Net shaped substrate material for substrate joint
11759845 · 2023-09-19
Assignee
Inventors
Cpc classification
B29L2031/3002
PERFORMING OPERATIONS; TRANSPORTING
B32B15/04
PERFORMING OPERATIONS; TRANSPORTING
F16B5/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y10T428/24322
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B32B15/20
PERFORMING OPERATIONS; TRANSPORTING
B29C65/64
PERFORMING OPERATIONS; TRANSPORTING
B32B7/05
PERFORMING OPERATIONS; TRANSPORTING
B32B5/24
PERFORMING OPERATIONS; TRANSPORTING
International classification
B21J15/14
PERFORMING OPERATIONS; TRANSPORTING
B32B15/04
PERFORMING OPERATIONS; TRANSPORTING
B32B15/20
PERFORMING OPERATIONS; TRANSPORTING
B32B5/24
PERFORMING OPERATIONS; TRANSPORTING
B32B7/05
PERFORMING OPERATIONS; TRANSPORTING
Abstract
An assembly includes an upper substrate, a lower substrate, and a self-piercing rivet. The lower substrate defines a preformed interior cavity and a preformed exterior profile adjacent the interior cavity to define a variable thickness wall. The self-piercing rivet extends through the upper substrate and into the preformed interior cavity of the lower substrate.
Claims
1. An assembly comprising: a first substrate; a second substrate, a front side of the second substrate facing the first substrate and defining a preformed interior cavity, a rear side of the second substrate being opposite the front side of the second substrate and defining a preformed exterior profile that cooperates with the interior cavity to define a variable thickness wall, wherein the preformed interior cavity defines a circular trench and a raised central region such that, before and after installation of the self-piercing rivet, the variable thickness wall has a greater thickness in the raised central region than in the circular trench; and a self-piercing rivet extending through the first substrate and into the preformed interior cavity of the second substrate, wherein the preformed interior cavity is configured to receive material from the first substrate during installation of the self-piercing rivet and the variable thickness wall is configured to direct flaring of the self-piercing rivet.
2. The assembly according to claim 1, wherein the preformed interior cavity of the second substrate is plastically deformed during installation of the self-piercing rivet.
3. The assembly according to claim 1, wherein the second substrate is an aluminum casting or an aluminum extrusion such that the preformed interior cavity and preformed exterior profile are formed by a corresponding casting or extrusion process.
4. The assembly according to claim 1, wherein the second substrate is a composite material.
5. The assembly according to claim 1, wherein the preformed exterior profile defines a closed cylinder.
6. The assembly according to claim 5, wherein the preformed exterior profile further defines a radiused area extending between a rear surface of the second substrate and the cylinder.
7. The assembly according to claim 1, wherein the preformed exterior profile includes a bottom wall that is substantially flat in a region that is aligned with the raised central region.
8. An assembly comprising: a first substrate; a second substrate, a front side of the second substrate defining a plurality of preformed interior cavities and a back side of the second substrate defining a corresponding plurality of preformed exterior profiles that cooperate with the interior cavities to define variable thickness walls therebetween, wherein each preformed interior cavity defines a circular trench and a raised central region such that, before and after installation of the self-piercing rivets, each variable thickness wall has a greater thickness in the raised central region than in the circular trench; and a plurality of self-piercing rivets extending through the first substrate and into the preformed interior cavities of the second substrate, wherein the preformed interior cavities and variable thickness walls are configured to direct flaring of the self-piercing rivets.
9. The assembly according to claim 8, wherein the second substrate is an aluminum casting or an aluminum extrusion.
10. The assembly according to claim 8, wherein the second substrate is a composite material.
11. The assembly according to claim 8, wherein preformed exterior profiles define closed cylinders.
12. A motor vehicle having the assembly according to claim 8.
13. The assembly according to claim 8, wherein the preformed exterior profile includes a bottom wall that is substantially flat in a region that is aligned with the raised central region.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) The present disclosure will become more fully understood from the detailed description and the accompanying drawings, wherein:
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(8) Corresponding reference numerals indicate corresponding parts throughout the several views of the drawings.
DETAILED DESCRIPTION
(9) The following description is merely exemplary in nature and is not intended to limit the present disclosure, application, or uses.
(10) Referring to
(11) Referring to
(12) Referring to
(13) Referring to
(14) Referring to
(15) The self-piercing rivet 20 is placed inside the self-piercing rivet tool 80 and immediately above the preformed interior cavity 28 of the lower substrate 12. The self-piercing rivet 20 has an insertion end 88 to pierce through the upper substrate 14 and to be inserted into the preformed interior cavity 28 of the lower substrate 12 to engage the bottom wall 26 of the button 18. It should be understood that the reference to a top side is not limiting and that the lower and the upper substrates 12, 14 may be arranged in any orientation.
(16) Referring back to
(17) The self-piercing rivet 20 penetrates the lower substrate 12 to create a mechanical interlock, thereby joining the lower substrate 12 and the upper substrate 14 together. The preformed interior cavity 28 of the lower substrate 12 may or may not be plastically deformed after installation of the self-piercing rivet 20. The preformed button 18 and the preformed internal cavity 28 receive the displaced material 92, 94 and reduce the force exerted on the lower substrate 12 in the area of the preformed button 18. By preforming the button 18, any tendency for the button 18 to crack or split is substantially reduced.
(18) With the lower substrate 12 having a preformed exterior profile, the lower substrate 12 may be made of a brittle material. Therefore, a brittle material or a low-strain material may be easily joined to another material by a self-piercing rivet.
(19) The joined composite or assembly 10 constructed in accordance with the teachings of the present application may be used to form vehicle body and closure parts in automobiles or in any applications which require joining of two or more layers of materials.
(20) It should be noted that the disclosure is not limited to the embodiment described and illustrated as examples. A large variety of modifications have been described and more are part of the knowledge of the person skilled in the art. These and further modifications as well as any replacement by technical equivalents may be added to the description and figures, without leaving the scope of the protection of the disclosure and of the present patent.