which was directed onto the workpiece to be machined flowing around it. The known device had the drawback that the diameter of the water jet was never allowed to be smaller than that in the glass fiber carrying the laser radiation. A further drawback resulted from a region of dead water beneath the end of the glass fiber, causing, among other things, disturbances in the water jet flow and ultimately leading to this jet rapidly breaking down into drops.
EP-A 0 515 983 has attempted to avoid these drawbacks by designing an optics unit with a nozzle block which shapes the water jet. Upstream of the nozzle which shapes the water jet was a water retention chamber having a water inlet and a focusing lens, which closes off the chamber from the nozzle entry, for focusing the laser radiation. The location and focal length of the focusing lens were selected in such a manner that the focal point of the laser radiation was located in the axial center inside the nozzle channel. In operation during machining, it has been found that the nozzle was very quickly damaged by the laser radiation, and consequently the shaping of the radiation was no longer perfect.
An improvement to the way in which the laser beam is injected into the liquid jet was made in WO 95/32834, in which the focal point of the laser radiation to be injected was placed in the plane of the nozzle opening and the water retention chamber in front of the nozzle opening was eliminated. The nozzle which shapes the liquid jet is in this case positioned in a liquid supply space which extends radially with respect to the nozzle axis and into which a plurality of coaxially distributed, axial liquid channels open out. Even with this arrangement, the nozzle was damaged during operation for the machining of material.

object of the invention
The object of the invention is to provide a method for machining the material and a material-machining device having a laser beam which is injected into a liquid jet, which method and device ensure that material can be machined over a prolonged running time. Interruption in machining is to occur only at predetermined service intervals. There should be no possibility of unforeseeable interruption, in particular caused by damage to the nozzle block which shapes the liquid jet.
Solution to the object
The solution to the object for the process according to the invention is described by the features of patent claim 1 and for the material-machining device according to the invention is described by the features of patent claim 4.
According to the invention, it is ensured that, on the one hand, the radiation to be injected into the liquid jet is focused into the nozzle entry plane of the nozzle channel which shapes the liquid, and the liquid is supplied to the nozzle entry flowing at a high velocity (without liquid retention spaces) and without turbulence. These three requirements together are satisfied by a corresponding design of an optics unit as described below.
Exemplary embodiments of the invention
Examples of the process according to the
invention and the device according to the invention are
explained in more detail below with reference to
figures. Further advantages of the invention will
emerge from the following descriptive text. In the
drawing:

Fig. 1 shows a cross section through an optics unit of the material machining device according to the invention.
Fig. 2 shows a longitudinal section through the optics unit illustrated in Figure 1, with an enlarged view of the liquid feeds to the nozzle block which shapes the liquid jet,

Fig. 3 shows a longitudinal section through the nozzle block which is illustrated in Figure 2 and is held in a nozzle mount,
Fig. 4 shows a cross section on line IV - IV in Figure 2, and
Fig. 5 shows an enlarged view of the illustration in Figure 3, showing in particular the generation and guidance of the liquid jet in the nozzle channel.
The optics unit 1, which is illustrated in cross section in Figure 1, of the material-machining device according to the invention is connected to a laser radiation source 6 by means of a radiation conductor 3 via a radiation conductor connector 5. The radiation source 6 is only diagrammatically illustrated in this figure. It is a high-power laser, such as a Nd:YAG laser. The radiation 7 emerging from the radiation conductor 3 in the connector 5 is collimated by means of a collimator 9 to form a beam 10. The beam 10 is guided to a beam-expanding unit 11. The beam-expanding unit 11 can be used to change, i.e. expand, the diameter of the beam 10 which enters it to that of the beam 13 which emerges from it. A diameter factor of from two to eight is envisaged for the beam expansion. This expanding ratio makes it possible to vary the beam width 15 (diameter of the focal point) of the laser beam 13 which is described below. The beam-expanding factor of the beam expanding unit can be changed by motor means through signals of an adjustment unit which is not shown ("motorized beam expander"). The expanded beam 13 is then deflected through 90° by a deflecting mirror 17 and is diverted onto focusing optics 23 as focusing unit by means of a further deflecting mirror 21 which has an adjustment unit 19. The way in which the adjustment unit 19 operates and is used is described below.

It should be pointed out that the theoretical focal point of the focusing optic 23 does not necessarily have to coincide with the beam width 15 of the focused laser beam 13. A deviation of both locations results from beam divergence of the laser beam 13, which can be influenced, inter alia, by the beam-expanding unit 11.
A nozzle block 27 having a nozzle channel 29 is used to shape a liquid jet 25. The focusing optic 23 and the beam-expanding unit 11 are adjusted or arranged in such a manner that the beam width 15 of the focused beam 13 comes to lie in the nozzle-channel entry plane 30 of the nozzle-channel opening 28. The nozzle-channel entry plane 30 continues on both sides into the surface of the nozzle block 27. Figures 2 to 5 show the area immediately surrounding the entry to the nozzle channel 29 which shapes the liquid jet. Figure 3 shows the nozzle block 27 on an even larger scale than Figure 2. The nozzle channel 29 is of cylindrical design. The nozzle block 27 is made from a material which is transparent to the laser radiation (in this case with a wavelength of 1.06 μm) and is mechanically hard, such as for example quartz. However, since it is extremely small, it may also consist of diamond. Compared to a nozzle block 27 made from quartz, a nozzle block 27 made from diamond has a longer service life, the end of the service life making itself obvious through a liquid jet 25 which breaks up even after a short liquid jet length.
The nozzle block does not necessarily have to consist of a material which is transparent to the laser radiation in order to utilize the conditions of total reflection against the nozzle-channel wall. It may also consist of a material which is not transparent and absorbs radiation, provided that the nozzle-channel wall is provided with a coating which reflects the laser radiation and should be able to resist abrasion from the liquid jet. In the case of a nozzle block

material which is not transparent, the nozzle surface should also have a reflective coating (to protect against adjustment errors), and so should the underside of the nozzle block (to protect against radiation which is thrown back onto the workpiece from the workpiece of the cloud of plasma)..
The nozzle block 27 illustrated in Figure 3 has a planar surface 30 to which the axis 32 of the nozzle channel 2 9 runs perpendicular. The edge 31 at the nozzle-channel opening 28 between the surface 30 and the channel wall is of sharp-edged design and preferably has a radius of less than 5 μm. This rounded edge 31 is one of further preconditions, which are described below, for generating a liquid jet 25 of great length. This is because it suppresses the formation of turbulence in the liquid. The nozzle block 27 is inserted into a nozzle mount 33. The transition 34 between nozzle mount 33 and nozzle block 27 is designed in such a manner that there is no step present. A step would likewise generate turbulence in the liquid, and this would propagate into the liquid jet 25 shapeed with the nozzle channel 29. The nozzle block 27 illustrated in Figure 3 has an external diameter of 2 mm and a height of 0.9 mm. A nozzle block of this order of magnitude can be manufactured from a diamond at acceptable cost.
As has already been stated above, the nozzle channel 29 which shapes the liquid jet is of cylindrical design, in this case, for example, with a diameter of 150 μm and a length of approximately 300 μm. The length of the nozzle channel 29 should be no greater than twice the diameter of the nozzle channel. The exit of the nozzle channel 29 is adjoined by a conically expanded opening 26. The cone apex angle is in this case eighty degrees. The inner lateral surface 35 of this cone merges continuously into the nozzle mount 33.

The conical design of the inner lateral surface 35 makes it easier to apply a reflective coating, does not interfere with the liquid jet in any way and, on account of its inclination, intensifies the reflection for any radiation which emerges from the liquid jet 25 on account of mechanical inhomogeneities (shock wave, contaminations which have passed through despite filtering ...) . The cone angle is selected to be sufficiently great for radiation which emerges from the liquid jet not to impinge thereon at all or to impinge thereon at only a very shallow angle.
The liquid is supplied to the nozzle channel 29 via a narrow, disk-like inner space 36, the height of which corresponds to approximately half the diameter of the nozzle channel 29. The diameter of the inner space 36 corresponds to the diameter of the nozzle mount 33. Twenty feed lines 37, which are round in cross section and the adjacent side walls of which merge into one another as they enter the inner space 36, .open into this inner space 36 in a star-shaped arrangement radially with respect to the axis 32 of the nozzle channel 29. This arrangement of the feed lines 37 promotes turbulence-free (radial) supply of liquid to the nozzle channel 27. A pressure-reducing filter 39 is arranged at the entry side of the feed lines 37. This filter 39 is adjoined by an annular space 40 which is supplied with liquid via a supply line 41. The filter 39 is used to generate a uniform liquid pressure in the twenty feed lines 37, resulting in a symmetrical flow of liquid to the nozzle entry. Since the supply line 41 is on only one side, without filter 39 the feed lines 37 adjacent to the supply line 41 would be at a higher pressure than those lying opposite the supply line. Consequently, it is impossible for tangential flow components to form in the region of the nozzle-channel opening 28. To allow the laser radiation to reach the nozzle-entry opening, the disk-like inner space 36 is

covered in a liquid-tight manner by a cover 43 which is transparent to the laser radiation used.
The low height of the inner space 36 provides a high flow velocity of the liquid. Due to the high flow velocity, there is no (or a considerably reduced) possibility of the liquid being heated in the focusing cone 38 by the laser radiation passing through it. On account of the design described above, the disk-like inner space 36 is such that it is impossible, in particular in the radiation-focusing cone 38 of the laser radiation, for a liquid retention space, which would preferentially promote the formation of a thermal lens through radiation absorption, to form. A thermal lens would make perfect, stable focusing of the laser beam into the center (axis 32) of the nozzle-channel opening 28 impossible. The presence of a thermal lens would cause the focusing of the radiation to deteriorate, since the thermal lens acts as a diverging lens. The laser radiation would impinge on the edge of the opening of the nozzle and/or the nozzle surface and would therefore damage the nozzle. Furthermore, the thermal lens formed as a result of the liquid heating would not have a stable location. The radiation would no longer be optimally injected into the liquid jet 25. On account of the star-shaped (radial) arrangement of the feed 37, a pressure-reducing filter 39 between the entry to the feeds 37 and the annular space 40, a continuous transition 34 in the flow region of the liquid between nozzle block 27 and nozzle mount 33, and the small rounding (radius >5 μm) of the edge 31 where the liquid enters the nozzle, for the first time turbulence-free flow is achieved as a precondition for a liquid jet 25 of great length. Furthermore, degassing of the liquid and removal of particles from the liquid have a positive effect on the production of a great jet length. It should also be ensured that the supply of liquid is free of pressure pulses. This is because the cylindrical shape of the free liquid jet is

unstable. On account of its surface tension, the liquid seeks to change into a different shape, namely that of a bail. Therefore, after a certain spreading length, the jet of liquid breaks down into individual drops. An infinitesimally small radial disturbance in the liquid jet during its shaping becomes rapidly more intensive, so that the jet may become constricted, causing it to break up into drops. The air surrounding the jet which is entrained by friction additionally increases this effect. A liquid jet of great length can only be produced by the measures listed above for creating a liquid supply which is free from disturbance.
Furthermore, it has surprisingly been found that, when the liquid jet 25 impinges on an as yet unmachined workpiece surface, a shock wave begins to rise upward in the jet. This shock wave means that the flow of liquid is no longer laminar and some of the laser radiation which has been injected into the liquid jet 25 at the entry to the nozzle opening emerges from the liquid jet 25 on account of irregularities on the lateral surface of the liquid jet caused by the shock wave. This emerging radiation would then come into contact with the nozzle block 27, would pass through the latter and would then be thrown onto the metal wall of the nozzle mount 33. Then, the radiation would be absorbed on this wall causing local heating. This could lead to the material of the nozzle mount 33 melting or vaporizing, which would lead to destruction of the nozzle mount 33 and the nozzle block 27. To prevent this from happening, the inner wall 35 is of conical design and is provided with a reflective coating. The laser radiation emerging on account of irregularities in the lateral surface of the liquid jet is therefore reflected by this coating and cannot penetrate through the nozzle block 27 to the absorbent material. Once the workpiece 4 5 has been bored or cut through, there are no shock waves or only shock waves with a minimal energy formed.

The nozzle block 27 although having a long life in the arrangement described here, is arranged so that it can easily be exchanged. To exchange the nozzle block, it is merely necessary to unscrew an insert 46.
To check that a seal is produced, the insert 4 8 accommodating the transparent cover 43 has a groove 54 which runs around its outer lateral surface and opens into a monitoring bore 50. If there is liquid in the monitoring bore 50, the sealing ring 58a has lost its seal. If the sealing ring 58b were then also to lose its seal, liquid could reach the surface 60 of the transparent cover 43, which would considerably impair the focusing and guidance of the laser beam. To avoid this, the sealing rings 58a and 58b are exchanged whenever liquid is registered in the monitoring bore 50.
A force sensor 47 is arranged beneath the workpiece 45 which is to be machined. The position of the force sensor 47 is selected in such a manner that it emits a maximum electrical signal to a control device 49 when the liquid jet 25 is fully impinging on it (without any deflection) . The force sensor 47 is arranged in the geometric axis 32 of the liquid jet 25. If the liquid jet 25 with the laser beam which has been injected into it impinges on a workpiece 45 which has not yet been machined, there is no signal, since the jet 25 first has to bore through the workpiece 45. If the workpiece 45 has already been bored through or if there is an initial cut through which the jet 25 is passing, the jet 25 impinges on the slot side wall or bored hole wall when the workpiece 45 is moving. In this case, still only part of the jet 25 impinges on the force sensor 47. The signal emitted to the control device 4 9 is lower than if the full beam 25 were impinging on it. Therefore, the amount of material which has been removed can be determined by means of the force sensor 47.

The control device 4 9 is also connected to a displacement device for the workpiece 45. The displacement device is only diagrammatically indicated in Figure 1 by two double arrows in the horizontal directions x and y 51a and 51b, intending to indicate that displacement is possible in one plane and two dimensions. Now, depending on the value determined by the force sensor 47, the control device 49 controls the displacement speed of the workpiece 4 5 according to a predetermined cutting pattern in the two directions 51a and 51b. The advance of the workpiece 45 which is to be machined can therefore be regulated and optimized in terms of energy by means of the force sensor 47 in that the workpiece 45 is displaced whenever sufficient amounts of material have been removed.
The control device 4 9 is also connected to the radiation source 6. Therefore, the laser output power can also be adjusted as a function of the measured value from the force sensor and the workpiece displacement velocity. If, in the case of a pulsed laser, by way of example a stepper mode is used for workpiece displacement, the laser emits a plurality of pulses at one location before the workpiece 45 is moved one step onward. The stepper mode may, for example, take place with a step sequence frequency of 100 Hz.
In addition to the guidance of the laser beam which has already been explained above, the optics unit 1, as can be seen from Figure 1, also has means for optimum adjustment and monitoring of the position of the laser beam width (focal point of the radiation), with respect to the nozzle entry opening or the axis 32 of the nozzle channel 29. For this purpose, the radiation 52 from a white light source 53 is superimposed congruently on the expanded laser beam 13. This is carried out by means of the deflecting mirror 17. The deflecting mirror 17 fully reflects the laser radiation but transmits the white light radiation 52 from the white light source 53 behind it. The radiation

from the source 53, together with the laser radiation, is guided via the deflecting mirror 21 into the focusing unit 23 and, given correct optical orientation in the nozzle entry plane 30, is focused at the location of the axis 32. The deflecting mirror 21 is designed to partially transmit the white light radiation 52.
To check the correct beam adjustment, only the radiation from the source 53 is used without a laser beam. If there is any incorrect adjustment, the white light radiation which has been focused by means of the focusing unit 23, illuminates the nozzle edge 31 or the area surrounding it. The surface area surrounding the nozzle-entry opening is observed by means of a video camera 55 via a telescope 56 and the deflecting mirror 21, which partially transmits the white light radiation. As it passes through the deflecting mirror 21, on account of the thickness of the latter, the white light undergoes beam displacement. This beam displacement is corrected by a plane-parallel glass sheet 57.
The deflecting mirror 21 can be tilted by an adjustment unit 19. The adjustment elements are then used to tilt the deflecting mirror 21 in such a manner that the focal point of the white light beam comes to lie symmetrically with respect to the location of the channel axis 32.
To achieve this, the procedure is as follows: the deflecting mirror 21 is tilted until radiation reflection can be determined at the nozzle-channel edge 31, and is then tilted in the opposite direction, while measuring the tilting angle (~ displacement distance of the beam on the nozzle-channel opening) until radiation reflection of the same reflected intensity can also be determined on the opposite nozzle-channel edge 31, and this is followed by a further movement involving tilting back by half the tilting angle. The focal point is then in a plane which includes the nozzle-channel

axis 32. For alignment onto the location of the channel axis 32, a further, similar adjustment of the beam axis is then carried out perpendicular to the previous direction of tilting.
The white light source 53 can be dispensed with if the deflecting • mirror 21 is made slightly transparent (approximately 2%) for the radiation of the laser source 6. In this case too, the telescope and the glass sheet 57 have to be designed for the laser radiation and provided with an antireflective coating. The video camera 55 must be provided with a chip which is sensitive to the laser radiation. In this case, in the event of incorrect adjustment, the laser radiation is reflected from the nozzle edge or its surrounding region. The reflected radiation is then observed by the video camera 55 via the telescope and an adjustment is performed via the adjustment unit 19 described above and the beam-expanding unit 11. To prevent damage to the nozzle channel and the nozzle surface, the adjustment is carried out with reduced laser power. Since the laser beam properties at high beam intensities may change compared to those at lower power, the adjustment of the deflecting mirror 21 and if appropriate of the beam-expanding unit 11 is commenced with a continuous increase in the laser power.
To check the central setting, the output lens of the beam-expanding unit 11 can then be adjusted in such a manner that the diameter of the beam width of the laser beam 13 is increased until the nozzle-channel edge 31 (i.e. the nozzle-channel opening 28) is uniformly illuminated. Only if illumination is uniform has central alignment been achieved beforehand. The output lens of the beam-expanding unit 11 is then displaced in the opposite direction until uniform illumination of the nozzle-opening edge once again occurs. The position between these two settings then provides optimum focusing onto the nozzle-channel entry

plane with the focused beam lying symmetrically with respect to the channel axis 32.
If a Nd:YAG laser is used, the liquid used for the liquid jet may be water. Water exhibits low radiation absorption at 1.06 |im. However, this low absorption may be sufficient for the formation of thermal lenses in front of the nozzle entry. Therefore, for certain applications it is preferable to use a silicone oil in particular selected from the group of polymethylsiloxanes.
If the liquid used is water, the laser radiation used should have an absorption of less than 0.2 cm-1 preferably of less than 0.15 cm1. If radiation with higher absorption is used, too much radiation power is aborbed in the liquid jet. High levels of radiation absorption in the liquid may lead to evaporation effects. It is then also impossible, for example, to sufficiently suppress the formation of the thermal lens in the focal point ahead of the nozzle entry even with optimized flow. Low absorption levels with water used as the liquid result at radiations in the wavelength range from 150 nm to 1100 nm, preferably from 190 nm to 920 nm and between 1040 nm and 1080 nm (there is an absorption peak, in the range around 1000 nm) . Therefore, it is preferably possible to use diode lasers, YAG lasers, frequency-doubled YAG lasers, excimer lasers and copper vapor lasers. A YAG laser has the advantage, for example, that developed, commercially available units are available; they are also able to achieve high mean powers.
The radiation may be continuous or pulsed. In the case of pulsed radiation, the liquid can cool cut edges produced using the process explained above. Heat generated by absorbed radiation in the liquid jet is also dissipated. Therefore, since water has a very high heat absorption capacity, it is possible for high radiation powers to be injected into the liquid jet in pulsed fashion. If a Nd:YAG laser and water as the

liquid are used, up to 20 kW pulsed power can be injected with pulse lengths of some 20 to 500 μs, a mean power of 600 W and a pulse rate of up to 5 kHz.
However, it is also possible to use Q-switched Nd:YAG lasers with pulse lengths of typically 50 to 250 ns with a mean power of 20 to 120 W and a pulse rate of up to 60 kHz. It is also possible to use mode-coupled lasers with pulse lengths in the femtosecond range.
Continuously emitting lasers (e.g. cw YAG) can also be used. In this case, however, the mean power is limited by the lack of interruption to the radiation. It is then only possible to inject approximately 700 W radiation power from an NdrYAG laser into a water jet which is 80 μm thick. At higher laser power densities, the water would be heated to such an extent by the radiation absorption that evaporation would commence beyond a certain jet length. Consequently, the jet would begin to break up into drops; perfect beam guidance would no longer be possible.
The nozzle block 27 described above was produced from quartz or diamond, i.e. from a material which is transparent to the laser radiation. The nozzle exit and the adjoining wall of the nozzle mount 33 were of conical design and were provided with a reflective coating for the laser radiation. It is then also possible to produce the nozzle block 27 from a material which is highly reflective for the laser radiation. For laser radiation of 1.06 μm, it is possible to use a nozzle block made from gold. Since pure gold is too soft, traces of copper and silver have to be added in order to reach a hardness of some 150 to 225 HV.


We Claim:
1. A process for machining the material of workpieces (45) using a laser beam which is injected into and guided in a liquid jet (25), characterized in that in this process three requirements have to be satisfied together, namely in a first processing step the laser beam being with a radiation focusing cone (38) onto a channel-entry plane (30) of a nozzle channel (29) which shapes the liquid jet, in a second processing step said liquid which is to be shaped into a jet (25) by the nozzle channel (29) be supplied to the nozzle-channel opening (28) without turbulence, and in a third processing step said liquid being supplied to the channel opening (28) without a tangential flow component with respect to the nozzle-channel axis (32) and with a rapid flow velocity and without liquid retention spaces, into the immediate vicinity of the radiation-focusing cone (38), as a result of the flow of liquid being divided into a plurality of equal partial flows (37) which flow in radially and are spaced apart at uniform angles.
2. The process according to claim 1, wherein the presence of a liquid jet (25) at the location of an extension of the nozzle-channel axis (32) beneath the workpiece (45) is detected, and the workpiece (45) is moved and the laser power to be injected is changed only when this detection occurs.
3. The process according to claim 1 or 2, wherein the nozzle-channel opening (28) and its edge region being optically imaged in order to direct the laser beam centrally onto the nozzle channel which shapes the jet of liquid, in a fourth processing step the beam axis of the laser beam, which is focused onto the channel entry plane and has an energy which does not remove material, or of an illuminating beam, which runs congruently with the laser beam, being displaced parallel to the nozzle axis (32) until a radiation reflection can be determined at the nozzle edge, in a fifth processing step the beam axis being moved in the opposite direction, with the displacement distance being measured, until a radiation reflection of the same reflected intensity can be determined at the opposite nozzle-edge region, in a sixth processing step the beam axis is once again moved back by half the displacement distance, in a seventh processing step a further similar adjustment of the beam axis take place perpendicular to this direction of displacement likewise parallel to the nozzle axis (32).

4. A material machining device for machining workpieces (45) for a method according to one of claims 1 to 3, having a laser radiation source (6) and a liquid jet (25) which is shaped by means of a nozzle channel (29) of a nozzle block (27) and into which the laser beam of the laser source (6) is injected and guided by an optical focusing unit (23), characterized in that the focusing unit (23) is provided and arranged in such a manner, with respect to the entry opening (28) of the nozzle channel (29), that the focal point of the laser radiation lies in the plane (30) of the nozzle opening (28), and there are a plurality of liquid feed equal [sic] (36, 37, 39, 40), which run radially with respect to the nozzle axis 32, are spaced apart by equal angles, supply the focusing cone (38), which is positioned on the plane of the nozzle opening (28), of the laser radiation and the region immediately surrounding it without any liquid retention spaces and do not allow any turbulence to occur in the liquid even in the region of the nozzle opening (28) and the nozzle 5 channel (29).
5. The material-machining device according to claim 4, wherein disk-like prespace (36) which surrounds the nozzle-channel opening (28) and has a plurality of liquid feed lines (37) opening out radially into it, the height of the prespace (36) corresponding to the nozzle-channel radius, in order, so as to avoid a liquid retention space even in the region upstream of the nozzle-channel opening (28), to have a liquid flow velocity which is only slightly lower than in the nozzle channel (29), and the side walls of the liquid feed lines (37), at the location where they open out into the prespace (36), merge into one another, and in particular the liquid feed lines (37) being arranged so as to radiate outwards, the axes of adjacent liquid feed lines (37) preferably each having the same central angle, so that the liquid flowing to the nozzle-channel opening (28) does not acquire any tangential flow components with respect to the nozzle-channel axis (32).
6. The device according to claim 4 or 5, wherein shortest possible nozzle-channel length, which is preferably less than twice the nozzle-channel diameter, and the nozzle-channel exit (26) has a conically shaped exit part, the aperture angle of which is larger than a possible partial radiation from the injected laser radiation which may emerge from the liquid jet (25) as a result of any instability, and preferably, in the case of laser radiation with a wavelength in the range from 150 nm to 1100 nm, in particular in the range from 190 nm to 920 nm and 1040 nm to 1080 nm, is greater than sixty degrees, in particular eighty degrees.

7. The device according to claim 6, wherein the nozzle exit (26), which is provided as a cone
(35), for the laser radiation has a reflective coating, and preferably the nozzle block (27), for
a wavelength of the radiation source used which lies in the range from 150 nm to 1100 nm,
preferably in the range from 1040 nm to 1080 nm, is made from quartz, in particular from
diamond.
8. The device according to one of claims 4 to 6, wherein the nozzle block (27) is made from a
material which is highly reflective for the laser radiation.
9. The device according to one of claims 4 to 8, wherein a force sensor (47) is arranged as an
extension of the nozzle-channel axis (32) beneath the nozzle exit and above which the
workpiece (45) to be machined can be arranged, the sensor (47) being provided in such a
manner that, when the liquid jet (25) impinges on it, it emits a signal, so that it is possible to
determine when the liquid jet (25) carrying the laser beam has penetrated through the
workpiece (45) in the direction of the nozzle-channel axis.
10. The device according to one of claims 4 to 9, wherein liquid-supply control unit which
eliminates liquid-pressure pulses in the liquid to be supplied to the nozzle entry, preferably
degasses the liquid and in particular removes particles therefrom.
11. The device according to one of claims 4 to 10, wherein an observation unit (21, 57, 56,
55) for the nozzle-channel opening (28) and its surrounding area, and an adjustment unit (19,
21) for displacing the focused laser beam (13) which is incident on the nozzle-channel
opening (28) in such a manner that it comes to be positioned centrally in the opening (28).

Documents:

in-pct-2000-0580-che abstract-duplicate.pdf

in-pct-2000-0580-che abstract.pdf

in-pct-2000-0580-che claims-duplicate.pdf

in-pct-2000-0580-che claims.pdf

in-pct-2000-0580-che correspondence-others.pdf

in-pct-2000-0580-che correspondence-po.pdf

in-pct-2000-0580-che description (complete)-duplicate.pdf

in-pct-2000-0580-che description (complete).pdf

in-pct-2000-0580-che drawings-duplicate.pdf

in-pct-2000-0580-che drawings.pdf

in-pct-2000-0580-che form-1.pdf

in-pct-2000-0580-che form-19.pdf

in-pct-2000-0580-che form-26.pdf

in-pct-2000-0580-che form-3.pdf

in-pct-2000-0580-che form-5.pdf

in-pct-2000-0580-che pct.pdf

in-pct-2000-0580-che petition.pdf


Patent Number 215453
Indian Patent Application Number IN/PCT/2000/580/CHE
PG Journal Number 13/2008
Publication Date 31-Mar-2008
Grant Date 26-Feb-2008
Date of Filing 30-Oct-2000
Name of Patentee SYNOVA S.A
Applicant Address Parc Scientifique de l'EPFL, CH-1024 Ecublens,
Inventors:
# Inventor's Name Inventor's Address
1 RICHERZHAGEN, Bernold Chemin de l'Ochettaz 15b CH-1015 St. Sulpice,
PCT International Classification Number B23K 26/06
PCT International Application Number PCT/CH1999/000180
PCT International Filing date 1999-04-30
PCT Conventions:
# PCT Application Number Date of Convention Priority Country
1 198 19 429.3 1998-04-30 Germany