Composite structures and methods of manufacturing the same

Abstract: A composite structure is manufactured by joining a first material (2) preferably made of a magnetically permeable material having a first joining surface (11a) in which a recess (7) having an overhang surface (6) is formed, to a second material (3) preferably made of an electrically conductive material having a second joining surface (11b), to be joined to the first joining surface (11a) of the first material. On the second joining surface (11b), a protrusion (9) having an outer configuration substantially corresponding to the inner shape of the recess (7) is integrally formed. The first and second materials (2, 3) are firmly mechanically joined to each other by, for example, a casting method, a rolling method, a pressing method, or a method by utilizing a plastic flow of the second material (3).

Description: This invention relates to a method of manufacturing a composite structure as stated in the precharacterizing portion of claim 1, to be utilized, for example, as a secondary plate of a linear motor car railway track, for inducing electric driving force for such motor car. Such a method is known from US-A-3,131,471. This document, however, discloses the joining of a pair of materials wherein both joining surfaces are provided with grooves and projections, such that a groove of the first joining surface mates with a projection of the second joining surface and vice versa. As is well known, traffic facilities have occupied a significant and important position in the social life, and among various traffic facilities, transportation means such as railways play an important role in the rapid mass transportation apart from the transportation by means of automobiles. However, as speeding up of the railway transportation has been desired, vibrations and noises caused by the transportation means has become factors which cannot be neglected in the social life. In another aspect, excavating and drilling operations as for a underground railway tunnel have become large scale ones with more and more increasing cost, and for this reason, development of a linear motor car capable of travelling along an iron railway track without generating violent vibrations or noises is highly desired and has been partially realized. In connection with the linear motor car of the character described above, a structure of a secondary plate, which functions to produce eddy current, in a primary side of the motor car for producing a driving force, must be used on the railway track. Such secondary plate is required to have high electric conductivity and magnetic permeability as well as a great resistance against shearing forces and separating forces which are generated as counter forces against the great driving force. However, in the current technique, a single metal or metallic material having these characteristics has not been developed, and accordingly, a composite structure fabricated by tightly and firmly joining materials of different kinds having a high electric conductivity and a high magnetic permiability, respectively, is utilized as the secondary plates. For example, there are known composite structures fabricated by fixedly joining face to face an aluminum plate having a high electric conductivity on a soft steel plate having a high magnetic permeability. In an example of such composite structures, the aluminum plate is press-fitted at the opposite ends thereof on the two end surfaces of the soft steel plate, and fastening screws are passed through the aluminum plate into the soft steel plate to mechanically join both the plates as a combined metallic structure. In another example, a composite structure is obtained by joining the aluminum plate to the soft steel plate by an explosion bonding method into an explosion bonded clad plate. However, as described hereinbefore, it is required for the secondary plate to possess a mechanical strength against the strong reacting forces to the driving force, acting frequently and repeatedly, and accordingly, the secondary plate must have a large resistance against shearing forces along the interface between the two elementary plates as well as against vertical separating forces imparted to the two elementary plates of the secondary plate. Particularly, when a composite structure is applied to the railway track of a subway, it is required for the composite structure to have mechanical strength or resistance against additional thermal behavior and separating forces due to temperature variations and dynamic vibrations. However, the composite structures fabricated by press-forming the two plates and then clamping by fastening screws or fabricated by the explosion bonding method cannot maintain sufficient resistance for a long period of time. Particularly, the composite structure, in which an aluminum plate and a soft steel plate are mechanically joined by pressing them and clamping them by means of bolts, tends to be loosened as time elapses, while the explosion bonding method is extremely expensive, thus being not advantageous. Moreover, when the composite structures of the characters described above are applied to the railway track of the subways, for example, sited near seasides, the railway tracks are exposed to severe environmental conditions such as corrosion or submergence and the interface between the soft steel plate and the aluminum plate are corroded. When corrosion occurs, the composite structure cannot attain the function as the secondary plate for the railway track. Accordingly, an object of this invention is to substantially eliminate defects or drawbacks encountered in the conventional technique described hereinbefore and to provide a method for manufacturing composite structures fabricated by materials of different kinds capable of maintaining for a long time firm mechanically joined condition of the different materials without causing relative shifting and separation of the joined surfaces of the materials even when the composite structure is exposed to an environment in which repeatedly acting strong shearing stresses and violent thermal behavior are imparted to the composite structure. Another object of this invention is to provide a method for manufacturing composite structures of the characters described above capable of being manufactured with low cost. According to this invention, there is further provided a method of manufacturing a composite structure fabricated from materials of different kinds, which method comprises the steps of preparing a first material having a first joining surface, forming at least a recess having an overhang side surface in the first joining surface of the first material, preparing a second material having a second joining surface, and opposing the first and second joining surfaces of the first and second materials and pressing the opposed first and second materials from one side thereof to cause plastic flow of the second material into the recess to cause the second material to be filled into the recess of the first material. In preferred embodiments of this invention, the first material is made of a magnetically permeable material and the second material is made of an electrically conductive material. The composite structure thus manufactured can provide a firm mechanically joined condition between the first and second materials by virtue of the firm engagement of the overhang surface of the recess of the first material with the underhang surface of the protrusion of the second material. In the accompanying drawings: Fig. 1A is a cross sectional view of one embodiment of a composite structure comprising materials of different kinds according to this invention; Fig. 1B is a cross sectional view of the materials, shown as being separated, of the composite structure shown in Fig. 1A; Fig. 2 is a cross sectional view of another embodiment of the composite structure according to this invention; Figs. 3 to 7 are cross sectional views of further embodiments of the composite structures, respectively, according to this invention; Fig. 8 is a fragmentary perspective view of a still further embodiment of the composite structure according to this invention; Figs. 9 and 10 are fragmentary perspective views illustrative of recesses formed in first materials of further embodiments according to this invention; Fig. 11 is a plan view showing one example of a joining surface of a first material of the composite structure according to this invention; Figs. 12 and 13 are end views as seen in the directions of arrows XII-XII and XIII-XIII of Fig. 11, respectively; Fig. 14 is a perspective view showing a first material of a composite structure according to a still further embodiment of this invention; Fig. 15 is a plan view of a first material similar to the first material shown in Fig. 14; Figs. 16 and 17 are sections taken along the lines XVI-XVI and XVII-XVII shown in Fig. 15, respectively; Fig. 18 is a sectional view illustrative of a composite structure in which a second material is firmly engaged with the material shown in Fig. 16; Fig. 19 is a cross sectional view of a first material in which a recess is to be formed; Fig. 20 is a cross sectional view showing a step to form a recess in the material shown in Fig. 19; Fig. 21 is a cross sectional view representing a next step subsequent to the step shown in Fig. 20 to form the recess; Fig. 22 is a cross sectional view showing a step to form a recess having a cross-sectional shape different from that shown in Fig. 20 in the material shown in Fig. 19; Fig. 23 is a cross sectional view showing a next step subsequent to the step shown in Fig. 22 to form the recess; Fig. 24 is a cross sectional view representing a step to form a recess in a surface of a first material of a composite structure according to a still further embodiment of this invention; Fig. 25 is a plan view showing a portion of the first material in which a recess is formed by the step shown in Fig. 24; Figs. 26 to 28 are cross sectional views illustrative of steps in sequence of forming recesses in a first material constituting a composite structure, according to a method of this invention; Figs. 29 to 32 are views explanatory of steps in sequence of joining two different materials due to plastic flow of a first material to form a composite structure; Figs. 33 to 37 are views explanatory of other steps in sequence of joining two different material due to plastic flow of a first material to form a composite structure; DESCRIPTION OF THE PREFERRED EMBODIMENTS Preferred embodiments of this invention will be described hereunder with reference to a secondary plate of an iron track for a linear motor car railway in conjunction with the accompanying drawings Fig. 1A shows a composite structure manufactured according to this invention in the form of a secondary plate 111 of an iron track, formed as a composite structure made of materials of dissimilar or different kinds. The composite structure comprises a soft steel plate 2 as a first material having a high magnetic permiability, and an aluminum plate 3 as a second material having a good electric conductivity and disposed on the soft steel plate 2, both plates 2 and 3 being joined mechanically along an interface 11. Fig. 1B shows the composite structure in a state wherein the two plates 2 and 3 are separated. As is apparent from Fig. 1B the steel plate 2 is provided with an upper joining surface 11a in which are formed a plurality of grooves or recesses 7 each converging downwardly in cross section to form a V-shape and each being obliquely oriented so as to have one side surface 6 constituted as an overhang surface, which protrudes horizontally as it extends upwards as viewed in Fig. 1B. The angle of the oblique direction and the arrangement of the grooves 7 may be changed or modified in accordance with conditions of design. The aluminum plate 3 is provided with a lower joining surface 11b on which are formed a plurality of projections or protrusions 9 each converging downwardly in cross section to form a V-shape and each obliquely projecting obliquely so as to have one side surface 8 constituted as an underhang surface which protrudes horizontally as it extends downwards as viewed in Fig. 1B. The locations and shapes of the grooves 7 of the steel plate 2 are made to accord with those of the corresponding projections 9 of the aluminum plate 3 in the joined state. Although, in the illustration of Fig. 1B, the plates 2 and 3 are separated, actually these plates 2 and 3 are firmly mechanically joined together in the manufacturing process of the composite structure 111 according to this invention, for example, by pressing the plate 3 against the plate 2 by means of a pressing roll to establish firm engagement of the projections 9 with the corresponding grooves 7 as described in detail hereafter. The composite structure 111 can thus be formed integrally as one body with extremely high joining force and resistance against shearing forces in both the longitudinal and transverse directions, as well as against vertical separating forces based on the thermal behavior due to temperature changes. With the composite structure of the character described above, in a case where a linear motor car, not shown, travels above the secondary plate 111 with a predetermined height of floatation, eddy currents are generated through the aluminum plate 3, which produces a driving force for the linear motor car. During the travel of the car, the aluminum plate 3 receives a large reaction force as a result of the driving force in the longitudinal direction thereof. However, because of great resisting forces aginst the reaction forces and the shearing forces in a direction normal to the longitudinal direction and because of a great resistance in a vertical direction as viewed in Fig. 1A against separation of the two plates due to the strong mechanical engagement between the overhang surfaces 6 of the grooves 7 of the steel plate 2 and the underhang surfaces 8 of the projections 9 of the aluminum plate 3, the secondary plate is prevented from shifting in height more than a designed allowable change in height. In addition, the tight joining along the interface between the steel plate 2 and the aluminum plate 3 can positively prevent the possibility of corrosion which may be caused by salty sea winds or submergence by flooding and so on, whereby the two plates are prevented from separating, constantly maintaining the bonded condition originally designed, thereby enabling a linear motor car to travel as designed. Fig. 2 shows another composite structure 112 manufactured according to this invention, in which all grooves or recesses 7 formed in the upper joining surface of the steel plate 2 have therein intermediate ridges or projections 10 directed upwardly to enlarge the joining surface area of the grooves 7 to thereby increase the resistance against the shearing forces. The composite structure 112 according to this embodiment is advantageous in that the projections 10 make easy plastic flows of the material of the aluminum plate 3 into the recesses 7, when the material of the plate 3 is to be pressed into the recesses 7, thus enabling better charging of the material of the plate 3 in the recesses 7. Fig. 3 shows a further composite structure 113 manufactured according to this invention, in which the overhang surfaces 6 of the recesses of the steel plate 2 and the underhang surfaces 8 of the projections or protrusions 9 of the aluminum plate 3 are arranged in a symmetrical relation with respect to a plane along the line P-P, and in which the projections 9 extend obliquely in directions away from the plane along the line P-P. This embodiment of the composite structure 113 is effective in a case where the composite structure 113 is installed in a linear portion of a railway track, and is advantageous in that it can be manufactured at low cost because of the symmetrical structure. Fig. 4 shows a composite structure 114 also manufactured according to this invention, in which the grooves or recesses 7 of the steel plate 2 and the projections or protrusions 9 of the aluminum plate 3 are both formed in a dovetail shape in cross-section with suitable distances between adjoining pairs of the recess 7 and the projection 9. The composite structure 114 according to this embodiment is advantageous in that it can be produced at low cost with a possibility of various design and arrangement of the recesses 7 and the projections 9. Fig. 5 shows a composite structure 115 also manufactured according to this invention, which has an arrangement of the grooves 7 of the steel plate 2 and the projections or protrusions 9 of the aluminum plate 3, similar to those shown in Fig. 1 but has waved overhang surface 6 and underhang surface 8 with minute pitches far smaller than those of the groove 7 and the projection 9 to facilitate firm engagement between the grooves 7 and the projections 9, whereby a strong bond between the steel plate 2 and the aluminum plate 3 can be obtained. According to this embodiment, a strong resisting force against shearing forces and separating forces which may be produced in curved portions of the railway track can be obtained. Fig. 6 shows a composite structure 116 manufactured according to this invention, in which a layer 12 of thin plate made of an electrically insulating material is interposed between the joining surfaces of the soft steel plate 2 and the aluminum plate 3, instead of the direct contact of the metallic materials of different kinds constituting the metal plates 2 and 3 in the aforementioned embodiments. According to the construction of the composite structure 116 shown in Fig. 6, corrosion, which may be caused by an electric potential difference generated between both the plates 2 and 3, can be effectively prevented. In addition, since the steel plate 2 and the aluminum plate 3 are tightly joined through the layer 16, a sufficient resisting force against the shearing forces and separating forces can be obtained. Fig. 7 shows a composite structure 117 manufactured according to this invention, in which a corrosion proof priming coat 12' is applied to the lower surface of the insulating layer 12 of the embodiment of Fig. 6 for increasing corrosion proof effect for the steel plate 2. In this embodiment, the corrosion proof coat may be applied to the upper surface of the insulating layer 12, and in a preferred modification a bonding agent having a corrosion proof characteristic may be applied instead of the corrosion proof coat. The arrangements or orientations of the grooves or recesses 7 having the overhang surfaces 6 and the projections or protrusions 9 having the underhang surfaces 8 may be optionally made as shown in Figs, 8, 9 and 10, but not limited to these arrangements. In Fig. 8, the recesses 7 and projections 9 extend linearly in the same longitudinal or transverse direction. In Fig. 9, the recesses 7 and the projections not shown have a bent form. In Fig. 10, the recesses 7 and the projections not shown extend obliquely. Figs. 11 and 13 shows a steel plate 2 of a composite structure 120 manufactured according to this invention, in which a plurality of grooves 7 are formed in the upper joining surface 11a of the steel plate 2 so as to linearly extend in parallel with each other, and each groove 7 has a cross sectional shape substantially the same as that shown in Fig. 2. A plurality of other grooves 14 are formed in the upper joining surface 11a of the steel plate 2 so as to extend in a direction to intersect the grooves 7, for example, in a direction normal to the grooves 7 as shown in Fig. 11. Figs. 12 and 13 are side views as seen in the directions of arrows XII and XIII of Fig. 11, respectively. An aluminum plate 3 to be joined with the steel plate 2 shown in Fig. 11 has projections each having substantially the same configuration as that shown in Fig. 2 as well as underhang surfaces corresponding to the overhang surfaces 6 of the steel plate 2. The aluminum plate 3 of this embodiment is further provided with ridges to be firmly engaged with the grooves 14. According thereto, the composite structure 120 is endowed with an increased resistance against external forces in the longitudinal direction of the groove 7 due to the existance of the additional grooves 14. In a steel plate 2 of a composite structure 121 shown in Fig. 14, each groove 7 has protruding portions 16 in the shape of waves along the opening thereof. The wave-shaped protruding portions 16 can be formed, for example, by punched holes 15 shown in Figs. 15 to 17. The formation of the punched holes 15 deforms the inner walls of the grooves 7 near the opening thereof so as to partially form inward protrusions 16 in wave form as shown in Fig. 15. Figs. 16 and 17 illustrate cross sections of the steel plate 2 to show the shapes of the grooves 7 and the punched holes 15. Fig. 18 shows a cross section of the composite structure 121 constructed by joining an aluminum plate 3 to the steel plate 2 shown in Fig. 14. According to this embodiment, the aluminum plate 3 are strongly joined with the steel plate 2 by virtue of the existance of the additionally provided punched holes 15. The embodiments shown in Figs. 9 to 18 are advantageous in that the resistance against shearing forces in all directions along the interface can be increased. It should be noted that the composite structures manufactured according to this invention have been described hereinbefore with reference to the preferred embodiments, but it is not limited to these embodiments and other various changes or modifications may be made. For example, ridges or grooves may be formed in zigzag shape on the underhang surfaces and overhang surfaces in plural stages in the direction of height of the protrusions and of the depth of the recesses, respectively. Further, the soft steel plate 2 and the aluminum plate 3 may be replaced with other metallic plate members of different kinds, respectively. Moreover, the composite structures manufactured according to this invention can be used not only as a secondary plate of a linear motor car track but also as composite structures requiring firm engagement between two plates or members, for example, for use in motor cars, machine tools, or as composite structures which are used under severe, violent conditions accompanied by sliding movements, vibrations or temperature variations. According to the composite structures of the characters described above, a firm engaging state between two materials can be maintained stably even under great, frequently repeated shearing and separating forces imparted to the composite structures, with the result that the function or operation of a linear motor car, for instance, can be stably maintained as designed. In addition, the joining surfaces of the two metal plates are kept in tightly bonded state in a manner of a labyrinth seal, so that separation of the two materials does not occur and any corrosive substance does not intrude to the interface even if the composite structure is exposed to corrosive atmosphere. The formation of the V-shaped grooves 7 having overhang surfaces 6 in the joining surface of the soft steel plate 2 can be made in accordance with methods described hereunder with reference to the accompanying drawings. In a first method, a blank soft steel plate 2 having a flat joining surface 11a to be bonded or joined, as shown in Fig. 19, is first prepared, and a formation roll 10 having flat opposite side surfaces and a circumferential surface provided therearound with a ridge formed so as to define a predetermined tapered peripheral surface is pressed with a predetermined pressure against the planar joining surface 11a of the steel plate 2 as shown in Fig. 20. When the formation roll 20 is rolled under the pressing condition, a sharply raised portion 24 is formed on the joining surface 11a at one side of the roll 20, as shown in Fig. 20, and simultaneously, a valley portion 25 and a slightly raised portion 26 are also formed below the formation roll 20 and at the other side thereof, respectively. A valley portion 25 flanked by the raised portion 24 of a predetermined height is formed by repeating the pressing process described above by means of the formation roll 20. In the next step, as shown in Fig. 21, when a cylindrical levelling roll 27 is rolled on the joining surface 11a in which the valley portion 25 has been formed by the pressing operation, the raised portions 24 and 26 are made flat so as to accord with the level of the other general portion of the joining surface 11a, whereby a V-shaped groove or recess 7 having the overhang surface 6 can be thus formed without carrying out a troublesome and difficult machining for cutting a sloping V-shaped groove. A method of formation of a groove 7 having such a shape as shown in Fig. 2 will be described with reference to Fig. 22. In this method, a pulley-type formation roll 20a is pressed against the joining surface 11a of the blank soft steel plate 2 shown in Fig. 19. When the formation roll 20a is rolled on the joining surface 11a while pressing the same, a groove having an intermediate ridge 28, substantially vertical side walls and raised portions 29 is formed, and by repeating the rolling steps, a V-shaped valley portion for the groove and the raised portions 29 each having a predetermined height are formed. In the next step, when a cylindrical formation roll 27a is rolled by a predetermined number of revolution on the valley portion of the joining surface 11a, the raised portions 29 are pressed into a flat state, and a groove having overhang surfaces 6 sloping outwards with respect to the ridge portion 28 can be formed. Fig. 24 is explanatory of a further method of forming grooves 7 in the joining surface of the steel plate 2. In this method a pulley-type formation roll 20a similar to that shown in Fig. 22 is utilized. A plurality of depressions 30 are formed in the outer surface of the roll 20a so as to extend in the axial direction in circumferentially equally spaced relation. When the formation roll 20a is rolled on the joining surface of the steel plate 2, protrusions 31 are formed at equal intervals on the bottom of the groove 7 as shown in Fig. 25. Instead of the depressions 30, protrusions may be provided. In this case, depressions are formed in the bottom of the groove 7. According to this embodiment, the projections of the aluminum plate 3 can be firmly engaged with the protrusions 31 when the aluminum plate 3 is joined with the steel plate 2, and accordingly, resistance of the grooves 7 against external forces in the longitudinal direction thereof is increased. Figs. 26 to 28 are explanatory of another method of forming grooves, each having a shape similar to that shown in Fig. 4, in the joining surface of the steel plate. According to this method, as shown in Fig. 26, a formation roll provided with annular roll portions 45 having a substantially rectangular cross-sectional shape is pressed against and then rolled on the joining surface 11a of the steel plate 2 to effect plastic working and to form grooves therein with raised portions 46 on both sides thereof. In the next step, as shown in Fig. 27, a roll 48 provided with circumferential grooves 47 of a substantially triangular cross section at portions corresponding to the locations of the grooves 7 of the steel plate 2 formed by the formation roll 45 is pressed and rolled so as to plastically deform the raised portions 46 towards the insides of the grooves 7 as denoted by the reference numeral 46'. In the final stage, as shown in Fig. 28, when a formation roll 49 having a cylindrical configuration is pressed against and rolled on the joining surface 11a, the raised portion 46' are further deformed inwardly to thereby form the grooves 7 each having the overhang surfaces 6 on both sides. Firm bonding or joining between the steel plate 2 and the aluminum plate 3 is be performed by a method utilizing plastic flow described hereunder. Before carrying out this method, a soft steel plate 2 with a joining surface 11a having grooves 7 provided with overhang surfaces 6, as shown in Fig 29, is first prepared, while a flat aluminum plate 3 having a joining surface 11b as shown in Fig. 30 is prepared. The thus prepared plates 2 and 3 are superimposed with their joining surfaces 11a and 11b opposed as shown in Fig. 31 and the two plates are pressed entirely uniformly by means of a pressing device or rolling device, not shown, in the arrowed direction F. The application of the pressure in the direction F causes plastic flow of the aluminum material forming the joining surface 11b of the aluminum plate 3, which has a yielding point lower than that of the steel plate 2, into the grooves 7 thereof, and continuous application of the pressure causes the aluminum material of the joining surface 11b to completely fill the grooves 7 along the entire overhang surfaces 6 thereof to achieve firm engagement of both the plates 2 and 3, which is maintained even after the pressing force has been released. The plastic flow of the material of the aluminum plate 3 into the grooves 7 of the steel plate 2 will be assisted by heating the joining surface 11b of the aluminum plate 3 by means of a high frequency heating device, for example, during the pressure application process. A final product can be obtained by carrying out a trimming operation on the thus obtained composite block of the plates 2 and 3. The composite structure 112 shown in Fig. 2 can also be manufactured by a method described below with reference to Figs. 33 to 37. According to this manufacturing method, a soft steel plate 2 having a joining surface 11a in which grooves 7 provided with overhang surfaces 6 are formed preliminarily is first prepared as shown in Fig. 33, while an aluminum plate 3 having a joining surface 11b on which projections 66 are preliminarily formed at positions corresponding to the grooves 7 as shown in Fig. 34 is prepared. The tip end of each projection 66 is formed with a groove 67 of V-shaped cross section. The aluminum plate 3 of Fig. 34 can be obtained as a section of the desired profile available in the market. It is desirable that the volumetric amount of each projection 66 on the joining surface 11b be slightly greater than the volumetric amount of each groove 7 of the steel plate 2. In the next step, as shown in Fig. 35, the aluminum plate 3 and the metal plate 2 are arranged to oppose to each other so as to achieve a positional alignment of the corresponding projections 66 and grooves 7, respectively. Thereafter, the tip end of each projection 66 is fitted into each groove 7 as shown in Fig. 36, and a pressing force F is applied uniformly to the entire aluminum plate 3 towards the metal plate 2 by means of a pressing device or rolling device. The application of the pressing force F causes plastic flow of the aluminum material forming the projections 66 of the aluminum plate 3 as described with reference to the former embodiment, and the aluminum material of the projections 66 is charged into the grooves 7 of the steel plate 2 along the entire overhang surfaces 6 as shown in Fig. 36. During this pressure application process, the plastic flow of the aluminum material into the grooves 7 along the overhang surfaces 6 can be more effectively achieved by a cotter function due to the presence of the inclined surfaces of projections formed on the bottoms of the grooves 7. In addition, the plastic flow of the material of the aluminum plate 3 upon the application of the pressing force F can be attained more precisely due to the fact that the volumetric amount of each projection 66 on the joining surface 11b of the aluminum plate 3 is designed to be slightly greater than the volumetric amount of the corresponding groove 7, whereby firm mechanical engagement between the aluminum plate 3 and the steel plate 2 is realized. The plastic flow of the aluminum material can be effected more precisely by heating the projections 66 to a predetermined temperature to reduce the yielding stress of the aluminum plate 3 during the pressure applying process as described with reference to the former embodiment. Furthermore, even after the projections 66 has contracted due to the cooling during the pressure applying process, complete filling of the aluminum material in the grooves is attained since the volumetric amount of the projections 66 is made slightly greater than that of the grooves 7. That is, the flow of the aluminum material into the grooves 7 after the contraction can be achieved without leaving vacant spaces or gaps therebetween, thus enabling to attain firm mechanical engagement between the aluminum plate 3 and the steel plate 2. In the thus manufactured composite structure, since the joining area of the aluminum plate 3 to the soft steel plate 2 is enlarged, the composite structure can be endowed with a strong resisting force against the horizontal shearing displacement and the vertical separating displacement. The methods of forming the recesses in the first material, as described hereinbefore, can be used in any type of the composite structures described hereinbefore.

Claims: A method of manufacturing a composite structure made from a pair of materials of different types mechanically joined to each other, wherein a first material (2) having a planar first joining surface (11a) is formed with a groove by rolling with a roll and then the first joining surface (11a) is subjected to rolling and pressing by means of another roll to plastically deform the groove to have an overhang side wall, and wherein a second material (3) is forced plastically against said first joining surface (11a) and into said groove to thereby mechanically join the second material to the first material, characterised in that : when forming said groove in said first joining surface (11a), a raised portion (46;24;29) is produced which is caused to protrude from the first joining surface (11a) and to extend along at least one longitudinal side of the groove as a result of plastic flow of the first material (2) adjacent the groove as said first mentioned roll (45;20;20a) is rolled on the first joining surface (11a); said raised portion (46;24;29) is deformed inwardly of the groove by said other roll (49;27;27a) to produce said overhang side wall of the groove; and said second material (3) is softer than said first material (2) so that the second material (3) plastically flows into said groove when the second material (3) is forced against the first joining surface (11a). The method of manufacturing a composite structure according to claim 1, characterised by the steps of: rolling and pressing on the first joining surface (11a) a first formation roll having radially protruding parallel annular roll portions (45) of a substantially rectangular cross-sectional shape, thereby forming in said first joining surface (11a) parallel grooves each having parallel side walls, and simultaneously forming raised portions (46) on said first joining surface (11a) along opposite longitudinal sides of each of said grooves due to plastic flow of said first material (2) adjacent each said groove as said annular roll portions (45) are pressed to form the respective grooves; then rolling and pressing on the first joining surface (11a) a second formation roll (48) having parallel circumferential grooves (47) of a substantially triangular cross-sectional shape, with respective said circumferential grooves (47) coinciding in position with respective said grooves (7) in the first joining surface, to thereby plastically deform said raised portions (46') inwardly of each groove in the first joining surface to thereby form the side walls of each groove into overhang side walls; thereafter rolling and pressing a third formation roll (49) of cylindrical configuration on the first joining surface to make it planar and to form completed overhang grooves; opposing a second joining surface of the second material (3) to said first joining surface of the first material (2); and pressing said first and second materials (2, 3) against each other to cause forced plastic flow of said softer second material into said overhang grooves in said first material (2) in a manner fully filling said over hang grooves (7), thereby obtaining firm engagement between said first and second materials. The method of manufacturing a composite structure according to claim 1, characterised by the steps of: rolling and pressing on said first joining surface a formation roll (20) having flat opposite side surfaces and a tapered peripheral surface defining a circumferential ridge of V-shaped cross section, thereby forming in said first joining surface (11a) a groove (25) of a substantially V-shaped cross section having an upright side wall and an opposite sloping side wall defining a valley portion of said groove, and simultaneously forming a raised portion (24) on said first joining surface along said upright side wall of the groove due to plastic flow of said first material adjacent said groove as said formation roll is pressed to form said groove; then rolling and pressing a cylindrical formation roll (27) on said first joining surface (11a) to plastically deform said raised portion (24) inwardly of said groove, to thereby make said first joining surface (11a) planar and to form said upright side wall into an overhang side wall (6), thus forming a completed overhang groove (7); opposing a second joining surface of the second material (3) to said first joining surface of the first material (2); and pressing said first and second materials (2, 3) against each other to cause forced plastic flow of said softer second material (3) into said overhang groove (7) in the first material in a manner fully filling said overhang groove, thereby obtaining firm engagement between said first and second materials. The method of manufacturing a composite structure according to claim 1, characterised by the steps of: rolling and pressing on said first joining surface (11a) a pulley-type formation roll (20a) having flat opposite side surfaces and a peripheral surface with a circumferential groove of a V-shaped cross section, thereby forming in said first joining surface (11a) a groove having parallel side walls and a bottom ridge (28), and simultaneously forming raised portions (29) on said first joining surface along opposite longitudinal sides of said groove due to plastic flow of said first material adjacent said groove as said formation roll (20a) is pressed to form said groove; then rolling and pressing on said first joining surface (11a) a cylindrical formation roll (27a) to plastically deform said raised portions (29) inwardly of said groove in said first joining surface, to thereby form said side walls of said groove into overhang side walls (6) and to form a completed overhang groove; opposing a second joining surface of the second material (3) to said first joining surface of the first material (2); and pressing said first and second materials (2, 3) against each other to cause forced plastic flow of said softer second material (3) into said overhang groove in said first material (2) in a manner fully filling said overhang groove, thereby obtaining firm engagement between said first and second materials.

Inventors: ASARI HIROATSU, ATSUTA TOSHIO, ISHIZUKA TOSHIHIKO, KOE SHIGEKI, KOGA SHINJI, KUMON YASUHIRO, MATSUI SHIGETOMO, MATSUMURA HIROYUKI, MURAKAMI SHIGEMI, RYOJI MAKOTO, UEKADO MASAKI, YAMADA TAKESHI, ASARI, HIROATSU, ATSUTA, TOSHIO, ISHIZUKA, TOSHIHIKO, KOE, SHIGEKI, KOGA, SHINJI,, KUMON, YASUHIRO, MATSUI, SHIGETOMO, MATSUMURA, HIROYUKI, MURAKAMI, SHIGEMI, RYOJI, MAKOTO, UEKADO, MASAKI, YAMADA, TAKESHI, KOGA, SHINJI, 2-104, KAWAJU NISHISUZU SHATAKU
Applicants: KAWASAKI HEAVY IND LTD, KAWASAKI JUKOGYO KABUSHIKI KAISHA
Application year: 1988
Main classification: B21H7
IPC codes: B21H7, H02K15, B21K25, B22D19, H02K41, B21D39, B23P11