Carrier Component for a Vehicle Application, and Method for Producing a Carrier Component of This Type

Abstract

A carrier component for a vehicle application, formed by two half-shells that are welded to one another at contact sides. When assembling the two half-shells for joining same at the contact sides, in a position in which the two half-shells are arranged above one another, the point of contact of the lower half-shell protrudes in relation to the external closed side of the other half-shell. The point of contact of one of the two half-shells protrudes inward in relation to the internal closed side of the other half-shell. A method for producing a carrier component from two half-shells is also disclosed.

Claims

1-11. (canceled)

12. A carrier component for a vehicle application, comprising: two half-shells, which form the carrier component, that are welded to one another at contact sides; wherein, in a position in which one of the two half-shells is arranged above the other half-shell, the point of contact of the lower half-shell protrudes outward in relation to the external closed side of the other half-shell in the assembling of the half-shells for external joining of same; wherein the point of contact of one of the two half-shells protrudes inward in relation to the internal closed side of the other half-shell; wherein the points of contact of the half-shells are connected over the entire contact width with friction-locking; and wherein the outward protrusion of the point of contact of the one half-shell is greater than 0.0 mm and less than or equal to 0.5 mm in relation to the point of contact of the other half-shell.

13. The carrier component of claim 12, wherein the inward protrusion of the one half-shell, in relation to the other half-shell, is integrated into a weld seam with formation of a fillet weld with the other half-shell.

14. The carrier component of claim 12, wherein the external protrusion of the point of contact of the one half-shell is greater than 0.0 mm and less than or equal to 0.1 mm in relation to the point of contact of the other half-shell.

15. The carrier component of claim 12, wherein the overlap of adjacent points of contact of the two half-shells is 90% or more in relation to the point-of-contact width, wherein, upon the presence of points of contact with differing point-of-contact width, said overlap relates to the lesser point-of-contact width.

16. The carrier component of claim 12, wherein the points of contact of the same half-shell protrude inward at the points of contact to be joined in relation to the internal closed side of the other half-shell.

17. The carrier component of claim 12, wherein wall sections, providing the points of contact, of the adjoining half-shells are in the same spatial position, at least with their end section supporting the point of contact.

18. The carrier component of claim 12, wherein an outer wall spacing between wall sections, supporting the points of contact, of the one half-shell is greater than the outer wall spacing of the other half-shell by double the width of the outward protrusion.

19. The carrier component of claim 12, wherein the carrier component is a rail, a sub-frame, or a component of a sub-frame.

20. The carrier component of claim 12, wherein each half-shell is a formed steel sheet or aluminum sheet component.

21. A method to produce a carrier component formed by two half-shells, which are U-shaped in cross-section, for a vehicle application, comprising the following steps: providing two half-shells adjacent to one another at contact sides with differing span of points of contact; arranging and retaining the half-shells with their points of contact adjoining one another, with allowance of a capillary gap, such that the points of contact of one of the two half-shells protrude outward as relates to the points of contact of the other half-shell and said protrusion is pointing upward, and the points of contact of the other half-shell protrude inward as relates to the points of contact of the first half-shell and said protrusion is pointing downward; and subsequently simultaneous fusioning of the points of contact, being held adjacent one another, of wall sections of the two half-shells opposite one another externally to form a weld seam extending over the point-of-contact overlap; wherein the fusioning is carried out such that the inward protrusion is used as a weld filler metal and integrated into the weld seam with the formation of a fillet weld and that the half-shells are arranged in such a way that the outward protrusion of the point of contact of the one half-shell is greater than 0.0 mm and less than or equal to 0.5 mm in relation to the point of contact of the other half-shell.

22. The method of claim 21, wherein the fusioning is carried out as welding.

23. The method of claim 22, wherein welding is carried out as MIG/MAG, 2-wire, double-wire, WIG, plasma, laser, or laser hybrid welding.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0025] The present disclosure is described below using example embodiments with reference to the attached figures:

[0026] FIG. 1 shows a schematic cross-section through a carrier component according to a first embodiment;

[0027] FIG. 2 shows a schematic cross-section through a carrier component according to a further embodiment;

[0028] FIG. 3 shows a schematic cross-section through a carrier component according to yet a further embodiment; and

[0029] FIG. 4 shows a schematic perspective view of the carrier component from FIG. 2 with the process of joining its two half-shells.

[0030] Before further explaining the depicted embodiments, it is to be understood that the invention is not limited in its application to the details of the particular arrangements shown, since the invention is capable of other embodiments. It is intended that the embodiments and figures disclosed herein are to be considered illustrative rather than limiting. Also, the terminology used herein is for the purposes of description and not limitation.

DETAILED DESCRIPTION

[0031] A carrier component 1 for a vehicle application is produced from two half-shells 2, 3. The two half-shells 2, 3 have a U-shaped cross-sectional geometry and each comprise a belt 4 (only indicated for the half-shell 4), on which two legs 5, 6 are formed. The legs 5, 6 are beveled as relates to the belt 4 and extend parallel to one another. The material thickness of half-shell 2 is 2 mm in the embodiment shown. The end surfaces of the belts 5, 6 each form a point of contact 7, 8. Half-shell 3 is constructed just as half-shell 2 and has its points of contact placed on the points of contact 7, 8 of half-shell 2 in the arrangement shown in FIG. 1. The two half-shells 2, 3 differ in their outer wall spacing A between the points of contact being held adjacent to one another. The outer wall spacing A of half-shell 2the span of the point of contactis a few tenths of a millimeter greater than the span of the point of contact of half-shell 3. The larger design of half-shell 2 with respect to this can be seen in the sectional enlargement shown for FIG. 1. Due to this design, the point of contact 8 of half-shell 2 protrudes outward with respect to the complementary point of contact of half-shell 3. This protrusion 9 is 0.15 mm on each side in the embodiment shown; however, an embodiment with 0.5 mm is also possible. The surface formed by the protrusion 9 is used to connect the two half-shells 2, 3 with one another in a welding process as a weld pool support. The welding process itself is described further below with reference to FIG. 4.

[0032] With the carrier component 1, the inner wall spacing I of the two half-shells 2, 3 also differ from one another. The inner wall spacing I is indicated on the upper half-shell 3 in FIG. 1. The protrusion of the point of contact 7 of half-shell 3 as relates to the point of contact of half-shell 2 corresponds to the dimension of the protrusion 9 and thus is likewise about 0.15 mm, as can be seen in the sectional enlargement.

[0033] FIG. 2 shows a further carrier component 10, which is constructed just as carrier component 1 from FIG. 1. Carrier component 10 differs from carrier component 1 in that the span of the point of contact of half-shell 3.1 is discernibly less as relates to the point of contact or the outer wall spacing A of half-shell 2. The result is that the protrusion 9.1 with this carrier component 10 is greater than with carrier component 1 of FIG. 1. With this carrier component 10 as well, an inward protrusion is formed as relates to the inner wall of the lower half-shell 2 by the point of contact of the upper half-shell 3.1.

[0034] Because the wall thickness of the half-shells 2, 3, 3.1 is the same with carrier components 1, 10, carrier components 1 and 10 differ with respect to the degree of overlap of the adjacent points of contact of the half-shells. If an overlap of 92.5% is achieved with carrier 1, it is thus only the minimum required 50% with carrier 10.

[0035] FIG. 3 shows yet a further carrier component 11. The lower half-shell 12 of carrier component 11 has a larger wall thickness than the upper half-shell 13. The larger wall thickness with this embodiment is used to also form the desired protrusion 9.2, which is also kept very minimal with this embodiment and is likewise only about 0.15 mm Due to the larger material thickness of the lower half-shell 12 of carrier component 11 of this embodiment, the inner protrusion is also provided by the point of contact of the lower half-shell 12.

[0036] Carrier components 1, 10, 11 are shown with the half-shells adjoined with their points of contact in the figures before the half-shells are welded to one another.

[0037] In order to fuse the two half-shells 1, 2; 2, 3.1; 12, 13 of the carrier components 1, 10, 11, they are positioned with respect to one another such that the respective protrusion 9, 9.1, 9.2 is established on the elongated sides. This positioning is shown in FIGS. 1 to 3 as relates to carrier components 1, 10, 11. In doing so, it is provided that the respective protrusion 9, 9.1, 9.2 is always greater than 0.0 mm with the welding process, even with consideration of a differing distortion of the points of contact being held adjacent one another. A change in the span of the protrusion 9, 9.1, 9.2 can take place by heating during the joining.

[0038] Due to the unavoidable unevenness of the adjacent points of contact of the half-shells 2, 3.1, a gap is located between the points of contact, which supports degassing during the welding process.

[0039] Referring now to FIG. 4, after the positioning of the two half-shells, wherein there is lifting onto carrier component 10 from FIG. 2, and thus after positioning of half-shells 2 and 3.1 into their proper joining arrangement with provision of the protrusions 9.1 following the longitudinal extension of carrier component 10, the two half-shells 2, 3.1 are joined along said carrier, and that is by MAG welding in the embodiment shown. The welding apparatuses are shown in schematic form in FIG. 4 with reference numerals 14, 14.1. The welding direction is indicated by the arrow in FIG. 4. The welding process is carried out simultaneously on both contact sides, wherein this can be carried out in the same or in the opposite direction with respect to one another. This enables a single-step and thus simultaneous joining of the two half-shells 2, 3.1 with one another. A heat-related distortion as well as a twisting thereby caused is thereby kept as small as possible. The sectional enlargement from FIG. 4 indicates the weld seam created with reference numeral 15. However, other welding processes such as 2-wire, double-wire, MIG, WIG, plasma, laser, or laser hybrid welding are also possible here. Melted material for forming an inward fillet weld extends up to the inward protrusion, which is available for forming said fillet weld as weld filler material. The formation of a fillet weld on the inside counteracts a notch effect, which accounts for the special strength properties of the carrier component 10. Despite the small amount of melted material, the previously described weld seam can still be formed. Although welding only takes place externally, the points of contact are connected with one another with a full penetration weld.

[0040] With carrier components that are a rail and thus longitudinally extended, like carrier component 10, the welding process can be carried out very quickly, because preferably both sides can be welded simultaneously, which the previous prior art did not allow for with the type of contact points shown. Thus, conventional welding speeds, which are normally between 0.5 m/min and 1.5 m/min with MAG welding, can theoretically be doubled by the simultaneous use of a second welding torch. Due to the rapid cooling of the weld pool during the welding process, even small weld pool supports in the previously mentioned scope of greater than 0.0 mm can be considered completely sufficient. This is primarily also against the backdrop that the respectively liquid weld pool quantity is only minimal.

[0041] There are numerous options for one of ordinary skill in the art to implement the invention within the scope of the asserted claims without this having to be shown in greater detail within the scope of these embodiments. While a number of aspects and embodiments have been discussed above, those of skill in the art will recognize certain modifications, permutations, additions and sub-combinations therefor. It is therefore intended that the following appended claims hereinafter introduced are interpreted to include all such modifications, permutations, additions and sub-combinations, which are within their true spirit and scope. Each embodiment described herein has numerous equivalents.

[0042] The terms and expressions which have been employed are used as terms of description and not of limitation, and there is no intention in the use of such terms and expressions of excluding any equivalents of the features shown and described or portions thereof, but it is recognized that various modifications are possible within the scope of the invention claimed. Thus, it should be understood that although the present invention has been specifically disclosed by preferred embodiments and optional features, modification and variation of the concepts herein disclosed may be resorted to by those skilled in the art, and that such modifications and variations are considered to be within the scope of this invention as defined by the appended claims. Whenever a range is given in the specification, all intermediate ranges and subranges, as well as all individual values included in the ranges given are intended to be included in the disclosure. When a Markush group or other grouping is used herein, all individual members of the group and all combinations and sub-combinations possible of the group are intended to be individually included in the disclosure.

[0043] In general, the terms and phrases used herein have their art-recognized meaning, which can be found by reference to standard texts, journal references and contexts known to those skilled in the art. The above definitions are provided to clarify their specific use in the context of the invention.

LIST OF REFERENCE NUMERALS

[0044] 1 Carrier component [0045] 2 Half-shell [0046] 3, 3.1 Half-shell [0047] 4 Belt [0048] 5 Leg [0049] 6 Leg [0050] 7 Point of contact [0051] 8 Point of contact [0052] 9, 9.1, 9.2 Protrusion [0053] 10 Carrier component [0054] 11 Carrier component [0055] 12 Half-shell [0056] 13 Half-shell [0057] 14, 14.1 Welding apparatus [0058] 15 Weld seam [0059] A Outer wall spacing/span of the point of contact [0060] I Inner wall spacing