Abstract:
A method of joining metal components having the steps of depositing adhesive material between the components and welding the components together via solid-state or fusion welding. The welds are spaced apart from the adhesive material and are produced so as to prevent exposure of the adhesive material to the welding. The two types of bonds (adhesive and welding) are produced in the components separated by time and space.

Description:
BACKGROUND OF THE INVENTION 
   1. Field of the Invention 
   The present invention relates to methods of joining metal components, more particularly to a method of joining metal components involving welding the components together and inserting an adhesive between the welded components. 
   2. Prior Art 
   Metal components are conventionally joined together in a variety of techniques including fusion welding, solid state bonding, chemical/mechanical bonding and mechanical engagement and locking. In fusion welding, the components are joined together through coalescence of molten metals. A weld between the components occurs when the molten metals of the components intermix and solidify. Conventional processes which are based upon fusion welding include gas metal arc welding (e.g. gas tungsten arc welding) and laser beam welding. In solid-state joining of metal components, interfacial diffusion between the mating surfaces is achieved by forcing the parts together under pressure and application of heat at the interface between the components or forcing together simultaneously plasticized metals such as in friction stir welding and forging. Chemical/mechanical bonding of metal components includes the use of adhesives, mechanical engagement of locking of components such as via bolts, rivets, and other such fasteners. 
   In certain circumstances where structural redundancy is important or additional sealing is required between the two components, two of these joining processes may be combined to impart their particular beneficial characteristics to the overall performance of the joint. This approach of using two joining processes has been utilized in the aerospace, automotive and transportation industries. Typically, mechanical fasteners are used to join components along with adhesives or sealants. Such joints that include mechanical fasteners and adhesives have been strong and reliable. 
   However, a combination of fusion and solid state based welding processes with chemical/mechanical bonding processes (e.g., using adhesives) has been problematic. Metallurgical incompatibilities arise when these two processes are applied either simultaneously at the same joining area or even when the two processes are performed sequentially. Contact between adhesive (typically an organic material) and hot molten plasticized metals, which form during welding, results in serious damage to the integrity of both the welded joint and the adhesive bond. In some instances, contact between the molten metal of the weld and the adhesive causes the adhesive to violently disintegrate into hydrocarbonaceous fumes which disrupts the stability of the welding process (such as the welding arc, laser beam generated plasma over a keyhole and molten pool), introduces contaminants into solidifying welds (producing gross open and bulk pores, craters, inclusions and excessive crud on the surface) and leads to inconsistent weld geometries. If an adhesive is applied while welding is occurring, the weld may become displaced or change shape by the fumes erupting from the adhesive, become petrified in distinct locations or develop uncontrolled pores and skips, all of which lead to compromised joint quality and uniformity. When hot plasticized metal contacts an adhesive, some of the adhesive may be incorporated into the metal and distributed as continuous (e.g. films) or fragmented contaminants throughout the weld. 
   Accordingly, a need remains for a method of joining metal components using fusion or solid state welding along with adhesive bonding which avoids these problems. 
   SUMMARY OF THE INVENTION 
   This need is met by the method of the present invention which combines joining via welding and via adhesive/sealants by physically separating the two joining processes, either through physical separation between the application of the two processes and/or sequencing their use. The method includes steps of providing a first metal component having a first joint surface, providing a second metal component having a second joint surface, fusion or solid state welding the first and second joint surfaces together and depositing adhesive material between the first and second joint surfaces. Adhesive material may be dispensed into a recess defined in the second joint surface. The first component may define an opening for delivery of the adhesive into the recess in the second joint surface. The adhesive may be pre-placed prior to welding (using a curable adhesive that may be expandable) or applied after welding through controlled injection. 
   The welds may be elongated or the components may be welded in a plurality of locations with adhesive located at positions between the welds. The recess in the second component may surround the welds. 
   The adhesive material may include a reinforcing member such as fibers or mesh. The reinforcing member may further comprise a locking member which engages with at least one of the first and second joint surfaces. Alternatively, the adhesive material may be expandable. 
   The present invention further includes an assembly of joined metal components produced according to the method of the present invention. The method of the present invention is particularly suited for producing joints between the first and second components of an aircraft fuselage such as between a skin member and a stringer or for joining components of an automobile. 
   A complete understanding of the invention will be obtained from the following description when taken in connection with the accompanying drawing figures wherein like reference characters identify like parts throughout. 

   
     BRIEF DESCRIPTION OF THE DRAWINGS 
       FIG. 1  is a cross section of a pair of metal components prior to joining; 
       FIG. 2  shows the components of  FIG. 1  after welding and dispensing of adhesive according to the present invention using a backing plate; 
       FIG. 3  is a top view of the welded components of  FIG. 2 ; 
       FIG. 4  is a cross section of an alternative arrangement of welds and adhesive in a joint between two components; 
       FIG. 5  is a cross section of an alternative arrangement of welds and adhesive in a joint between two components; 
       FIG. 6  is a cross section of a pair of joined metal components utilizing expandable adhesive and welding; 
       FIG. 7  is a cross section of welded components joined according to the present invention using an adhesive with a reinforcing member; 
       FIG. 8  is a cross section of welded components joined according to the present invention using an adhesive with a reinforcing member; 
       FIG. 9  is a cross section of welded components joined according to the present invention using an adhesive with a reinforcing member; and 
       FIG. 10  is a cross section of metal components joined using a locking member, adhesive and welding. 
   

   DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS 
   For purposes of the description hereinafter, the terms “upper”, “lower”, “right”, “left”, “vertical”, “horizontal”, “top”, “bottom” and derivatives thereof relate to the invention as it is oriented in the drawing figures. However, it is to be understood that the invention may assume various alternative variations and step sequences, except where expressly specified to the contrary. It is also to be understood that the specific devices and processes illustrated in the attached drawings, and described in the following specification, are simply exemplary embodiments of the invention. Hence, specific dimensions and other physical characteristics related to the embodiments disclosed herein are not to be considered as limiting. 
   The present invention is directed to a method of producing joined metal components using fusion or solid-state welding with adhesives or sealants. An important feature of the present invention is that the adverse interactions of these two types of joining processes can be avoided by separating the joints produced by each process in time and space. The welds produced according to the present invention are fusion welds or solid-state welds and are referred to generically hereinafter as “welds” or “welding”. Suitable fusion welding processes include gas metal arc welding, laser beam welding, electron beam welding, and resistance seam welding Suitable sold-state welding processes include friction stir welding, forging, clinching and ultrasonic seam welding. The present invention is particularly suited for use in joining aluminum alloy components. 
   Referring to  FIGS. 1 and 2 , a first metal component  2  having an exposed surface  4  and a first joint surface  6  is positioned against a second metal component  8  having a second joint surface  10 .  FIG. 1  depicts the first component  2  as being a sheet product and a second component  8  as being a structural component such as a rib. This arrangement is not meant to be limiting; other shapes of metal components may be joined according to the method of the present invention. The first component  2  defines at least one opening  12  therethrough. The opening  12  is aligned with a recess  14  defined in the second component  8 . The opening  12  and the recess  14  are sized and configured for dispensing adhesive through the opening  12  into the recess  14 . The recesses  14  are shown and described as being defined in the second component  8 , however they may instead be defined in the first joint surface  6  of the first component  2  or in both of the components  2 ,  8 . 
   Referring to  FIG. 2 , adhesive material  16  is inserted (e.g. injected) through the opening  12  and fills the recess  14 . Adhesive  16  may also fill the opening  12 . Prior to dispensing adhesive or after dispensing the adhesive into the recess  14 , the components  2  and  8  are welded together at location  18 . The weld  18  shown in  FIG. 2  is depicted as being the result of friction stir welding. If the adhesive  16  is introduced into recesses  14  before the weld  18  is formed (through placement of an adhesive/sealant pad or the like), it may be helpful to support the second component  8  with a support member such as backing plate  20  that provides a surface against which the second component  8  bears when urging the first component  2  against the second component  8  to ensure contact of the adhesive  16  with the first joint surface until the adhesive  16  sets. Nonlimiting examples of injectable adhesive/sealant material for use in the present invention include epoxy-based structural adhesives, silicones and polysulfides. 
   Referring to  FIG. 3 , the recess  14  may be continuous and surround the length of the weld  18 . A plurality of openings  12  in component  2  are shown. The quantity and placement of the openings  12  is dependent on the size of the recess  14 . The adhesive surrounding the weld  18  serves to strengthen the bond between the components  2  and  8  as wells as to seal off the portion of the weld  18  between the components  2 , 8  from the environment. 
   In the embodiment of  FIG. 4 , sealing welds  22  are produced outside the periphery of the recess  14  prior to dispensing the adhesive  16 . By joining the edges of the components  2  and  8  together, adhesive  16  may be dispensed into the recess  14  without use of a backing plate  20  or other device to force mating between components  2  and  8 . 
   Another embodiment shown in  FIG. 5  features adhesive dams (or pads)  24  positioned at the edges of the second component  8 . The adhesive dams  24  occupy a peripheral portion of recesses  14 ′ which extend to the edge of the second component  18 . Adhesive dams  24  are inserted into the peripheries of recesses  14 ′ prior to dispensing the adhesive  16 . The adhesive dams  24  adhere to both of the first and second components  2  and  8  and maintain the components  2  and  8  in contact with each other during welding or dispensing of the adhesive  16  thereby obviating the need for a backing plate  20  or the like. The pre-formed dams  24  may be epoxy-based structural adhesives in the form of a tape. 
   Joints between the first and second components  2 ,  8  described above may generally be joined according to the following process. The components  2 ,  8  to be joined are placed in their proper relative spatial relationship with the aid of a fixturing device and/or use of tack spot joints such as via resistance spot welding or riveting or optionally by applying sealing welds  22  or adhesive dams  24 . The first component  2  is fusion or solid state welded to the second component  8 . Adhesive  16  is injected through openings  12  into the recesses  14  while maintaining the first component  2  abutting the second component  8 , optionally with backing plate  20  as needed. The adhesive  16  may require curing at room temperature or heating to set. Alternatively, adhesive/sealant pads may be placed in the recesses between components  2  and  8  prior to welding, thereby eliminating the need to inject adhesive after welding. 
   Referring to  FIG. 6 , the present invention may be practiced without using recesses in the components to be joined. Expandable adhesive members  101  are sandwiched between first component  102  and second component  108  prior to welding. Welds  18  are formed in between the locations of adhesive members  101 . The material of the adhesive members  101  is cured or activated to expand their size, shown exaggerated in  FIG. 6 . Pressure indicated by the arrows is applied to the first component  102  in the locations of the adhesive members  101  to adhere the components  102  and  108  together. 
   As shown in  FIGS. 7–9 , the recesses  14  may include reinforcing members in addition to the adhesive material  16 . Suitable reinforcing members includes metal fibers  110  ( FIG. 7 ) and metal mesh  112  ( FIG. 8 ) or combinations thereof as shown in  FIG. 9  where recess  14  contains adhesive material  16  along with fibers  110  and mesh  112 . 
   In yet another embodiment of the invention, both components to be joined define recesses for receiving adhesive material. In  FIG. 10 , first component  202  has a first joint surface  206  and second component  208  has a second joint surface  210 . Joint surface  206  defines recesses  214   a  having a plurality of extensions  215   a . Joint surface  210  likewise defines recesses  214   b  with extensions  215   b . Adhesive material  216  lines the interior surfaces of the recesses  214   a  and  214   b . A locking member  230  is shaped and configured to fit within adjoining recesses  214   a  and  214   b . Locking member  230  may be made of a plastic, fiber-reinforced material or the like. The adhesive material  216  serves to adhere the locking member  230  to each of the first and second components  202  and  206 . As in other embodiments, a fusion or solid-state weld  18  is formed between the location of the adhesive joints using locking members  230 . Other configurations for the recesses  214   a  and  215   b  and the locking members  230  are possible. 
   Assembly of metal components according to the present invention is beneficial in the structural redundancy of two joining processes. Most welding processes that involve heat such as gas metal arc welding, laser beam welding and friction stir welding, produce welds and heat affected zones that have mechanical properties which are inferior to the properties of the metals being joined. By combining adhesive bonding with welding, the strength of the adhesive bonding can compensate for the weakened welded regions. In addition, adhesive bonding overcomes some of the inherently lower fatigue life of certain welded joints such as lap penetration joints. The assembly of joint components is more tolerant to damage and minimizes crack propagation. Adhesives or adhesive/sealants isolate the interface between the components to prevent migration of moisture or other corrosive materials could otherwise trigger accelerated crevice-corrosion attack. In general, it is beneficial to space apart the edges of the welding from the adhesive material by about 1–3 mm. 
   It will be readily appreciated by those skilled in the art that modifications may be made to the invention without departing from the concepts disclosed in the foregoing description. Such modifications are to be considered as included within the following claims unless the claims, by their language, expressly state otherwise. Accordingly, the particular embodiments described in detail herein are illustrative only and are not limiting to the scope of the invention which is to be given the full breadth of the appended claims and any and all equivalents thereof.