Patent Application
20160167353
The present technology relates generally to joining components. More specifically, the present technology relates to systems and methods for interlocking components being joined.
Joining workpieces with similar or dissimilar material properties has become increasingly important as industries strive for reduced weight and improved performance from engineering structures such as automotive, aeronautical, and nautical, among others.
Processes for joining similar or dissimilar materials include mechanical joining (e.g., bolts and rivets), fusion joining (e.g., fusion arc welding and laser welding), solid-state joining (e.g., friction-stir welding and ultrasonic welding), brazing and soldering, and adhesive bonding, among others.
Joining dissimilar materials presents challenges due to different chemical, mechanical, and thermal behaviors of materials that are not present when joining similar materials. When designing a dissimilar-material joint, factors such as, but not limited to, material thicknesses, surface energy, differences in melting temperature, thermal expansion/contraction of each material must be taken into consideration. Even taking the aforementioned factors into consideration, joining techniques such as welding and soldering provide surface bonding that can be prone to failure under certain directional loads such as peel stress.
Joining dissimilar materials includes challenges such as avoiding distortion and stress that tend to form within the materials due to differing coefficients of thermal expansion. These unwanted conditions can cause stress corrosion cracking, which weakens the bond and can lead to premature failure of the joint.
Other methods to join dissimilar materials use fasteners such as adhesives, rivets, and bolts. However, these fasteners lead to issues such as structural breakdown of the adhesives and galvanic corrosion of the rivets and bolts. Additionally, these fasteners add a relatively-large amount of weight, which is contrary to trends towards lighter components in most industries.
Due to the aforementioned deficiencies, the need exists for systems and methods to join securely workpieces that contain dissimilar materials without added fasteners such as adhesives, rivets, or bolts. The proposed systems and methods would join the workpieces by mechanically interlocking the materials of the workpieces according to unique techniques that do not use additional fasteners.
The present technology includes a system by which mechanical interlocking is accomplished through forming grooves at a joint interface of at least one of the workpieces. The grooves are configured to receive melted material from the joining workpiece for forming a robust joint when the melted material cools.
In some embodiments, the materials joined are similar in composition. In these embodiments, the grooves can be formed in either or both of the workpieces. In one embodiment, a first workpiece is configured to melt and fill the grooves of the second workpiece. As the first workpiece fills the grooves of the second workpiece, the grooves slightly melt to increase interlock at the joint.
In other embodiments, the materials joined are dissimilar in composition. In these embodiments, the grooves should be formed within the material having the highest melting temperature. Forming grooves into the workpiece having the higher melting temperature allows the material having the lower melting temperature to melt and flow into the grooves. In some implementations for joining components having dissimilar composition, depending, for instance, on the a value of the higher melting point and a temperature of the molten material from the lower-melting-point component, the molten material could flow into the grooves without deforming the grooves, or only deforming the grooves slightly. While in some cases deforming grooves can be beneficial by promoting interlock as referenced above, maintaining groove structure substantially or entirely can also, based on groove shape, groove dimensions, and materials, for instance, promote interlocking and formation of stronger welds compared with welding without the use of grooves.
Another of many benefits of the present technology includes the ability to form a joining interfaces having minimal or no negative affect on an appearance of at least one of the surfaces opposite the joint interface.
In some embodiments, negative impact on appearance of at least one of the surfaces opposite the joint interface is minimized or avoided completely by using laser heating to melt the material of one of the workpieces to be introduced to grooves of the other workpiece. In other embodiments, the negative impact is limited or avoided by using induction heating to melt the workpiece opposite the grooves.
Other aspects of the present technology will be in part apparent and in part pointed out hereinafter.
As required, detailed embodiments of the present disclosure are disclosed herein. The disclosed embodiments are merely examples that may be embodied in various and alternative forms, and combinations thereof. As used herein, for example, exemplary, illustrative, and similar terms, refer expansively to embodiments that serve as an illustration, specimen, model or pattern.
The figures are not necessarily to scale and some features may be exaggerated or minimized, such as to show details of particular components. In some instances, well-known components, systems, materials or methods have not been described in detail in order to avoid obscuring the present disclosure. Specific structural and functional details disclosed herein are therefore not to be interpreted as limiting, but merely as a basis for the claims and as a representative basis for teaching one skilled in the art to variously employ the present disclosure.
In some embodiments, at least one of the workpieces 110, 120 include a polymer such as polycarbonate, polyolefin (e.g., polyethylene and polypropylene), polyamide (e.g., nylons), polyacrylate, or acrylonitrile butadiene styrene.
In some embodiments, at least one of the workpieces 110, 120 include a composites such as a reinforced thermoplastic. The plastics may include any of the exemplary polymers listed above, and the reinforcement may include one or more of clay, glass, carbon, polymer in the form of particulate, fibers (short or long), platelets, and whiskers, among others.
The first workpiece 110 includes a first surface 112 and a second surface 114, and the second workpiece 120 includes a first surface 122 and a second surface 124. In one embodiment, the first workpiece 110 is positioned above the second workpiece 120 for joining, in which case the second surface 114 of the first workpiece 110 and the first surface 122 of the second workpiece contact upon joining.
To create enhanced interlock between the workpieces 110, 120 at least one groove is formed within a joining surface of the workpieces 110, 120 (e.g., the second surface 114 of the first workpiece 110 or the first surface 122 of the second workpiece 120). The groove(s) form a cavity within the workpieces 110, 120 are configured to receive melted material from the joining workpiece.
Grooves can be formed within either workpiece where the first workpiece 110 and the second workpiece 120 are made of similar materials. Similarity of the workpieces 110, 120 may be on characteristics such as, but not limited to, whether the workpieces 110, 120 are composed of the same material composition, have similar coefficient of thermal expansion, or have similar melting points.
In an embodiment in which the workpieces 110, 120 comprise similar materials, the first workpiece 110 is configured to melt and fill the grooves of the second workpiece 120. As material of the first workpiece 110 increases in temperature (due, e.g., to ultrasonic energy and/or compressional force used to join the workpieces 110, 120), the material of the first workpiece 110 melts and begins to fills the grooves of the second workpiece 120.
As the grooves of the second workpiece 120 begin to fill with melted (e.g., molten) material flowing from the first workpiece 110, walls of the grooves, which are defined by the cavity, may slightly soften (e.g., melt). At least some of the wall material is softened before the molten material from the first workpiece flows in the groove in the second workpiece 120. Slight softening of the groove wall(s) may provide additional interlock at the joint interface because the two separate surfaces (e.g., melting surface of the first workpiece 110 and softening surface of the groove) interact more than the surfaces would if the groove wall did not melt, cool to form a highly joined interface.
In some implementations of the embodiment, some of the materials of the first workpiece 110 and the second workpiece 120 intermix in the groove to form enhanced interlocking of the second surface 114 of the first workpiece 110 and the first surface 122 of the second workpiece 120. In an implementation, the second surface 114 of the first workpiece 110 and the first surface 122 of the second workpiece 120 join to form a connection in the groove lacking distinguishable surfaces that would be present if the materials did not meld together in the area.
When the first workpiece 110 and the second workpiece 120 comprise dissimilar materials, the grooves should be formed within the material with the highest melting temperature. For example, when bonding a metal workpiece, which can have a melting temperature of 600 to approximately 1200° C., with a thermoplastic workpiece, which can have a melting temperature between approximately 100 and approximately 300° C., the grooves should be formed within the metal workpiece. The thermoplastic workpiece will melt at a lower temperature than the metal workpiece causing thermoplastic material to flow into the grooves formed within the metal workpiece.
Grooves can be created using mechanical methods (e.g., sawing and stamping), electrical methods (e.g., laser and electrical discharge machining (EDM)), chemical methods (e.g., etching), among others. In the exemplary embodiment of
A slot groove 130 can be inserted into the second workpiece 120 using a laser, EDM, or other machining of incisions. The slot groove 130 provides additional interlock of the first workpiece 110 with the second workpiece 120. As the first workpiece 110 is heated during bonding, the material begins to melt and fills the slot groove.
Illustrated as the first slot groove 130 in
The slot groove 130 has a length 132 sufficient to receive material from the first workpiece 110. The length 132 of the slot groove 130 may be between approximately 10 microns (μm) and approximately 1000 millimeters (mm).
The slot groove 130 is formed at an angle 134 to the joining surface of the workpiece (e.g., the first surface 122 of the second workpiece 120). The angle 134 enhances interlock of the melted material from the first workpiece 110 with the voids created by the slot groove 130. The angle 134 may provide additional structure to strengthen the joint from fracture (e.g., peel fracture).
The angle 134 can have a range between 0 and 90 degrees from the first surface 122. In some embodiments, the angle 134 may be between approximately 30 and 60 degrees. In some embodiments, the angle 134 may be approximately 45 degrees.
In some embodiments, two or more slot grooves 130 are positioned to overlap creating an opening for increased contact surface area for receiving material from the first workpiece 110 upon melting (illustrated as the second and third slot groove 130 in
In multi-slot groove embodiments, each slot groove 130 can be positioned relative to the first surface 122 (e.g., the angle 134). A first slot groove 130, in multi-slot groove embodiments, can have a side extending at a first angle from the first surface 122 of the second workpiece 120. The first angle can for example range between 0 degrees and 90 degrees. A second slot groove 130 can have a side extending at a second angle from the first surface 122 of the second workpiece 120, forming overlap with the first slot groove 130. The second angle for example can range between 90 degrees and 180 degrees.
Additionally or alternatively, each slot groove, in multi-slot groove embodiments, can be positioned in reference to the other slot grooves 130 (e.g., an angle 136). The angle 136 for example can range between 0 and 180 degrees.
Additionally in the multi-slot groove embodiment, at least one of the slot grooves 130 may have the length 132. Alternatively, at least one of the slot grooves 130 may vary in length between approximately 10 μm and approximately 1000 mm.
A shaped groove 140 can be inserted into the second workpiece 120 using stamping or other mechanical and/or electrical manufacturing process. As seen in
The shaped groove 140 can have a depth 142 into the second workpiece 120. The depth should be sufficient to receive material from the first workpiece 110 (e.g., between approximately 10 μm and approximately 100 mm).
In some embodiments, the shaped groove 140 is positioned at an angle to the first surface 122 of the second workpiece 120. For example, if the shaped groove 140 is in the form of a trapezoid, an angle 144 to the first surface 122 can be an acute angle. However, where the shaped groove 140 is in the form of an inverted triangle, an angle 146 to the first surface 122 can be an obtuse angle.
An etched groove 150 can be inserted to the second workpiece 120 using chemicals (e.g., acid and mordant) to cut into the first surface 122. The etched groove 150 may be formed with or without an etch mask (not shown).
Where etching forms an indentation, as seen in
The etched groove 150 can be formed using a liquid-phase wet etchant (e.g., buffered hydrofluoric acid (HF), phosphoric acid (H3PO4), and nitric acid (HNO3)), or a plasma-phase dry etchant (e.g., carbon tetrachloride (CCl4), silicon tetrachloride (SiCl4), and boron trichloride (BCl3)), or other etchant. For example, the etched groove 150 may be formed using an isotropic process or an anisotropic process including phosphoric acid, where the second workpiece 120 is aluminum in composition.
In some embodiments the groves 130, 140, 150 form a continuous groove through a length (not shown) of the first workpiece 110 or the second workpiece 120. Continuous grooves may be desirable where continuous joining is desired between the first workpiece 110 and the second workpiece 120. For example continuous contact may be desired where the workpieces 110, 120 are subject to conditions of shear force and/or peel force.
In some embodiments, additional material is added to the workpiece with the lower melting temperature (e.g., the first workpiece 110 in
The additional material can be positioned at a location that corresponds to the grooves 130, 140, 150 on the second workpiece 120, thus allowing the additional material to flow directly into the grooves 130, 140, 150.
In one embodiment, the additional material includes a cast material 160, which can be molded directly onto the second surface 114 of the first workpiece 110. In another embodiment, the additional material can include a separate material 170, which can be affixed to the second surface 114 of the first workpiece 110 during a manufacturing process. Alternatively, the separate material 170 may be introduced during joining.
The cast material 160 and/or the separate material 170 have a thickness 165 that is sufficient to fill the grooves 130, 140, 150 without leaving sink marks on the first surface 112 of the first workpiece 110. The thickness 165 can directly correspond to the length and/or depth of the grooves 130, 140, 150. For example, the thickness 165 can be between approximately 10 μm and approximately 100 mm.
Any of the grooves 130, 140, 150 formed within the second workpiece 120 may be prefabricated prior to joining. Additionally the cast material 160 and/or the separate material 170 may be prefabricated onto or attached to the first workpiece 110.
The joining system 100 can be formed through a number of conventional forming processes such as, but not limited to, laser heating, induction heating, and ultrasonic welding. Each process is illustrated with one of the example grooves 130, 140, 150 described above. However, each process can utilize any of the aforementioned grooves to facilitate joining the workpieces 110, 120.
In the exemplary laser heating process, a joint is formed by compressing (compressional force denoted by arrows) the second surface 114 of the first workpiece 110 proximal to the first surface 122 of the second workpiece 120, having a melting temperature higher than that of the first workpiece 110. A laser beam 205 then provides concentrated heat on the second surface 124 of the second workpiece 120. Concentrated heating of the second workpiece 120 forms a laser weld area 200 (illustrated as an area within a circle in
In the exemplary induction heating process, compressional force abuts the second surface 114 of the first workpiece 110, comprising thermoplastic materials, with the first surface 122 of the second workpiece 120, comprising conductive materials. An induction heater 305 (e.g., a heating coil) passes electrical current (e.g., eddy current) through the second workpiece 120 and resistance leads to heating of the second surface 124 of the second workpiece 120. Heating the second workpiece 120 forms an induction weld area 300 (illustrated as an area within a circle in
Alternatively, the induction heater 305 can generate heat using losses associated with magnetic hysteresis. Generating heat using losses from magnetic hysteresis may be beneficial were the material of the second workpiece 120 has permeability.
In the exemplary ultrasonic process, compressional force of the weld horn 405 and the anvil 407 abuts the second surface 114 of the first workpiece 110 with the first surface 122 of the second workpiece 120. Vibrations from the weld horn 405 generating heat within the first surface 112 of the first workpiece 110, forming an ultrasonic weld area 400 (illustrated as an area within a circle in
Within the joining system 100, the grooves 130, 140, 150 can produce the patterns seen within
The joining system 100 as described above can include grooves 130, 140, 150 with random patterns on at least one of the workpieces 110, 120, as seen within a random distribution 510. Alternatively, the groves 130, 140, 150 may be formed within one of the workpieces 110, 120 in patterns which provide benefit to the joining application.
Patterns may provide additional strength within the joint where at least one surface of at least one of the workpieces 110, 120 contained curvilinear properties (e.g., the first workpiece 110 is curved). In one embodiment, the grooves 130, 140, 150 form a parallel line pattern 520, where the grooves 130, 140, 150 are spaced along a length and/or a width of at least one of the workpieces 110, 120. In one embodiment, the grooves 130, 140, 150 form a cross-hatch line pattern 525 to provide additional strength in more than one direction.
In one embodiment, the grooves 130, 140, 150 form a continuous line pattern 527. The continuous line pattern 527 can consist of parallel lines as seen in
Additionally, patterns may be used to provide additional strength within the joint where at least one of the workpieces 110, 120 is geometrically shaped (e.g., the first workpiece 110 is circular). Patterns can be formed using geometric shapes such as squares, circles, ovals, and triangles, among others.
Geometric patterns can be concentric in nature as seen by a concentric square pattern 530 and a concentric circle pattern 535 of
In one embodiment, the grooves 130, 140, 150 form a continuous concentric pattern 537 or a continuous independent pattern 547. The continuous concentric pattern 537 and the continuous independent pattern 547 can form any number of geometric shapes as mentioned above.
Other patterns are possible and may be preferred to a system designer depending on the application.
Many features of the present technology are described herein above. The present section presents in summary some selected features of the present technology. The present section highlights only a few of the many features of the technology and the following paragraphs are not meant to be limiting.
One benefit of the present technology is the workpieces are joined robustly through mechanical interlock provided by grooves formed on a joining surface of at least one workpiece. Mechanical interlock occurs through forming grooves on the workpiece(s) at the joining surface, which can improve joint strength, such as peel strength, over workpieces joined without grooves.
Another benefit of the present technology is physical properties of the grooves can be altered for a specific joining application. The size, shape, and depth of the grooves can be varied according to design requirements such as strength or required joining speed. Additionally, the grooves can be formed in patterns within the workpiece according to design requirements and/or workpiece shape.
Another benefit of the present technology is the mechanical interlocking at the joint surface can be accomplished without using separate mechanical interlocking items such as adhesives, rivets, or bolts. Eliminating the need for separate mechanical interlocking items can reduce the weight of the joint and provide a smooth joint surface, uninterrupted by bolt/rivet heads.
Another benefit of the present technology is the smooth joint surface is accomplished through one-sided joining. One-sided joining leaves no visible appearance impact on the workpiece surfaces opposite the joint surface. Eliminating visible impact on the workpieces allows freedom of joint design and application design freedom.
Various embodiments of the present disclosure are disclosed herein. The disclosed embodiments are merely examples that may be embodied in various and alternative forms, and combinations thereof.
Variations, modifications, and combinations may be made to the above-described embodiments without departing from the scope of the claims. All such variations, modifications, and combinations are included herein by the scope of this disclosure and the following claims.
