US20190105702A1 - Net shaped substrate material for substrate joint - Google Patents

Net shaped substrate material for substrate joint Download PDF

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Publication number
US20190105702A1
US20190105702A1 US15/726,172 US201715726172A US2019105702A1 US 20190105702 A1 US20190105702 A1 US 20190105702A1 US 201715726172 A US201715726172 A US 201715726172A US 2019105702 A1 US2019105702 A1 US 2019105702A1
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United States
Prior art keywords
preformed
substrate
lower substrate
interior cavity
self
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Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
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US15/726,172
Inventor
Garret Sankey Huff
Amanda Kay Freis
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Ford Global Technologies LLC
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Ford Global Technologies LLC
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Publication date
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Priority to US15/726,172 priority Critical patent/US20190105702A1/en
Assigned to FORD GLOBAL TECHNOLOGIES, LLC reassignment FORD GLOBAL TECHNOLOGIES, LLC ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: FREIS, AMANDA KAY, HUFF, GARRET SANKEY
Priority to CN201811084726.2A priority patent/CN109630514A/en
Publication of US20190105702A1 publication Critical patent/US20190105702A1/en
Priority to US17/352,638 priority patent/US11759845B2/en
Abandoned legal-status Critical Current

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J15/00—Riveting
    • B21J15/02—Riveting procedures
    • B21J15/025—Setting self-piercing rivets
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/04—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of riveting
    • F16B5/045—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of riveting without the use of separate rivets
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
    • B21C23/00—Extruding metal; Impact extrusion
    • B21C23/02—Making uncoated products
    • B21C23/04—Making uncoated products by direct extrusion
    • B21C23/14—Making other products
    • B21C23/142—Making profiles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J15/00—Riveting
    • B21J15/02—Riveting procedures
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J15/00—Riveting
    • B21J15/10—Riveting machines
    • B21J15/14—Riveting machines specially adapted for riveting specific articles, e.g. brake lining machines
    • B21J15/147—Composite articles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/20—Layered products comprising a layer of metal comprising aluminium or copper
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
    • B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04—Interconnection of layers
    • B32B7/05—Interconnection of layers the layers not being connected over the whole surface, e.g. discontinuous connection or patterned connection
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04—Interconnection of layers
    • B32B7/08—Interconnection of layers by mechanical means
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
    • B32B9/04—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B9/041—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material of metal
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/04—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of riveting
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/56—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits
    • B29C65/64—Joining a non-plastics element to a plastics element, e.g. by force
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/74—Joining plastics material to non-plastics material
    • B29C66/742—Joining plastics material to non-plastics material to metals or their alloys
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3002—Superstructures characterized by combining metal and plastics, i.e. hybrid parts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2250/00—Layers arrangement
    • B32B2250/02—2 layers
    • Y—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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24273—Structurally defined web or sheet [e.g., overall dimension, etc.] including aperture
    • Y10T428/24322—Composite web or sheet

Definitions

  • the present disclosure relates to the joining of various materials in an assembly, including dissimilar materials having advanced high strength and light weight.
  • self-piercing rivet technology prevails.
  • One advantage of self-piercing rivet technology is that it is a high production volume assembly process.
  • Self-piercing rivet technology is compatible with adhesive and both methods can be used together.
  • the challenge often faced with self-piercing rivet technology, however, is that the substrate material must be ductile enough to form a “button”, i.e., protrusion, which is the result of creating the joint and the necessary deformation to provide mechanical interlock.
  • a button i.e., protrusion
  • fibers may be exposed through cracks in this surface. Surface cracking and fiber displacement are undesirable, as they may reduce the durability of the joint and result in premature failure.
  • fibers in the area where the rivet is inserted may result in surface cracking or fiber displacement.
  • Composite materials such as carbon fiber, glass fiber or natural fiber composites, can be limited in application due to challenges relating to joining parts together. Frequently, these composites have limited ductility and are not well adapted to large displacements and deformation required to join parts together with self-piercing rivets. Other non-composite materials having higher strength and light weight are also often brittle and challenging to join using SPR technology.
  • an assembly which 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.
  • the preformed interior cavity of the lower substrate is may or not be plastically deformed after installation of the self-piercing rivet.
  • the lower substrate is an aluminum casting or an aluminum extrusion.
  • the lower substrate is a composite material.
  • the preformed interior cavity in one form defines a circular trench having a raised central region, and in another form, the preformed exterior profile defines a closed cylinder.
  • the preformed exterior profile may further define a radiused area extending between a lower surface of the lower substrate and the cylinder.
  • the preformed interior cavity is configured to direct flaring of the self-piercing rivet.
  • a dimpled substrate for use in an assembly having joined substrates.
  • the dimpled substrate defines at least one preformed interior cavity and at least one preformed exterior profile adjacent the interior cavity to define a variable thickness wall.
  • the preformed interior cavity is configured to receive a fastening system that plastically deforms at least one of the substrates during joining.
  • an assembly which includes an upper substrate, a lower substrate, and a plurality of self-piercing rivets.
  • the lower substrate defines a plurality of preformed interior cavities and a corresponding plurality of preformed exterior profiles adjacent the interior cavities to define variable thickness walls therebetween.
  • the plurality of self-piercing rivets extend through the upper substrate and into the preformed interior cavities of the lower substrate.
  • the preformed interior cavities are configured to direct flaring of the self-piercing rivets.
  • FIG. 1 is a cross-sectional view of a joined assembly constructed in accordance with the teachings of the present disclosure
  • FIG. 2 is a top perspective view of a lower substrate of the joined assembly of FIG. 1 having a preformed interior cavity according to the teachings of the present disclosure
  • FIG. 3 is a bottom perspective view of the lower substrate of FIG. 2 ;
  • FIG. 4 is a cross-sectional view of the lower substrate of FIG. 2 ;
  • FIG. 5 is a cross-sectional view of a variant of a lower substrate of a joined assembly constructed in accordance with the teachings of the present disclosure
  • FIG. 6 is a cross-sectional view of an upper substrate and a lower substrate with a self-piercing rivet tool including a riveter punch and a back-up die with a self-piercing rivet in position to be driven into the upper and lower substrates.
  • a joined composite or assembly 10 includes a lower substrate 12 , an upper substrate 14 , and at least one self-piercing rivet 20 that secures the lower substrate 12 to the upper substrate 14 . While only one self-piercing rivet 20 is shown, the joined composite or assembly 10 may include a plurality of self-piercing rivets 20 spaced across the surface of the joined composite or assembly 10 .
  • the lower substrate 12 may be a dimpled substrate and includes at least one preformed exterior profile in the form of a button shaped protrusion or “button” 18 .
  • the button 18 extends downwardly from a lower surface 22 of the lower substrate 12 and is disposed in a predetermined location where a corresponding self-piercing rivet 20 is planned to be inserted into the lower substrate 12 .
  • the upper substrate 14 may be made of steel, aluminum, a fiber reinforced composite material, or other materials.
  • the lower substrate 12 may be a cast part, a molded part, or a 3 D-printed part, among others. In various forms of the present disclosure, the substrate 12 is an aluminum casting, an aluminum extrusion, or a composite material.
  • the button 18 of the lower substrate 12 is configured to be a closed cylinder which has a peripheral wall 24 and a bottom wall 26 .
  • the peripheral wall 24 and the bottom wall 26 jointly define a preformed exterior profile having a preformed interior cavity 28 .
  • the preformed interior cavity 28 is configured to receive a fastening system, such as the self-piercing rivet 20 , which plastically deforms at least one of the lower and upper substrates 12 , 14 during joining.
  • the bottom wall 26 has a variable thickness and has the largest thickness adjacent a central region, thereby defining a raised central region 30 .
  • a circular or annular trench 32 is defined between the raised central region 30 and the sidewall 24 of the button 18 and surrounds the raised central region 30 .
  • the button 18 has a substantially flat bottom surface 34 in one form of the present disclosure.
  • the raised central region 30 has a top surface 36 that is lower than a lower surface 22 of the lower substrate 12 .
  • a lower substrate 50 in accordance with a variant of the present disclosure is structurally similar to the lower substrate 12 of FIGS. 1 to 4 except for the configuration of the button. More specifically, the lower substrate 50 includes a button 52 defining a preformed internal cavity 54 and includes a bottom wall 62 .
  • the bottom wall 62 has a variable thickness and has the largest thickness adjacent a central region, thereby defining a raised central region 64 .
  • An annular or circular trench 66 is defined inside the preformed internal cavity 54 and surrounds the raised central region 64 .
  • the raised central region 64 defines a top surface 68 raised to a height above the lower surface 72 of the lower substrate 50 .
  • the bottom surface 70 of bottom wall 70 of the button 52 is substantially flat.
  • the button 52 further includes a radiused area 74 that joins the bottom surface 70 of the bottom wall 70 to the lower surface 72 the lower substrate 50 where no button is formed.
  • the upper substrate 14 is placed over the lower substrate 12 in a self-piercing rivet tool 80 .
  • the self-piercing rivet tool 80 includes a riveter punch 82 and a back-up die 84 .
  • the preformed interior cavity 28 of the button 18 of the lower substrate 12 is closed by the upper substrate 14 .
  • 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.
  • the insertion end 88 of the self-piercing rivet 20 is spread apart as the self-piercing rivet 20 is driven through the upper substrate 14 .
  • the preformed interior cavity 28 is configured to direct flaring of the self-piercing rivet 20 .
  • a portion of the upper substrate 14 adjacent the self-piercing rivet 20 is plastically deformed. Material from the upper substrate 14 may be deformed and directed into the preformed interior cavity 28 to fill the preformed interior cavity 28 .
  • Radially displaced material 92 fills in between the side of the self-piercing rivet 20 and the button 18 .
  • Axially displaced material 94 fills in between the insertion end 88 of the self-piercing rivet 20 and the bottom wall 26 of the button 18 of the lower substrate 12 .
  • 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.
  • 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.
  • 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.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Insertion Pins And Rivets (AREA)
  • Connection Of Plates (AREA)
  • Body Structure For Vehicles (AREA)

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.

Description

    FIELD
  • The present disclosure relates to the joining of various materials in an assembly, including dissimilar materials having advanced high strength and light weight.
    • BACKGROUND
  • The statements in this section merely provide background information related to the present disclosure and may not constitute prior art.
  • As the automotive industry continues to focus on reducing the weight of vehicles to meet customer expectations on fuel economy and CAFE (Corporate Average Fuel Economy) requirements, interest in alternative materials including carbon fiber composite applications has increased. In body-in-white structures, joining methods have traditionally relied on resistance-spot welding (e.g., in steel structures).
  • In the case of aluminum intensive vehicles and other mixed metal joining applications, self-piercing rivet technology prevails. One advantage of self-piercing rivet technology is that it is a high production volume assembly process. Self-piercing rivet technology is compatible with adhesive and both methods can be used together. The challenge often faced with self-piercing rivet technology, however, is that the substrate material must be ductile enough to form a “button”, i.e., protrusion, which is the result of creating the joint and the necessary deformation to provide mechanical interlock. When composite parts do not have sufficient ductility to form a button on the obverse side, fibers may be exposed through cracks in this surface. Surface cracking and fiber displacement are undesirable, as they may reduce the durability of the joint and result in premature failure. With a self-piercing rivet, fibers in the area where the rivet is inserted may result in surface cracking or fiber displacement.
  • Composite materials, such as carbon fiber, glass fiber or natural fiber composites, can be limited in application due to challenges relating to joining parts together. Frequently, these composites have limited ductility and are not well adapted to large displacements and deformation required to join parts together with self-piercing rivets. Other non-composite materials having higher strength and light weight are also often brittle and challenging to join using SPR technology.
  • The joining of advanced high strength and lightweight materials, among other assembly issues, is addressed by the present disclosure.
    • SUMMARY
  • In one form, an assembly is provided, which 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. The preformed interior cavity of the lower substrate is may or not be plastically deformed after installation of the self-piercing rivet.
  • In one form, the lower substrate is an aluminum casting or an aluminum extrusion. In another form, the lower substrate is a composite material. The preformed interior cavity in one form defines a circular trench having a raised central region, and in another form, the preformed exterior profile defines a closed cylinder. The preformed exterior profile may further define a radiused area extending between a lower surface of the lower substrate and the cylinder. Generally, the preformed interior cavity is configured to direct flaring of the self-piercing rivet.
  • In another form, a dimpled substrate for use in an assembly having joined substrates is provided. The dimpled substrate defines at least one preformed interior cavity and at least one preformed exterior profile adjacent the interior cavity to define a variable thickness wall. The preformed interior cavity is configured to receive a fastening system that plastically deforms at least one of the substrates during joining.
  • In still another form, an assembly is provided, which includes an upper substrate, a lower substrate, and a plurality of self-piercing rivets. The lower substrate defines a plurality of preformed interior cavities and a corresponding plurality of preformed exterior profiles adjacent the interior cavities to define variable thickness walls therebetween. The plurality of self-piercing rivets extend through the upper substrate and into the preformed interior cavities of the lower substrate. The preformed interior cavities are configured to direct flaring of the self-piercing rivets.
  • Further areas of applicability will become apparent from the description provided herein. It should be understood that the description and specific examples are intended for purposes of illustration only and are not intended to limit the scope of the present disclosure.
    • BRIEF DESCRIPTION OF THE DRAWINGS
  • The present disclosure will become more fully understood from the detailed description and the accompanying drawings, wherein:
  • FIG. 1 is a cross-sectional view of a joined assembly constructed in accordance with the teachings of the present disclosure;
  • FIG. 2 is a top perspective view of a lower substrate of the joined assembly of FIG. 1 having a preformed interior cavity according to the teachings of the present disclosure;
  • FIG. 3 is a bottom perspective view of the lower substrate of FIG. 2;
  • FIG. 4 is a cross-sectional view of the lower substrate of FIG. 2;
  • FIG. 5 is a cross-sectional view of a variant of a lower substrate of a joined assembly constructed in accordance with the teachings of the present disclosure;
  • and
  • FIG. 6 is a cross-sectional view of an upper substrate and a lower substrate with a self-piercing rivet tool including a riveter punch and a back-up die with a self-piercing rivet in position to be driven into the upper and lower substrates.
    •
  • Corresponding reference numerals indicate corresponding parts throughout the several views of the drawings.
    • DETAILED DESCRIPTION
  • The following description is merely exemplary in nature and is not intended to limit the present disclosure, application, or uses.
  • Referring to FIG. 1, a joined composite or assembly 10 includes a lower substrate 12, an upper substrate 14, and at least one self-piercing rivet 20 that secures the lower substrate 12 to the upper substrate 14. While only one self-piercing rivet 20 is shown, the joined composite or assembly 10 may include a plurality of self-piercing rivets 20 spaced across the surface of the joined composite or assembly 10. The lower substrate 12 may be a dimpled substrate and includes at least one preformed exterior profile in the form of a button shaped protrusion or “button” 18. The button 18 extends downwardly from a lower surface 22 of the lower substrate 12 and is disposed in a predetermined location where a corresponding self-piercing rivet 20 is planned to be inserted into the lower substrate 12. The upper substrate 14 may be made of steel, aluminum, a fiber reinforced composite material, or other materials. The lower substrate 12 may be a cast part, a molded part, or a 3D-printed part, among others. In various forms of the present disclosure, the substrate 12 is an aluminum casting, an aluminum extrusion, or a composite material.
  • Referring to FIGS. 2 and 3, the button 18 of the lower substrate 12 is configured to be a closed cylinder which has a peripheral wall 24 and a bottom wall 26. The peripheral wall 24 and the bottom wall 26 jointly define a preformed exterior profile having a preformed interior cavity 28. The preformed interior cavity 28 is configured to receive a fastening system, such as the self-piercing rivet 20, which plastically deforms at least one of the lower and upper substrates 12, 14 during joining.
  • Referring to FIG. 4, the bottom wall 26 has a variable thickness and has the largest thickness adjacent a central region, thereby defining a raised central region 30. A circular or annular trench 32 is defined between the raised central region 30 and the sidewall 24 of the button 18 and surrounds the raised central region 30. The button 18 has a substantially flat bottom surface 34 in one form of the present disclosure. The raised central region 30 has a top surface 36 that is lower than a lower surface 22 of the lower substrate 12.
  • Referring to FIG. 5, a lower substrate 50 in accordance with a variant of the present disclosure is structurally similar to the lower substrate 12 of FIGS. 1 to 4 except for the configuration of the button. More specifically, the lower substrate 50 includes a button 52 defining a preformed internal cavity 54 and includes a bottom wall 62. The bottom wall 62 has a variable thickness and has the largest thickness adjacent a central region, thereby defining a raised central region 64. An annular or circular trench 66 is defined inside the preformed internal cavity 54 and surrounds the raised central region 64. The raised central region 64 defines a top surface 68 raised to a height above the lower surface 72 of the lower substrate 50. The bottom surface 70 of bottom wall 70 of the button 52 is substantially flat. The button 52 further includes a radiused area 74 that joins the bottom surface 70 of the bottom wall 70 to the lower surface 72 the lower substrate 50 where no button is formed.
  • Referring to FIG. 6, to join the lower substrate 12 to the upper substrate 14, the upper substrate 14 is placed over the lower substrate 12 in a self-piercing rivet tool 80. The self-piercing rivet tool 80 includes a riveter punch 82 and a back-up die 84. The preformed interior cavity 28 of the button 18 of the lower substrate 12 is closed by the upper substrate 14.
  • 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.
  • Referring back to FIG. 1, when the self-piercing rivet 20 is completely inserted into the joined composite or assembly 10, the insertion end 88 of the self-piercing rivet 20 is spread apart as the self-piercing rivet 20 is driven through the upper substrate 14. The preformed interior cavity 28 is configured to direct flaring of the self-piercing rivet 20. A portion of the upper substrate 14 adjacent the self-piercing rivet 20 is plastically deformed. Material from the upper substrate 14 may be deformed and directed into the preformed interior cavity 28 to fill the preformed interior cavity 28. Radially displaced material 92 fills in between the side of the self-piercing rivet 20 and the button 18. Axially displaced material 94 fills in between the insertion end 88 of the self-piercing rivet 20 and the bottom wall 26 of the button 18 of the lower substrate 12.
  • 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.
  • 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.
  • 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.
  • 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.

Claims (20)

What is claimed is:
1. An assembly comprising:
an upper substrate;
a lower substrate defining a preformed interior cavity and a preformed exterior profile adjacent the interior cavity to define a variable thickness wall; and
a self-piercing rivet extending through the upper substrate and into the preformed interior cavity of the lower substrate.
2. The assembly according to claim 1, wherein the preformed interior cavity of the lower substrate is not plastically deformed after installation of the self-piercing rivet.
3. The assembly according to claim 1, wherein the preformed interior cavity of the lower substrate is plastically deformed after installation of the self-piercing rivet.
4. The assembly according to claim 1, wherein the lower substrate is an aluminum casting or an aluminum extrusion.
5. The assembly according to claim 1, wherein the lower substrate is a composite material.
6. The assembly according to claim 1, wherein the preformed interior cavity defines a circular trench having a raised central region.
7. The assembly according to claim 1, wherein the preformed exterior profile defines a closed cylinder.
8. The assembly according to claim 7, wherein the preformed exterior profile further defines a radiused area extending between a lower surface of the lower substrate and the cylinder.
9. The assembly according to claim 1, wherein the preformed interior cavity is configured to direct flaring of the self-piercing rivet.
10. A dimpled substrate for use in an assembly having joined substrates, the dimpled substrate defining at least one preformed interior cavity and at least one preformed exterior profile adjacent the interior cavity to define a variable thickness wall, wherein the preformed interior cavity is configured to receive a fastening system that plastically deforms at least one of the substrates during joining.
11. The substrate according to claim 10, wherein the dimpled substrate defines a plurality of preformed interior cavities and a corresponding plurality of preformed exterior profiles, the plurality of preformed interior cavities being evenly spaced.
12. The substrate according to claim 10, wherein the lower substrate is an aluminum casting or an aluminum extrusion.
13. The substrate according to claim 10, wherein the lower substrate is a composite material.
14. The substrate according to claim 10, wherein the preformed interior cavity defines a circular trench having a raised central region.
15. The substrate according to claim 10, wherein preformed exterior profile defines a closed cylinder.
16. An assembly comprising:
an upper substrate;
a lower substrate defining a plurality of preformed interior cavities and a corresponding plurality of preformed exterior profiles adjacent the interior cavities to define variable thickness walls therebetween; and
a plurality of self-piercing rivets extending through the upper substrate and into the preformed interior cavities of the lower substrate,
wherein the preformed interior cavities are configured to direct flaring of the self-piercing rivets.
17. The assembly according to claim 16, wherein the lower substrate is an aluminum casting or an aluminum extrusion.
18. The assembly according to claim 16, wherein the lower substrate is a composite material.
19. The assembly according to claim 16, wherein preformed exterior profiles define closed cylinders.
20. A motor vehicle having the assembly according to claim 16.
US15/726,172 2017-10-05 2017-10-05 Net shaped substrate material for substrate joint Abandoned US20190105702A1 (en)

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CN201811084726.2A CN109630514A (en) 2017-10-05 2018-09-18 Net forming board material for substrate engagement
US17/352,638 US11759845B2 (en) 2017-10-05 2021-06-21 Net shaped substrate material for substrate joint

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US20210308742A1 (en) 2021-10-07
CN109630514A (en) 2019-04-16

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