Double-sided friction stir welding method for metal sheets and double-sided friction stir welding device

Abstract

There is provided a friction stir welding method in which, when double-sided friction stir welding is performed, enough plastic flow to obtain a welded state uniform in the thickness direction of metal sheets can be obtained, in which an increase in welding speed is achieved while the occurrence of defects during welding is prevented, and in which sufficient strength and improvement in welding workability can be achieved. There is also provided a friction stir welding device suitable for the friction stir welding.

Claims

1. A double-sided friction stir welding method comprising: disposing a first rotating tool on a top side of a butt joint between two metal sheets and a second rotating tool on a bottom side of the butt joint; moving the rotating tools along the butt joint in a welding direction while the rotating tools are rotated to thereby soften a portion of the metal sheets by heat of friction between the rotating tools and the metal sheets; and stirring the softened portion with the rotating tools to generate plastic flow to thereby join the metal sheets together, wherein each of the rotating tools includes a shoulder and a pin that is disposed on the shoulder and shares a rotation axis with the shoulder, at least the shoulder and the pin being formed of a material harder than the metal sheets, with the metal sheets fixed by a holding unit, the rotating tools are pressed against the respective top and bottom sides of the metal sheets and moved in the welding direction while rotated, the rotation axes of the rotating tools are tilted at a tilt angle α)(°) with respect to a direction normal to the metal sheets such that tips of the pins are located on a leading side in the welding direction, and the tilt angle α satisfies:
0<α≤3, a gap G (mm) between the shoulders that is created by forming a gap g (mm) between the tips of the pins of the rotating tools satisfies:
(0.5×t)−(0.2×D×sin α)≤G≤t−(0.2×D×sin α), where t is the thickness (mm) of each of the metal sheets, and D is the diameter (mm) of the shoulders of the rotating tools, the diameter D (mm) of the shoulders and the thickness t (mm) of each of the metal sheets satisfy:
4×t≤D≤20×t, the gap g, the thickness t (mm) of each of the metal sheets, and the diameter D (mm) of the shoulders of the rotating tools satisfy:
[0.1−0.09×exp{−0.011×(D/t).sup.2}]×t≤g≤[1−0.09×exp{−0.011×(D/t).sup.2}]×t, the pair of rotating tools are rotated in opposite directions to perform friction stir welding, and numbers of revolutions S (rpm) of the rotating tools rotated in the opposite directions are the same, and a ratio T/S of a welding speed T (m/min) of the rotating tools to the number of revolutions S of the rotating tools, the gap G (mm) between the shoulders, the diameter D (mm) of the shoulders, and the thickness t (mm) of each of the metal sheets satisfy:
T/S≤( 1/1000)×(D/t)×{34.5−32.2×(G/t)}/{53−3.4×(D/t)}.

2. A double-sided friction stir welding method comprising: disposing a first rotating tool on a top side of a lap joint between two metal sheets and a second rotating tool on a bottom side of the lap joint; moving the rotating tools along the lap joint in a welding direction while the rotating tools are rotated to thereby soften a portion of the metal sheets by heat of friction between the rotating tools and the metal sheets; and stirring the softened portion with the rotating tools to generate plastic flow to thereby join the metal sheets together, wherein each of the rotating tools includes a shoulder and a pin that is disposed on the shoulder and shares a rotation axis with the shoulder, at least the shoulder and the pin being formed of a material harder than the metal sheets, with the metal sheets fixed by a holding unit, the rotating tools are pressed against the respective top and bottom sides of the metal sheets and moved in the welding direction while rotated, the rotation axes of the rotating tools are tilted at a tilt angle α(°) with respect to a direction normal to the metal sheets such that tips of the pins are located on a leading side in the welding direction, and the tilt angle α satisfies:
0<α≤3, a gap G (mm) between the shoulders that is created by forming a gap g (mm) between the tips of the pins of the rotating tools satisfies:
(0.5×t)−(0.2×D×sin α)≤G≤t−(0.2×D×sin α), where t is the total thickness (mm) of the lapped metal sheets, and D is the diameter (mm) of the shoulders of the rotating tools, the diameter D (mm) of the shoulders and the total thickness t (mm) of the metal sheets satisfy:
4×t≤D≤20×t, the gap g, the total thickness t (mm) of the metal sheets, and the diameter D (mm) of the shoulders of the rotating tools satisfy:
[0.1−0.09×exp{−0.011×(D/t).sup.2}]×t≤g≤[1−0.09×exp{−0.011×(D/t).sup.2}]×t, the pair of rotating tools are rotated in opposite directions to perform friction stir welding, and numbers of revolutions S (rpm) of the pair of rotating tools rotated in the opposite directions are the same, and a ratio T/S of a welding speed T (m/min) of the rotating tools to the number of revolutions S of the rotating tools, the gap G (mm) between the shoulders, the diameter D (mm) of the shoulders, and the total thickness t (mm) of the metal sheets satisfy:
T/S≤( 1/1000)×(D/t)×{34.5−32.2×(G/t)}/{53−3.4×(D/t)}.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIGS. 1A and 1B show schematic perspective views of examples of the arrangement of rotating tools and metal sheets in the disclosed embodiments, with FIG. 1A showing the case of a butt joint, and FIG. 1B showing the case of a lap joint.

(2) FIG. 2A is a plan view of one of the rotating tools and the metal sheets in FIGS. 1A and 1B, and FIG. 2B is a cross-sectional view taken along arrow A-A.

(3) FIGS. 3A and 3B show cross-sectional views illustrating the cross-sectional dimensions of rotating tools used in Examples.

(4) FIG. 4 shows the relation between the axial load between opposed rotating tools and the gap between shoulders of the opposed rotating tools.

(5) FIG. 5 shows the relation between the axial load and the ratio of the welding speed to the number of revolutions.

DETAILED DESCRIPTION

(6) In the disclosed embodiments, two metal sheets are butted or lapped together, and a pair of rotating tools are disposed on the top and bottom sides of the butt joint or the lap joint. Then double-sided friction stir welding is performed.

(7) Referring to FIGS. 1A-2B, double-sided friction stir welding of a butt joint will be described in detail.

(8) As shown in FIGS. 1A and 1B, a pair of rotating tools 1 and 8 opposed to each other are disposed on the top and bottom sides of two butted metal sheets 3. The rotating tools 1 and 8 are inserted into an unwelded joint 12 from both the top and bottom sides of the metal sheets 3 and moved in a welding direction while rotated. An arrow P in FIGS. 1A and 1B represents the moving direction of the rotating tools 1 and 8 (i.e., a welding direction). An arrow Q represents the rotation direction of the rotating tool 1 disposed on the top side, and an arrow R represents the rotation direction of the rotating tool 8 disposed on the bottom side.

(9) The pair of opposed rotating tools 1 and 8 are rotated to generate frictional heat to thereby soften a portion of the metal sheets 3, and the softened portion is stirred with the pair of rotating tools 1 and 8 to generate plastic flow to thereby join the metal sheets 3 together. The thus-obtained welded joint 4 is formed linearly in the moving direction of the rotating tools 1 and 8. A straight line 7 (hereinafter referred to as a joint center line) extending from the unwelded joint 12 in FIGS. 1A and 1B through the center of the welded joint 4 in its width direction coincides with the trajectory of the rotating tools 1 and 8 moving in the direction of the arrow P (see FIG. 2A).

(10) The two metal sheets 3 are held by a holding unit (not shown) when the rotating tools 1 and 8 are moved along the joint center line 7, and the metal sheets 3 are thereby fixed at prescribed positions. No particular limitation is imposed on the structure of the holding unit, so long as the holding unit used can prevent changes in the positions of the metal sheets 3 during movement of the rotating tools 1 and 8.

(11) The tip of a pin 6 of the top side rotating tool 1 and the tip of a pin 10 of the bottom side rotating tool 8 do not abut against each other, and a gap g (mm) is present therebetween as shown in FIG. 2B. A gap G (mm) is formed between stepped portions 5 and 9 (hereinafter referred to as shoulders) generated by the difference between the diameter D (mm) of the rotating tools 1 and 8 and the diameter a (mm) of the tips of the pins 6 and 10.

(12) As viewed from the top side, the bottom side rotating tool 8 is rotated in a direction (a direction of arrow R) opposite to the rotation direction of the top side rotating tool 1 (i.e., the direction of arrow Q). For example, as shown in FIG. 2A that is a plan view when the metal sheets 3 are viewed from the top side, when the rotating tool 1 is rotated clockwise, the rotating tool 8 is rotated counterclockwise. Although not illustrated, when the rotating tool 1 is rotated counterclockwise, the rotating tool 8 is rotated clockwise.

(13) As described above, the gap g is formed between the tip of the pin 6 of the rotating tool 1 and the tip of the pin 10 of the rotating tool 8, and the gap G is formed between the shoulder 5 of the rotating tool 1 and the shoulder 9 of the rotating tool 8. Moreover, the rotating tool 1 and the rotating tool 8 are rotated in opposite directions. Since a sufficient temperature increase and sufficient shear stress are applied from both sides, the differences in temperature and plastic flow that are generated in the thickness direction of the metal sheets 3 at the welded joint 4 are reduced, and a uniform welded state can be obtained. Since poor plastic flow that occurs locally in the welded joint 4 can be eliminated, welding defects can be advantageously eliminated. Therefore, sufficient strength can be obtained, and welding workability, particularly the welding speed, can be improved.

(14) The top side rotating tool 1 includes the shoulder 5 and the pin 6 that is disposed on the shoulder 5 and shares a rotation axis 2 with the shoulder 5. The bottom side rotating tool 8 includes the shoulder 9 and the pin 10 that is disposed on the shoulder 9 and shares a rotation axis 11 with the shoulder 9. At least the shoulders 5 and 9 and the pins 6 and 10 are formed of a material harder than the metal sheets 3.

(15) Since the rotation directions Q and R of the opposed rotating tools 1 and 8 on the top and bottom sides are opposite to each other, rotating torques applied to the metal sheets 3 by the rotation of the rotating tools 1 and 8 cancel each other. Therefore, jigs holding the metal sheets 3 can have a simpler structure than those used in a conventional friction stir welding method in which a rotating tool is pressed against metal sheets from one side to join the metal sheets together.

(16) If the rotation directions of the opposed rotating tools 1 and 8 on the top and bottom sides are the same, the relative speed of the bottom side rotating tool 8 with respect to the top side rotating tool 1 is zero. Therefore, as the plastic flow in the metal sheets 3 at the gap between the shoulders 5 and 9 of the rotating tools 1 and 8 approaches a uniform state, plastic deformation decreases, and heat generation due to the plastic deformation of the metal sheets 3 is not obtained, so that a good welded state cannot be achieved.

(17) In order that a temperature increase and shear stress enough to achieve a good welded state are obtained uniformly in the thickness direction of the workpieces, the rotation directions Q and R of the opposed rotating tools 1 and 8 on the top and bottom sides are opposite to each other.

(18) In the disclosed embodiments, adjusting the arrangement of the rotating tools as follows is effective in improving the service life of the rotating tools, preventing the occurrence of welding defects, and increasing the welding speed.

(19) First, the tilt angle α (° of the top and bottom side rotating tools will be described.

(20) The rotation axes 2 and 11 of the rotating tools 1 and 8 are tilted at an angle α (° with respect to a direction normal to the metal sheets 3, so that the tips of the pins 6 and 10 are located on a leading side in the welding direction P. In this case, loads on the rotating tools 1 and 8 are applied thereto as compressive force components in the direction of the rotation axes 2 and 11. It is necessary that the pair of rotating tools 1 and 8 be formed of a material harder than the metal sheets 3. When a low-toughness material such as a ceramic is used, if a force in a bending direction is applied to the pins 6 and 10, stress is concentrated locally, and the pins 6 and 10 may break. Therefore, by tiling the rotation axes 2 and 11 of the pair of rotating tools 1 and 8 at the angle α (hereinafter referred to as a tilt angle), the loads on the rotating tools 1 and 8 are applied as the compressive force components in the rotation axes 2 and 11. In this case, the force in the bending direction can be reduced, and breakage of the rotating tools 1 and 8 can be avoided.

(21) The above effect can be obtained when the tilt angle α exceeds 0°. However, if the tilt angle α exceeds 3°, the top and bottom surfaces of the welded joint are concaved, and this adversely affects the welded joint strength. Therefore, the upper limit of the tilt angle α is 3°. Specifically, the tilt angle α is within the range of 0<α≤.sub.3.

(22) Next, the gap G (mm) between the shoulders of the top and bottom side rotating tools will be described.

(23) In the double-sided friction stir welding, to increase the welding speed while the occurrence of defects during welding is prevented, it is necessary to strictly control the gap G between the shoulders 5 and 9 of the pair of rotating tools 1 and 8. The gap G is important in order that a temperature increase and shear stress enough to achieve a welded state are obtained uniformly in the thickness direction of the metal sheets 3.

(24) The tilt angle α of the top and bottom side rotating tools 1 and 8 is set to 0°<α≤3°. The gap G (mm) is set within the range of from (0.5×t)−(0.2×D×sin α) to t−(0.2×D×sin α) inclusive using the diameter D (mm) of the shoulders 5 and 9 of the rotating tools 1 and 8 and the thickness t (mm) of each of the metal sheets 3 when they are butt welded or the total thickness t (mm) of the metal sheets 3 when they are lap welded. In this case, the shoulders 5 and 9 of the opposed rotating tools 1 and 8 come into intimate contact with or are pressed into the top and bottom sides of the metal sheets 3. Therefore, the metal sheets 3 are pressed under a sufficient load from the top and bottom sides by the shoulders 5 and 9 of the rotating tools 1 and 8.

(25) FIG. 4 shows the gap G between the shoulders of the top and bottom side rotating tools and an axial load F therebetween. In this case, steel sheets having the thickness, chemical composition, and tensile strength shown in No. 1 in Table 1 were used. The butt joint surface had a surface state equivalent to that obtained by milling, and were a so-called I-type groove with no beveling. Rotating tools having a cross-sectional shape shown in FIG. 3A and formed of tungsten carbide (WC) were disposed on the top and bottom sides and pressed against the steel sheets at a tilt angle α of 1.5° to perform friction stir welding with the number of revolutions of the top and bottom side rotating tools set to 1,000 rpm and the welding speed set to 2 m/min. In this case, the limited range of the gap G is from 0.74 mm to 1.54 mm inclusive, and the axial load F can be 10 kN or more when the gap G is 1.54 mm or less. When the metal sheets are pressed under a sufficient load, friction by the shoulders 5 and 9 of the rotating tools 1 and 8 and plastic deformation in a shear direction facilitate heat generation and plastic flow. The plastic flow is thereby facilitated uniformly in the thickness direction, and a good welded state can be achieved. If the gap G between the shoulders 5 and 9 of the pair of rotating tools 1 and 8 exceeds t−(0.2×D×sin α), the shoulders 5 and 9 of the rotating tools 1 and 8 cannot press the top and bottom sides of the metal sheets 3 under a sufficient load, and the above effect cannot be obtained. If the gap G is less than (0.5×t)−(0.2×D×sin α), the top and bottom sides of the welded joint are concaved, and this adversely affect the welded joint strength. Therefore, the gap G satisfies (0.5×t)−(0.2×D×sin α)≤G≤t−(0.2×D×sin α).

(26) Next, the gap g (mm) between the tips of the pins of the top and bottom side rotating tools will be described.

(27) To obtain a temperature increase and shear stress uniformly in the thickness direction of the metal sheets 3 to thereby achieve an increase in welding speed while the occurrence of defects during welding is prevented, strictly controlling the gap g between the tips of the pins 6 and 10 of the opposed rotating tools 1 and 8 is effective. In particular, when the ratio (D/t) of the diameter D of the shoulders 5 and 9 of the rotating tools 1 and 8 to the thickness t (mm) of each of the metal sheets 3 (when they are butt welded) or the total thickness t (mm) of the lapped metal sheets (when they are lap welded) is small, the frictional heat generated at the shoulders of the top and bottom side rotating tools is less likely to be transferred in the thickness direction, and softening of the material by the heat from the shoulders does not proceed, so that plastic flow is unlikely to occur uniformly in the thickness direction. Since it is necessary to generate frictional heat and plastic flow necessary and sufficient to obtain a welded state from the pins, limiting the gap g between the tips of the pins 6 and 10 within the range of from [0.1-0.09×exp{−0.011×(D/t).sup.2}]×t to [1−0.9×exp{−0.011×(D/t).sup.2}]×t inclusive is effective. As can be seen from this formula, as D/t decreases, the upper and lower limits of the gap g are controlled at lower values. The gap g can be adjusted by changing the positions of the top and bottom side rotating tools or the length b of the pins of the rotating tools.

(28) A gap g between the tips of the pins 6 and 10 of less than [0.1−0.09×exp{−0.011×(D/t).sup.2}]×t is not preferable because the tips of the pins 6 and 10 of the opposed rotating tools 1 and 8 may come into contact with each other and break. If the gap g exceeds [1−0.9×exp{−0.011×(D/t).sup.2}]×t, the plastic flow and frictional heat are not effectively obtained uniformly in the thickness direction. Therefore, gap g is [0.1−0.09×exp{−0.011×(D/t).sup.2}]×t≤g [1−0.9×exp{−0.011×(D/t).sup.2}]×t.

(29) Next, the diameter D (mm) of the shoulders of the top and bottom side rotating tools will be described.

(30) Controlling the diameter D of the shoulders 5 and 9 of the opposed rotating tools 1 and 8 strictly in addition to the gaps G and g described above is effective in obtaining a temperature increase and shear stress uniformly in the thickness direction of the metal sheets 3 to thereby achieve an increase in welding speed while the occurrence of defects during welding is prevented. When the ratio of the diameter D to t is small, the frictional heat generated at the shoulders of the top and bottom side rotating tools is less likely to be transferred in the thickness direction, and softening of the material by the heat from the shoulders does not proceed, so that plastic flow is unlikely to occur uniformly in the thickness direction. Therefore, in particular, by limiting the diameter D within the range of from 4×t to 20×t inclusive using the thickness t (mm) of the metal sheets 3, the effect can be obtained.

(31) If the diameter D is less than 4×t, plastic flow uniform in the thickness direction cannot be effectively obtained. A diameter D exceeding 20×t is not preferable because the region in which the plastic flow occurs is unnecessarily broad and an excessive load is applied to the device. Therefore, the diameter D is 4×t≤D≤20×t. The thickness t is the thickness t of each of the metal sheets 3 when they are butt welded and is the total thickness t of the lapped metal sheets 3 when they are lap welded.

(32) Next, the ratio T/S of the welding speed T (m/min) of the top and bottom side rotating tools to the number of revolutions S of the rotating tools will be described.

(33) To obtain a temperature increase and shear stress uniformly in the thickness direction of the metal sheets 3 to thereby achieve an increase in the welding speed while the occurrence of defects during welding is prevented, controlling the ratio (T/S) of the welding speed T (m/min) of the opposed rotating tools 1 and 8 to the number of revolutions S (rpm) of the rotating tools strictly is effective.

(34) In double-sided friction stir welding, frictional heat per unit time Q.sub.time increases as the axial load F between the top and bottom side rotating tools, the diameter D of the shoulders, or the number of revolutions S increases. Therefore, the following relation may hold.
Q.sub.time(J/min)∝F×D×S

(35) By dividing the frictional heat per unit time by the welding speed T (m/min) and the thickness t (mm), the amount of heat can be standardized by the distances in the welding direction and the thickness direction.
Q.sub.J-t(J/mm.sup.2)=Q.sub.time/(T×t)∝F×D×S/(1000×T×t)

(36) As for the axial load F (kN), it is necessary to give consideration to the relation between the gap G between the shoulders of the top and bottom side rotating tools and the axial load F as shown in FIG. 4 and to the relation between the welding speed T and the number of revolutions S of the top and bottom side rotating tools as shown in FIG. 5.

(37) FIG. 5 shows the relation between the axial load F (kN) and the welding speed T×1000/the number of revolutions S (mm). In this case, steel sheets having the thickness, chemical composition, and tensile strength shown in No. 1 in Table 1 were used. The butt joint surface had a surface state equivalent to that obtained by milling, and were a so-called I-type groove with no beveling. Rotating tools having a cross-sectional shape shown in FIG. 3A and formed of tungsten carbide (WC) were disposed on the top and bottom sides and pressed against the steel sheets at a tilt angle α of 1.5° to perform friction stir welding with the gap G between the rotating tools set to 1.0 mm, the number of revolutions of the top and bottom side rotating tools set to 2,000 to 3,000 rpm, and the welding speed set to 4 to 5 m/min. As the welding speed T/the number of revolutions S increases, the axial load F tends to increase.

(38) As can be seen from the experimental tendencies shown in FIGS. 4 and 5, the axial load F is represented by the following formula using the welding speed T, the number of revolutions S of the top and bottom side rotating tools, and the sheet thickness t:
F=3.4×T×1000/S−32.2×G/t+34.5.
The Q.sub.J-t described above is thereby represented as follows.
Q.sub.J-t(J/mm.sup.2)∝F×D×S/(1000×T×t)
=(3.4×T×1000/S−32.2×G/t+34.5)×D×S/(1000×T×t)

(39) Friction stir welding was performed using steel sheets having the thickness, chemical composition, and tensile strength shown in No. 1 in Table 1. The butt joint surface had a surface state equivalent to that obtained by milling, and were a so-called I-type groove with no beveling. Rotating tools having a cross-sectional shape shown in FIG. 3A and formed of tungsten carbide (WC) were disposed on the top and bottom sides and pressed against the steel sheets at a tilt angle α of 1.5° to perform friction stir welding with the gap G between the shoulders of the rotating tools set to 0.8 to 1.5 mm, the number of revolutions of the top and bottom side rotating tools set to 400 to 3,000 rpm, and the welding speed set to 1 to 5 m/min. When the right hand side of the above formula that is proportional to Q.sub.J-t satisfies
(3.4×T×1000/S−32.2×G/t+34.5)×D×S/(1000×T×t)≥53,

(40) heat input is sufficient, and a sound joint with no defects is obtained.

(41) By modifying the above formula,
T/S≤( 1/1000)×(D/t)×{34.5−32.2×(G/t)}/{53−3.4×(D/t)}
is obtained. The ratio T/S of the welding speed T (m/min) to the number of revolutions S (rpm) of the rotating tools is represented using the ratio D/t of the diameter D (mm) of the shoulders of the top and bottom side rotating tools to the thickness t (mm) of each of the metal sheets 3 (when they are butted) or the total thickness t (mm) of the lapped metal sheets 3 (when they are lapped) and the ratio G/t of the gap G (mm) between the shoulders 5 and 9 of the rotating tools 1 and 8 to the thickness t (mm) of each of the metal sheets 3 (when they are butted) or the total thickness t (mm) of the lapped metal sheets 3 (when they are lapped).

(42) In particular, when the ratio D/t of the diameter D (mm) of the shoulders 5 and 9 of the rotating tools 1 and 8 to the thickness t (mm) of each of the metal sheets 3 (when they are butted) or the total thickness t (mm) of the lapped metal sheets 3 (when they are lapped) is small, i.e., when the frictional heat generated at the shoulders of the top and bottom side rotating tools is less likely to be transferred in the thickness direction and softening of the material by the heat from the shoulders does not proceed, plastic flow is less likely to occur uniformly in the thickness direction. Alternatively, when the ratio G/t of the gap G between the shoulders 5 and 9 of the rotating tools 1 and 8 to the thickness t (mm) of each of the metal sheets 3 (when they are butted) or the total thickness t (mm) of the lapped metal sheets 3 (when they are lapped) is large, i.e., when the axial load between the top and bottom side rotating tools is small relative to the thickness t and the frictional heat generated between the material and the rotating tools is small, compositional flow is less likely to occur uniformly in the thickness direction. Therefore, limiting the ratio T/S of the welding speed T of the opposed rotating tools 1 and 8 to the number of revolutions S to equal to or less than ( 1/1000)×(D/t)×{34.5−32.2×(G/t)}/{53−3.4×(D/t)} is effective. Note that the numbers of revolutions S of the opposed rotating tools 1 and 8 are the same.

(43) The pins of the top and bottom side rotating tools 1 and 8 may be tapered from the interfaces with the shoulders toward their forward end. The length b of the pins 6 and 10 may be appropriately determined according to the tilt angle α, the gap G, the gap g, the diameter D, and the thickness t. The diameter a (mm) of the tips of the pins 6 and 10 may be set as a matter of design change by one skilled in the art.

(44) Other welding conditions may be set as a matter of design choice by one skilled in the art. In this manner, the number of revolutions of the opposed rotating tools 1 and 8 can be set within the range of 100 to 5,000 rpm, and the welding speed can be increased to 1,000 mm/min or higher.

(45) The metal sheets 3 used in the disclosed embodiments may be preferably general structural steel sheets, carbon steel sheets, steel sheets corresponding to, for example, JIS G 3106 and JIS G 4051, etc. The disclosed embodiments are advantageously applicable to high-strength structural steel sheets with a tensile strength of 800 MPa or more. Even in this case, the welded joint can have a strength of 85% or more and even 90% or more of the tensile strength of the steel sheets.

Examples

(46) Steel sheets having the thicknesses, chemical compositions, tensile strengths shown in Table 1 were used to perform friction stir welding. When the steel sheets were butt welded, the butt joint surface had a surface state equivalent to that obtained by milling, and were a so-called I-type groove with no beveling. Rotating tools were pressed against the butt joint of the steel sheets from both the top and bottom sides to perform welding. When the steel sheets were lap welded, two steel sheets of the same type were lapped, and the rotating tools were pressed against the lap joint of the steel sheets from both the top and bottom sides to perform welding. As for the rotation directions of the top and bottom side rotating tools, the top side rotating tool (the rotating tool 1) was rotated clockwise in a plan view when the steel sheets (the metal sheets 3) were viewed from the top side as shown in FIG. 2A, and the bottom side rotating tool (the rotating tool 8) was rotated counterclockwise. The welding conditions for the friction stir welding are shown in Table 2. Two types of rotating tools formed of tungsten carbide (WC) and having cross sectional shapes shown in FIGS. 3A and 3B were used.

(47) TABLE-US-00001 TABLE 1 Sheet Tensile thickness Chemical composition (% by mass) strength No. (mm) C Si Mn P S (MPa) 1 1.6 0.3 0.21 0.69 0.012 0.003 1010 2 2.4 0.16 0.07 0.69 0.016 0.009 425 3 1.2 0.3 0.21 0.69 0.012 0.003 1012

(48) TABLE-US-00002 TABLE 2 Diameter D of Tilt angle α Thickness Bottom shoulders of top of top and Test of test Type Top side side and bottom side bottom side steel steel sheet of welding welding rotating tools rotating tools sheet (mm) joint tool tool D (mm) (°) Example 1 1 1.6 Butt 12ϕ-0.5 L 12ϕ-0.5 L 12 0.5 Example 2 1 1.6 Butt 12ϕ-0.5 L 12ϕ-0.5 L 12 1.5 Example 3 1 1.6 Butt 12ϕ-0.5 L 12ϕ-0.5 L 12 3.0 Example 4 1 1.6 Butt 12ϕ-0.5 L 12ϕ-0.5 L 12 1.5 Example 5 1 1.6 Butt 12ϕ-0.5 L 12ϕ-0.5 L 12 1.5 Example 6 1 1.6 Butt 12ϕ-0.5 L 12ϕ-0.5 L 12 1.5 Example 7 1 1.6 Butt 20ϕ-0.7 L 20ϕ-0.7 L 20 1.5 Example 8 2 2.4 Butt 12ϕ-0.5 L 12ϕ-0.5 L 12 1.5 Example 9 2 2.4 Butt 20ϕ-0.7 L 20ϕ-0.7 L 20 1.5 Example 10 2 2.4 Butt 20ϕ-0.7 L 20ϕ-0.7 L 20 1.5 Example 11 3 1.2 Lap 20ϕ-0.7 L 20ϕ-0.7 L 20 1.5 Example 12 3 1.2 Lap 20ϕ-0.7 L 20ϕ-0.7 L 20 1.5 Comparative Example 1 1 1.6 Butt 12ϕ-0.5 L 12ϕ-0.5 L 12 3.0 Comparative Example 2 1 1.6 Butt 12ϕ-0.5 L 12ϕ-0.5 L 12 4.0 Comparative Example 3 1 1.6 Butt 12ϕ-0.5 L 12ϕ-0.5 L 12 3.0 Comparative Example 4 1 1.6 Butt 12ϕ-0.5 L 12ϕ-0.5 L 12 1.5 Comparative Example 5 1 1.6 Butt 20ϕ-0.7 L 20ϕ-0.7 L 20 4.0 Comparative Example 6 2 2.4 Butt 12ϕ-0.5 L 12ϕ-0.5 L 12 1.5 Comparative Example 7 2 2.4 Butt 20ϕ-0.7 L 20ϕ-0.7 L 20 0.5 Comparative Example 8 2 2.4 Butt 20ϕ-0.7 L 20ϕ-0.7 L 20 4.0 Comparative Example 9 3 1.2 Lap 20ϕ-0.7 L 20ϕ-0.7 L 20 0.5 Comparative Example 10 3 1.2 Lap 20ϕ-0.7 L 20ϕ-0.7 L 20 4.0 Number of Gap G between Gap g between revolutions S of shoulders of top tips of pins of top rotating tools and bottom side and bottom side Top Bottom Welding rotating tools rotating tools side side speed T (mm) (mm) (rpm) (rpm) (m/min) T/S Example 1 1.20 0.27 2000 2000 4 0.0020 Example 2 1.10 0.31 1500 1500 4 0.0027 Example 3 0.90 0.32 1500 1500 4 0.0027 Example 4 1.00 0.17 2500 2500 5 0.0020 Example 5 1.40 0.61 3000 3000 3 0.0010 Example 6 0.90 0.11 2500 2500 5 0.0020 Example 7 1.30 0.25 600 600 3 0.0050 Example 8 1.50 0.71 3000 3000 2 0.0007 Example 9 2.20 1.15 2500 2500 2 0.0008 Example 10 1.80 0.75 2000 2000 2 0.0010 Example 11 2.20 1.15 2500 2500 2 0.0008 Example 12 1.80 0.75 2000 2000 2 0.0010 Comparative Example 1 1.50 0.92 3000 3000 4 0.0013 Comparative Example 2 1.30 0.86 2000 2000 4 0.0020 Comparative Example 3 0.65 0.07 1500 1500 4 0.0027 Comparative Example 4 1.10 0.31 1000 1000 4 0.0040 Comparative Example 5 1.40 0.93 600 600 3 0.0050 Comparative Example 6 1.80 1.01 3000 3000 2 0.0007 Comparative Example 7 1.10 0.24 2500 2500 2 0.0008 Comparative Example 8 1.20 1.32 2000 2000 2 0.0010 Comparative Example 9 1.10 0.24 2500 2500 2 0.0008 Comparative Example 10 1.20 1.32 2000 2000 2 0.0010

(49) Table 3 shows the presence or absence of surface defects in observation of the appearance of each weld joint, the presence and absence of internal defects in observation of a cross section of each joint, and the tensile strength of each weld joint obtained. The tensile strength was determined by cutting a tensile test piece with dimensions of No. 1 test specimen defined in JIS Z 3121 from the weld joint obtained and subjecting the test piece to a tensile test.

(50) TABLE-US-00003 TABLE 3 Surface defects Internal defects in Tensile in observation of observation of cross strength appearance of joint section of joint (MPa) Example 1 No No 1003 Example 2 No No 1005 Example 3 No No 1006 Example 4 No No 1003 Example 5 No No 998 Example 6 No No 1002 Example 7 No No 995 Example 8 No No 421 Example 9 No No 422 Example 10 No No 423 Example 11 No No 994 Example 12 No No 999 Comparative Yes Yes 552 Example 1 (unwelded portion) Comparative Yes (concaved) Yes 534 Example 2 Comparative Yes (concaved) No 772 Example 3 Comparative Yes Yes 631 Example 4 (unwelded portion) Comparative Yes Yes 589 Example 5 (unwelded portion) Comparative Good Yes 281 Example 6 Comparative Yes (concaved) No 275 Example 7 Comparative Yes (concaved) No 284 Example 8 Comparative Yes (concaved) No 687 Example 9 Comparative Yes (concaved) No 632 Example 10

(51) As shown in Table 3, in Examples 1 to 10 of the butt joint and Examples 11 and 12 of the lap joint, even when the welding speed was increased to 2 m/min or higher, no surface defects were found in the observation of the appearances of the joints, and no internal defects were found in the observation of the cross sections of the joints, so that a sound welded state was found to be obtained. The joint strength was 95% more of the tensile strength of the steel sheets used as base materials.

(52) In Comparative Examples 1 to 7 of the butt joint and Comparative Examples 8 to 10 of the lap joint, surface defects were found in the joint appearance observation, or internal defects were found in the joint cross section observation. Both were found in some cases. Therefore, a sound welded state was not obtained. Moreover, the joint strength was 70% or less of the tensile strength of the steel sheets used as base materials.