Method for preparing a workpiece for subsequent laser welding and method for joining workpieces through laser welding with lap joint
09849542 · 2017-12-26
Assignee
Inventors
Cpc classification
B23K26/082
PERFORMING OPERATIONS; TRANSPORTING
B23K26/0876
PERFORMING OPERATIONS; TRANSPORTING
B23K2103/08
PERFORMING OPERATIONS; TRANSPORTING
B23K26/361
PERFORMING OPERATIONS; TRANSPORTING
B23K2101/34
PERFORMING OPERATIONS; TRANSPORTING
International classification
B23K26/16
PERFORMING OPERATIONS; TRANSPORTING
B23K26/082
PERFORMING OPERATIONS; TRANSPORTING
B23K26/32
PERFORMING OPERATIONS; TRANSPORTING
B23K26/00
PERFORMING OPERATIONS; TRANSPORTING
B23K26/361
PERFORMING OPERATIONS; TRANSPORTING
Abstract
In a method for preparing a workpiece for subsequent laser welding, a recessed structure in the form of at least two grooved line elements is formed by a laser beam in a surface of the workplace, with the line elements having a common starting point from which the laser beam moves onwards to produce the line elements. Solidifying material melt of the workpiece is hereby accumulated in an area of the starting point to produce a nub-like elevation sized to extend out beyond the surface of the workpiece.
Claims
1. A method for preparing a workpiece for subsequent laser welding, comprising moving a laser beam from a common starting point onward to produce in a surface of the workpiece a recessed structure in the form of at least two grooved line elements that meet in the common starting point and thereby accumulate solidifying material melt of the workpiece in an area of the common starting point to produce a nub-like elevation sized to extend out beyond the surface of the workpiece.
2. The method of claim 1, wherein the line elements are formed sequentially with the same laser beam.
3. The method of claim 1, wherein the line elements extend in the shape of a V, with the laser beam forming a first one of the line elements by starting from the common starting point and forming a second one of the line element also by starting from the common starting point.
4. The method of claim 3, wherein the line elements define an angle of about 90° there between.
5. The method of claim 1, wherein the recessed structure is formed by at least three grooved line elements arranged in a star-shaped configuration.
6. The method of claim 1, wherein the line elements have each a length of 1 mm to 5 mm.
7. The method of claim 1, wherein a plurality of said recessed structure is formed in the surface of the workpiece.
8. The method of claim 1, further comprising applying on the workpiece a zinc-containing coating.
9. A method of joining at least two workpieces, with at least one of the workpieces being coated, comprising: moving a laser beam from a common starting point onward to produce in a surface of at least one of the workpieces in a joining region with the other one of the workpieces a plurality of recessed structures, each in the form of at least two grooved line elements that meet in the common starting point and thereby accumulate solidifying material melt of the at least one of the workpieces in an area of the common starting point to produce a plurality of nub-like elevations sized to extend out beyond the surface of the at least one of the workpieces; positioning and aligning the workpieces such as to form a degassing gap in a region of overlap of the workpieces; and joining the workpieces through laser welding, with evaporating coating material being able to escape via the degassing gap.
10. The method of claim 9, wherein both workpieces are formed in their joining regions with the plurality of recessed structures and elevations and aligned such that the recessed structures and elevations of one of the workpieces are positioned in intermediate spaces of the recessed structures and elevations of the other one of the workpieces.
11. The method of claim 9, wherein the line elements are formed sequentially with the same laser beam.
12. The method of claim 9, wherein the line elements extend in the shape of a V, with the laser beam forming a first one of the line elements by starting from the common starting point and forming a second one of the line element also starting from the common starting point.
13. The method of claim 12, wherein the line elements define an angle of about 90° there between.
14. The method of claim 9, wherein the recessed structure is formed by at least three grooved line elements arranged in a star-shaped configuration.
15. The method of claim 9, wherein the line elements have each a length of 1 mm to 5 mm.
16. The method of claim 9, wherein the workpiece is coated with a zinc-containing coating.
17. A method, comprising moving a laser beam from a same starting point onward in at least two directions in succession to produce in a surface of the workpiece a recessed structure in the form of at least two grooves and thereby build up solidifying material melt of the workpiece in an area of the starting point to produce in relation to the surface of the workpiece a nub-like elevation that serves as a spacer sufficient to define a degassing gap in an overlap region between the workpiece and another workpiece to be joined with the workpiece.
Description
BRIEF DESCRIPTION OF THE DRAWING
(1) Other features and advantages of the present invention will be more readily apparent upon reading the following description of currently preferred exemplified embodiments of the invention with reference to the accompanying drawing, in which:
(2)
(3)
(4) FIG, 2A is an enlarged detailed view of the area of the workpiece encircled in
(5)
(6)
DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS
(7) Throughout all the figures, same or corresponding elements may generally be indicated by same reference numerals. These depicted embodiments are to be understood as illustrative of the invention and not as limiting in any way. It should also be understood that the figures are not necessarily to scale and that the embodiments are sometimes illustrated by graphic symbols, phantom lines, diagrammatic representations and fragmentary views. In certain instances, details which are not necessary for an understanding of the present invention or which render other details difficult to perceive may have been omitted.
(8) Turning now to the drawing, and in particular to
(9) The degassing gap S is realized in accordance with the present invention by several nub-like elevations 150 which, prior to subjecting the workpieces 110, 120 to laser welding, are formed by a preceding process step on at least one of the workpieces 110, 120 in a joining region F which corresponds to the overlap region U, as shown in
(10)
(11) As is readily apparent from the detailed view of
(12)
(13) Currently preferred is the use of scanner optics to produce the recessed structures 140 in the joining region F of the workpiece 120, with the line elements 142, 143 of a recessed structure 140 being formed in succession before the next recessed structure 140 is then formed in a same. manner. The recessed structure 140 which in plan view has a V-shaped or wedge-shaped configuration, can be realized fairly quickly, i.e. in a short time, so that the joining region F can also be worked on relatively fast and the heat input is also slight. The joining region F, in which the recessed structures 140 are formed, may also have a spatial configuration.
(14) In the embodiment of
(15)
(16) While the invention has been illustrated and described in connection with currently preferred embodiments shown and described in detail, it is not intended to be limited to the details shown since various modifications and structural changes may be made without departing in any way from the spirit and scope of the present invention. The embodiments were chosen and described in order to explain the principles of the invention and practical application to thereby enable a person skilled in the art to best utilize the invention and various embodiments with various modifications as are suited to the particular use contemplated.