METHOD FOR WELDING A CONNECTION BETWEEN A FIRST JOINING SURFACE OF A FIRST MOLDED PART AND A SECOND JOINING SURFACE OF A SECOND MOLDED PART

Abstract

The invention relates to a method for welding a connection between a first joining surface of a first molded part and a second joining surface of a second molded part, which by means of a clamping device are moved and braced with their joining surfaces in contact with one another, wherein the first molded part is at least partially transparent for a primary beam of a first radiation source and at least partially absorbent for a secondary beam of a second radiation source, and the second molded part is at least partially absorbent for the primary beam, wherein sequentially the second molded part is irradiated with the primary beam and the first molded part is irradiated with the secondary beam.

Claims

1-13. (canceled)

14. A method for welding a connection between a first joining surface of a first molded part (2) and a second joining surface of a second molded part (3), which by means of a clamping device (4) are moved and braced with their joining surfaces in contact with one another, wherein the first molded part (2) is at least partially transparent for a primary beam (10) of a first radiation source (7) and at least partially absorbent for a secondary beam (11) of a second radiation source (8), and the second molded part (3) is at least partially absorbent for the primary beam (10), wherein sequentially chronologically one after the other and in alternation the second molded part (3) is irradiated with the primary beam (10) and the first molded part (2) is irradiated with the secondary beam (11), characterized in that a first focus (14) of the primary beam (10) lies on the second joining surface and a second focus (13) of the secondary radiation (11) lies within the volume of the first molded part (2).

15. The method according to claim 14, characterized in that a monochromatic beam is used as primary beam (10) and a polychromatic beam is used as secondary beam (11).

16. The method according to claim 14, characterized in that laser radiation is used as primary beam (10) or as primary beam (10) and as secondary beam (11).

17. The method according to claim 14, characterized in that the wavelength of the primary beam (10) and/or the wavelength of the secondary beam (11) lies in a first interval of 500-1100 nm or in a second interval of 900-2400 nm.

18. The method according to claim 14, characterized in that a control device switches the primary beam (10) on and off depending on a first parameter and switches the secondary beam (11) on and off depending on a second parameter.

19. The method according to claim 18, characterized in that the primary beam (10) and the secondary beam (11) are switched on and off in alternation in at least two sequences.

20. The method according to claim 18, characterized in that the first parameter and/or the second parameter and/or a writing speed of the primary beam (10) and/or of the secondary beam (11) and/or an intensity of the primary beam (10) and/or of the secondary beam (11) is or are defined in such a way that the energy input by the irradiation in the first and in the second molded part (2, 3) is greater than the energy discharge by heat conduction.

21. The method according to claim 20, characterized in that a minimum value of the energy input in the first and/or in the second molded part (2, 3) is defined in such a way that a state of fusion of the first and/or of the second joining surface is maintained.

22. The method according to claim 20, characterized in that a maximum value of the energy input in the first and/or in second molded part (2, 3) is defined in such a way that a decomposition temperature of the first and/or of the second molded part (2, 3) is not reached.

23. The method according to claim 21, characterized in that the first and/or the second molded part (2, 3) is mounted movably in such a way that the two molded parts (2, 3) fused by a defined path during the state of fusion.

24. The method according to claim 14, characterized in that a galvanometer scanner is used as a movement system.

Description

[0024] The invention will be explained in greater detail hereinafter on the basis of exemplary embodiments with reference to the drawings. The drawings are schematic illustrations and show:

[0025] FIG. 1 an apparatus which is suitable for carrying out the method according to the invention;

[0026] FIG. 2 a detail of the apparatus according to the invention of FIG. 1;

[0027] FIG. 3 a welding contour at a joining surface of a molded part; and

[0028] FIG. 4 an energy/time graph.

[0029] FIG. 1 shows an apparatus 1 for welding a connection between a first molded part 2 and a second molded part 3. Both molded parts 2, 3 are thermoplastics. The apparatus 1 comprises a clamping device 4, which is designed to bring both molded parts 2, 3 into abutment with one another and to brace them. The bracing is illustrated schematically by the arrows 5, 6. The apparatus 1 also comprises two radiation sources 7, 8, which are arranged in a common housing 9. The first radiation source 7 here emits a primary beam 10, and the second radiation source 8 emits a secondary beam 11 (see FIG. 2).

[0030] In this exemplary embodiment the radiation sources 7, 8 are formed as individual radiation sources which are each equipped with a laser, which emit in different wavelength ranges. The two radiation sources 7, 8 can be controlled separately from one another in respect of their emission and intensity. A movement system 12, in this case a galvanometer scanner, is also shown, in which the beam of the two radiation sources 7, 8 is guided.

[0031] The first molded part 2 is transparent for the primary beam 10, such that said beam can radiate through the first molded part 2 and can be absorbed in the second molded part 3. The second molded part 3 absorbs the primary beam 10 in a surface-near layer. The secondary beam 11 is absorbed by the first molded part 2, such that the first molded part 2 can be heated by the irradiation with the secondary beam 11. The first molded part 2 and the second molded part 3 can be irradiated sequentially with the primary beam 10 and the secondary beam 11 with appropriate control of the radiation sources 7, 8. The two molded parts 2, 3 are therefore irradiated chronologically in succession and therefore alternately with the primary beam 10 and the secondary beam 11.

[0032] FIG. 2 shows a detail of the apparatus 1 from FIG. 1. As can be seen, the secondary beam 11 is deposited in the first molded part 2, in particular in the volume thereof. A focus 13 of the secondary beam 11 thus lies in the volume of the first molded part 2. The primary beam 10 has a focus 14 which lies in the surface-near layer in the second molded part 3, such that the joining surface of the second molded part 3, which faces towards the first molded part 2, is heated selectively.

[0033] FIG. 3 shows an exemplary processing contour of the first molded part 2 and of the second molded part 3 from above, that is to say as considered from the movement system 12. The primary beam 10 and the secondary beam 11 are guided with high writing speeds along a shown contour 15 and are switched on with freely selectable alternation over time with freely selectable intensities. This results in selective and speedy heating of the two molded parts 2, 3 at their joining surfaces.

[0034] FIG. 4 shows an energy/time graph for an exemplary welding process. Here, the time is plotted on the abscissa and the energy of the particular radiation source 7, 8 or of the primary beam 10 and the secondary beam 11 is plotted on the ordinate. The energy of the primary beam 10 is provided in a first interval with reference sign 16, and the energy of the secondary beam 11 is provided in a second interval with reference sign 17. It can be seen that the two molded parts 2, 3 are irradiated sequentially by the primary beam 10 and a secondary beam 11. At the start of the welding process the primary beam 10 is firstly switched on, which is shown by the energy value 16. The secondary beam 11 is switched off at this time. At a time 18, the primary beam 10 is switched off and the secondary beam 11 is switched on, which is indicated in the graph by the energy value 17 of the secondary beam 11. At a time 19, the secondary beam 11 is switched off and the primary beam 10 is switched on again, but with a higher intensity, which leads to an increased energy value 20 of the primary beam 10 relative to the energy value 16. At a time 21, the primary beam 10 is then switched off again and the secondary beam 11 is switched on again, but with a lower intensity than between the times 18 and 19, such that an energy value 22 lower than the energy value 17 is provided. At a time 23, the secondary beam 11 is switched off, such that the joining surfaces of the two molded parts 2, 3 cool and can be connected to one another.

[0035] Due to the reciprocal (alternating) switching on and off of the primary beam 10 and of the secondary beam 11, these can be operated with higher energies compared to conventional welding methods, since the energy of the two radiation sources 7, 8, i.e. of the primary beam 10 or secondary beam 11, can be deposited in each case selectively in one of the two molded parts 2, 3. Excessive energy is thus prevented from being introduced into the second molded part 3 simultaneously by the primary beam 10 and the secondary beam 11 and thus damaging said second molded part.