a) Field of the Invention
The invention is directed to a device for quasi-simultaneous welding of two plastic parts along a joining contour by means of laser radiation.
b) Description of the Related Art
By joining contour is meant, within the meaning of the invention, the geometry of the welding between the joining surfaces of the parts (workpiece) to be welded. In principle, the joining contour can be punctiform, line-shaped or planar and may lie in three-dimensional space or only in a plane. Depending upon the parts to be welded, their extension may vary within a range of only a few millimeters to several meters.
By quasi-simultaneous welding is meant that the joining surfaces in the area of the joining contour are heated, plasticized and welded together with placement path virtually simultaneously in that an energy beam repeatedly sweeps over the joining contour before the melting of the two plastic parts to be welded. In simultaneous welding, the entire joining contour is acted upon by energy simultaneously.
The suitability of the generic devices known from the prior art to weld the joining contours to be joined with an appropriate expenditure on time and mechanical apparatus varies depending on the joining contour and its size in particular.
Devices known from the prior art for welding extended joining contours comprise, in addition to a laser radiation source, a scanning device which basically comprises at least a beam-shaping optical element and a beam-deflecting optical element. The object of the beam-shaping element is to concentrate the beam bundle on the workpiece surface. The beam bundle is guided over the workpiece surface in one dimension or two dimensions by means of the beam-deflecting elements which are connected to a drive unit.
Conventional collective lenses or lens arrangements with collective action are used as beam-shaping optical elements.
Polygon mirrors, galvanometer mirrors and prisms which are driven in an oscillating or rotating manner are used in particular as beam-deflecting optical elements. Devices of this kind, in which the scanning device is arranged at a fixed distance from the workpiece surface, can only scan limited areas of the workpiece surface, i.e., only joining contours whose size is smaller than the scanning area can be produced.
If the joining contour is only punctiform, the driven beam-deflecting elements can basically be dispensed with. The beam-deflecting elements are also not necessary when the joining contour is a line and the light source is projected on the workpiece surface as a line, e.g., by means of a cylindrical lens, in order to weld the workpiece simultaneously.
In order to produce extended joining contours, the beam bundle is normally directed to the workpiece surface by an articulated mirror arm that is guided by a robot arm. Therefore, a simultaneous or quasi-simultaneous welding of the entire joining contour is impossible.
Combinations of articulated mirror arms and scanning devices are also known. The scanning movement can be a superimposed movement of the beam-deflecting elements of the scanning device and of the robot arm or a movement exclusively of the beam-deflecting elements of the device by which adjacent scanning areas are scanned, the device being successively positioned relative to these adjacent scanning areas by the robot arm. Simultaneous or quasi-simultaneous welding of the entire joining contour is also impossible with a solution of this kind.
The devices known from the prior art for quasi-simultaneous welding comprising beam-shaping and beam-deflecting elements are uneconomical with respect to apparatus and design and generally have a large space requirement. Therefore, they are not suited to be arranged next to one another for welding a larger joining contour quasi-simultaneously by simultaneous scanning of adjacent partial joining contours.
Known devices for simultaneous welding take up less space because they do not require a mechanism for generating relative movement. However, they do require extensive adjustment if they are to be arranged next to one another so as to make up a more complex apparatus in order to weld a larger joining contour comprising a plurality of partial joining surfaces. Faulty adjustments result in overlapping areas receiving twice the amount of radiation or in areas of the joining surface that are not welded.
It is the primary object of the invention to provide a device for the quasi-simultaneous welding of joining contours or partial joining contours which can be produced economically with respect to apparatus and design, has an appreciably reduced space requirement and, when a plurality of such devices are arranged next to one another, is suitable for the simultaneous welding of a plurality of partial joining contours forming a larger closed joining contour.
According to the invention, this object is met by a device for welding a joining contour by laser radiation comprising a laser diode and a light-conducting fiber which is arranged in front with reference to the radiating direction of the laser diode, the beam bundle emitted by the laser diode being coupled into an entrance surface of the light-conducting fiber and an exit surface of the light-conducting fiber being arranged in front of a beam-shaping optical unit with reference to the direction of radiation so that the beam bundle images a focal spot, by way of the beam-shaping optical unit, on a workpiece surface arranged downstream of the beam-shaping optical unit. The beam-shaping optical unit comprising at least one gradient index lens which is connected to at least one linear movement unit by which the gradient index lens is deflected radial to the exit surface by a displacement path in order to generate a deflection of the beam bundle so that the focal spot scans a joining contour on the workpiece surface.
An essential idea of the invention consists in that a gradient index lens, such as is used in many areas of technology as a fiber coupling, is employed as beam-shaping optical element. Instead of beam-deflecting elements such as those used in the prior art to guide the beam bundle over the workpiece surface, the gradient index lens is moved relative to the exit surface of the light-conducting fiber and is constructed in such a way that even a slight deflection (displacement path) of the gradient index lens relative to the light-conducting fiber is sufficient to generate a large deflection (welding path) of the beam bundle on the workpiece surface. The required relative movement between the gradient index lens and the exit surface of the light-conducting fiber can also be realized by deflection of the light-conducting fiber or by a combined movement of the light-conducting fiber and gradient index lens instead of by the gradient index lens.
A device according to the invention whose size and external dimensions are determined substantially by the movement unit can be constructed so as to be substantially smaller and lighter than conventional devices for simultaneous welding by means of laser. In particular, this has the advantage that a plurality of devices of this kind can be adjacent to one another to form a more complex apparatus in order to weld larger joining contours.
The invention will be described more fully in the following with reference to several embodiment examples shown in the drawings.
In the drawings:
Further, the first gradient index lens 4.1 is constructed in such a way that it images the exit surface 3 on the workpiece surface 5 with a large imaging scale. The greater the imaging scale, the smaller the deflection path (adjustment path) by which the first gradient index lens 4.1 must be deflected in order to cause a large deflection (welding path) of the beam bundle on the workpiece surface 5.
In order to deflect the first gradient index lens 4.1 relative to the exit surface 3, it is connected to the first piezo actuator 6.1 which moves the first gradient index lens 4.1 back and forth within its possible adjustment path at a frequency of up to 100 Hz or can guide it into various positions along the displacement path, i.e., static and dynamic positioning is possible within the full range of the displacement path.
A displacement path (amplitude) of less than 500 μm is sufficient to generate lines up to a length of 20 mm when, e.g., a light-conducting fiber 2 with a diameter of 50 μm is increased forty-fold. In this regard, a particular advantage over a conventional collective lens is that the far-axis images do not have such extensive distortion, i.e., the focal spot of about 2 mm formed on the workpiece surface 5 remains constant in diameter on the generated line.
A focal spot size of about 1 mm is more favorable for the input of energy into the workpiece. This is achieved, for example, for a light-conducting fiber 2 with a diameter of 50 μm at a magnification of 20 and a displacement path of about 1500 μm. The welding path can then be up to 30 mm, i.e., the joining contour can be up to 30 mm×30 mm.
A device according to the first embodiment example is particularly suitable for carrying out spot welding along a straight line of less than 30 mm or for carrying out a weld seam with a joining contour equal to a straight line of less than 30 mm.
In contrast to the first embodiment example, a second embodiment example, not shown in the drawings, has an additional adjusting device 9. In order to vary the diameter of the focal spot, the workpiece distance 8 (distance between the workpiece surface 5 when the first gradient index lens 4.1 is not deflected and the second plane surface of the first gradient index lens 4.1) can be changed by means of the adjusting device 9 so that the exit surface 3 is imaged out of focus on the workpiece surface 5. This adjusting device 9 is also useful when the workpiece surface 5 has no plane surface. The adjusting device 9 then provides for a constant workpiece distance 8. However, insofar as the deviations of the workpiece surface 5 from a plane lie within the depth of focus range, it is not necessary to readjust the workpiece distance 8.
In a fourth embodiment example shown in
A specific construction for a device according to the invention is described in a fifth embodiment example.
Three piezo actuators 6.1, 6.2 of identical construction are fixedly connected by one end on a base plate 13 parallel to one another accompanied by pretensioning, while the second end of the piezo actuators 6.1, 6.2, respectively, is connected to the bearing plate 12 which is oriented parallel to the base plate 13 in the inactive state. The third piezo actuator 6.3 only functions as a spacer with a thermal coefficient of expansion equal to that of the acting piezo actuator 6.1, 6.2. The connection of the second end of the third piezo actuator 6.3 to the bearing plate 12 is formed by a pivot joint that defines a pivot point around which the bearing plate 12 is swiveled when the piezo actuators 6.1, 6.2 are activated. The deflection of the bearing plate 12 is determined by the actuating path of the piezo actuators 6.1 and 6.2 contacting the bearing plate 12 by their second ends. The bearing plate 12 is a terminating part of an arm 10. The length of the arm 10 is determined by the desired distance that must exist between the end plate 11, which forms a second terminating part of the arm 10 and to which the second gradient index lens 4.2 is fixed, and the bearing plate 12 in order for the actuating path of the piezo actuators 6.1, 6.2 to result in displacement paths of desired length for the first gradient index lens 4.1. At a total length of the arm 10 of, e.g., about 15 cm, an actuating path of 50 μm can be multiplied to a displacement path of 1.5 mm. The arm 10 itself must be rigid, torsion-resistant and as light as possible.
Two housing angles 14 which enclose the subassembly described above are fastened to the circumference of the base plate 13 by connection elements 16. A first housing angle 14 is shown in
With a light-conducting fiber 2 having a diameter of 100 μm, a working distance 7 between the exit surface 3 and entrance surface of the first gradient index lens 4.1 of 100 μm, a lens diameter of 1.8 mm, and a lens magnification of 14, welding paths of 20 mm can be realized, i.e., a joining contour of 20 mm×20 mm can be welded quasi-simultaneously.
It is particularly advantageous that the device does not exceed the dimensions of the weldable joining contour parallel to the workpiece surface 5, so that the devices can easily be arranged in series for simultaneous welding of closed, larger joining contours.
In a sixth embodiment form, not shown in the drawing, a device comprises a plurality of devices as was shown in embodiment examples 1 to 5. Common to all of the embodiment examples 1 to 5 is that a joining contour whose dimensions are determined by the deflection area that can be traversed by the beam bundle on the workpiece surface 5 can be generated quasi-simultaneously. The advantage of the invention becomes especially clear in this connection. Because of the small space requirement which is determined essentially only by the piezo actuators 6.1, 6.2, a plurality of modules can be arranged close together and are adapted to one another with respect to function so as to jointly, simultaneously generate a larger joining contour made up of individual partial joining contours. The entire joining contour is acted upon by the beam in that all of the modules sweep over a partial joining contour simultaneously; i.e., the workpiece comprising two parts whose joining surfaces contact one another is heated, plasticized and welded in the area of the joining contour simultaneously and quasi-simultaneously.
In all of the embodiment examples described above, it was assumed that the beam-shaping optical unit comprising one or two gradient index lenses 4.1, 4.2 images the exit surface 3 of the light-conducting fiber 2 on the workpiece surface 5. The gradient index lenses 4.1, 4.2 can also be dimensioned in such a way and arranged relative to the exit surface 3 such that the beam bundle is collimated and focused on the workpiece surface 5.
Instead of the piezo actuators 6.1, 6.2, other linear movement units known from the prior art such as capacitive actuators or electromagnetic actuators can also be used.
It is self-evident that the device according to the invention can also be applied in combination with robot arms. Compared to conventional devices of the same type, its low weight is a chief advantage.
Spot welds can also be generated simultaneously at a fixed distance from one another with the same number of devices positioned relative to one another that is used for generating weld spots. Devices of this kind do not require linear movement units.
While the foregoing description and drawings represent the present invention, it will be obvious to those skilled in the art that various changes may be made therein without departing from the true spirit and scope of the present invention.
Number | Date | Country | Kind |
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102 46 198.8 | Oct 2002 | DE | national |
This application claims priority of International Application No. PCT/DE2003/003026, filed Sep. 10, 2003 and German Application No. 102 46 198.8, filed Oct. 1, 2002, the complete disclosures of which are hereby incorporated by reference.
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/DE03/03026 | 9/10/2003 | WO | 4/1/2005 |