Method and Device for Producing Formed, in Particular Flanged, Sheet Metal Components
20190193136 ยท 2019-06-27
Inventors
Cpc classification
B21D22/30
PERFORMING OPERATIONS; TRANSPORTING
International classification
Abstract
A method for producing a formed, flanged component is disclosed. The method includes the steps of: preforming a workpiece a preformed component; and calibrating the preformed component to a substantially completely formed component. The method strengthens the reinforcement in the component and widens the spectrum of application to components in particular, to tub-shaped components. The calibrating of the preformed component to the completely formed component includes stretching the preformed component at least in portions. The present disclosure relates further to a device for producing a formed, flanged component.
Claims
1. A method for producing a formed, flanged component, the method comprising the following steps: preforming a workpiece a preformed component; and calibrating the preformed component to a substantially completely formed component, wherein the calibrating of the preformed component to the substantially completely formed component comprises at stretching the preformed component at least in portions.
2. The method as claimed in claim 1, wherein a region of the preformed component is configured so as to have a material deficiency in relation to the completely formed component.
3. The method as claimed in claim 1, wherein a region of the preformed component in terms of a geometric size, is dimensioned so as to be smaller in comparison to the substantially completely formed component.
4. The method as claimed in claim 1, wherein material elevations are permitted while preforming the workpiece to the preformed component.
5. The method as claimed in claim 1, wherein the material elevations are permitted by at least one of providing a gap and a blank-holder spacing in the region of the material elevation.
6. The method as claimed in claim 4, wherein the material elevations are incorporated in a targeted manner by way of at least one preforming tool.
7. The method as claimed in claim 4, wherein the material elevations are substantially free of material thickenings.
8. The method as claimed in claim 4, wherein the material elevations are ironed by stretching the preformed component.
9. The method as claimed in claim 1, wherein a region of the preformed component, in terms of a geometric size, is dimensioned so as to be larger as compared to the substantially completely formed component.
10. The method as claimed in claim 1, wherein the calibrating of the preformed component to the completely formed component comprises compressing the preformed component at least in regions.
11. The method as claimed in claim 1, wherein the preformed component by way of the calibrating is subjected to a plastic flow procedure in one of an entirety of the component and only in portions of the component.
12. A device for producing a formed, flanged component, comprising: a preforming tool for preforming a workpiece to a preformed component; and a calibrating tool for calibrating the preformed component to a substantially completely formed component, wherein the preforming tool and the calibrating tool are configured in such a manner that the calibrating of the preformed component to the substantially completely formed component comprises stretching the preformed component at least in regions.
13. The device as claimed in claim 12, wherein the preforming tool, while preforming the workpiece to the preformed component, is configured for permitting material elevations by use of a gap that remains in at least one of a closed stated and a blank holder spacing of the preforming tool.
14. The device as claimed in claim 13, wherein the preforming tool comprises a preforming die and a preforming swage, and the gap defined at least between the preforming die and the preforming swage.
15. The device as claimed in claim 12, wherein the calibrating tool comprises a calibrating die and a calibrating swage, wherein the calibrating die comprises a first calibrating die portion and a second calibrating die portion which is movable relative to said first calibrating die portion and which forms the calibrating die base.
16. The method as claimed in claim 2, wherein the region is a side-plate region.
17. The method as claimed in claim 3, wherein the region is a side-plate region.
18. The method as claimed in claim 9, wherein the region is one of a side-plate region and a flanged region.
19. The device as claimed in claim 15, wherein the calibrating swage comprises a first calibrating swage portion and a second calibrating swage portion which is movable relative to said first calibrating swage portion and which forms the calibrating swage base.
Description
[0045] The invention is furthermore to be explained in more detail by means of an exemplary embodiment in conjunction with the drawing in which:
[0046]
[0047]
[0048]
[0049]
[0050]
[0051] A workpiece 3a, here a flat steel sheet, is initially placed into the preforming tool 1 and optionally positionally fixed therein (
[0052] The individual tool parts of the preforming tool 1 herein are conceived for being received in a press. To the extent that no further auxiliary drives are used, the preforming die 8 stands for example on a press base plate, the preforming blank holder 4 is driven, for example by mandrels of the lower cushion, the preforming swage base 6b is driven, for example, by mandrels of the upper cushion, and the first preforming swage portion 6a is driven, for example, by a die plate of the press. However, the drives of the upper cushion and the lower cushion as well as the swage and the die can also be reversed in an individual case.
[0053] The preforming die 8 and the preforming blank holder 4 are subsequently lowered onto the workpiece 3a (
[0054] The preforming die 8 and the preforming swage 6 presently are mutually adapted in such a manner that a gap 10 is formed (
[0055] On account thereof, radially or otherwise directed corrugations 12 are permitted in the side-plated region of the preformed component 3b (and selectively also in the base region and/or in the flange region) when preforming (cf.
[0056] On account of a gap 10 and a blank-holder spacing being provided which can assume a multiple of the sheet-metal thickness, the corrugations 12 are not flattened by way of contact with the tool parts 6a, 8 such that no uncontrollable thickenings are created.
[0057] As is schematically illustrated in
[0058] As will be described in more detail in the context of
[0059] The calibrating tool 2 comprises a calibrating die 20 and the calibrating swage 22. The calibrating die 20 has a first outer calibrating die portion 20a and a second inner calibrating die portion 20b or calibrating die base which is movable relative to said first outer calibrating die portion 20a. The calibrating swage 22 comprises a first outer calibrating swage portion 22a and a second inner calibrating swage portion 22b or calibrating swage base which is movable relative to said first outer calibrating swage portion 22a. The first calibrating swage portion 22a in the region of the flange of the preformed component 3b furthermore includes a lowered feature 24 such that a shoulder 26 protruding on the calibrating die 22 fits thereinto in form-fitting manner.
[0060] The calibrating die 20 and the calibrating swage 22 of the calibrating tool 2 are embodied such that the completely formed component in the terminal position is completely defined by the intervening cavity.
[0061] The calibrating tool 2 is also conceived for being received in a press. To the extent that no auxiliary drives are used, the calibrating die base 20b is driven, for example, by mandrels of the lower cushion, the calibrating swage base 22b is driven, for example, by the mandrels of the upper cushion. The first calibrating swage portion 22a is driven, for example, by the die plate of the press, the first calibrating die portion 20a stands, for example, on the press base plate. The upper cushion and the lower cushion, as well as the swage and the die, can also be reversed in an individual case.
[0062] As is illustrated in
[0063] In order for the completely formed component 3c to be obtained, the second, outer calibrating die portion 20a of the calibrating die 20 moves into the preformed component 3b and progressively widens the latter. The stretching herein ensures that existing corrugations 12 in the side-plate region of the preformed component 3b are ironed in the circumferential direction and herein are eliminated, and that the site-plate region of the preformed component 3b assumes the shape of the site-plate region of the completely formed component 3c. The material for said widening is retrieved by the procedure both from the site-prate region as well as from the base region, the latter on account of the spacing not yet having been finally molded.
[0064] The outer edge of the flange region of the preformed component 3b reaches the vertical wall of the calibrating swage 22 just before reaching the terminal position illustrated in
[0065] The side-plate region of the preformed component 3b is simultaneously compressed when said site-plate region has optionally been embodied so as to be somewhat longer than required. The spacing of the calibrating die base 22b from the calibrating swage base 20b is also eliminated simultaneously with the calibrating die 20 reaching the terminal position, such that the base region of the now completely formed component 3c at this point in time is likewise completely molded (
[0066] The material of all regions of the completely formed component 3c has accordingly been subjected to a final flow procedure in the terminal position. Said material is thus widened, compressed to shape, and by virtue of the plastic flow of all volumetric parts is present in a dimensionally highly accurate manner, having minor or no rebounding.
[0067] The calibrating tool 2 is subsequently diverged and the substantially completely formed component 3c, which requires if at all or only minor peripheral trimming is ejected. Since comparatively large regions have only been widened and not compressed in the method, a lower force requirement moreover results when calibrating than in the case of the methods from the prior art in which substantially all planar regions of the part have to be compressed.
[0068] The device and the method here have been explained with reference to a component in the form of a cup having oblique side-plates. However, other component shapes are also possible and require accordingly adapted tool contours.