The present disclosure relates generally to a double-action clinching method and a tool for performing the same.
Materials may be secured together using many different methods, including, for example, hot clinching and friction stir spot welding. Hot clinching techniques often result in the thermal expansion of the materials, while friction stir spot welding often results in brittle phase formation when joining different materials (e.g., aluminum and magnesium). Other clinching techniques may require the precise alignment of the clinching tool with particular features of the materials to be clinched and/or may result in the splitting or cracking of the clinch button.
A double-action clinching method includes establishing a first layer on a second layer, where the first layer has less ductility than the second layer. The first and second layers are secured between a punch and a clinching punch of a double action clinching tool such that: i) a support of the tool receives a portion of a surface of the second layer, and ii) the clinching punch slidably positioned in the support is adjacent to another portion of the surface of the second layer; and the punch, positioned opposed to the clinching punch, is adjacent to a portion of a surface of the first layer. The punch has a first diameter, and the clinching punch has a second diameter that is smaller than the first diameter. The punch is pressed into the portion of the surface of the first layer, thereby forming an aperture through the first layer. The clinching punch is pressed into the other portion of the surface of the second layer in a direction opposite to the pressing of the punch, thereby forcing at least a portion of the second layer into the aperture and forming at least a flush-back joint with micro-interlocking between a side wall of the aperture and the at least the portion of the second layer.
Features and advantages of the present disclosure will become apparent by reference to the following detailed description and drawings, in which like reference numerals correspond to similar, though perhaps not identical, components. For the sake of brevity, reference numerals or features having a previously described function may or may not be described in connection with other drawings in which they appear.
Embodiments of the double-action clinching method disclosed herein advantageously enable the formation of a mechanical joint with interlocking at the microscopic level or at microscopic and macroscopic levels. The method clinches overlapping sheets of material, but does not require precise alignment of the clinching tool with any particular area (e.g., a preformed aperture) of the sheets. Furthermore, it is believed that because the method pierces an aperture in one of the materials (instead of both materials), the resulting joint is watertight.
Referring now to
The first and second layers 12, 14 are, in an embodiment, preformed sheets or components such as, for example, preformed automotive body parts (e.g., fenders and reinforcing panels). It is to be understood, however, that the layers 12, 14 may otherwise be formed into a particular component after they are joined together.
One layer 12 overlies at least a portion of the other layer 14 at least at an area where it is desirable to join the two layers 12, 14 together. In some instances, the first layer 12 will completely overlie the second layer 14, and in other instances, the first layer 12 will partially overlie the second layer 14. The first layer 12 (i.e., the layer that will receive a punch 20, described further hereinbelow) is generally less ductile than the second layer 14 (i.e., the layer that will receive a clinching punch 22, described further hereinbelow). As used herein, “ductility” is expressed in terms of percent (%) elongation achieved when a strip sample is pulled to failure in a uni-axial tensile test at room temperature. For the double-action clinching process disclosed herein, it is believed that desirable ductility values are as follows: the first layer 12 has less than 20% elongation and the second layer 14 has more than 30% elongation. It is to be understood, however, that the ductility of the layers 12, 14 may vary depending, at least in part, on the tool design and desired workpiece thickness.
Non-limiting examples of the first layer 12 include magnesium alloyed with at least aluminum and zinc such as, e.g., Magnesium Alloy AZ31B and AZ91D. Non-limiting examples of the second layer 14 include aluminum alloyed with magnesium such as, e.g., Aluminum Alloy 5754 and Aluminum Alloy 5083.
The tool 10 further includes the previously mentioned punch 20 and clinching punch 22. In a non-limiting example, the punch 20 and the clinching punch 22 are both made from hardened tool steel. The clinching punch 22 is slidably positioned in the support aperture 18, and the punch 20 is positioned opposite to the clinching punch 22. In one example, both the punch 20 and the clinching punch 22 have a circular cross section, but the diameter of the punch 20 is larger than the diameter of the clinching punch 22. In an example, the diameter of the punch 20 ranges from about 10 mm to about 50 mm, and the diameter of the clinching punch 22 ranges from about 8 mm to about 48 mm. It is to be understood, however, that the diameter of the punch 20 and the clinching punch 22 may be selected based on several factors including, for example, the thickness of the layers 12, 14, a desired strength of the joint between the layers 12, 14, the amount of space or overlap available on the layers 12, 14, and combinations thereof. It is to be further understood that the cross sectional shape of the punch 20 and clinching punch 22 may be some shape other than circular, but the diameter (or other suitable measurement) of the punch 20 is always larger than that of the clinching punch 22. For example, if the cross sectional shapes of the punch 20 and clinching punch 22 are square, the respective diameters are the diagonal length of each square. In this example, the diagonal length of the punch 20 would be larger than the diagonal length of the clinching punch 22.
When the layers 12, 14 are positioned in the tool 10, the support 16 receives a portion of a surface S2 of the second layer 14, the clinching punch 22 is adjacent to another portion of the surface S2, and the punch 20 is adjacent to a portion of a surface S1 of the first layer 12. As previously mentioned, the punch 20 and clinching punch 22 are positioned opposite to each other. Such positioning enables the punch 20 (when engaged) to form an aperture (labeled 26 and shown in
The tool 10 also includes a retractable clinching die 24. When the layers 12, 14 are positioned in the tool 10, the retractable clinching die 24 contacts the first layer 12. In addition to being positioned between the punch 20 and clinching punch 22, the layers 12, 14 are also positioned between the retractable clinching die 24 and the support 16. The clinching die 24 generally functions as a stripper ring to facilitate removal of the punch 20 from the first layer 12 (which occurs between
Referring now to
A slug 28 of the first layer 12 is displaced from the first layer 12 when the aperture 26 is formed therein. The slug 28 may be removed from the tool 10 and workpiece area upon completion of pressing the punch 20 and pressing the clinching punch 22 (described further hereinbelow). In one example, the slug 28 is pushed away from the layers 12, 14 as a result of the pressing of the clinching punch 22 into the second layer 14. The slug 28 may be trapped between the punch 20 and the flush-back joint (shown in
With reference now to
As shown in the Figures, one end of the support aperture 18 opens into a cavity C that is configured with a diameter and a depth that are large enough to receive the slug 28 and the portion of the second layer 14 that stretches when the punch 20 is engaged. As such, the dimensions of the cavity C depend, at least in part, on the diameters and shapes of punches 20, 22, and the thicknesses of the layers 12, 14. Furthermore, since the support aperture 18 opens into the cavity C, the clinching punch 22 may extend through the cavity C when it is engaged.
After the aperture 26 is formed in the first layer 12, the punch 20 is no longer pressed, and the clinching punch 22 is pressed in a direction opposite to the direction in which the punch 20 is pressed. As shown in
As shown in
As shown in
When the layer 14 contacts the interior walls(s) 32, the die 24 shifts such that one area of the interior walls(s) 32 continues to contact the punch 20, while the other area of the interior walls(s) 32 is pushed radially outward from the punch 20. Once the desirable amount of the second layer 14 flows onto the surface S1, the clinching punch 22 is no longer pressed. The clinched layers 12, 14 may then be removed from the tool 10.
The punch 20, the clinching punch 22, and the support 16 are retracted axially away from the layers 12, 14. This allows the joined layers 12, 14 to be laterally removed from the tool 10. When the retractable clinching die 24 retracts, the walls 32 return to the initial position, and the tool 10 is ready to receive other layers 12, 14.
While several embodiments have been described in detail, it will be apparent to those skilled in the art that the disclosed embodiments may be modified. Therefore, the foregoing description is to be considered exemplary rather than limiting.