Patent Application
20240269730
The present application relates to self-piercing riveting (SPR) technologies. More specifically, the present application relates to dies used in the installation of self-piercing rivets.
Self-piercing riveting (SPR) is a high-speed mechanical fastening process for joining two or more sheets of material without a predrilled or punched hole. Typically, SPR processes are conducted by driving a semi-tubular rivet through top layers of material and upsetting the rivet in a lower layer (without completely piercing the lower layer) to form a durable mechanical joint. Attempts have been made to use existing SPR technologies to join materials with reduced ductility and formability, such as magnesium alloys, which offer the potential for weight reduction over steel and aluminum alloys. However, the mechanical properties of magnesium alloys limit their use in SPR processes. For example, as a result of their reduced formability, magnesium alloys may become easily damaged during installation of the rivet into the material, and the structural integrity of the resulting magnesium alloy casting is reduced.
It would be advantageous to provide an improved method and/or system to facilitate the fastening of magnesium alloys during SPR operations that overcomes the foregoing challenges.
At least one embodiment of the present disclosure relates to a self-piercing riveting (SPR) die. The SPR die includes a die body including an outer surface, a lower surface that is parallel to and offset from the outer surface, and a side surface that circumscribes the lower surface and extends between the lower surface and the outer surface. A distance between the lower surface and the outer surface is within a range between approximately 0.4 mm to 1.2 mm. An angle between the side surface and the lower surface is within a range between approximately 55 to 80 degrees. An inner diameter of the outer surface is within a range between approximately 13 to 18 mm.
In some embodiments, the inner diameter is within a range between 14 mm to 18 mm.
In some embodiments, the outer surface, the lower surface, and the side surface are disposed at a first end of the die body. In some embodiments, the outer surface is concentric with the lower surface.
In some embodiments, the side surface is a tapered surface having a greater diameter proximate to the outer surface than the lower surface. For example, the side surface may be a frustoconical shaped surface.
In some embodiments, the angle between the side surface and the lower surface is within a range between approximately 59 degrees and 69.4 degrees relative to the lower surface.
In some embodiments, a radius at a transition between the side surface and the outer surface is approximately the same as a radius at a transition between the lower surface and the side surface.
In some embodiments, the side surface and the lower surface together define a recessed area having a die volume within a range between 80 mm3 to 150 mm3.
Another embodiment of the present disclosure relates to an SPR joint. The SPR joint includes an upper layer, a lower layer including a magnesium material, and a rivet extending through the upper layer and into the lower layer. The rivet includes a head, a cylindrical extension extending away from the head, and a web extending radially inwardly of the cylindrical extension. A thickness of the web is less than or approximately equal to a thickness of the head.
In some embodiments, the thickness of the web is less than or equal to approximately 1.5 mm.
In some embodiments, the head and the cylindrical extension together defining an interior cavity. In such embodiments, the upper layer may extend axially into the interior cavity to a region that is approximately axially aligned with the head.
In some embodiments, the rivet forms a protrusion in the lower layer, a volume of the protrusion being within a range between (i) cVp, and (ii) cVp+138, where Vp represents a pierced volume of the upper layer that is occupied by the rivet, and c is a constant that varies within a range between approximately 12.5 to 13.
In some embodiments, the upper layer includes one of a steel material, an aluminum material, or the magnesium material.
In some embodiments, a thickness of the upper layer is less than or equal to approximately 2.5 mm, and a thickness of the lower layer is within a range between approximately 3 to 3.6 mm.
In some embodiments, the thickness of the web is less than or equal to approximately 1.5 mm when an upper layer material of the upper layer has an ultimate tensile strength (UTS) of greater than or equal to approximately 700 MPa, less than or equal to approximately 0.5 mm when the UTS of the upper layer material is within a range between approximately 400 to 700 MPa, and less than or equal to approximately 0.2 mm when the UTS of the upper layer material is within a range between approximately 250 to 400 MPa.
Another embodiment relates to a method of forming an SPR joint. The method includes providing a stack including an upper layer and a lower layer, where the upper layer and/or lower layer includes a magnesium layer. The method also includes engaging an outer surface of the SPR die with a surface of the stack. The SPR die includes a lower surface and a side surface circumscribing the lower surface and extending between the lower surface and the outer surface. The lower surface is spaced apart from the outer surface by a distance that is within a range between approximately 0.4 mm to 1.2 mm. An angle between the side surface and the lower surface is within a range between approximately 55 degrees to 80 degrees. An inner diameter of the outer surface is within a range between approximately 13 mm to 18 mm. The method further includes pressing an SPR rivet through the stack toward the SPR die.
In some embodiments, the method further includes determining a web thickness of the rivet based on a material property of the upper layer, and selecting the rivet based on the web thickness. The material property may be an ultimate tensile strength of the upper layer.
In some embodiments, the method further includes determining a die volume of the SPR die based on a pierced volume of the upper layer.
In some embodiments, pressing the rivet through the stack includes pressing a head of the rivet toward the stack to deform the upper layer into an interior cavity defined by the rivet so that the upper layer extends axially into the interior cavity to a region that is approximately axially aligned with the head.
This summary is illustrative only and should not be regarded as limiting.
The disclosure will become more fully understood from the following detailed description, taken in conjunction with the accompanying figures, wherein like reference numerals refer to like elements, in which:
Before turning to the figures, which illustrate certain exemplary embodiments in detail, it should be understood that the present disclosure is not limited to the details or methodology set forth in the description or illustrated in the figures. It should also be understood that the terminology used herein is for the purpose of description only and should not be regarded as limiting.
The present disclosure relates to self-piercing riveting (SPR) technologies and forming tools for SPR processes. SPR is a technique used to join sheets of materials (either the same material or dissimilar materials) together. These SPR technologies are particularly useful in automotive applications, such as in joining materials at the location of shock towers for vehicle suspension systems and installation of vehicle body panels. Unlike conventional riveting operations, which require hole and/or openings to guide the rivets through the sheets before fastening the materials together, the rivets used in SPR joints require no predrilling or machining of the receiving materials. Rather, the rivets are pressed through unformed sheets and deform and/or pierce the sheets to create a robust mechanical interlock. Although the SPR processes are described herein as being applied to or forming part of a vehicle body or structural layer, it should be understood that the same SPR design and process may be implemented in other non-vehicle applications where lightweight castings may be used.
To install the SPR rivet, the sheets of material are layered on top of one another in a desired orientation. The stack of materials is then clamped between a die and a blank holder (e.g., fixture, etc.) that holds the stack against the die. Next, a press drives the rivet, from an upper side of the stack, into the stack and toward the die, piercing the upper sheet(s) and causing the lower sheet to deform into the die. The shape of the die causes the rivet and the lower sheet to flair outwards, forming a button-shaped protrusion in the lower sheet and a robust mechanical connection to hold the sheets together. SPR joining techniques work particularly well for connecting sheets made from steel and aluminum alloys (e.g., metals having a face-centered cubic metal crystalline structure (FCC) or face-centered cubic crystalline structure (BCC) which provide enough slip planed during deformation), which have high ductility and formability to reduce the likelihood of cracking during rivet installation.
Magnesium alloys provide a strong and lightweight alternative to aluminum and other metals used in vehicle applications, and can increase the overall performance of the vehicle by reducing vehicle weight. However, compared to their aluminum and steel counterparts, the hexagonal closed pack crystalline structure of magnesium alloys reduces the maximum allowable deformation of the material before cracking occurs. Such cracking at the SPR joint can reduce the structural integrity of castings.
By way of example,
Referring now to
In at least one embodiment, the forming die includes a recessed area (e.g., cavity, depression, etc.) that is uniquely shaped to control the volume of deformed magnesium alloy during rivet installation, to reduce overall deformation, and to reduce transitions (e.g., sharp edges, corners, etc.) at the outer edge of the button. Among other benefits, the forming die and die selection method have proved capable of joining a wide range of materials and material thicknesses using existing die installation devices without cracking the magnesium alloy sheet.
In at least one exemplary embodiment, the shank 104 is a cylindrically-shaped extension (e.g., rod, post, etc.) that extends parallel to a central axis 110 of the die body 102, such that the shank 104 is concentric with the die body 102. The shank 104 may include at least one slot, notch, cut, groove, channel, or the like to facilitate engagement with the joining device or coupling between the shank 104 and the joining device. As shown in
As shown in
The upper layer 602 may be a rivet-facing layer through which the rivet enters the casting. In at least one embodiment, the upper layer 602 (e.g., the first layer, the top layer, sheet, etc.) includes at least one steel material layer and/or one aluminum material layer and/or another metallic layer. In other embodiments, the upper layer 602 may include a plastic layer. In some embodiments, the upper layer 602 includes multiple layers of the same or different materials. The steel layer(s) may have a variety of different compositions. For example, in one embodiment, the steel may be a low carbon steel (e.g., mild steel) having iron alloyed with about 0.25 wt % carbon. In another embodiment, the steel may be a high carbon steel having iron alloyed with up to about 2.5 wt % carbon. In other embodiments, the steel may be a stainless steel having iron alloyed with chromium and nickel. According to other embodiments, steel may be used including at least one of iron, carbon, manganese, chromium, nickel, tungsten, molybdenum, boron, titanium, vanadium, cobalt, niobium, or a combination thereof. For example, the steel layer may include CR3 steel, which includes about 0.10% carbon (C), about 0.45% manganese (Mn), at most 0.03% sulfur (S), at most 0.04% phosphorus (P), balance iron (Fe), and trace impurities, a CR2 steel (e.g., a mild steel CR2 having an ultimate tensile strength (UTS) of approximately 319 MPa, etc.), a ferrite-martensite dual phase (DP) 600 steel (e.g., a dual phase steel DP600 having a UTS of approximately 640 MPa, a dual phase steel DP780 having an UTS of approximately 767 MPa, etc.), which includes about 0.10% carbon (C), about 1.4% manganese (Mn), about 0.14% silicon (Si), balance iron (Fe), and trace impurities, galfan (GF) steel and/or cold formed (CF) steel composite, advanced high strength (AHSS) steel, and/or another steel or steel alloy.
The aluminum layer(s) may include an aluminum casting, an aluminum extrusion, an aluminum sheet, or the like. In one embodiment, at least one layer of aluminum may be a 1000 series aluminum alloy, a 2000 series aluminum alloy, a 3000 series aluminum alloy, a 4000 series aluminum alloy, a 5000 series aluminum alloy (e.g., an aluminum 5083 having an UTS of approximately 276 MPa), a 6000 series aluminum alloy (e.g., an aluminum 6061-T6 having an UTS of approximately 326 MPa, etc.), a 7000 series aluminum alloy, or an 8000 series aluminum alloy.
The 1000 series aluminum alloy (i.e. 1050, 1060, 1070, 1100, 1145, 1199, 1350, etc.) is essentially pure aluminum with a minimum 99 wt % aluminum content and may be work hardened. The 2000 series aluminum alloy (i.e. 2011, 2014, 2024, 2036, 2048, 2090, 2091, 2099, 2124, 2195, 2218, 2219, 2319, 2618, etc.) is alloyed with copper and may be precipitation hardened to strengths comparable to steel. The 3000 series aluminum alloy (i.e. 3003, 3004, 3005, 3102, 3103, 3105, 3303, etc.) is alloyed with manganese and may be work hardened. The 4000 series aluminum alloy (i.e. 4006, 4007, 4015, 4032, 4043, etc.) is alloyed with silicon. The 5000 series aluminum alloy (i.e. 5005, 5010, 5019, 5026, 5050, 5052, 5056, 5059, 5083, 5086, 5154, 5182, 5252, 5254, 5356, 5454, 5456, 5457, 5652, 5657, 5754, Al3Mg, etc.) is alloyed with magnesium and offer enhanced corrosion resistance. The 6000 series aluminum alloy (i.e. 6005, 6009, 6010, 6060, 6061, 6063, 6063A, 6065, 6066, 6070, 6081, 6082, 6101, 6105, 6151, 6162, 6201, 6205, 6262, 6351, 6463, etc.) is alloyed with magnesium and silicon and is machinable, weldable, and may be precipitation hardened. The 7000 series aluminum alloy (i.e. 7005, 7039, 7049, 7050, 7068, 7072, 7075, 7079, 7116, 7129, 7175, 7178, 7475, etc.) is alloyed with zinc and may be precipitation hardened to the highest strengths of any aluminum alloy, with a tensile strength up to 700 MPa. The 8000 series aluminum alloy (i.e. 8011, 8090, etc.) is alloyed with elements which are not covered by 1000-7000 series aluminum alloys.
In at least one embodiment, the upper layer 602 instead includes a magnesium casting, magnesium extrusion, magnesium sheet, or another magnesium material layer.
In at least one embodiment, the lower layer 604 (e.g., the second layer, the bottom layer, sheet, etc.) includes a magnesium layer, such as a magnesium alloy, which may or may not form part of a vehicle structure (e.g., a shock tower, a vehicle frame or support member, etc.). The magnesium alloy may be, for example, AE42, AE44, AM20, AM40, AM50, AM60, AM60B, AS21, AS41, AZ31, AZ61, AZ63, AZ80, AZ81, AZ91, Elektron 21, Elektron 675, EZ33, HK31, HM21, HZ32, KIA, LA141, LA103, LAZ43, MI, MIA, QE22, QH21, WE43, WE54, ZC63, ZC71, ZE41, ZK10, ZK20, ZK30, ZK40, ZK51, ZK60, ZK61, ZM21, ZMC711, any alloys with magnesium contents of 80% of higher, or a combination thereof. In at least one exemplary embodiment, the magnesium layer may include AM60B magnesium alloy, which includes about 5.5-6.5% aluminum (Al), about 0.24-0.6% manganese (Mn), at most about 0.22% zinc (Zn), at most about 0.1% silicon (Si), at most about 0.01% copper (Cu), at most about 0.005% iron (Fe), at most about 0.002% nickel (Ni), balance magnesium (Mg), and trace impurities. The lower layer 604 may be a magnesium casting, a magnesium extrusion, a magnesium sheet, or the like. In at least one exemplary embodiment, the magnesium layer may include a coating material. For example, the magnesium layer may be pre-coated using an electrophoretic coating or may include a powder coat on a lower surface that faces the die body 102. In some embodiments, the lower layer 604 includes another material with reduced formability relative to the upper layer(s) 602.
The thickness of each material layer may vary depending on the desired properties of the stack 600. Among other benefits, the same die body 102 design may be used to accommodate a wide variety of material layer thicknesses without causing cracking of the magnesium die casting. As shown in
As utilized herein with respect to numerical ranges, the terms “approximately,” “about,” “substantially,” and similar terms generally mean+/−10% of the disclosed values, unless specified otherwise. As utilized herein with respect to structural features (e.g., to describe shape, size, orientation, direction, relative position, etc.), the terms “approximately,” “about,” “substantially,” and similar terms are meant to cover minor variations in structure that may result from, for example, the manufacturing or assembly process and are intended to have a broad meaning in harmony with the common and accepted usage by those of ordinary skill in the art to which the subject matter of this disclosure pertains. Accordingly, these terms should be interpreted as indicating that insubstantial or inconsequential modifications or alterations of the subject matter described and claimed are considered to be within the scope of the disclosure as recited in the appended claims.
The die body 102 is uniquely shaped to limit the deformation of the magnesium layer (e.g., the lower layer 604) while allowing the rivet to achieve proper volume displacement during the joining operation to ensure a robust mechanical interlock between the sheets in the stack 600 with reducing the risk of cracking at the SPR joint. As shown in
As shown in
As shown in
In some embodiments, the dimensions of the die body 102 (e.g., the recessed area 114), and the button or protrusion at the SPR joint may be determined based on the material properties of at least one material layer of the die casting, as will be further described. For example, the die volume (e.g., a diameter of the die volume inclusive of the inner diameter 128, a depth of the recessed area that defines the die volume such as the axial distance 126, etc.) may be determined based on a volume of displaced material from the upper layer 602 (e.g., the rivet-facing layer, the non-magnesium layer, etc.) during the riveting operation. For example, the die volume may be determined based on a volume of the upper layer 602 that is pierced by the rivet. The pierced volume of the upper layer 602 may be determined based on (i) the thickness 603 (see
In at least one embodiment, the die volume of the die used in the SPR operation (and/or the volume of the button-shaped protrusion in the lower layer formed by the SPR operation) increases with the pierced volume of the upper layer 602, such as with the thickness 603 of the upper layer 602. The die volume may increase approximately linearly with the pierced volume of the upper layer 602. For example, the die volume may increase approximately linearly between an upper and a lower threshold die volume, as determined based on Equations (1) and (2) below:
where Vd,u represents the upper threshold die volume, Vd,l represents the lower threshold die volume, Vp represents the pierced volume of the upper layer 602, and c is a constant that varies within a range between approximately 12.5 to 13 (e.g., within a range between 12.7 to 12.9, approximately 12.8, etc.). In at least one embodiment, the die volume may be an average of the upper and lower threshold die volumes.
The design of the rivet used in the SPR process can also affect the strength of the casting. For example,
In at least one embodiment, as shown in
In some embodiments, the thickness 808 of the web 802 may be determined based on the material properties of at least one material layer of the die casting, as will be further described. For example, the thickness 808 may be determined based on a UTS of the upper layer 810 (e.g., the rivet-facing layer, the non-magnesium layer, etc.), regardless of other properties of the material for the upper layer 810. The thickness 808 of the web 802 may decrease with the UTS of the upper layer 810. In at least one embodiment, the thickness 808 of the web 802 may be determined as shown in the table 900 of
At 1002, an upper layer (e.g., the upper layer 602 of
At 1004, a rivet and die combination are determined and selected based on a material characteristic, such as a size and/or material properties of the upper layer and/or the lower layer.
At 1106, a web thickness of the rivet is determined based on a strength of the upper layer (e.g., the rivet-facing layer, the non-magnesium layer, etc.). Operation 1106 may include scaling the web thickness proportionately to the strength of the upper layer. In some embodiments, operation 1106 may include determining the web thickness using a table and/or algorithm, as described with reference to
Returning to method 1000, once the rivet and die are selected, the SPR die is brought into engagement with the stack that includes the upper layer and the lower layer, at 1006. Operation 1006 may include engaging an outer surface of the SPR die with a lower surface of the lower layer, manually or by activating an SPR joining device to draw the SPR die up against the lower surface of the lower layer. The SPR die may be the same as or similar to the SPR die described with reference to
At 1008, an SPR rivet is provided and pressed through the stack into the SPR die to couple the upper sheet and the lower sheet together (with the SPR rivet). Operation 1008 may include providing a tubular rivet made from steel (e.g., inserting the SPR rivet into a joining tool that includes the SPR die) and applying a force to the SPR rivet and/or die to deform and/or pierce the sheets in the stack. Operation 1008 may include using a press to drive the rivet from an upper side of the stack, into the stack and toward the die, piercing the upper sheet and causing the lower sheet to expand into the SPR die to form a button-shaped protrusion in the lower sheet.
The forming die structure, rivet design, and rivet/die selection process of the present disclosure provides several benefits over traditional SPR techniques. The forming die includes a recessed area that is uniquely shaped to control the volume of the deformed magnesium alloy, to reduce deformation of the magnesium alloy during rivet installation, and to reduce transitions (e.g., sharp edges, corners, etc.) along the outer edge of the recessed area. This unique shape reduces the likelihood of cracking during rivet installation into the magnesium alloy. The rivet die complements benefits provided by the forming die, by providing increased volume in the area of the SPR joint for material deflection of the upper layer. When used in an appropriate combination, as described with reference to method 1000 and 1100, a strong and durable magnesium alloy casting can be formed using existing SPR joining devices. For example,
It should be noted that the term “exemplary” and variations thereof, as used herein to describe various embodiments, are intended to indicate that such embodiments are possible examples, representations, or illustrations of possible embodiments (and such terms are not intended to connote that such embodiments are necessarily extraordinary or superlative examples).
The term “coupled” and variations thereof, as used herein, means the joining of two members directly or indirectly to one another. Such joining may be stationary (e.g., permanent or fixed) or moveable (e.g., removable or releasable). Such joining may be achieved with the two members coupled directly to each other, with the two members coupled to each other using a separate intervening member and any additional intermediate members coupled with one another, or with the two members coupled to each other using an intervening member that is integrally formed as a single unitary body with one of the two members. If “coupled” or variations thereof are modified by an additional term (e.g., directly coupled), the generic definition of “coupled” provided above is modified by the plain language meaning of the additional term (e.g., “directly coupled” means the joining of two members without any separate intervening member), resulting in a narrower definition than the generic definition of “coupled” provided above. Such coupling may be mechanical, electrical, or fluidic.
References herein to the positions of elements (e.g., “top,” “bottom,” “above,” “below”) are merely used to describe the orientation of various elements in the FIGURES. It should be noted that the orientation of various elements may differ according to other exemplary embodiments, and that such variations are intended to be encompassed by the present disclosure.
The construction and arrangement of the elements of the SPR joint as shown in the exemplary embodiments are illustrative only. Although only a few embodiments of the present disclosure have been described in detail, those skilled in the art who review this disclosure will readily appreciate that many modifications are possible (e.g., variations in sizes, dimensions, structures, shapes and proportions of the various elements, values of parameters, mounting arrangements, use of materials, colors, orientations, etc.) without materially departing from the novel teachings and advantages of the subject matter recited. For example, elements shown as integrally formed may be constructed of multiple parts or elements, the position of elements may be reversed or otherwise varied, and the nature or number of discrete elements or positions may be altered or varied.
Although the figures and description may illustrate a specific order of method steps, the order of such steps may differ from what is depicted and described, unless specified differently above. Also, two or more steps may be performed concurrently or with partial concurrence, unless specified differently above.
Other substitutions, modifications, changes and omissions may also be made in the design, operating conditions and arrangement of the various exemplary embodiments without departing from the scope of the present invention. For example, any element disclosed in one embodiment may be incorporated or utilized with any other embodiment disclosed herein. Also, for example, the order or sequence of any process or method steps may be varied or re-sequenced according to alternative embodiments. Any means-plus-function clause is intended to cover the structures described herein as performing the recited function and not only structural equivalents but also equivalent structures. Other substitutions, modifications, changes and omissions may be made in the design, operating configuration, and arrangement of the preferred and other exemplary embodiments without departing from the scope of the appended claims.
This application claims the benefit of and priority to U.S. Provisional Patent Application No. 63/484,779, filed Feb. 14, 2023, the entire disclosure of which is hereby incorporated by reference herein.
| Number | Date | Country | |
|---|---|---|---|
| 63484779 | Feb 2023 | US |
