1. Introduction
Until recently, techniques based on resistance welding, welding, or laser welding were the most common methods of joining car body elements. Due to the fact that these processes generate harmful gaseous compounds and influence mechanically and thermally the material structure of the joined elements, other joining processes have been developed. For some time, the clinching process with an additional rivet and self-piercing riveting has been one of the methods most frequently used than welding [
1,
2]. The mentioned joining techniques allow to obtain a joint with relatively high stiffness and strength compared to clinch joints (”CL”) [
3]. Clinching can be used to join galvanized sheets or sheets with other coatings [
4]. The clinching technology can replace resistance welding in some cases [
5]. Clinching technology has such great potential that it is constantly being developed [
6]. Modifications to this technology are being introduced, and one of them is additional local heating of the materials before joining [
7] or welding the bottom of the embossment [
8]. Another modification of clinching joining technology is joining sheets with a hole already been made in the lower layer [
9]. This method is suitable for joining composites with metals. One of the other methods of connecting without the need to make holes is self-piercing riveting (”SPR”) [
10,
11]. In the ”SPR” joining process, the upper sheet is pierced. Hole-less riveting can be used to join together various metal materials, including aluminum alloys, but also to join together various construction materials, e.g., various metal compositions [
12,
13] or titanium alloys [
14,
15].
When joining using the clinch-riveting method, the continuity of the material of the joined sheets is maintained, and there is no intentional puncture of the joined material layers. As a result of the use of an additional rivet to form the clinch joint, a relatively large increase in the maximum load capacity is achieved [
16,
17,
18,
19].
The formation of the clinch-rivet joint can be performed using a full deformable steel rivet of various hardness [
20]. The authors of work [
20] presented the results of research on the influence of different hardnesses of the rivets (350HV1, 400HV1, 420HV1) on the forming force, geometric parameters and the load capacity of the joint for steel sheets.
In the case of selected materials, it is also possible to join them with an additional rivet (without damaging the joined sheets) using a die with a flat surface. In [
18], a flat die was used to join aluminum alloy sheets. An analysis of the influence of the blank holder force on the geometric parameters and the load capacity of the joint was presented.
The full rivet can be used to repair clinch joints with damage of the joined sheets in the embossment area [
21,
22]. A rivet with a hole allows for reducing the energy consumption of the forming process while maintaining a high load capacity of the joint [
23]. The paper [
23] presents the influence of different diameters of the hole in the rivet on the formation and load capacity of the lap joint of DX51D steel sheets. The lowest forming force was observed for a through hole with a diameter of 2.5 [mm]. The formation of the ”CR” joint was done using a rivet made of material of different hardness.
A rivet made of aluminum alloy with a hole can also be used to strengthen a damaged clinch joint [
24]. In [
25], the authors presented research on joining using a solid rivet and a hole rivet in a two-stage forming process. It is also possible to completely simplify the shape of the die and use a special blank holder in the process of pressing the rivet into the joined materials [
26]. Another method of joining using a full rivet was presented in works [
27,
28,
29,
30,
31,
32]. To join layers of different materials, a high-hardness rivet was used. The rivet punched a hole, and afterward it was blocked with the joined material.
All modifications and innovations in pressure joining technologies are one of the trends in the automotive industry [
33,
34]. It should be mentioned that each method of joining thin-walled elements causes deformation of the material around the joining point. During joining, there is a local change in the structure of the material and there is a specific deformation of the surface of the joined sheets [
35].
This work presents research, results, and analysis of the possibility of using a steel deformable rivet with a hardness of 400HV1 as an additional element for forming a clinch joints for sheets made of micro-alloyed steel and F type zinc coating (ZiNc). A solid full rivet was used to form the clinch-rivet joints. The rivet was pressed to a different depth (offset) relative to the upper surface of the sheets using an ‘SKB’ die. Forming with different offsets was carried out for three different ‘SKB’ die depths with movable and fixed segments. In addition, the energy consumption of the forming process was analysed for various variants of the die depth. The basic geometry in the cross-section of the joints was measured, and the deformation of the sheets was measured in the case of the highest observed values of sheet deviation, i.e. for the case of the matrix depth hd=1.45 [mm]. The load capacity of the joints was also tested for a lap joint made of 1.5 [mm] thick HX340 steel sheets.
Author Contributions
Conceptualization, Ł.B., J.M. and W.W.; methodology, Ł.B., J.M. and W.W; software, W.W.; validation, Ł.B., W.W.; formal analysis, J.M.; investigation, Ł.B., J.M. and W.W; resources, J.M.; data curation, Ł.B.; writing—original draft preparation, J.M.; writing—review and editing, Ł. B., W.W.; visualization, Ł.B., J.M. and W.W.; supervision, J.M.; project administration, Ł.B.; funding acquisition, Ł.B., J.M. and W.W. All authors have read and agreed to the published version of the manuscript.
Figure 1.
The main phases of the sheet joining process: a) the rivet positioning in the clinch riveting punch system before placing the sheets for joining - phase I, b) pressing the rivet into the joined layers of materials - phase II, c) final pressing of the rivet at the bottom of the die - phase III, d) clinch-rivet joint after retraction of the clinch riveting punch system; 1-SKB die with movable segments, 2-sliders in the punch system, 3-punch, 4-joined sheets, 5-bush of the punch system, 6-rivet after forming process, 7-bush of the die system, 8-pin of the die system, 9- bush die with movable segments.
Figure 1.
The main phases of the sheet joining process: a) the rivet positioning in the clinch riveting punch system before placing the sheets for joining - phase I, b) pressing the rivet into the joined layers of materials - phase II, c) final pressing of the rivet at the bottom of the die - phase III, d) clinch-rivet joint after retraction of the clinch riveting punch system; 1-SKB die with movable segments, 2-sliders in the punch system, 3-punch, 4-joined sheets, 5-bush of the punch system, 6-rivet after forming process, 7-bush of the die system, 8-pin of the die system, 9- bush die with movable segments.
Figure 2.
The set of tools used for the experimental formation of “CR” joints: a) the clinch riveting punch system, b) set of pins with a depth of hd=1.45 [mm], 1.60 [mm], 1.75 [mm], c) bush die with pin and movable segments, d) top view of die with flat bottom.
Figure 2.
The set of tools used for the experimental formation of “CR” joints: a) the clinch riveting punch system, b) set of pins with a depth of hd=1.45 [mm], 1.60 [mm], 1.75 [mm], c) bush die with pin and movable segments, d) top view of die with flat bottom.
Figure 3.
The basic geometry and dimension of: a) the rivets, b) the die and rivet pressing punch (in [mm]).
Figure 3.
The basic geometry and dimension of: a) the rivets, b) the die and rivet pressing punch (in [mm]).
Figure 4.
The relative position of the upper surface of the rivet in the joint: a) rivet final position for offset of =0, b) rivet final position for offset of =0.6 (of in [mm]).
Figure 4.
The relative position of the upper surface of the rivet in the joint: a) rivet final position for offset of =0, b) rivet final position for offset of =0.6 (of in [mm]).
Figure 5.
The characteristics of: a) the base external surface of the lower sheet, b) the transverse plane of the joint cross-section, c) the initial position of the sheets in relation to the bottom of the die; 1-upper sheet metal, 2-lower sheet metal, 3-surface of the bottom of the die (reference surface for the position of the sheets), 4-embossment, 5-outer lower surface of the embossment, 6-cross-sectional plane of the joint, 7-boundaries of the scanned area of the upper and lower surfaces of the joint , 8-die with movable segments, 9-places of interaction of fixed segments of the die.
Figure 5.
The characteristics of: a) the base external surface of the lower sheet, b) the transverse plane of the joint cross-section, c) the initial position of the sheets in relation to the bottom of the die; 1-upper sheet metal, 2-lower sheet metal, 3-surface of the bottom of the die (reference surface for the position of the sheets), 4-embossment, 5-outer lower surface of the embossment, 6-cross-sectional plane of the joint, 7-boundaries of the scanned area of the upper and lower surfaces of the joint , 8-die with movable segments, 9-places of interaction of fixed segments of the die.
Figure 6.
The characteristics of: a) the flatness of the base surface of the sheets, before joining (in [mm]), b) comparison of the 3D scan model with the base model of the location of the characteristic joint surfaces (1-upper base surface, 2-bottom base surface).
Figure 6.
The characteristics of: a) the flatness of the base surface of the sheets, before joining (in [mm]), b) comparison of the 3D scan model with the base model of the location of the characteristic joint surfaces (1-upper base surface, 2-bottom base surface).
Figure 7.
The basic interlock parameters of the “CR” joint.
Figure 7.
The basic interlock parameters of the “CR” joint.
Figure 8.
The “CR” joint lap samples: a) dimensions (in [mm]), b) mounted on the tensile test machine with an extensometer system.
Figure 8.
The “CR” joint lap samples: a) dimensions (in [mm]), b) mounted on the tensile test machine with an extensometer system.
Figure 9.
The examples of forming force-displacement diagrams for “CR” joining with the die with three values of the depth (hd in [mm]).
Figure 9.
The examples of forming force-displacement diagrams for “CR” joining with the die with three values of the depth (hd in [mm]).
Figure 10.
The influence of the offset value of on: a) the forming force Ff, b) forming energy consumption Ef (hd in [mm]).
Figure 10.
The influence of the offset value of on: a) the forming force Ff, b) forming energy consumption Ef (hd in [mm]).
Figure 11.
The view of the embossment form the die side of the “CR” joint and the depth of the die: a) hd =1.45, b) hd =1.60, c) hd=1.75 (in [mm]).
Figure 11.
The view of the embossment form the die side of the “CR” joint and the depth of the die: a) hd =1.45, b) hd =1.60, c) hd=1.75 (in [mm]).
Figure 12.
The “CR” joint cross-sections on macro scale (in [mm]).
Figure 12.
The “CR” joint cross-sections on macro scale (in [mm]).
Figure 13.
The influence of the depth of the die (hd) and the offset value (of) on: a) the maximum diameter of the rivet – d1, b) the minimum thickness of the sheet in the interlock – h2 and h3.
Figure 13.
The influence of the depth of the die (hd) and the offset value (of) on: a) the maximum diameter of the rivet – d1, b) the minimum thickness of the sheet in the interlock – h2 and h3.
Figure 14.
The influence of the depth of the die (hd) and the offset value (of) on the interlock parameters: a) tu, b) tn.
Figure 14.
The influence of the depth of the die (hd) and the offset value (of) on the interlock parameters: a) tu, b) tn.
Figure 15.
The comparison of the interlock shape for different values of the depth of the die (hd) and the offset value (of): a) for rivet, b) line between lower and upper sheets.
Figure 15.
The comparison of the interlock shape for different values of the depth of the die (hd) and the offset value (of): a) for rivet, b) line between lower and upper sheets.
Figure 16.
The influence of the offset value (of) on the sheet deformation in the join axis area (hd=1.45 [mm]).
Figure 16.
The influence of the offset value (of) on the sheet deformation in the join axis area (hd=1.45 [mm]).
Figure 17.
The schematics of: a) the blank holder acting during formation process, b) the effect of the sheet material relaxation after the tools were withdrawn.
Figure 17.
The schematics of: a) the blank holder acting during formation process, b) the effect of the sheet material relaxation after the tools were withdrawn.
Figure 18.
The examples of the influence of the offset value (of) on the sheet deviations – hd=1.45 [mm].
Figure 18.
The examples of the influence of the offset value (of) on the sheet deviations – hd=1.45 [mm].
Figure 19.
The influence of the depth of the die (hd) and the offset value (of) on the maximum shear force during tensile shear tests of the “CR” joint.
Figure 19.
The influence of the depth of the die (hd) and the offset value (of) on the maximum shear force during tensile shear tests of the “CR” joint.
Figure 20.
The examples of the forming force-displacement diagrams for “CR” joint formed with the different values of the depth of the die (hd in [mm]) and offset value of=0 [mm].
Figure 20.
The examples of the forming force-displacement diagrams for “CR” joint formed with the different values of the depth of the die (hd in [mm]) and offset value of=0 [mm].
Figure 21.
The examples of the forming force-displacement diagrams and stiffness-displacement diagrams for “CR” joint formed with the depth of the die hd: a) 1.45 [mm], b) 1.60 [mm], c) 1.75 [mm].
Figure 21.
The examples of the forming force-displacement diagrams and stiffness-displacement diagrams for “CR” joint formed with the depth of the die hd: a) 1.45 [mm], b) 1.60 [mm], c) 1.75 [mm].
Figure 22.
The influence of the depth of the die (hd) on the joint stiffness for different values of displacement for offsets of: a) 0 [mm], b) 0.3 [mm], c) 0.6 [mm].
Figure 22.
The influence of the depth of the die (hd) on the joint stiffness for different values of displacement for offsets of: a) 0 [mm], b) 0.3 [mm], c) 0.6 [mm].
Figure 23.
The example of the samples deformation stages during tensile shear test.
Figure 23.
The example of the samples deformation stages during tensile shear test.
Figure 24.
The forces acting scheme during the tensile shear test of the “CR” joint.
Figure 24.
The forces acting scheme during the tensile shear test of the “CR” joint.
Figure 25.
The influence of the depth of the die (hd) and the offset value (of) on the deviations of the sheets after tensile shear test.
Figure 25.
The influence of the depth of the die (hd) and the offset value (of) on the deviations of the sheets after tensile shear test.
Figure 26.
The macrostructure of the “CR” joint after tensile shear with a marked deviation of the joint axis.
Figure 26.
The macrostructure of the “CR” joint after tensile shear with a marked deviation of the joint axis.
Table 1.
Chemical composition of HX340LAD+Z sheet (maximum percentage by weight [%]).
Table 1.
Chemical composition of HX340LAD+Z sheet (maximum percentage by weight [%]).
Mn |
Si |
Ti |
C |
Nb |
P |
S |
Al |
Fe |
0.88 |
0.01 |
0.011 |
0.09 |
0.031 |
0.02 |
0.007 |
0.032 |
remainder |
Table 2.
Mechanical properties of sheets HX340LAD+Z.
Table 2.
Mechanical properties of sheets HX340LAD+Z.
Material designation |
Surface finish +Z [g/m2] |
Young’s modulus E, [GPa] |
Poisson’s ratio |
Yield strength Rp0.2 [MPa] |
Tensile strength Rm, [MPa] |
Elongation after fracture A80, [%] |
Strength coefficient K, [MPa] |
Strain hardening exponent n, [-] |
HX340 |
zinc layer quality 100 |
188 |
0.29 |
365 |
463 |
29 |
807 |
0.16 |
Table 3.
The list of “CR” joint variants.
Table 3.
The list of “CR” joint variants.
Offset dimension of [mm] |
Die depth hd [mm] |
1.45 |
1.60 |
1.75 |
0 |
I-00 |
II-00 |
III-00 |
0.15 |
I-15 |
II-15 |
III-15 |
0.30 |
I-30 |
II-30 |
III-30 |
0.45 |
I-45 |
II-45 |
III-45 |
0.60 |
I-60 |
II-60 |
III-60 |