Patent Application
20170297084
The present disclosure relates to methods of joining polymeric composites and other materials using self-piercing rivets.
The background description provided here is for the purpose of generally presenting the context of the disclosure. Work of the presently named inventors, to the extent it is described in this background section, as well as aspects of the description that may not otherwise qualify as prior art at the time of filing, are neither expressly nor impliedly admitted as prior art against the present disclosure.
Carbon fiber reinforced thermoplastics (CFRTP) such as carbon fiber reinforced nylon composites have a high strength-to-weight ratio, which makes these materials desirable for use in automotive applications. For example, to reduce vehicle weight, these materials have been used in parts such as air intake manifolds, air filter housings, resonators, timing gears, radiator fans, and radiator tanks. Despite these advantages, the number of applications for CRFTP materials is limited due to the current processes available for joining CRFTP materials. Therefore, a need exists for improved processes for joining CRFTP materials.
A first example method of joining first and second layers of material according to the principles of the present disclosure includes applying a layer of adhesive between the first and second layers and allowing the adhesive layer to fully cure, or at least partially cure. The first example method further includes piercing the first layer with a headless end of a rivet after the adhesive layer is cured, deforming the second layer with the headless end of the rivet, and bending the headless end of the rivet radially outward.
A second example method of joining first and second layers of material according to the principles of the present disclosure includes applying a layer of adhesive between the first and second layers and allowing the adhesive layer to fully cure, or at least partially cure. The second example method further includes piercing the first layer with a headless end of a rivet after the adhesive layer is cured, deforming the second layer with the headless end of the rivet, and bending the headless end of the rivet radially outward and axially upward toward the first layer.
Further areas of applicability of the present disclosure will become apparent from the detailed description, the claims and the drawings. The detailed description and specific examples are intended for purposes of illustration only and are not intended to limit the scope of the disclosure.
The present disclosure will become more fully understood from the detailed description and the accompanying drawings, wherein:
In the drawings, reference numbers may be reused to identify similar and/or identical elements.
One process for joining CRFTP materials is referred to as self-piercing riveting. In this process, a self-piercing rivet is inserted into multiple layers of material (or workpieces) to join the layers together. The rivet includes a head and a headless end or tail designed to pierce through material. When the rivet is inserted downward into the layers, the tail pierces through the top layer and then deforms the bottom layer without piercing into the bottom layer. As the tail deforms the bottom layer, the head is seated in the top layer, and a die bends the tail radially outward so that the layers are clamped between the head and the tail.
Joining CRFTP materials using self-piercing riveting satisfies fastening speed and peel strength requirements of most vehicle applications. However, due to the large amount of deformation associated with this process and the limited formability of CRFTP materials at room temperature, self-piercing riveting may result in part cracking. Part cracking may decrease the strength of the riveted joint, which may reduce part quality.
A self-piercing riveting process according to the present disclosure addresses these issues by using a rivet and a die that are designed so that the tail of the rivet pierces into the bottom layer before the tail is bent radially outward and upward. In addition, the rivet and die are designed so that the tail of the rivet is not only bent radially outward, but is also bent upward toward the workpieces to form an undercut. In turn, a mechanical interlock forms between the rivet and the workpieces, which minimizes part cracking and reduces the sensitivity of the joint strength to part cracking.
There are several parameters related to the design of the rivet and the die that influence whether the tail of the rivet pierces the bottom layer and whether the tail is bent upward toward the workpieces after piercing through the workpieces. In addition, the gage (or thickness) of the workpieces and the order in which the workpieces are stacked onto one another affects the behavior of the rivet during the joining operation. Therefore, exhaustive trial-and-error testing may be required to find the optimum process parameters, such as rivet and die designs, which yield maximum joint strength.
In one example, the designs of a rivet and a die may be optimized to yield maximum joint strength when the rivet is used to join a 3-millimeter (mm) layer of CRFTP material is stacked on top of a 2-mm layer of CRFTP material. However, if the 2-mm layer is stacked on top of the 3-mm layer, the rivet and die may have to be redesigned to yield maximum joint strength. Thus, the rivet and die may have to be redesigned each time that the stacking order of the layers changes.
A self-piercing riveting process according to the present disclosure addresses these issues by applying an adhesive between two layers of material and allowing the adhesive to fully cure, or at least partially cure, before inserting the rivet into the two layers. By applying adhesive between the two layers and allowing the adhesive to cure, the rivet is essentially inserted into a single workpiece having two layers instead of being inserted into two separate workpieces. As a result, the designs of the rivet and die may be optimized to yield maximum joint strength regardless of the order in which the layers are stacked onto one another. Thus, a self-piercing riveting process using adhesive according to the present disclosure may be used to reduce the number of rivet and die designs.
As indicated above, in conventional self-piercing riveting processes, when the rivet is inserted downward into two layers of CRFTP material, the tail pierces through the top layer and then deforms the bottom layer without piercing into the bottom layer. Thus, if adhesive is applied between the top and bottom layers and the adhesive is allowed to cure before the rivet is inserted downward into the layers, inserting the rivet may cause part cracking, which may lead to part delamination around the adhesive. Therefore, conventional self-piercing riveting processes do not involve applying adhesive between two layers of CRFTP material before inserting a rivet into the cured layers.
In contrast, as discussed above, in a self-piercing riveting process according to the present disclosure, when the rivet is inserted downward into two layers of CRFTP material, the tail pierces the bottom layer. In addition, the tail is bent radially outward and upward to form a mechanical interlock between the rivet and the workpieces. Thus, adhesive may be applied between the two layers and allowed to cure before inserting the rivet into the two layers since the mechanical interlock minimizes part cracking and delamination that may otherwise occur when adhesive is applied between the layers. Thus, adhesive may be used to reduce the number of rivet and die designs required for a vehicle application without reducing the peel strength of the riveted joint.
Referring now to
Once the first and second layers 10 and 12 are positioned on the die 14, the rivet insertion tool 16 is moved in a downward direction 17 until the tube 20 of the rivet insertion tool 16 contacts the first layer 10 as shown in
As the piston 24 moves the rivet 26 in the downward direction 17, the tail 30 of the rivet 26 pierces the first layer 10 as shown in
When the piston 24 stops moving in the downward direction 17, the head 28 of the rivet 26 is fully seated in the first layer 10, and the tail 30 is bent radially outward and upward so as to form a mechanical interlock. As a result, the first and second layers 10 and 12 are clamped between the head 28 of the rivet 26 and the tail 30 of the rivet 26 such that the first and second layers 10 and 12 are joined together by the rivet 26. The rivet insertion tool 16 is then moved in the upward direction 35, leaving the rivet 26 in place in the first and second layers 10 and 12. The downward and upward directions 17 and 35 may be referred to as axial directions, and the radially outward direction in which the tail 30 is bent is perpendicular to these axial directions.
The tail 30 may be inserted only partially into the second layer 12, or the tail 30 may be inserted completely through the second layer 12. In addition, the tail 30 may be bent upward toward the first layer 10 by varying degrees. For example, the tail 30 may be bent only slightly upward as shown in
Several parameters related to the design of the rivet 26 and the die 14 may be optimized to ensure that the tail 30 pierces the second layer 12 and the tail 30 is bent upward toward the first layer 10 after piercing the first and second layers 10 and 12. These design parameters may include a length 36 of the rivet 26, a height 38 of the protrusion 34, other geometric aspects of the protrusion 34, a depth 40 of the cavity 18 in the die 14, a diameter 42 of the cavity 18, a volume of the cavity 18, and/or a relationship between two or more of the aforementioned parameters. In addition, one or more of these design parameters may be determined based on a first thickness 44 of the first layer 10, a second thickness 46 of the second layer 12, the type(s) of material included in the first and second layers 10 and 12, and/or the strength of the material(s) included in the first and second layers 10 and 12.
In one example, the length 36 of the rivet 26 may be at least 40 percent greater than a sum of the first and second thicknesses 44 and 46. Thus, if the first and second thicknesses 44 and 46 are each 2.5 mm, the length 36 of the rivet 26 may be at least 7 mm. In other examples, the height 38 of the protrusion 34 may be in a range from 0 mm to 2 mm, and the depth 40 of the cavity 18 may be in a range from 0.5 mm to 2 mm.
In
Referring now to
The adhesive layer 48 has a third thickness 50, which may be a function of the first and second thicknesses 44 and 46 of the first and second layers 10 and 12 and/or the material strength of the first and second layers 10 and 12. In one example, the third thickness 50 may be between 3 percent and 30 percent of the sum of the first and second thicknesses 44 and 46. Thus, if the first and second thicknesses 44 and 46 are each 2.5 mm, the third thickness 50 may be between 0.15 mm and 1.5 mm. In another example, the third thickness 50 may be between 5 percent and 25 percent of the sum of the first and second thicknesses 44 and 46. Thus, if the first and second thicknesses 44 and 46 are each 2.5 mm, the third thickness 50 may be between 0.25 mm and 1.25 mm.
After the adhesive layer 48 is applied between the first and second layers 10 and 12, the adhesive layer 48 is allowed to fully cure, or at least partially cure. In one example, allowing the adhesive layer 48 to fully cure includes exposing the adhesive layer 48 to room temperature for a first predetermined period (e.g., 60 minutes to 90 minutes). In another example, allowing the adhesive layer 48 to fully cure includes heating the adhesive layer 48 to a predetermined temperature (e.g., approximately 100 degrees Celsius (° C.)) for a second predetermined period (e.g., 10 minutes). In another example, allowing the adhesive layer 48 to at least partially cure includes exposing the adhesive layer 48 to room temperature for at least a first predetermined percentage (e.g., 10 percent (%), 20%, 30%, 40%, 50%, 60%, 70%, 80%, 90%, or 100%) of the first predetermined period. In another example, allowing the adhesive layer 48 to at least partially cure includes heating the adhesive layer 48 to the predetermined temperature for at least a second predetermined percentage (e.g., 10%, 20%, 30%, 40%, 50%, 60%, 70%, 80%, 90%, or 100%) of the second predetermined period.
Once the adhesive layer 48 is fully cured, or at least partially cured, the first and second layers 10 and 12 and the adhesive layer 48 are positioned on the die 14 as shown in
Once the first and second layers 10 and 12 are positioned on the die 14, the rivet insertion tool 16 is moved in the downward direction 17 until the tube 20 of the rivet insertion tool 16 contacts the first layer 10 as shown in
As the piston 24 moves the rivet 26 in the downward direction 17, the tail 30 of the rivet 26 pierces the first layer 10 as shown in
When the piston 24 stops moving in the downward direction 17, the head 28 of the rivet 26 is fully seated in the first layer 10, and the tail 30 is bent radially outward and upward so as to form a mechanical interlock. As a result, the first and second layers 10 and 12 are clamped between the head 28 of the rivet 26 and the tail 30 of the rivet 26 such that the first and second layers 10 and 12 are joined together by the rivet 26. The rivet insertion tool 16 is then moved in the upward direction 35, leaving the rivet 26 in place in the first and second layers 10 and 12 and the adhesive layer 48.
The tail 30 may be inserted only partially into the second layer 12, or the tail 30 may be inserted completely through the second layer 12. In addition, the tail 30 may be bent upward toward the first layer 10 by varying degrees. For example, the tail 30 may be bent only slightly upward as shown in
Several parameters related to the design of the rivet 26 and the die 14 may be optimized to ensure that the tail 30 pierces the second layer 12 and the tail 30 is bent upward toward the first layer 10 after piercing the first and second layers 10 and 12. These design parameters may include the length 36 of the rivet 26, the height 38 of the protrusion 34, other geometric aspects of the protrusion 34, the depth 40 of the cavity 18 in the die 14, the diameter 42 of the cavity 18, the volume of the cavity 18, and/or a relationship between two or more of the aforementioned parameters. In addition, one or more of these design parameters may be determined based on the first thickness 44 of the first layer 10, the second thickness 46 of the second layer 12, the type(s) of material included in the first and second layers 10 and 12, and/or the strength of the material(s) included in the first and second layers 10 and 12.
In one example, the length 36 of the rivet 26 may be at least 40 percent greater than a sum of the first and second thicknesses 44 and 46. Thus, if the first and second thicknesses 44 and 46 are each 2.5 mm, the length 36 of the rivet 26 may be at least 7 mm. In other examples, the height 38 of the protrusion 34 may be in a range from 0 mm to 2 mm, and the depth 40 of the cavity 18 may be in a range from 0.5 mm to 2 mm.
The self-piercing riveting processes described above may be used to join multiple layers of CRFTP material, to join multiple layers of another type of material, or to join multiple layers of dissimilar materials. In one example, each of the first and second layers 10 and 12 includes or consists of a polymeric composite such as CRFTP. In another example, one of the first and second layers 10 and 12 includes or consists of a polymeric composite such as CRFTP, and the other one of the first and second layers includes a metal such as stainless steel. In yet another example, each of the first and second layers 10 and 12 includes or consists of a metal such as stainless steel.
An example of a riveted joint 52 without adhesive is shown in
In addition, like the riveted joint 52 without adhesive, the stacking order of the layers 56 and 58 in the riveted joint 64 affects the behavior of the rivet 60 as the rivet 60 is inserted into the layers 56 and 58. Thus, like the riveted joint 52, exhaustive trial-and-error testing may be required to find the optimum process parameters for the riveted joint 64, such as rivet and die designs, which yield maximum joint strength. Therefore, allowing the adhesive to fully cure, or at least partially cure, before inserting the rivet 60 into the layers 56 and 58 avoids this additional work and associated costs.
Referring now to
At 78, the method 70 determines whether the adhesive layer 48 is fully cured or at least partially cured. In one example, the method 70 may determine that the adhesive layer 48 is fully cured when the adhesive layer 48 has been heated to the predetermined temperature for the second predetermined period. If the adhesive layer 48 is fully cured or at least partially cured, the method 70 continues at 80. Otherwise, the method 70 returns to 76.
At 80, the first and second layers 10 and 12 are positioned on the die 14. At 82, the rivet 26 is inserted through the first layer 10 and at least partially into the second layer 12. At 84, the headless end or tail 30 of the rivet 26 is bent radially outward and axially upward toward the first layer 10. The method 70 ends at 86.
The foregoing description is merely illustrative in nature and is in no way intended to limit the disclosure, its application, or uses. The broad teachings of the disclosure can be implemented in a variety of forms. Therefore, while this disclosure includes particular examples, the true scope of the disclosure should not be so limited since other modifications will become apparent upon a study of the drawings, the specification, and the following claims. It should be understood that one or more steps within a method may be executed in different order (or concurrently) without altering the principles of the present disclosure. Further, although each of the embodiments is described above as having certain features, any one or more of those features described with respect to any embodiment of the disclosure can be implemented in and/or combined with features of any of the other embodiments, even if that combination is not explicitly described. In other words, the described embodiments are not mutually exclusive, and permutations of one or more embodiments with one another remain within the scope of this disclosure.
Spatial and functional relationships between elements (for example, between modules, circuit elements, semiconductor layers, etc.) are described using various terms, including “connected,” “engaged,” “coupled,” “adjacent,” “next to,” “on top of,” “above,” “below,” and “disposed.” Unless explicitly described as being “direct,” when a relationship between first and second elements is described in the above disclosure, that relationship can be a direct relationship where no other intervening elements are present between the first and second elements, but can also be an indirect relationship where one or more intervening elements are present (either spatially or functionally) between the first and second elements. As used herein, the phrase at least one of A, B, and C should be construed to mean a logical (A OR B OR C), using a non-exclusive logical OR, and should not be construed to mean “at least one of A, at least one of B, and at least one of C.”
None of the elements recited in the claims are intended to be a means-plus-function element within the meaning of 35 U.S.C. §112(f) unless an element is expressly recited using the phrase “means for,” or in the case of a method claim using the phrases “operation for” or “step for.”
This application claims the benefit of U.S. Provisional Application No. 62/322,588, filed on Apr. 14, 2016. The disclosure of the above application is incorporated herein by reference in its entirety.
| Number | Date | Country | |
|---|---|---|---|
| 62322588 | Apr 2016 | US |
