Impact Joining of Pure Copper C1100 and Aluminum Alloy A6061-T6 Plates at Edges

: Joining of pure copper C1100 and aluminum alloy A6061-T6 plates of 5 mm thickness was investigated. The method was developed by one of the authors, in which the newly created surfaces of a pair of plates obtained by high-speed shear were immediately in contact with a sliding motion with a small overlap length. The total processing time was just about a few milliseconds. To create the new surface, high-speed shaving was also tested. The joining was not possible for the full thickness of the plates. A sharp notch was observed at the joint boundary due to a large shear droop in the copper. Shaving decreased the shear droop, and the joint length through the plate thickness became longer. The joining performance was evaluated by a uniaxial tensile test. The joint efﬁciency reached 100% using the specimen cut out from the really joined boundary. The affected zone of joining was conﬁrmed by the hardness distribution near the boundary. It was about 30% of the thickness of the plate, which was much smaller than that in welding by heat, and no softened zone was found in both materials.


Introduction
The joining of dissimilar metals has been investigated to create a new function in parts, etc. Various metal combinations were tested in welding, bonding and mechanical joining methods. Cold joining methods of the metals by severe plastic deformation have been developed over several decades. Dissimilar metals are usually joined by friction stir welding (FSW) or a laser welding technique.
A wider range of material combinations are provided by FSW, in which the plates are stacked or butted, and the dedicated rotation tool is controlled to move along the path. The evolution of the intermetallic components and the microstructure were investigated in the FSW technique, which has a strong effect on the strength of the joint boundary of dissimilar titanium alloys and that of dissimilar aluminum materials [1,2]. The joining of aluminum to copper has been attractive in electric or battery parts, and it has been investigated [3][4][5]. Further, the addition of Ni at the interface and the coating of the titanium layer on the copper side increased the strength [6,7]. Friction stir "spot" welding technique is also applied to the joining of aluminum, copper and other metals, where the rotating tool stays [8,9]. A simple technique using drilling tool was found to join stainless steel and aluminum [10].
It is well known that time and temperature play important roles in solid-state joining by atomic diffusion at elevated temperatures. On the other hand, under cold conditions, if the surface expansion is relatively large, two metal parts can join at the newly created surface, in which the brittle oxidized surface layer fractures. Cold diffusion bonding is often achieved by very high compressive stress with large plastic deformation. The surface exposure and the pressure affect the welding strength [11]. Diffusion bonding was also tested at high temperatures [12][13][14]. Severe plastic deformation breaks the thin brittle oxide reaches the prescribed position. The method is a unique joining method that does not require heating. The joining mechanism is diffusion bonding of the newly created surface.

Joining Device and Experimental Conditions
The two joining methods were examined, one of which uses the sheared surface. Figure 2 shows the schematic and the photograph of the joining device. It is composed of the rectangular parts, because the structural simplicity is necessary to avoid excessive impulsive stress on the parts, which may cause a catastrophic damage during impact. The joining device is driven by the kinetic energy of the drop weight. The impact velocity was 10 m/s, and the mass was 22 kg. The top edge of Punch 1 is impacted by the drop weight, then the simultaneous shearing of Plates 1 and 2 begins. The illustration of Figure 2a represents the initial state. The left half side, which is the movable side, is supported by a backup plate, under which a circular pipe (A6061, 12 mm outer diameter and 1 mm-thick wall) is placed. The pipe is compressed and exhibits buckling lobes, generating a backup force.

Joining Device and Experimental Conditions
The two joining methods were examined, one of which uses the sheared surface. Figure 2 shows the schematic and the photograph of the joining device. It is composed of the rectangular parts, because the structural simplicity is necessary to avoid excessive impulsive stress on the parts, which may cause a catastrophic damage during impact. The joining device is driven by the kinetic energy of the drop weight. The impact velocity was 10 m/s, and the mass was 22 kg. The top edge of Punch 1 is impacted by the drop weight, then the simultaneous shearing of Plates 1 and 2 begins. The illustration of Figure 2a represents the initial state. The left half side, which is the movable side, is supported by a backup plate, under which a circular pipe (A6061, 12 mm outer diameter and 1 mmthick wall) is placed. The pipe is compressed and exhibits buckling lobes, generating a backup force.  Figure 3 shows the illustration of the working tools and the plates. The shearing or shaving tools were made with SKD11 tool steel (60 HRC). Die 1 and Punch 2 have a land length of 2 mm. Pre-hardened steel (40 HRC) was chosen for the material of the other parts. The width of the Plate is 50 mm, which corresponds to the length of the joint bound-   Figure 3 shows the illustration of the working tools and the plates. The shearing or shaving tools were made with SKD11 tool steel (60 HRC). Die 1 and Punch 2 have a land length of 2 mm. Pre-hardened steel (40 HRC) was chosen for the material of the other parts. The width of the Plate is 50 mm, which corresponds to the length of the joint boundary. In the shear process shown in the Figure 3a, no clearance was set between the shearing tools. To keep the prescribed overlap length, two small rubber spacers were inserted between Punch 2 and Die 1 only at both ends. Hence, the joining was not completed near both edges of the joint boundary.  Figure 3 shows the illustration of the working tools and the plates. The shearing or shaving tools were made with SKD11 tool steel (60 HRC). Die 1 and Punch 2 have a land length of 2 mm. Pre-hardened steel (40 HRC) was chosen for the material of the other parts. The width of the Plate is 50 mm, which corresponds to the length of the joint boundary. In the shear process shown in the Figure 3a, no clearance was set between the shearing tools. To keep the prescribed overlap length, two small rubber spacers were inserted between Punch 2 and Die 1 only at both ends. Hence, the joining was not completed near both edges of the joint boundary.  Further, the joining test of dissimilar materials was examined for the shaved surfaces. In the shaving of the plates, the right side of Plate 1 and the left side of Plate 2 in Figure  3a are replaced by the spacers with the same thickness. The width of the plate was 31 or 30.5 mm. The shaving allowance of the upper plate was 1.0 or 0.5 mm, and that of the lower plate was reduced by the overlap length. The mechanical properties of the test material are listed in Table 1. The materials were a pure copper C1100-1/4H and an aluminum alloy A6061-T6. The thickness of the plates was 5.0 mm. In the joining test using the sheared surface, the similar metal and the dissimilar ones were combined. The dissimilar metals were combined in the joining test using the shaved surface. Further, the joining test of dissimilar materials was examined for the shaved surfaces. In the shaving of the plates, the right side of Plate 1 and the left side of Plate 2 in Figure 3a are replaced by the spacers with the same thickness. The width of the plate was 31 or 30.5 mm. The shaving allowance of the upper plate was 1.0 or 0.5 mm, and that of the lower plate was reduced by the overlap length. The mechanical properties of the test material are listed in Table 1. The materials were a pure copper C1100-1/4H and an aluminum alloy A6061-T6. The thickness of the plates was 5.0 mm. In the joining test using the sheared surface, the similar metal and the dissimilar ones were combined. The dissimilar metals were combined in the joining test using the shaved surface.

Joining Using Sheared Surface
The examples of the joined plates are shown in Figure 4 for similar and dissimilar combinations of the materials. In these cases, the impact speed of the drop weight was 10 m/s, and the overlap length was 0.3 mm. The rubber spacer, whose color is black, is seen at the ends of the boundary. It was dragged into the boundary during the joining process. Figure 5 shows the cross-section of the joint boundary for the cases of Figure 4. The weld mismatch was caused by the vibration and the dimensional error of the stopper in the joining device. The device will be improved in future study. Gaps are observed near the plate surface. They are large in the combination of C1100 and C1100, because the shear droop of C1100 is larger than that of A6061 due to the fact that the strain hardening exponent of C1100 is greater than that of A6061.
at the ends of the boundary. It was dragged into the boundary during the joining process. Figure 5 shows the cross-section of the joint boundary for the cases of Figure 4. The weld mismatch was caused by the vibration and the dimensional error of the stopper in the joining device. The device will be improved in future study. Gaps are observed near the plate surface. They are large in the combination of C1100 and C1100, because the shear droop of C1100 is larger than that of A6061 due to the fact that the strain hardening exponent of C1100 is greater than that of A6061.  In the joining of dissimilar materials, the softened aluminum by the shear deformation is squeezed out, though the copper is not. A6061 is harder than C1100 at room temperature. However, it becomes softer than C1100 when the temperature elevates by the large deformation under impact; hence, the aluminum was squeezed out.
The joint efficiency was defined by the following equation. at the ends of the boundary. It was dragged into the boundary during the joining process. Figure 5 shows the cross-section of the joint boundary for the cases of Figure 4. The weld mismatch was caused by the vibration and the dimensional error of the stopper in the joining device. The device will be improved in future study. Gaps are observed near the plate surface. They are large in the combination of C1100 and C1100, because the shear droop of C1100 is larger than that of A6061 due to the fact that the strain hardening exponent of C1100 is greater than that of A6061.  In the joining of dissimilar materials, the softened aluminum by the shear deformation is squeezed out, though the copper is not. A6061 is harder than C1100 at room temperature. However, it becomes softer than C1100 when the temperature elevates by the large deformation under impact; hence, the aluminum was squeezed out.
The joint efficiency was defined by the following equation. In the joining of dissimilar materials, the softened aluminum by the shear deformation is squeezed out, though the copper is not. A6061 is harder than C1100 at room temperature. However, it becomes softer than C1100 when the temperature elevates by the large deformation under impact; hence, the aluminum was squeezed out.
The joint efficiency was defined by the following equation.
Joint efficiency (%) = Fracture strength/Strength of base material × 100 (1) The tensile test was performed. The width of the specimen was 10 mm. It was machined out from the central portion, and the force was loaded in the direction vertical to the joint boundary. The joint efficiency is shown in Figure 6. It was roughly evaluated for the full thickness (5 mm) and the observed contact lengths of 1.7, 3.3 or 2.5 mm. Even for the contact length, the joint efficiency is low. This implies that the contact length is not the actual joined length similar to the ultrasonic welding [31]. The notch effect also weakens the strength due to the stress concentration at the tip of the gap opening. In addition, the joining condition is not uniform over the boundary. Increasing the test sample may yield more accurate results, though the obtained result is reasonable.
With respect to the joining of C1100 and A6061, the joint efficiency calculated with a contact length of 2.5 mm is about 20%. Therefore, the actual joint length is much shorter than the contact length. When the notch effect was ignored, the calculated joint length is only about 0.5 mm.
The tensile test specimen with 4 mm width was machined out from the joined plate. The tensile speed was as low as 0.1 mm/s to avoid the speed effect on the deformation behavior, and eight specimens were used for each condition. Figure 7 shows the fracture strength and joint efficiency of the joining of C1100 and A6061 evaluated for the overlap lengths of 0.1, 0.3, 0.5 and 0.7 mm. The average fracture strength and the joint efficiency are also given in the figure. In the case of the 0.1 mm overlap length, the joint efficiency is very The tensile test was performed. The width of the specimen was 10 mm. It was machined out from the central portion, and the force was loaded in the direction vertical to the joint boundary. The joint efficiency is shown in Figure 6. It was roughly evaluated for the full thickness (5 mm) and the observed contact lengths of 1.7, 3.3 or 2.5 mm. Even for the contact length, the joint efficiency is low. This implies that the contact length is not the actual joined length similar to the ultrasonic welding [31]. The notch effect also weakens the strength due to the stress concentration at the tip of the gap opening. In addition, the joining condition is not uniform over the boundary. Increasing the test sample may yield more accurate results, though the obtained result is reasonable. With respect to the joining of C1100 and A6061, the joint efficiency calculated with a contact length of 2.5 mm is about 20%. Therefore, the actual joint length is much shorter than the contact length. When the notch effect was ignored, the calculated joint length is only about 0.5 mm.
The tensile test specimen with 4 mm width was machined out from the joined plate. The tensile speed was as low as 0.1 mm/s to avoid the speed effect on the deformation behavior, and eight specimens were used for each condition. Figure 7 shows the fracture strength and joint efficiency of the joining of C1100 and A6061 evaluated for the overlap lengths of 0.1, 0.3, 0.5 and 0.7 mm. The average fracture strength and the joint efficiency are also given in the figure. In the case of the 0.1 mm overlap length, the joint efficiency is very low or zero. It is about 30% for the case of 0.3 or 0.5 mm. It is almost zero for 0.7 mm. The suitable overlap length was determined to be 0.3 mm considering the average value of the joint efficiency. An example of fractured boundary is shown in Figure 8, which was separated by bending. The actually joined zone exhibits the gray surface. The shape of these zones is mirror symmetrical, as clearly observed in the magnified photograph. The joined part is a band with of about 1 mm width, which is about 0.7 mm apart from the center of the thickness. Considering the calculated joint length of 0.5 mm, the small tensile specimen with An example of fractured boundary is shown in Figure 8, which was separated by bending. The actually joined zone exhibits the gray surface. The shape of these zones is mirror symmetrical, as clearly observed in the magnified photograph. The joined part is a band with of about 1 mm width, which is about 0.7 mm apart from the center of the thickness. Considering the calculated joint length of 0.5 mm, the small tensile specimen with 0.5 mm thickness shown in Figure 9 was cut out from the band using a wire discharge cutting machine (Mitsubishi Electric Ltd., Japan).
(c) (d) An example of fractured boundary is shown in Figure 8, which was separated by bending. The actually joined zone exhibits the gray surface. The shape of these zones is mirror symmetrical, as clearly observed in the magnified photograph. The joined part is a band with of about 1 mm width, which is about 0.7 mm apart from the center of the thickness. Considering the calculated joint length of 0.5 mm, the small tensile specimen with 0.5 mm thickness shown in Figure 9 was cut out from the band using a wire discharge cutting machine (Mitsubishi Electric Ltd., Japan).  The joint efficiency is shown in Figure 10. The average is as high as about 80% fractured specimens are shown in Figure 11. It should be noted that the No. 3 spe fractured at the material of C1100 exhibit a diffuse necking. However, the joint effi is 95%. This is because the ultimate tensile strength of the material was evaluated original thickness of 5 mm, which was 10-times thicker than the thickness of the spe It is well known that the strength depends on the thickness, where it weakens as the ness decreases [36]. Further, the surface of the small specimen is rougher than th rolled original plate, because the specimen was made using a wire discharge cuttin chine. The joint efficiency is shown in Figure 10. The average is as high as about 80%. The fractured specimens are shown in Figure 11. It should be noted that the No. 3 specimen fractured at the material of C1100 exhibit a diffuse necking. However, the joint efficiency is 95%. This is because the ultimate tensile strength of the material was evaluated for the original thickness of 5 mm, which was 10-times thicker than the thickness of the specimen. It is well known that the strength depends on the thickness, where it weakens as the thickness decreases [36]. Further, the surface of the small specimen is rougher than the cold-rolled original plate, because the specimen was made using a wire discharge cutting machine.
The joint boundary was analyzed using the scanning electron microscopy (JEOL Ltd., Tokyo, Japan) with energy dispersive X-ray analysis (SEM-EDX) as shown in Figure 12. A thin layer whose contrast differs from those of the copper and aluminum is observed, and it is clearer in the magnified photograph. The boundary shows an irregular wavy pattern. The intensity of the aluminum with a blue line and that of the copper with a green one cross at the boundary. The intermetallic phase was not inspected at present. The temperature could not be measured, because the processing time is only a few milliseconds. Heterogeneous mixtures of Al and Cu possibly result in their intermetallic phase found in the friction stir welding of similar metals [3]. fractured at the material of C1100 exhibit a diffuse necking. However, the joint efficiency is 95%. This is because the ultimate tensile strength of the material was evaluated for the original thickness of 5 mm, which was 10-times thicker than the thickness of the specimen. It is well known that the strength depends on the thickness, where it weakens as the thickness decreases [36]. Further, the surface of the small specimen is rougher than the coldrolled original plate, because the specimen was made using a wire discharge cutting machine. The joint boundary was analyzed using the scanning electron microscopy (JEOL Ltd., Japan) with energy dispersive X-ray analysis (SEM-EDX) as shown in Figure 12. A thin layer whose contrast differs from those of the copper and aluminum is observed, and it is clearer in the magnified photograph. The boundary shows an irregular wavy pattern. The intensity of the aluminum with a blue line and that of the copper with a green one cross at the boundary. The intermetallic phase was not inspected at present. The temperature could not be measured, because the processing time is only a few milliseconds. is 95%. This is because the ultimate tensile strength of the material was evaluated for the original thickness of 5 mm, which was 10-times thicker than the thickness of the specimen. It is well known that the strength depends on the thickness, where it weakens as the thickness decreases [36]. Further, the surface of the small specimen is rougher than the coldrolled original plate, because the specimen was made using a wire discharge cutting machine. (a) (b) Figure 11. Fractured tensile test specimen joined using sheared surface: (a) Fracture at base metal of copper C1100; (b) Fracture at joint boundary.
The joint boundary was analyzed using the scanning electron microscopy (JEOL Ltd., Japan) with energy dispersive X-ray analysis (SEM-EDX) as shown in Figure 12. A thin layer whose contrast differs from those of the copper and aluminum is observed, and it is clearer in the magnified photograph. The boundary shows an irregular wavy pattern. The intensity of the aluminum with a blue line and that of the copper with a green one cross at the boundary. The intermetallic phase was not inspected at present. The temperature could not be measured, because the processing time is only a few milliseconds.

Joining Using Shaved Surface
The joining of C1100 and A6061 was investigated. An example of the joined plate shown in Figure 13. The cross-sections are shown in Figure 14 for two different over lengths. Comparing these cross-sectional profiles with those in Figure 5c, the shear dro is almost prevented. The contact length in the thickness direction of the plate is abou mm, which is longer than that in Figure 5c, though the gap opening is observed near b surfaces. The tensile test specimen shown in Figure 15 was made using a wire discha cutting machine. The thickness is 2 mm, which is half of the contact length. This length expected to be the actual joining length. This estimation may be reasonable because undulation of the boundary is also small in Figure 14 compared with that in Figure 5c

Joining Using Shaved Surface
The joining of C1100 and A6061 was investigated. An example of the joined plates is shown in Figure 13. The cross-sections are shown in Figure 14 for two different overlap lengths. Comparing these cross-sectional profiles with those in Figure 5c, the shear droop is almost prevented. The contact length in the thickness direction of the plate is about 4 mm, which is longer than that in Figure 5c, though the gap opening is observed near both surfaces. The tensile test specimen shown in Figure 15 was made using a wire discharge cutting machine. The thickness is 2 mm, which is half of the contact length. This length is expected to be the actual joining length. This estimation may be reasonable because the undulation of the boundary is also small in Figure 14 compared with that in Figure 5c. lengths. Comparing these cross-sectional profiles with those in Figure 5c, the shear droop is almost prevented. The contact length in the thickness direction of the plate is about 4 mm, which is longer than that in Figure 5c, though the gap opening is observed near both surfaces. The tensile test specimen shown in Figure 15 was made using a wire discharge cutting machine. The thickness is 2 mm, which is half of the contact length. This length is expected to be the actual joining length. This estimation may be reasonable because the undulation of the boundary is also small in Figure 14 compared with that in Figure 5c.    Figure 16 shows the joint efficiency for the three experimental conditions. The shaving allowance of A6061 is smaller than that of C1100 by the overlap length, as mentioned above. When the overlap length is 0.1 mm, the number of tests was increased. This is because the experiment was started in this condition, and the dispersion was also roughly checked. Examples of the fractured specimen are shown in Figure 17. Diffuse necking often occurs at the C1100 part, where the joint boundary is not damaged. A joint efficiency of 100% was achieved for the setting with overlap lengths of 0.1 or 0.3 mm. The possibility of perfect joining seems higher when the overlap length is set to be 0.3 mm.    Figure 16 shows the joint efficiency for the three experimental conditions. The shaving allowance of A6061 is smaller than that of C1100 by the overlap length, as mentioned above. When the overlap length is 0.1 mm, the number of tests was increased. This is because the experiment was started in this condition, and the dispersion was also roughly checked. Examples of the fractured specimen are shown in Figure 17. Diffuse necking often occurs at the C1100 part, where the joint boundary is not damaged. A joint efficiency of 100% was achieved for the setting with overlap lengths of 0.1 or 0.3 mm. The possibility of perfect joining seems higher when the overlap length is set to be 0.3 mm.   Figure 16 shows the joint efficiency for the three experimental conditions. The shaving allowance of A6061 is smaller than that of C1100 by the overlap length, as mentioned above. When the overlap length is 0.1 mm, the number of tests was increased. This is because the experiment was started in this condition, and the dispersion was also roughly checked. Examples of the fractured specimen are shown in Figure 17. Diffuse necking often occurs at the C1100 part, where the joint boundary is not damaged. A joint efficiency of 100% was achieved for the setting with overlap lengths of 0.1 or 0.3 mm. The possibility of perfect joining seems higher when the overlap length is set to be 0.3 mm.
ing allowance of A6061 is smaller than that of C1100 by the overlap length, as mentioned above. When the overlap length is 0.1 mm, the number of tests was increased. This is because the experiment was started in this condition, and the dispersion was also roughly checked. Examples of the fractured specimen are shown in Figure 17. Diffuse necking often occurs at the C1100 part, where the joint boundary is not damaged. A joint efficiency of 100% was achieved for the setting with overlap lengths of 0.1 or 0.3 mm. The possibility of perfect joining seems higher when the overlap length is set to be 0.3 mm.  It is worthwhile to confirm the affected zone by the joining. Micro Vickers' hardness was measured near the joint boundary. Figure 18 shows the distribution of the hardness for both materials. The hardness clearly increases as the measurement position is closer to the joint boundary. The affected zone due to the joining process is about 1.5 mm, which is quite small compared with the thickness of the plate. The increase in hardening is higher in C1100, because its strain hardening exponent or n-value is larger than that of A6061. The difference due to experimental condition is not observed. There is no softening region. This is a significant advantage of this joining method, because the A6061-T6 material does not weaken near the joint boundary. The strain distributions along the central line of the tensile specimen are shown in Figure 19, which were measured at the maximum load point using a digital image correlation (DIC) measurement system (GOM correlate V8 SR1, GOM, Germany). The thickness strain was calculated using the measured longitudinal and transverse strains by assuming a constant volume. The strain of A6061 is not exactly zero, but near zero, in both cases. It includes the measurement error to some extent. On the other hand, the strain of C1100 increases as the measurement point moves away from the boundary. The error is It is worthwhile to confirm the affected zone by the joining. Micro Vickers' hardness was measured near the joint boundary. Figure 18 shows the distribution of the hardness for both materials. The hardness clearly increases as the measurement position is closer to the joint boundary. The affected zone due to the joining process is about 1.5 mm, which is quite small compared with the thickness of the plate. The increase in hardening is higher in C1100, because its strain hardening exponent or n-value is larger than that of A6061. The difference due to experimental condition is not observed. There is no softening region. This is a significant advantage of this joining method, because the A6061-T6 material does not weaken near the joint boundary. It is worthwhile to confirm the affected zone by the joining. Micro Vickers' hardness was measured near the joint boundary. Figure 18 shows the distribution of the hardness for both materials. The hardness clearly increases as the measurement position is closer to the joint boundary. The affected zone due to the joining process is about 1.5 mm, which is quite small compared with the thickness of the plate. The increase in hardening is higher in C1100, because its strain hardening exponent or n-value is larger than that of A6061. The difference due to experimental condition is not observed. There is no softening region. This is a significant advantage of this joining method, because the A6061-T6 material does not weaken near the joint boundary. The strain distributions along the central line of the tensile specimen are shown in Figure 19, which were measured at the maximum load point using a digital image correlation (DIC) measurement system (GOM correlate V8 SR1, GOM, Germany). The thickness strain was calculated using the measured longitudinal and transverse strains by assuming a constant volume. The strain of A6061 is not exactly zero, but near zero, in both cases. It includes the measurement error to some extent. On the other hand, the strain of The strain distributions along the central line of the tensile specimen are shown in Figure 19, which were measured at the maximum load point using a digital image correlation (DIC) measurement system (GOM correlate V8 SR1, GOM, Germany). The thickness strain was calculated using the measured longitudinal and transverse strains by assuming a constant volume. The strain of A6061 is not exactly zero, but near zero, in both cases. It includes the measurement error to some extent. On the other hand, the strain of C1100 increases as the measurement point moves away from the boundary. The error is relatively larger in the thickness strain, because the error in the plane directions is accumulated. However, the trend is plausible, and the strain change through the boundary is smooth.

Conclusions
Impact joining at the edges of a pure copper C1100 and an aluminum alloy A6061 plates was carried out. Two different methods of generating newly created surfaces were examined. The joining was not performed through the full thickness of the plate, where the notches were observed at the plate surface. The joining test using the sheared surface exhibited the 100% joint efficiency, where the 0.5 mm thick tensile specimen machined out from the 5 mm thick joined plate was used. When the new surface was created by shaving, the shear droop in C1100 was successfully decreased, by which the contact length at the boundary was increased. The joint efficiency was 100% for the 2 mm thick specimens. The measurement of the hardness revealed that the affected zone by the joining process was quite narrow. It was only about 30% of the thickness of the plate, and no weakened zone was observed in A6061-T6. This is a significant advantage of this joining method. The strain distribution was continuous through the joint boundary.

Conclusions
Impact joining at the edges of a pure copper C1100 and an aluminum alloy A6061 plates was carried out. Two different methods of generating newly created surfaces were examined. The joining was not performed through the full thickness of the plate, where the notches were observed at the plate surface. The joining test using the sheared surface exhibited the 100% joint efficiency, where the 0.5 mm thick tensile specimen machined out from the 5 mm thick joined plate was used. When the new surface was created by shaving, the shear droop in C1100 was successfully decreased, by which the contact length at the boundary was increased. The joint efficiency was 100% for the 2 mm thick specimens. The measurement of the hardness revealed that the affected zone by the joining process was quite narrow. It was only about 30% of the thickness of the plate, and no weakened zone was observed in A6061-T6. This is a significant advantage of this joining method. The strain distribution was continuous through the joint boundary.