Patent Publication Number: US-2013228612-A1

Title: Friction bit joining of materials

Description:
BACKGROUND OF THE INVENTION 
     1. Field of the Invention 
     This invention relates generally to friction stir joining methods. More specifically, the present invention is a system and method of joining workpieces together using a friction stir tool that has at least a partially consumable pin or bit, wherein the bit may have a cutting edge that cuts through a first workpiece material when rotated at a first speed. After cutting through the first workpiece material to a sufficient depth, the rotational speed of the tool may be changed to cause plasticization of the bit itself, as well as the first workpiece material that is being joined to a second workpiece material. After sufficient heating of the first and second workpiece materials and the bit by the friction stir tool, the rotation of the tool may be rapidly decelerated or stopped completely to enable solid state bonding of the bit and the first and second workpiece materials. This process will be referred to throughout this document as friction bit joining, wherein the bit is a modified pin or rivet throughout this document. 
     2. Description of Related Art 
     There are many methods for joining metal workpieces together; some of which include welding, spot welding, fasteners (such as screws and bolts), friction stir welding, etc. The three fundamental principles that govern all joining methods include mechanical attachment, fusion joining (welding), and solid state joining (friction welding). Each principle technique has advantages; however the method often selected for an application is dictated by the one having the fewest tolerable disadvantages. 
     Examples of mechanical workpiece joining methods include screws, nuts and bolts, dovetail, swaging, riveting, interference attachment, etc. Many applications cannot use screws or bolts because the threads have limiting load carrying capability, the high cost of multiple components and assembly, the cost of the hole that must be placed in the workpieces and/or the space required for the fasteners. Dove tail and other workpieces locking methods lock in specified directions but can slide or rotate apart in other directions. Rivets have perhaps the greatest joining strength per unit area and volume of any mechanical fastener but the mechanical deformation of the rivet head reduces the energy absorbing capability as well as elongation. 
     When mechanical methods are not acceptable joining techniques, fusion welding methods are utilized unless the workpiece are not considered weldable. For example, aircraft components made from 7000 series aluminum are not considered weldable because the resulting weld strength is as low as 50% of base metal properties. High melting temperature materials (HMTM) such as steel, stainless steel and nickel base alloys can be welded but the joint strength is limited to problems associated with fusion welding. These problems include, but are not limited to, solidification defects, hard/soft zones within the weld macrostructure, residual stresses resulting from liquid to solid phase transformation, porosity, cracking, non-uniform and unpredictable microstructures, corrosion susceptibility, workpiece deformation, and loss of workpiece base material properties. 
     Post weld operations are often needed to repair distortion or evaluate the weld nondestructively and add cost to the process. In addition, there are health issues related to hexavalent chromium and manganese exposure as well as potential retina damage to the operator if proper safety procedures are not followed. In many cases, workpieces must be increased in size to use a base material of lower strength that is considered weldable in favor of a higher strength material that is not considered weldable. This is the case with automobile car bodies that are currently manufactured from lower strength steels. Advanced high strength steels (Dual Phase and TRIP steels) could be used in the frame construction to dramatically lower vehicle weight but these materials have not been used because of fusion weldability issues. 
     Friction stir welding is a solid state welding process that has many advantages over fusion welding methods.  FIG. 1  is a perspective view of a tool being used for friction stir welding that is characterized by a generally cylindrical tool  10  having a shoulder  12  and a pin  14  extending outward from the shoulder. The pin  14  is rotated against a workpiece  16  until sufficient heat is generated, at which point the pin of the tool is plunged into the plasticized workpiece material. The workpiece  16  is often two sheets or plates of material that are butted together at a joint line  18 . The pin  14  is plunged into the workpiece  16  at the joint line  18 . Although this tool has been disclosed in the prior art, it will be explained that the tool can be used for a new purpose. 
     It is noted that the terms “workpiece” and “base workpiece material” may be used interchangeably throughout this document. 
     The frictional heat caused by rotational motion of the pin  14  against the workpiece material  16  causes the workpiece material to soften without reaching a melting point. The tool  10  is moved transversely along the joint line  18 , thereby creating a weld as the plasticized material flows around the pin from a leading edge to a trailing edge. The result is a solid phase bond  20  at the joint line  18  that may be generally indistinguishable from the workpiece material  16  itself, in comparison to other welds. 
     It is observed that when the shoulder  12  contacts the surface of the workpiece, its rotation creates additional frictional heat that plasticizes a larger cylindrical column of material around the inserted pin  14 . The shoulder  12  provides a forging force that contains the upward metal flow caused by the tool pin  14 . 
     During FSW, the area to be welded and the tool are moved relative to each other such that the tool traverses a desired length of the weld joint. The rotating FSW tool provides a continual hot working action, plasticizing metal within a narrow zone as it moves transversely along the base metal, while transporting metal from the leading face of the pin to its trailing edge. As the weld zone cools, there is typically no solidification as no liquid is created as the tool passes. It is often the case, but not always, that the resulting weld is a defect-free, re-crystallized, fine grain microstructure formed in the area of the weld. 
     Travel speeds are typically 10 to 500 mm/min with rotation rates of 200 to 2000 rpm. Temperatures reached are usually close to, but below, solidus temperatures. Friction stir welding parameters are a function of a material&#39;s thermal properties, high temperature flow stress and penetration depth. 
     Previous patent documents have taught the benefits of being able to perform friction stir welding with materials that were previously considered to be functionally unweldable. Some of these materials are non-fusion weldable, or just difficult to weld at all. These materials include, for example, metal matrix composites, ferrous alloys such as steel and stainless steel and non-ferrous materials. Another class of materials that were also able to take advantage of friction stir welding is the superalloys. Superalloys can be materials having a higher melting temperature bronze or aluminum, and may have other elements mixed in as well. Some examples of superalloys are nickel, iron-nickel, and cobalt-based alloys generally used at temperatures above 1000 degrees F. Additional elements commonly found in superalloys include, but are not limited to, chromium, molybdenum, tungsten, aluminum, titanium, niobium, tantalum, and rhenium. 
     The previous patents teach that a tool is needed that is formed using a material that has a higher melting temperature than the material being friction stir welded. In some embodiments, a superabrasive was used in the tool. 
     It is also noted that the phrase “friction stir processing” may also be referred to interchangeably with “solid state processing”. Solid state processing is defined herein as a temporary transformation into a plasticized state that typically does not include a liquid phase. However, it is noted that some embodiments allow one or more elements to pass through a liquid phase, and still obtain the benefits of the present invention. 
     In friction stir processing, a tool pin is rotated and plunged into the material to be processed. The tool is moved transversely across a processing area of the material. It is the act of causing the material to undergo plasticization in a solid-state process that can result in the material being modified to have properties that are different from the original material. 
     Friction stir spot welding (FSSW) is now being used experimentally to join advanced high strength steels in lap welding configurations. FSSW is being used commercially to lap weld aluminum components as described in US Patent application 20050178817. Two approaches are currently used. 
     The first approach involves plunging a pin tool (a FSSW tool comprised of a pin and a shoulder) into workpieces until the workpieces are spot friction welded together. The disadvantage with this method is the hole  26  left behind from the pin as shown in  FIG. 2 . The bond between the workpieces  28  is achieved under the shoulder of the tool while the pin hole reduces the strength of the weld. 
     A second method involves the design of equipment to force material back into the pin hole (U.S. Pat. No. 6,722,556). This method is quite cumbersome because of the large spindle head, fixturing requirements, and loads needed to make a spot weld. 
     The embodiments of the present invention are generally concerned with these functionally unweldable materials, as well as the superalloys, and are hereinafter referred to as high melting temperature materials (HMTM) throughout this document. However, the principles of the present invention are also applicable to lower melting temperature materials such as aluminum and other metals and metal alloys that are not considered part of the high melting temperature materials. 
     Recent advancements in friction stir welding technologies have resulted in tools that can be used to join high melting temperature materials such as steel and stainless steel together during the solid state joining processes of friction stir welding. 
     As explained previously, this technology involves using a friction stir welding tool that may include a polycrystalline cubic boron nitride (PCBN) tip. Other designs of this tool are also shown in the prior art, and include monolithic tools and other designs. 
     When this special friction stir welding tool is used, it is effective at friction stir welding of various materials. This tool design is also effective when using a variety of tool tip materials besides PCBN and PCD (polycrystalline diamond). Some of these materials include refractories such as tungsten, rhenium, iridium, titanium, molybdenum, etc. 
     It would be an advantage over the state of the art in the joining of metal workpieces to be able to provide a system and method that may use a partially consumable tool to perform FSSW using a consumable bit in a rapid and economical manner. 
     BRIEF SUMMARY OF THE INVENTION 
     A method of friction bit joining of at least two workpieces, wherein a system and method of using a friction stir tool having a bit that is at least partially consumable may be improved by providing enhanced cutting geometries on the bit, modifying stop times to improve bit joining, including automated tracking in an automatic friction bit joining method, providing automated feeding and automated friction bit joining, making the friction bit joining system portable, enabling the friction stir tool to be usable by a robotic device or as a handheld device, friction bit joining a plurality of different layers even if only a base material is solid-state joinable with the consumable bit, performing metal stitching on traditionally unweldable materials, performing solid-state plug welding, and operating the friction bit tool at variable RPMs in order to improve bit joining characteristics. 
     These and other objects, features, advantages and alternative aspects of the present invention will become apparent to those skilled in the art from a consideration of the following detailed description taken in combination with the accompanying drawings. 
    
    
     
       BRIEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWINGS 
         FIG. 1  is a prior art perspective view of an existing friction stir welding tool capable of performing friction stir welding on high melting temperature materials. 
         FIG. 2  is a profile view of three welds performed using friction stir spot welding (FSSW) as done in the prior art. 
         FIG. 3  is a perspective view of a rotational tool that is constructed in accordance with the principles of the prior art that can perform fiction stir bit joining. 
         FIG. 4  is a profile view of the tool of  FIG. 3  wherein the consumable bit has fully penetrated two workpieces. 
         FIG. 5  is a profile view showing that the bit of the friction stir joining tool may operate at rake angles that are not normal to a workpiece surface. 
         FIG. 6  is a profile view showing multiple layers of workpieces, where only the bottom workpiece may form a solid-state bond with the at least partially consumable bit. 
         FIG. 7  is a top view of a workpiece with a crack, wherein metal stitching may be used to fill the crack with consumable bits. 
         FIG. 8  is a profile view of a workpiece and a friction bit joining tool having a core cutting geometry that enables solid-state plug welding of the hole. 
         FIG. 9  is a profile cut-away view of a tool having a central hole for a multi-segmented bit for rapid friction bit joining. 
     
    
    
     DETAILED DESCRIPTION OF THE INVENTION 
     Reference will now be made to the drawings in which the various elements of the present invention will be given numerical designations and in which the invention will be discussed so as to enable one skilled in the art to make and use the invention. It is to be understood that the following description is only exemplary of the principles of the present invention, and should not be viewed as narrowing the claims which follow. 
     The prior art teaches a rotating friction stirring tool having a non-consumable shoulder combined with a detachable and at least partially consumable bit that forms the basis of a friction bit joining method. The bit may be totally consumable or partially consumable.  FIG. 3  is an illustration of how the prior art teaches that the friction stirring tool may be constructed. 
       FIG. 3  is a perspective illustration of the prior art that shows a friction bit joining tool  30  having a shoulder area  32  and a detachable and at least partially consumable bit  34 . The bit  34  may also function as a rivet, but is generally referred to as a bit throughout this document. In this particular friction bit joining tool  30 , a detachable and at least partially consumable bit  34  includes a small gap  36 . A much smaller bit diameter portion  42  of the bit  34  forms the small gap  36 . This small bit diameter portion  42  of the bit  34  is caused to break. The small gap  36  enables the detachable portion  38  of the bit  34  to remain embedded within the workpieces as a bit. It is also noted that the non-detached portion  40  of the bit  34  might also be the top of another bit segment as will be explained. 
       FIG. 4  is also an illustration of the prior art and showing how to friction bit join (also known as “friction stir riveting”) steel or another metal. The friction bit joining tool  30  is rotated at a speed that allows the bit  34  of the tool to machine or cut a first workpiece material  50  away to form a hole  54  therein. Features were added to the end of the bit  34  to facilitate machining the desired hole. For example, a cutting feature  44  is shown in  FIG. 4 . 
     The present invention improves upon the prior art by teaching that the bit of the friction bit joining tool may cut into the workpieces at an angle. A first aspect of the first embodiment of the present invention is shown in  FIG. 5 . The first embodiment is directed to improving the use of friction bit joining tools when performing friction bit joining. The first embodiment teaches that a modified angle may be used for the friction bit joining tool  30 . 
     The prior art teaches cutting into the workpiece at an angle that is normal to the workpiece, as shown in  FIG. 4 . In contrast, the present invention teaches that the bit  34  on the friction bit joining tool may be able to enter the workpieces  80  at a positive or negative rake angle. The rake angle may be positive or negative without breaking the friction bit joining tool or prematurely breaking off the bit  34 . The rake angle may be anywhere from +45 degrees to −58 degrees and be within the limitations of the present invention. While the rake angle may vary between the indicated angles, the preferred rake angle of the bit  34  may be between plus or minus 7 degrees of normal. 
     The first embodiment also addresses other angles of operation. The angle that is formed by a working surface  82  of the workpieces  80  and the working end  40  or bottom relief angle of the bit  34 , may be anywhere between zero and 63 degrees. The cutting surface of the bit  34  may have a clearance relief of zero to 53 degrees. 
     The bit  34  may be characterized as a drill bit when it is used to cut into the workpieces. It has been determined that the bit  34  may have an outside cutting surface having a margin with relief. 
     The cutting features that may be used on the first embodiment of the bit  34  may be considered to include the Hosoi drill geometry with a helical cutting edge on the working end of the bit, but this should not be considered to be a limiting factor. Other cutting feature geometries may also be considered to be within the scope of the present invention. 
     Other cutting features of the present invention that may be included in the bit  34  of the first embodiment include a core cutting geometry (as shown in  FIG. 8 ) for making a hole into or through the workpieces, and a chip breaker. 
     Another aspect of the present invention expands upon the concept of using at least two different speeds for the bit  34 ; one speed for cutting, and another speed for creating a solid-state bond of the bit  34  to the workpiece. In the present invention, a single speed may be used, wherein the single speed may be sufficient for enabling cutting into the workpieces, and also for performing solid-state bonding at that same speed. 
     A feature of the prior art is that the materials used in the workpieces are all materials that may form a solid-state bond with the bit  34  when it is functioning as a rivet. In contrast, in another embodiment, the present invention teaches that there may be a plurality of different layers forming the workpieces. 
       FIG. 6  illustrates the new concept that in this embodiment there are one or more workpiece layers  90  that may not form a solid-state bond with the bit  34 . However, what may be different is that only the bottom workpiece layer  92  needs to be a material that may form a solid-state bond with the bit  34 . The bit  34  may cut through all the workpiece layers  90  above the bottom workpiece layer  92  in order to make the solid-state bond with the bottom workpiece layer. 
     In another embodiment, the workpiece layers  90  form a mechanical bond with the bit  34  and not a solid-state bond. In another embodiment, at least one workpiece layer  90  forms a mechanical bond while at least one other workpiece layer  90  forms a solid-state bond. The configuration of the workpiece layers  90 , some of which may form a mechanical bond and some of which may form a solid-state bond, may be changed as needed depending upon the application. The workpiece layers  90  may be formed of materials with vary different properties, including non-metallic materials such as plastics and composites. 
     The next aspect of the present invention is directed towards how the friction bit joining tool  30  is stopped. One example in the prior art is shown in  FIG. 4 . Once the depth  56  of the hole  54  has extended into the second workpiece  52  as shown, the rotational speed of the friction bit joining tool  30  is slowed down to generate heat between the bit  34  and the first and second workpieces  50 ,  52  that are being joined together. A spindle (not shown) that is holding and rotating the friction bit joining tool  30  may either be immediately stopped or slowed down until the torque required to rotate the tool exceeds the shear strength of the smaller bit diameter portion  42 . The smaller bit diameter portion  42  is designed to shear the detachable portion  38  of the bit  34  off of the friction bit joining tool  30  at a specified torque. 
     In contrast, the present invention teaches that rapid stopping of the friction bit joining tool  30  may cause problems for the motors that are driving the friction bit joining tool. In order to reduce wear on the motors, the present invention teaches a stopping cycle defined as the time that it takes for the friction bit joining tool  30  to go from a solid-state joining rotation rate to a complete stop. This embodiment includes slowing to a stop in less than 10 seconds, using a single-step stop time, using a multi-step stop time, using a variable RPM profile for the friction bit joining tool  30 , and including a dwell time in the stop cycle. All these stopping cycles may reduce wear on the motors controlling rotation of the friction bit joining tool  30 . 
     In another embodiment, the stopping cycle may be almost instantaneous through the use of a clutch on the motor. By using a clutch, the motor driving the spindle of the tool is free to slowly come to rest while the friction bit joining tool  30  may be stopped very rapidly, or as fast as less than one second. 
     In another embodiment of the present invention, instead of quickly stopping the rotation of the motors of the friction bit joining tool  30 , a bit is used that has a specific taper bit shape. This taper bit may only allow the bit  34  to move down into the workpieces but not come back out. Thus it is only necessary for the friction bit joining tool  30  to release the bit  34  as soon as the solid-state bond is formed. 
     In another alternative embodiment, a quick release mechanism is provided between the bit  34  and the friction bit joining tool  30 . The quick release mechanism may be spring-loaded in order to make the release of the bit  34  more rapid. 
     Another aspect of the present invention is directed towards providing a coating on at least a portion of a bit  34  for improved hardness. Improved hardness enables the bit  34  to penetrate harder workpieces. The coating may be any type that is known to those skilled in the art that will enable the bit  34  to cut into workpieces that are harder than the material used in the bit. 
     In a related embodiment, a coating may be disposed on at least a portion of a bit  34  that enables the bonding of the bit to the workpieces at a lower solid state bonding temperature than if the coating were not present. In another embodiment, a coating may be disposed on at least a portion of the bit  34  that will improve flow characteristics of the material in the workpiece around the bit. 
     In another embodiment, it may also be desirable to alter the flow characteristics of material in the workpieces during friction bit joining. Altering the flow characteristics may be achieved by reversing the rotational direction of a spindle that is rotating the friction bit joining tool  30  performing friction bit joining. 
     Another embodiment of the present invention is directed to providing a portable friction bit joining system. A portable friction bit joining system may range in size and weight from a large system that may be moved by a vehicle to various locations, down to a size and weight where the friction bit joining system may be operated by a single operator who is holding the system and supporting its&#39; weight by the operator&#39;s own hands. A portable friction bit joining tool system may also rest on the ground, be a tabletop unit, or be handheld. 
     Another embodiment of the present invention is directed towards holding or fixturing various workpieces so that they may be joined. The present invention envisions using magnetic fixturing. In this embodiment, steel is used as a backup with an electromagnetic base to hold the workpieces in place. This magnetic fixturing method may be useful for friction bit joining aluminum and composites. 
     The friction bit joining tool  30  of the present invention may also be capable of join high melting temperature materials such as steel and stainless steel together during the solid state joining processes of friction stir welding. This technology may require using a friction stir welding tool  30  with unique properties. For example, the shoulder may be created using materials such as polycrystalline cubic boron nitride (PCBN) and polycrystalline diamond (PCD). Other materials that may be included are refractories such as tungsten, rhenium, iridium, titanium, molybdenum, etc. 
     The workpieces that may be joined using the principles of the present invention include materials that have melting temperatures higher than bronze and aluminum. This class of materials includes, but is not limited to, metal matrix composites, ferrous alloys such as steel and stainless steel, non-ferrous materials, superalloys, titanium, cobalt alloys typically used for hard-facing, and air hardened or high speed steels. Furthermore, the present invention may also be used on materials that are considered to be lower melting temperature materials that are not included within the definition of the higher melting temperatures described above. 
     The shoulder  32  of the friction bit joining tool  30  may be made from polycrystalline cubic boron nitride or similarly described materials that may prevent adhesion of the shoulder to the first workpiece  50  and provide superior thermal stability and wear resistance characteristics. Several shoulder configurations may be used to form the shape of the bit head or even cut away the bit head after the bit  34  has been friction welded into the workpieces  50 ,  52 . 
     The materials used for the bit  34  are generally going to be those that may be consumed during the friction bit joining process. Such materials will preferably enhance the bond between the first and second workpiece materials, and are known to those skilled in the art of friction stir welding. 
     In another alternative embodiment, an important aspect of the present invention is creation of an automated friction bit joining system. An automated friction bit joining system may be used, for example, by a robotic friction bit joining system on an assembly line. For example, the assembly line may be used for constructing vehicles. The robotic friction bit joining system may include but is not limited to: an automated arm having the friction bit joining tool  30  on an end thereof; an automated movement system for moving the arm where the friction bit joining tool is to be used; an automated feeding system for supplying the friction bit joining tool with rivets; and an automated tracking system. These systems may also be operated manually. 
     The movement system must have at least one degree of freedom to allow the friction bit joining tool  30  to move forwards to cut and then insert a bit  34 , and then backwards to allow insertion of another bit from the feeding system, if necessary. 
     Ideally the movement system provides at least two degrees of freedom so that the friction bit joining tool  30  may be moved to various locations along a temporarily stationary workpiece so that it may insert a plurality of bits  34  before the workpiece is moved away from the robotic arm. 
     The feeding system of the present invention may be automated, but may also be manual. The feeding system may be able to supply bits  34  at a rate of at least one bit every five minutes, but preferably at a rate of one bit every few seconds as they are joined with the workpieces. 
     The feeding system may be capable of moving a bit  34  from a storage location to the friction bit joining tool  30 . Various embodiments of feeding systems are envisioned for the present invention, including the use of a retractable drive system in a spindle of the friction bit joining tool  30 , a magazine loading system, a chain feeding system, and a hopper/vibratory system for bit positioning. In another embodiment, the invention may also include the use of a second media such as tape for positioning and/or holding rivets in place, much like a nail gun, or even hand feeding rivets. 
     An automated tracking system enables the robotic arm to move the tool  30  along a specific path. The path may not be a straight line. For example, as shown in  FIG. 7 , it may be desirable to perform metal stitching where a plurality of bits  34  are being placed along a crack  100  in order to repair it. Instead of using threaded mechanical plugs, the present invention uses bits  34  that are driven into the crack  100 . The path of the crack  100  may either be pre-programmed into the movement system, or a visual scanning system may be coupled to an automated tracking system in order to follow the path of the crack and center each bit  34  before the bit is driven into the workpiece. The present invention may even be used to repair cracks in materials that are not traditionally weldable, such as cast iron. 
     Another embodiment is the use of the present invention to repair run-off holes  120  as shown in  FIG. 8 . When performing friction stir welding, a pin typically leaves behind a hole  120  when the tool is retracted. It is then necessary to plug the hole and finish the surface. In another embodiment, the present invention may be used to perform sold-state plug welding wherein a larger hole is cut into the workpiece  122  using a core cutting bit  104 , preferably centered on the existing hole  120  that is being repaired. Thus, the present invention would use a bit  104  having a core cutting geometry. The bit may cut into the workpiece  122  to a depth such that a top surface of the bit is substantially flush with the surface  124  of the workpiece  122 . 
     There are substantial benefits of using a consumable bit for the purpose of hole repair. These benefits include, but should not be considered limited to, elimination of oxidation on the workpiece, reducing stress risers on the workpiece, leaving behind a bit having a top surface that is at least as good as the material at the surface of the workpiece, if not better, and overall reduction of finishing costs. 
     In another alternative embodiment, inert gas such as argon or carbon dioxide may be caused to flow through the center of the tool  30  to prevent oxidation during friction bit joining. 
     In another alternative embodiment, more than two workpieces might be joined using the friction bit joining process of the present invention. The length of the segments of the bit  34  would therefore be adjusted accordingly. 
     In another alternative embodiment, it should be noted that the workpieces that are being joined may be the same or different materials, depending upon the application. 
     Similarly, the material used in the bit  34  may be a different material from all of the workpieces, the same material as at least one of the workpieces, or the same as the material on all the workpieces. 
     Bit profiles may be varied greatly. The bit profile may be a taper, hexagonal, or any desired shape that will perform both a cutting process and a friction bit joining process. The shape of the bit  34  will likely depend on various aspects, such as the desired bonding characteristics or the strength of the various materials being used. 
     In another embodiment, a friction bit joining tool  60  may have a hole  62  disposed through a central axis. The hole  62  allows a multi-segmented bit  64  (shown here with three segments separated by a smaller diameter pin portion  72 ) to be inserted and pushed through the hole  62  as needed. The multi-segmented bit  64  includes a plurality of gaps  66  having a smaller diameter pin portion  72 . A plunger mechanism  68  may be used to push the multi-segmented bit  64  through the tool  60  and out a working end  70 . As each segment of the multi-segmented bit  64  is broken off, the plunger mechanism  68  may push the multi-segmented bit down through the hole  62  until enough of the bit  64  is exposed for the next friction stir riveting process. In this way, multiple rivets may be inserted into work pieces without having to stop and reload a multi-segmented bit  64 . 
     The number of segments that may be used in a multi-segmented bit  64  should not be considered to be limited to three.  FIG. 9  is for illustration purposes only. More segments may be disposed on the multi-segmented bit  64 . The number of segments may also depend on the length of the tool  60  and the length of the plunger mechanism  68 . 
     The bit  64  may be in rod or wire form and fed automatically through the center of the friction bit joining tool  60 . When a square shape is used for the bit  64 , this may allow torque from the friction bit joining tool  60  to be transmitted to the bit. However, other torque transmitting profiles may be used. Even a round shape may be used for the bit  64  as long as a clamping force or clamping mechanism on the outside diameter of the bit  64  is sufficient to keep the bit from slipping within the friction bit joining tool  60  when forces are applied. 
     It should be understood that a hole  62  may be disposed completely through the shank of the friction bit joining tool  60  to a non-consumable shoulder. 
     The bit  64  may have a variety of hardnesses or hardness profiles to facilitate workpiece penetration. 
     The friction bit joining tool  60  may run to a specified position or load value at RPMs ranging from 1 to 10,000 RPM. 
     The friction bit joining tool  60  may be run in the same configuration as fusion spot welding. For example, rather than using clamping with welding tips in a C clamp configuration, a small diameter rotating tool ( FIG. 3 ) may be placed in a C clamp on the end of a robot arm. The C clamp configuration could also be used manually. 
     The bit  64  may have a fastener on the “head” so that a mechanical attachment may be used at that location. For example, the end of a bit  64  may have a threaded stub that is left to protrude above the workpieces after they have been joined. A nut may then be used to attach another component to the workpieces. 
     Some of the advantages of the friction bit joining process described in this document include, but should not be considered limited to, a solid state joining process that is rapid, low energy input process requirements, low residual stresses because of the solid state process, no predrilled hole is necessary as in conventional riveting, there is reduced or eliminated distortion of the workpieces, no hole is left in the workpieces as in FSSW, the process may be used in confined areas, Z-axis forces are comparable to current forces required to resistance spot weld, the shoulder/bit ratio may be sized to generate a specific heat profile to optimize joint strength, corrosion resistant bit materials may be used, because the process is completed at an elevated temperature the formation of the bit  34  has not yielded and will have greater energy absorption characteristics, the bit material may be overmatched to the workpiece material for greater strength, and the bit may be used at the tip of a crack to prevent further crack propagation in a workpiece. 
     It is generally the case that the bit  34  may be made using a material that is harder than the materials being joined. However, the bit  34  might be softer, but pushed with sufficient force and quickly enough; it may be used to join the harder workpiece materials. The bit  34  may also have a coating that allows penetration before the coating mechanically fails. 
     Another aspect of the invention is the option of removing the material being cut from the hole in the workpieces and being formed by the pin  34 . One method of removing the material is to use a pecking motion. A pecking motion of the friction bit joining tool  30  may also be combined with a fluid flow to remove the material. The fluid may be compressible or non-compressible, including gas, air, mist, and water. 
     As previously mentioned, the present invention may be used to join different materials together, and is not limited to three body (two workpieces and a bit) configurations. Multiple layers of materials may be joined simultaneously. Any number of materials may be bonded so long as the materials are subjected to a temperature gradient that is less than the melting temperature of the materials being bonded. 
     In another embodiment of the present invention, the bit  34  may be comprised of various materials. The bit  34  may be manufactured using materials that provide different operating characteristics that may be useful in a single bit. Thus, the bit  34  may be of bi-, tri- or multi-material construction. Furthermore, the bit  34  may be manufactured having a hardness gradient relative to a cross-sectional view of the bit. 
     The range of surface travel speeds of the friction bit joining tool  30  may be considered to be from 0.1 mm per minute to 10 meters per minute. The rotational speed of the friction bit joining tool  30  may vary from 1 rpm to 100,000 rpm. 
     The friction bit joining tool  30  of the present invention may be a composite tool, such as a tool having a CBN shoulder, or different materials having a higher or lower modulus than the materials being bonded. 
     The hardness of the materials being bonded may be considered to include all materials on the Rockwell Scales A, B and C. 
     The cutting edge on the bit  34  of the present invention may have any suitable cutting geometry. Thus, any feature may be included on the bit  34  that enables cutting, cutting and heating, and heating with the intent of causing a bond. The bit  34  may also be threaded. Thus, the bit may not have a cutting geometry. An alternative embodiment uses heating of the bit  34  to enable creation of a hole or an aperture in or through other workpieces materials. 
     The present invention enables diffusion bonding on multiple planes, include axially and the sides of the hole that is created. 
     It is to be understood that the above-described arrangements are only illustrative of the application of the principles of the present invention. Numerous modifications and alternative arrangements may be devised by those skilled in the art without departing from the spirit and scope of the present invention. The appended claims are intended to cover such modifications and arrangements.