Resistance spot welding method
11298773 · 2022-04-12
Assignee
Inventors
- Koichi Taniguchi (Tokyo, JP)
- Chikaumi Sawanishi (Tokyo, JP)
- Katsutoshi Takashima (Tokyo, JP)
- Hiroshi Matsuda (Tokyo, JP)
- Rinsei Ikeda (Tokyo, JP)
Cpc classification
B23K11/24
PERFORMING OPERATIONS; TRANSPORTING
B23K11/115
PERFORMING OPERATIONS; TRANSPORTING
B23K11/166
PERFORMING OPERATIONS; TRANSPORTING
International classification
B23K11/16
PERFORMING OPERATIONS; TRANSPORTING
Abstract
Provided is a resistance spot welding method. The resistance spot welding method for joining a sheet set including a plurality of lapped steel sheets includes: holding the sheet set between a pair of electrodes; and energizing the sheet set under application of electrode force to thereby join the steel sheets together. At least one of the plurality of lapped steel sheets is a surface-treated steel sheet including a metal coating layer on a surface thereof. The energizing includes: a primary energizing step of performing energization to form a nugget portion; a non-energizing step in which, after the primary energizing step, the energization is suspended for an energization suspension time Tc (cycles); and a secondary energizing step of, after the non-energizing step, performing energization for reheating while the nugget portion is prevented from growing. During the energizing, the relations of a particular formula are satisfied.
Claims
1. A resistance spot welding method for joining a sheet set including a plurality of lapped steel sheets, the method comprising: holding the sheet set between a pair of electrodes; and energizing the sheet set under application of electrode force to thereby join the steel sheets together, wherein at least one of the plurality of lapped steel sheets is a surface-treated steel sheet including a metal coating layer on a surface thereof, wherein the energizing comprises a primary energizing step of performing energization to form a nugget portion, a non-energizing step in which, after the primary energizing step, the energization is suspended for an energization suspension time Tc (cycles), and a secondary energizing step of, after the non-energizing step, performing energization for reheating while the nugget portion is prevented from growing, and wherein, during the energizing, the relations of the following formula (I) are satisfied:
(22+A).Math.B/100<Ip/Im<C when 0<A<3,
(17+A).Math.B/80<Ip/Im<C when 3≤A<7, and
(11+A).Math.B/60<Ip/Im<C when 7≤A<15, formula (I) where A is an electrode misalignment angle (degrees) of the electrodes, Im is a current value (kA) in the primary energizing step, Ip is a current value (kA) in the secondary energizing step, B is a variable defined as 1+0.1.Math.Tc, and C is a variable defined as 1+0.2.Math.Tc.
2. The resistance spot welding method according to claim 1, wherein, in the non-energizing step, the relations of the following formula (II) are satisfied:
0<Tc<(103−A).Math.t/D when 0<A<3,
0<Tc<5.Math.(23−A).Math.t/D when 3≤A<7, and
0<Tc<8.Math.(17−A).Math.t/D when 7≤A<15, formula (II) where t is the total thickness (mm) of the plurality of lapped steel sheets, and D is the tip diameter (mm) of the electrodes.
3. The resistance spot welding method according to claim 1, wherein, after the primary energizing step, the non-energizing step and the secondary energizing step are repeated in this order at least twice.
4. The resistance spot welding method according to claim 1, wherein at least one of the plurality of lapped steel sheets has a tensile strength of 590 MPa or more.
5. The resistance spot welding method according to claim 2, wherein, after the primary energizing step, the non-energizing step and the secondary energizing step are repeated in this order at least twice.
6. The resistance spot welding method according to claim 2, wherein at least one of the plurality of lapped steel sheets has a tensile strength of 590 MPa or more.
7. The resistance spot welding method according to claim 3, wherein at least one of the plurality of lapped steel sheets has a tensile strength of 590 MPa or more.
8. The resistance spot welding method according to claim 5, wherein at least one of the plurality of lapped steel sheets has a tensile strength of 590 MPa or more.
Description
BRIEF DESCRIPTION OF DRAWINGS
(1)
(2)
DETAILED DESCRIPTION OF EMBODIMENTS OF THE INVENTION
(3) Embodiments of the present invention will next be described specifically.
(4) Aspects of the present invention include a resistance spot welding method for joining a sheet set including a plurality of lapped steel sheets, the method including: holding the sheet set between a pair of electrodes; and energizing the sheet set under application of electrode force to thereby join the steel sheets together. At least one of the plurality of lapped steel sheets is a surface-treated steel sheet including a metal coating layer on a surface thereof. The energizing includes: a primary energizing step of performing energization to form a nugget portion; a non-energizing step in which, after the primary energizing step, the energization is suspended for an energization suspension time Tc (cycles); and a secondary energizing step of, after the non-energizing step, performing energization for reheating while the nugget portion is prevented from growing. During the energizing, the relations of the following formula (I) are satisfied:
(22+A).Math.B/100<Ip/Im<C when 0<A<3,
(17+A).Math.B/80<Ip/Im<C when 3≤A<7, and
(11+A).Math.B/60<Ip/Im<C when 7≤A<15, formula (I)
where A is an electrode misalignment angle (degrees) of the electrodes, Im is a current value (kA) in the primary energizing step, Ip is a current value (kA) in the secondary energizing step, B is a variable defined as 1+0.1.Math.Tc, and C is a variable defined as 1+0.2.Math.Tc.
(5) Aspects of the present invention will be described specifically using
(6) Aspects of the present invention include the resistance spot welding method for joining a sheet set including a plurality of lapped steel sheets, the method including: holding the sheet set between a pair of electrodes; and energizing the sheet set under application of electrode force to thereby join the steel sheets together. First, as shown in
(7) In accordance with aspects of the present invention, at least one of the steel sheets to be subjected to resistance spot welding is a surface-treated steel sheet having a metal coating layer on its surface. Preferably, the melting point of the metal coating layer is lower than the melting point of a base metal of the surface-treated steel sheet. The melting point of a general metal coating layer is lower than the melting point of each steel sheet. For example, the melting point of the base metal (base steel sheet) is 1,400 to 1,570° C., and the melting point of the metal coating layer is 300 to 1,200° C. No particular limitation is imposed on the metal coating layer, and examples of the metal coating layer include Zn-based coating layers and Al-based coating layers. For components that require corrosion resistance, Zn-based coating layers are better than Al-based coating layers. This is because the sacrificial corrosion protection action of zinc (Zn) can reduce the corrosion rate of the base steel sheet. Examples of the Zn-based coating layers include general hot-dip galvanized coatings (GI), hot-dip galvannealed coatings (GA), electrogalvanized coatings (EG), Zn—Ni-based coatings (e.g., a Zn—Ni-based coating containing 10 to 25% by mass of Ni), Zn—Al-based coatings, Zn—Mg-based coatings, and Zn—Al—Mg-based coatings. Examples of the Al-based coating layers include Al—Si-based coatings (e.g., an Al—Si-based coating containing 10 to 20% by mass of Si). It is only necessary that the metal coating, layer be provided on one side of the surface-treated steel sheet, but the metal coating layer may be provided on both sides. The metal coating layer may be provided on the surface that serves as the joint surface (mating surface) between the steel sheets, may be provided on the surface to be in contact with an electrode, or may be provided on that serves as the joint surface (mating surface) between the steel sheets and on the surface to be in contact with an electrode. The coating weight of the metal coating layer is not limited. From the viewpoint of weldability, the coating weight per side is preferably 120 g/m.sup.2 or less. In accordance with aspects of the present invention, no particular limitation is imposed on the type (chemical composition) of steel sheet to be subjected to resistance spot welding. A method for producing the steel sheet is not limited, and cold rolling, hot rolling, etc. may be used. Moreover, the microstructure of each steel sheet is not limited. A hot-pressed steel sheet can be used without any problem. No particular limitation is imposed on the thickness of the steel sheet. Preferably, the thickness falls within a range (about 0.5 to about 4.0 mm) that can be used for general automobile bodies.
(8) Preferably, at least one of the steel sheets is a high-strength steel sheet having a tensile strength of 590 MPa or more and 780 MPa or more. When the tensile strength is high, cracking is likely to occur. By applying aspects of the present invention to a sheet set including at least one steel sheet having a tensile strength of 590 MPa or more, the effects according to aspects of the present invention are obtained significantly. In particular, when the sheet set includes at least one steel sheet having a tensile strength of 780 MPa or more, the effects obtained are higher.
(9) The plurality of lapped steel sheets may be of the same type or different types. A plurality of steel sheets of the same type may be lapped, or a plurality of steel sheets of different types may be lapped. Steel sheets having different thicknesses can be used without any problem. A surface-treated steel sheet having a metal coating layer and a steel sheet having no metal coating layer may be lapped. In the example shown in
(10) Next, the sheet set including the plurality of lapped steel sheets is held between a pair of welding electrodes (electrodes 3 and 4) and energized under application of electrode force, and then the electrodes are released from the steel sheets. The welding machine that can be used for the resistance spot welding method according to aspects of the present invention is any welding machine that includes a vertical pair of electrodes and can perform welding while the electrode force and the welding current are controlled freely. No particular limitation is imposed on the pressurizing mechanism (such as an air cylinder or a servo motor) of the welding machine, its type (e.g., a stationary or robot gun type), and the shape of the electrodes. Aspects of the present invention can be applied to both DC and AC welding machines, and no particular limitation is imposed on the type of power source (a single-phase AC type, an AC inverter type, or a DC inverter type). When AC is used, the “current” means the “effective current.” No particular limitation is imposed on the shape of the electrodes. Examples of the type of electrode tip include a DR type (dome radius type), an R type (radius type), and a D type (dome type) specified in JIS C9304: 1999. The tip diameter of the electrodes is, for example, 4 mm to 16 mm, and the radius of curvature of the tips of the electrodes is, for example, 10 mm to 100 mm. The resistance spot welding is performed while the electrodes are always water-cooled.
(11) As described above, the sheet set including the plurality of lapped steel sheets (the steel sheets 1 and 2) is held between the pair of welding electrodes (the electrodes 3 and 4) and energized under application of electrode force. A nugget is thereby formed by heat generated by resistance heating, and the lapped steel sheets are joined together, whereby a joint is obtained.
(12) In accordance with aspects of the present invention, a specific energizing pattern is used, which includes the primary energizing step, the non-energizing step performed after the primary energizing step, and the secondary energizing step performed after the non-energizing step. After completion of the secondary energizing step, the energization is stopped.
(13) The primary energizing step is a step for forming a nugget portion that solidifies to form a nugget 5. No particular limitation is imposed on the energizing and pressurizing conditions for forming the nugget portion, and conventionally used welding conditions can be used. The “nugget” is a fused and solidified portion in a weld during lap resistance welding, and the “nugget portion” is a fused portion that solidifies to form the nugget (i.e., the fused portion before solidification).
(14) The non-energizing step is performed subsequent to the primary energizing step and is a step in which the energization is suspended for the energization suspension time Tc (cycles). When the energization is suspended, the nugget portion is cooled. Here, one cycle is 20 ms (50 Hz).
(15) The secondary energizing step is performed subsequent to the non-energizing step and is a step in which the nugget portion is reheated while prevented from growing.
(16) The welding conditions in accordance with aspects of the present invention are set such that the relations of formula (I) above are satisfied. In formula (I), A is the electrode misalignment angle (degrees) of the electrodes, and Im is the current value (kA) in the primary energizing step. Ip is the current value (kA) in the secondary energizing step. B is a variable defined as 1+0.1.Math.Tc, and C is a variable defined as 1+0.2.Math.Tc. As described above, the electrode misalignment angle A is the inclination angle of the core axis of the electrode 3 with respect to the normal to the surface of the steel sheet 1 shown in
(17) As described above, when the electrode misalignment angle is nonzero, bending stress acts on the weld, and large compressive plastic deformation is generated locally. In this case, the tensile stress after release of the electrodes is very large, and this causes cracking to occur. One effective way to prevent the occurrence of cracking when the electrode misalignment angle is large is to facilitate alloying in the coating layer on the surface layer of the steel sheet to thereby reduce the amount of metals such as molten zinc.
(18) From the viewpoint of obtaining the weld, the electrode misalignment angle A is 15 degrees of less. This is because, if the electrode misalignment angle A exceeds 15 degrees, it is difficult to form the weld itself.
(19) Specifically, when the electrode misalignment angle A is in the range of more than 0 degrees and less than 3 degrees, the bending stress applied to the weld due to the electrode misalignment angle is relatively small, and therefore the tensile stress generated after the release of the electrodes is not so large. In this case, metals such as molten zinc in the coating layer on the surface of the steel sheet may be alloyed only to a limited extent.
(20) When the electrode misalignment angle A is in the range of 3 degrees or more and less than 7 degrees, the rate of increase (the amount of increase) in the tensile stress generated in the weld after the release of the electrodes becomes significant as the electrode misalignment angle increases. In this case, it is necessary to perform the secondary energizing step using a higher current in order to facilitate the alloying.
(21) When the electrode misalignment angle A is in the range of 7 degrees or more and less than 15 degrees, the tensile stress generated in the weld is very large. In this case, it is necessary to perform the secondary energizing step using a higher current in order to facilitate the alloying. By shortening the energization suspension time (cooling time) in the non-energizing step performed before the secondary energizing step, the alloying effect by secondary heating (reheating) can be obtained effectively, as described later.
(22) When the electrode misalignment angle A is 15 degrees or more, it is difficult to perform welding itself. Therefore, when the electrode misalignment angle A is 15 degrees or more in formula (I) above, it is preferable to revise the welding method.
(23) When an excessively high secondary energization current is used in the secondary energizing step, expulsion occurs, and this causes a reduction in joint strength. The heat generation in the secondary energization is determined by the diameter of the nugget formed in the primary energization, and the upper limit of the secondary energization current in the secondary energization can be determined in relation to the primary energization. When the energization suspending step is prolonged, the temperature of the joint decreases, and its specific resistance decreases accordingly. Therefore, the secondary energization current in the secondary energizing step is determined using its ratio to the current in the primary energization, and the upper limit of the secondary energization current is determined in relation to Tc.
(24) The relational expressions in formula (I) above have been obtained by comprehensive examination of above issues. As for the coefficients in the relational expressions, optimal coefficients were determined experimentally.
(25) In accordance with aspects of the present invention, when the energization is performed such that the relations in formula (I) above are satisfied, the occurrence of cracking in the weld can be prevented irrespective of the type of steel, and high joint strength can be obtained. From the viewpoint of obtaining stability of the mode of facture, it is preferable that formula (I) above satisfies the following relations. The stability of the mode of facture means whether plug fracture is stably obtained in a cross tension test.
(22+A).Math.B/80<Ip/Im<1+0.15.Math.Tc when 0<A<3
(17+A).Math.B/64<Ip/Im<1+0.15.Math.Tc when 3≤A<7
(11+A).Math.B/48<Ip/Im<1+0.15.Math.Tc when 7≤A<15
(26) In accordance with aspects of the present invention, it is preferable that the relations of the following formula (II) are satisfied in addition to the relations of formula (I) above. In formula (II), t is the total thickness (mm) of the plurality of lapped steel sheets (the sum of the thicknesses of the plurality of lapped steel sheets), and D is the tip diameter (mm) of the electrodes (the diameter of the tips of the electrodes). When formula (II) is satisfied, the occurrence of cracking can be prevented more effectively, and sufficient joint strength can be obtained.
0<Tc<(103−A).Math.t/D when 0<A<3,
0<Tc<5.Math.(23−A).Math.t/D when 3≤A<7,
0<Tc<8.Math.(17−A).Math.t/D when 7≤A<15. Formula (II)
(27) As described above, when the electrode misalignment angle A is in the range of more than 0 degrees and less than 3 degrees, the bending stress applied to the weld due to the electrode misalignment angle is relatively small, and therefore the tensile stress generated after the release of the electrodes is not so large. Therefore, metals such as molten zinc in the coating layer on the surface of the steel sheet may be alloyed only to a limited extent. In this case, even when the energization suspension time Tc (cycles) in the non-energizing step is increased, the effect of preventing cracking in the secondary energizing step can be obtained.
(28) When the electrode misalignment angle A is in the range of 3 degrees or more and less than 7 degrees, the rate of increase (the amount of increase) in the tensile stress generated in the weld after the release of the electrodes becomes significant as the electrode misalignment angle increases. Therefore, it is preferable to facilitate alloying by performing the secondary energizing step using a higher current and by shortening the energization suspension in the non-energizing step performed before the secondary energizing step such that the energization suspension is shorter than that when the electrode misalignment angle A is in the range of more than 0 degrees and less than 3 degrees. In this manner, the effects of alloying can be effectively obtained.
(29) When the electrode misalignment angle A is in the range of 7 degrees or more and less than 15 degrees, the tensile stress generated in the weld is very large. In this case, by reducing the energization suspension time in the non-energizing step performed before the secondary energizing step such that the energization suspension time is shorter than that when the electrode misalignment angle A is in the range of more than 0 degrees and less than 3 degrees, the effect of alloying by the secondary heating (reheating) can be obtained effectively.
(30) Moreover, when the energization suspension time (cooling time) Tc in the non-energizing step is long and the current value Ip in the secondary energizing step is smaller than a prescribed value, the nugget is rapidly cooled and hardened, and its toughness may be reduced. However, when formula (II) above is satisfied, the rapid cooling and hardening can be suppressed.
(31) When the total thickness t (mm) of the steel sheets to be welded is large or the tip diameter D (mm) of the electrodes is small, heat removal to the electrodes is not sufficient, and the cooling rate of the weld is reduced. In this case, it is preferable to use a long energization suspension time Tc (cycles) in the non-energizing step. The energization suspension time Tc is preferably 4 cycles (50 Hz) or longer.
(32) If the non-energizing step is excessively long, the weld is cooled excessively. In this case, since the specific resistance is reduced, and the effects of the secondary energizing step are not easily obtained. The excessively long non-energizing step may increase the takt time of welding. Therefore, the non-energizing step is preferably 20 cycles (50 Hz) or shorter.
(33) No particular limitation is imposed on the tip diameter D (mm) of the electrodes. The tip diameter is preferably, for example, 6 mm to 8 mm. If the tip diameter is less than 6 mm, the nugget obtained may be insufficient. If the tip diameter is more than 8 mm, the electrode may tend to wear during the production welding.
(34) As described above, in accordance with aspects of the present invention, the welding is performed such that formula (I) or formulas (I) and (II) are satisfied. Specifically, for example, the welding conditions are determined using the above formulas classified according to the angle A (degrees) of the electrodes, and the welding is performed using the determined welding conditions. In this manner, the occurrence of cracking can be easily prevented, and sufficient joint strength can be easily obtained.
(35) In accordance with aspects of the present invention, after the primary energizing step, the energization suspending step and the secondary energizing step may be repeated in this order at least twice. By repeating the energization suspending step and the secondary energizing step at least twice, the alloying on the surface of the steel sheets is facilitated, and the effect of preventing cracking can be further improved. The larger the number of repetitions, the more preferable. However, this cause an increase in production cost. From the viewpoint of working efficiency, the number of repetitions is preferably 1 to 9.
(36) In the present description, formulas (I) and (II) define only numerical relations.
(37) No particular limitation is imposed on the welding current value (the current value during energization) in accordance with aspects of the present invention. The welding current is, for example, 4 to 18 kA. It is operationally necessary to obtain a prescribed nugget diameter, and an excessively large current value may cause expulsion. Therefore, the current value Im (kA) in the primary energizing step is, for example, 4 to 11 kA, and the current value Ip (kA) in the secondary energizing step is, for example, 5 to 12 kA.
(38) Preferably, the electrode force is, for example, 2,000 N to 7,000 N (2 kN to 7 kN).
(39) No particular limitation is imposed on the time (weld time) from the start of the energization to the end of the energization. The weld time in the primary energizing step is preferably 8 cycles to 30 cycles (50 Hz), and the weld time in the secondary energizing step is preferably 3 cycles to 10 cycles (50 Hz).
(40) In accordance with aspects of the present invention, a controlling method in which parameters such as resistance and voltage values during welding are monitored to change the current value and the weld time according to the changes in the parameters may be used without any problems.
(41) With the resistance spot welding method according to aspects of the present invention, a weld joint composed of a plurality of welded steel sheets including at least one surface-treated steel sheet having a metal coating layer on its surface can be obtained. Specifically, a weld joint can be produced by a production method including: the step of lapping a plurality of steel sheets including at least one surface-treated steel sheet having a metal coating layer on its surface to thereby obtain a sheet set; and the step of welding the sheet set using the above-described resistance spot welding method. When the above-described resistance spot welding method is used for welding, the occurrence of cracking in the weld can be prevented, and sufficient joint strength can be obtained. Therefore, a weld joint in which the occurrence of cracking in the weld is reduced and which has high joint strength can be produced.
EXAMPLES
(42) To further facilitate the understanding of the present invention, aspects of the invention will be described by way of Examples. However, these Examples do not limit the present invention.
Inventive Examples and Comparative Examples
(43) Examples of the present invention will next be shown. In accordance with aspects of the present invention, two or more steel sheets may be lapped together to form a sheet set. In some Examples, two steel sheets 1 and 2 were lapped together and held between a pair of electrodes 3 and 4 as shown in
(44) The tensile strength TS and thickness of each of the steel sheets used and the type of coating are shown in Table 1. The welding conditions are shown in Tables 2-1, 2-2, and 2-3.
(45) The welding machine used is an inverter DC resistance spot welding machine, and the two electrodes 3 and 4 have the same shape. The electrodes 3 and 4 used are each a DR-type chromium-copper electrode having a radius of curvature of 40 mm and a tip diameter D (mm) shown in Tables 2-1, 2-2 and 2-3. The resistance spot welding was performed at room temperature (20° C.) while the electrodes were always water-cooled. The electrode force (kN) was held constant over the primary energizing step, the non-energizing step, and the secondary energizing step. The holding time after completion of the secondary energizing step was set to 5 ms for all the welding conditions.
(46) The melting points of the base metals of the steel sheets in the Examples and Comparative Examples are in the range of 1,400 to 1,570° C., and the melting points of galvanized coatings (GI) and galvannealed coatings (GA) are in the range of 400 to 500° C. and the range of 600 to 950° C., respectively. The tensile strength TS (MPa) of each steel sheet shown in Table 1 was determined as follows. A JIS No. 5 tensile test piece of the steel sheet that extends in a direction parallel to its rolling direction was prepared. Then the test piece was subjected to a tensile test according to JIS Z 2241:2011 to determine the tensile strength.
(47) For each of the weld joints obtained, (1) the presence of cracking in the weld and (2) the form of fracture in a cross tension test were evaluated. For some of the weld joints, (3) the stability of the fracture mode in the cross tension test was also evaluated.
(48) (1) Evaluation of Presence of Cracking in Weld
(49) For each of the weld joints obtained, the weld was cut, and a cross section was mirror-polished and observed under a scanning electron microscope (magnification: 2,000×) to check the presence of cracking in the surface layer of the steel sheet around the weld. When no cracking was found in the weld, an evaluation symbol O was assigned. When cracking was found, an evaluation symbol x was assigned.
(50) (2) Evaluation of Fracture Mode in Cross Tension Test
(51) Each of the weld joints obtained was subjected to a cross tension test according to JIS Z 3137, and the diameter of the fractured portion was measured using a vernier caliper. The cross section was cut and etched with picric acid, and the diameter of the fused portion was measured in the cross section. The fracture mode in this case is plug fracture, and the fracture propagates to the base metal. When the ratio of the diameter of the fractured portion to the diameter of the fused portion was 110% or more, an evaluation symbol ⊙ was assigned. When the ratio of the diameter of the fractured portion to the diameter of the fused portion was 100% or more and less than 110%, an evaluation symbol ◯ was assigned. When the ratio of the diameter of the fractured portion to the diameter of the fused portion was less than 100%, i.e., when partial plug fracture or interfacial fracture in the nugget occurred, an evaluation symbol x was assigned.
(52) (3) Evaluation of Stability of Fracture Mode in Cross Tension Test
(53) For each of the Examples in which the ratio of the diameter of the fractured portion to the diameter of the fused portion was 110% or more in the evaluation results in (2), the stability of the fracture mode during the CTS was evaluated. 10 samples were produced for each weld joint used for the evaluation under the conditions shown in Tables 1, 2-1, 2-2, and 2-3. For each of the weld joint samples obtained, the diameter of the fractured portion and the diameter of the fused portion were determined by the same method as that shown in (2) above. The results were rated according to the following criteria, and one of the following rating symbols was assigned. The rating symbols A and B represent excellent, and the rating symbol C represents good.
(54) A rating: In 10 out of the 10 samples, the ratio of the diameter of the fractured portion to the diameter of the fused portion is 115% or more.
(55) B rating: In 5 to 9 out of the 10 samples, the ratio of the diameter of the fractured portion to the diameter of the fused portion is 115% or more.
(56) C rating: In 1 to 4 out of the 10 samples, the ratio of the diameter of the fractured portion to the diameter of the fused portion is 115% or more.
(57) The results obtained are shown in Tables 2-1, 2-2, and 2-3.
(58) As can be seen from Tables 2-1, 2-2, and 2-3, in the Inventive Examples in which the welding conditions satisfying the invention were used, good ratings (the symbol ◯ or ⊙) were assigned. Specifically, the occurrence of cracking in the weld was prevented, and high joint strength was obtained.
(59) TABLE-US-00001 TABLE 1 Tensile Steel strength TS Thickness sheet No. (MPa) (mm) Type of coating a 1020 1.0 Hot-dip galvannealed coating (GA) b 1012 1.4 Hot-dip galvannealed coating (GA) c 1032 1.4 Hot-dip galvanized coating (GI) d 992 2.3 Hot-dip galvannealed coating (GA) e 1502 1.4 Hot-dip galvannealed coating (GA) f 1992 1.4 Hot-dip galvannealed coating (GA) g 1230 1.6 Hot-dip galvannealed coating (GA) h 781 2.0 Hot-dip galvannealed coating (GA) i 1344 2.0 Cold rolled steel sheet j 601 1.6 Hot-dip galvannealed coating (GA) k 1223 1.5 Electrogalvanized coating (EG) l 1241 1.8 Al-based coated steel sheet
(60) TABLE-US-00002 TABLE 2-1 Non- Number of energizing Secondary repetitions Tip Primary energizing step energizing of non- Total Electrode diameter step Energization step energizing sheet misalignment of Current suspension Current and Steel Steel Steel thickness angle electrode Electrode value Energizing time value Energizing secondary sheet sheet sheet t A D force Im time Tc Ip time energizing B value No. 1 2 3 (mm) (degrees) (mm) (kN) (kA) (cyc) (cyc) (kA) (cyc) steps Ip/Im (*5) Formula (I) applied 1 b b — 2.8 2 6 3.5 6.0 14 10 7.0 10 1 1.17 2.0 (22 + A) .Math. B/100 < Ip/Im < C 2 b b — 2.8 2 6 3.5 6.0 14 50 26.0 3 1 4.33 6.0 (22 + A) .Math. B/100 < Ip/Im < C 3 b b — 2.8 5 6 3.5 6.0 14 1 5.4 5 1 0.90 1.1 (17 + A) .Math. B/80 < Ip/Im < C 4 b b — 2.8 5 6 3.5 6.0 14 4 7.0 3 1 1.17 1.4 (17 + A) .Math. B/80 < Ip/Im < C 5 b b — 2.8 5 6 3.5 6.0 14 8 9.0 3 1 1.50 1.8 (17 + A) .Math. B/80 < Ip/Im < C 6 b b — 2.8 5 6 3.5 6.0 14 20 15.0 3 1 2.50 3.0 (17 + A) .Math. B/80 < Ip/Im < C 7 b b — 2.8 5 6 3.5 6.0 14 4 19.0 5 1 3.17 1.4 (17 + A) .Math. B/80 < Ip/Im < C 8 b b — 2.8 5 6 3.5 6.0 14 8 19.0 5 1 3.17 1.8 (17 + A) .Math. B/80 < Ip/Im < C 9 b b — 2.8 7 6 3.5 6.0 14 4 8.0 5 1 1.33 1.4 (11 + A) .Math. B/60 < Ip/Im < C 10 b b — 2.8 7 6 3.5 6.0 14 10 8.0 5 1 1.33 2.0 (11 + A) .Math. B/60 < Ip/Im < C 11 a a — 2.0 5 6 3.5 6.0 14 8 8.0 4 1 1.33 1.8 (17 + A) .Math. B/80 < Ip/Im < C 12 a a — 2.0 5 6 3.5 6.0 14 8 16.0 4 1 2.67 1.8 (17 + A) .Math. B/80 < Ip/Im < C 13 c c — 2.8 5 6 3.5 6.0 14 4 7.0 3 1 1.17 1.4 (17 + A) .Math. B/80 < Ip/Im < C 14 c c — 2.8 5 6 3.5 6.0 14 4 19.0 5 1 3.17 1.4 (17 + A) .Math. B/80 < Ip/Im < C 15 d d — 4.6 5 6 4.5 6.0 18 4 7.0 3 1 1.17 1.4 (17 + A) .Math. B/80 < Ip/Im < C 16 d d — 4.6 5 6 4.5 6.0 18 4 19.0 5 1 3.17 1.4 (17 + A) .Math. B/80 < Ip/Im < C 17 e e — 2.8 5 6 4.5 6.5 18 4 7.0 3 1 1.08 1.4 (17 + A) .Math. B/80 < Ip/Im < C 18 e e — 2.8 5 6 4.5 6.5 18 4 19.0 5 1 2.92 1.4 (17 + A) .Math. B/80 < Ip/Im < C 19 f f — 2.8 5 6 4.5 6.5 18 4 7.0 3 1 1.08 1.4 (17 + A) .Math. B/80 < Ip/Im < C 20 f f — 2.8 5 6 4.5 6.5 18 4 19.0 5 1 2.92 1.4 (17 + A) .Math. B/80 < Ip/Im < C 21 a a — 2.0 5 6 3.5 6.0 14 8 8.0 4 3 1.33 1.8 (17 + A) .Math. B/80 < Ip/Im < C 22 a a — 2.0 5 6 3.5 6.0 14 8 8.0 4 5 1.33 1.8 (17 + A) .Math. B/80 < Ip/Im < C 23 a a — 2.0 5 6 3.5 6.0 14 8 8.0 4 9 1.33 1.8 (17 + A) .Math. B/80 < Ip/Im < C 24 d d — 4.6 5 6 4.5 6.0 18 4 7.0 3 5 1.17 1.4 (17 + A) .Math. B/80 < Ip/Im < C 25 d d — 4.6 5 6 4.5 6.0 18 4 7.0 3 9 1.17 1.4 (17 + A) .Math. B/80 < Ip/Im < C Upper Preferred Preferred limit of lower upper Right- Fracture Lower Ip/Im in limit of limit of hand mode limit of formula Ip/Im in Ip/Im in side of Preferred during Stability Ip/Im in (I) formula formula formula range of Presence cross of formula applied (I) (I) (II) Formula formula Formula of tension fracture (I) (C value) applied applied applied (I) (I) (II) cracking test mode applied (*5) (*6) (*6) Formula (II) applied (cyc) (*1) (*1) (*1) (*2) (*3) (*4) Remarks 1 0.48 3 0.6 2.5 0 < Tc < (103 − A) .Math. t/D 47.1 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 2 1.44 11 1.8 8.5 0 < Tc < (103 − A) .Math. t/D 47.1 ◯ ◯ X ◯ ◯ — Inventive Example 3 0.3025 1.2 0.3781 1.15 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.0 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 4 0.385 1.8 0.4813 1.6 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.0 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 5 0.495 2.6 0.6188 2.2 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.0 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 6 0.825 5 1.0313 4 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.0 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 7 0.385 1.8 0.4813 1.6 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.0 X X ◯ X X — Comparative Example 8 0.495 2.6 0.6188 2.2 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.0 X X ◯ X X — Comparative Example 9 0.42 1.8 0.525 1.6 0 < Tc < 8 .Math. (17 − A) .Math. t/D 37.3 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 10 0.6 3 0.75 2.5 0 < Tc < 8 .Math. (17 − A) .Math. t/D 37.3 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 11 0.495 2.6 0.6188 2.2 0 < Tc < 5 .Math. (23 − A) .Math. t/D 30.0 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 12 0.495 2.6 0.6188 2.2 0 < Tc < 5 .Math. (23 − A) .Math. t/D 30.0 X X ◯ X X — Comparative Example 13 0.385 1.8 0.4813 1.6 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.0 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 14 0.385 1.8 0.4813 1.6 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.0 X X ◯ X X — Comparative Example 15 0.385 1.8 0.4813 1.6 0 < Tc < 5 .Math. (23 − A) .Math. t/D 69.0 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 16 0.385 1.8 0.4813 1.6 0 < Tc < 5 .Math. (23 − A) .Math. t/D 69.0 X X ◯ X X — Comparative Example 17 0.385 1.8 0.4813 1.6 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.0 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 18 0.385 1.8 0.4813 1.6 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.0 X X ◯ X X — Comparative Example 19 0.385 1.8 0.4813 1.6 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.0 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 20 0.385 1.8 0.4813 1.6 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.0 X X ◯ X X — Comparative Example 21 0.495 2.6 0.6188 2.2 0 < Tc < 5 .Math. (23 − A) .Math. t/D 30.0 ◯ ◯ ◯ ◯ ⊚ A Inventive Example 22 0.495 2.6 0.6188 2.2 0 < Tc < 5 .Math. (23 − A) .Math. t/D 30.0 ◯ ◯ ◯ ◯ ⊚ A Inventive Example 23 0.495 2.6 0.6188 2.2 0 < Tc < 5 .Math. (23 − A) .Math. t/D 30.0 ◯ ◯ ◯ ◯ ⊚ A Inventive Example 24 0.385 1.8 0.4813 1.6 0 < Tc < 5 .Math. (23 − A) .Math. t/D 69.0 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 25 0.385 1.8 0.4813 1.6 0 < Tc < 5 .Math. (23 − A) .Math. t/D 69.0 ◯ ◯ ◯ ◯ ⊚ A Inventive Example (*1) ◯: Satisfying the formula. X: Not satisfying the formula. (*2) ◯: No cracking is found in weld. X: Cracking is found in weld. (*3) ⊚: Diameter of fractured portion is 110% or more of diameter of fused portion. ◯: Diameter of fractured portion is 100% or more and less than 110% of diameter of fused portion. X: Diameter of fractured portion is less than 100% of diameter of fused portion, or interfacial fracture. (*4) A: In 10 out of 10 samples, ratio of diameter of fractured portion to diameter of fused portion is 115% or more. B: In 5 to 9 out of 10 samples, ratio of diameter of fractured portion to diameter of fused portion is 115% or more. C: In 1 to 4 out of 10 samples, ratio of diameter of fractured portion to diameter of fused portion is 115% or more. (*5) B value: B = 1 + 0.1 .Math. Tc C value: C = 1 + 0.2 .Math. Tc (*6) Preferred lower limit of Ip/Im: when 0 < A < 3, (22 + A) .Math. B/80; when 3 ≤ A < 7, (17 + A) .Math. B/64; and when 7 ≤ A < 15, (11 + A) .Math. B/48. Preferred upper limit of Ip/Im: 1 + 0.15 .Math. Tc when 0 < A < 3, 3 ≤ A < 7, and 7 ≤ A < 15.
(61) TABLE-US-00003 TABLE 2-2 Non- Number of energizing repetitions Electrode Tip Primary energizing step Secondary of non- Total misalign- diameter step Energization energizing step energizing sheet ment of Current suspension Current and Steel Steel Steel thickness angle electrode Electrode value Energizing time value Energizing secondary B sheet sheet sheet t A D force Im time Tc Ip time energizing value No. 1 2 3 (mm) (degrees) (mm) (kN) (kA) (cyc) (cyc) (kA) (cyc) steps Ip/Im (*5) Formula (I) applied 26 b b — 2.8 5 6 3.5 6.0 14 1 6.6 3 1 1.10 1.1 (17 + A) .Math. B/80 < Ip/Im < C 27 b b — 2.8 5 6 3.5 6.0 14 4 8.0 3 2 1.33 1.4 (17 + A) .Math. B/80 < Ip/Im < C 28 b b — 2.8 5 6 3.5 6.0 14 4 8.0 3 3 1.33 1.4 (17 + A) .Math. B/80 < Ip/Im < C 29 b b — 2.8 5 6 3.5 6.0 14 4 8.0 3 5 1.33 1.4 (17 + A) .Math. B/80 < Ip/Im < C 30 b b — 2.8 5 6 3.5 6.0 14 4 8.0 3 9 1.33 1.4 (17 + A) .Math. B/80 < Ip/Im < C 31 b b — 2.8 5 6 3.5 6.0 14 4 9.5 3 1 1.58 1.4 (17 + A) .Math. B/80 < Ip/Im < C 32 b b — 2.8 5 6 3.5 6.0 14 4 9.9 3 1 1.65 1.4 (17 + A) .Math. B/80 < Ip/Im < C 33 b b — 2.8 5 6 3.5 6.0 14 0 5.9 3 1 0.98 1.0 (17 + A) .Math. B/80 < Ip/Im < C 34 b b — 2.8 5 6 3.5 6.0 14 4 10.8 3 1 1.80 1.4 (17 + A) .Math. B/80 < Ip/Im < C 35 b b — 2.8 5 6 3.5 6.0 14 4 2.2 3 1 0.37 1.4 (17 + A) .Math. B/80 < Ip/Im < C 36 b b — 2.8 5 6 3.5 6.0 14 — — — — — — (17 + A) .Math. B/80 < Ip/Im < C 37 b b — 2.8 5 6 3.5 6.0 14 0 9.5 3 1 1.58 1.0 (17 + A) .Math. B/80 < Ip/Im < C 38 f f — 2.8 5 6 4.5 6.5 18 4 8.0 3 1 1.23 1.4 (17 + A) .Math. B/80 < Ip/Im < C 39 f f — 2.8 5 6 4.5 6.5 18 4 8.0 3 2 1.23 1.4 (17 + A) .Math. B/80 < Ip/Im < C 40 f f — 2.8 5 6 4.5 6.5 18 — — — — — — (17 + A) .Math. B/80 < Ip/Im < C 41 f f — 2.8 5 6 4.5 6.5 18 — — — — — — (17 + A) .Math. B/80 < Ip/Im < C 42 b b — 2.8 0.2 5 3 5.4 14 4 7.2 3 1 1.33 1.4 (22 + A) .Math. B/100 < Ip/Im < C 43 b b — 2.8 0.2 5 3 5.4 14 4 8.5 3 1 1.57 1.4 (22 + A) .Math. B/100 < Ip/Im < C 44 b b — 2.8 0.2 5 3 5.4 14 4 9.0 3 1 1.67 1.4 (22 + A) .Math. B/100 < Ip/Im < C 45 b b — 2.8 0.2 5 3 5.4 14 4 7.2 3 2 1.33 1.4 (22 + A) .Math. B/100 < Ip/Im < C 46 g g — 3.2 3 8 6 4.7 14 6 5.0 3 1 1.06 1.6 (17 + A) .Math. B/80 < Ip/Im < C 47 g g — 3.2 3 8 6 4.7 14 6 8.7 3 1 1.85 1.6 (17 + A) .Math. B/80 < Ip/Im < C 48 g g — 3.2 3 8 6 4.7 14 6 9.2 3 1 1.96 1.6 (17 + A) .Math. B/80 < Ip/Im < C 49 g g — 3.2 3 8 6 4.7 14 6 5.0 3 2 1.06 1.6 (17 + A) .Math. B/80 < Ip/Im < C 50 g g — 3.2 3 8 6 4.7 14 6 11.0 3 1 2.34 1.6 (17 + A) .Math. B/80 < Ip/Im < C 51 g g — 3.2 3 8 6 4.7 14 6 2.5 10 1 0.53 1.6 (17 + A) .Math. B/80 < Ip/Im < C 52 g g — 3.2 3 8 6 4.7 14 6 2.3 10 1 0.49 1.6 (17 + A) .Math. B/80 < Ip/Im < C 53 g g — 3.2 3 8 6 4.7 14 6 1.8 10 1 0.38 1.6 (17 + A) .Math. B/80 < Ip/Im < C 54 h h — 4.0 8 6 7 7.0 24 5 7.2 3 1 1.03 1.5 (11 + A) .Math. B/60 < Ip/Im < C 55 h h — 4.0 8 6 7 7.0 24 5 7.2 3 3 1.03 1.5 (11 + A) .Math. B/60 < Ip/Im < C 56 h h — 4.0 8 6 7 7.0 24 5 7.2 3 5 1.03 1.5 (11 + A) .Math. B/60 < Ip/Im < C 57 h h — 4.0 8 6 7 7.0 24 5 7.2 3 9 1.03 1.5 (11 + A) .Math. B/60 < Ip/Im < C 58 h h — 4.0 8 6 7 7.0 24 5 9.0 3 1 1.29 1.5 (11 + A) .Math. B/60 < Ip/Im < C 59 h h — 4.0 8 6 7 7.0 24 5 9.0 3 2 1.29 1.5 (11 + A) .Math. B/60 < Ip/Im < C 60 h h — 4.0 8 6 7 7.0 24 5 12.0 3 1 1.71 1.5 (11 + A) .Math. B/60 < Ip/Im < C Upper Preferred Preferred limit of lower upper Right- Fracture Lower Ip/Im in limit of limit of hand mode limit of formula Ip/Im in Ip/Im in side of Preferred during Stability Ip/Im in (I) formula formula formula range of Presence cross of formula applied (I) (I) (II) Formula formula Formula of tension fracture (I) (C value) applied applied applied (I) (I) (II) cracking test mode No. applied (*5) (*6) (*6) Formula (II) applied (cyc) (*1) (*1) (*1) (*2) (*3) (*4) Remarks 26 0.3025 1.2 0.3781 1.15 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.0 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 27 0.385 1.8 0.4813 1.6 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.0 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 28 0.385 1.8 0.4813 1.6 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.0 ◯ ◯ ◯ ◯ ⊚ A Inventive Example 29 0.385 1.8 0.4813 1.6 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.0 ◯ ◯ ◯ ◯ ⊚ A Inventive Example 30 0.385 1.8 0.4813 1.6 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.0 ◯ ◯ ◯ ◯ ⊚ A Inventive Example 31 0.385 1.8 0.4813 1.6 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.0 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 32 0.385 1.8 0.4813 1.6 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.0 ◯ X ◯ ◯ ⊚ C Inventive Example 33 0.275 1 0.3438 1 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.0 ◯ ◯ X ◯ ◯ — Inventive Example 34 0.385 1.8 0.4813 1.6 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.0 X X ◯ X X — Comparative Example 35 0.385 1.8 0.4813 1.6 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.0 X X ◯ ◯ X — Comparative Example 36 N/A N/A N/A N/A 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.0 X X X X X — Comparative Example 37 0.275 1 0.3438 1 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.0 X X X X X — Comparative Example 38 0.385 1.8 0.4813 1.6 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.0 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 39 0.385 1.8 0.4813 1.6 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.0 ◯ ◯ ◯ ◯ ⊚ A Inventive Example 40 N/A N/A N/A N/A 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.0 X X X X X — Comparative Example 41 N/A N/A N/A N/A 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.0 X X X X X — Comparative Example 42 0.3108 1.8 0.3885 1.6 0 < Tc < (103 − A) .Math. t/D 57.6 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 43 0.3108 1.8 0.3885 1.6 0 < Tc < (103 − A) .Math. t/D 57.6 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 44 0.3108 1.8 0.3885 1.6 0 < Tc < (103 − A) .Math. t/D 57.6 ◯ X ◯ ◯ ⊚ C Inventive Example 45 0.3108 1.8 0.3885 1.6 0 < Tc < (103 − A) .Math. t/D 57.6 ◯ ◯ ◯ ◯ ⊚ A Inventive Example 46 0.4 2.2 0.5 1.9 0 < Tc < 5 .Math. (23 − A) .Math. t/D 40.0 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 47 0.4 2.2 0.5 1.9 0 < Tc < 5 .Math. (23 − A) .Math. t/D 40.0 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 48 0.4 2.2 0.5 1.9 0 < Tc < 5 .Math. (23 − A) .Math. t/D 40.0 ◯ X ◯ ◯ ⊚ C Inventive Example 49 0.4 2.2 0.5 1.9 0 < Tc < 5 .Math. (23 − A) .Math. t/D 40.0 ◯ ◯ ◯ ◯ ⊚ A Inventive Example 50 0.4 2.2 0.5 1.9 0 < Tc < 5 .Math. (23 − A) .Math. t/D 40.0 X X ◯ X X — Comparative Example 51 0.4 2.2 0.5 1.9 0 < Tc < 5 .Math. (23 − A) .Math. t/D 40.0 ◯ ◯ ◯ ◯ ⊚ C Inventive Example 52 0.4 2.2 0.5 1.9 0 < Tc < 5 .Math. (23 − A) .Math. t/D 40.0 ◯ X ◯ ◯ ◯ — Inventive Example 53 0.4 2.2 0.5 1.9 0 < Tc < 5 .Math. (23 − A) .Math. t/D 40.0 X X ◯ ◯ X — Comparative Example 54 0.475 2 0.5938 1.75 0 < Tc < 8 .Math. (17 − A) .Math. t/D 48.0 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 55 0.475 2 0.5938 1.75 0 < Tc < 8 .Math. (17 − A) .Math. t/D 48.0 ◯ ◯ ◯ ◯ ⊚ A Inventive Example 56 0.475 2 0.5938 1.75 0 < Tc < 8 .Math. (17 − A) .Math. t/D 48.0 ◯ ◯ ◯ ◯ ⊚ A Inventive Example 57 0.475 2 0.5938 1.75 0 < Tc < 8 .Math. (17 − A) .Math. t/D 48.0 ◯ ◯ ◯ ◯ ⊚ A Inventive Example 58 0.475 2 0.5938 1.75 0 < Tc < 8 .Math. (17 − A) .Math. t/D 48.0 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 59 0.475 2 0.5938 1.75 0 < Tc < 8 .Math. (17 − A) .Math. t/D 48.0 ◯ ◯ ◯ ◯ ⊚ A Inventive Example 60 0.475 2 0.5938 1.75 0 < Tc < 8 .Math. (17 − A) .Math. t/D 48.0 ◯ ◯ ◯ ◯ ⊚ B Inventive Example (*1) ◯: Satisfying the formula. X: Not satisfying the formula. (*2) ◯: No cracking is found in weld. X: Cracking is found in weld. (*3) ⊚: Diameter of fractured portion is 110% or more of diameter of fused portion. ◯: Diameter of fractured portion is 100% or more and less than 110% of diameter of fused portion. X: Diameter of fractured portion is less than 100% of diameter of fused portion, or interfacial fracture. (*4) A: In 10 out of 10 samples, ratio of diameter of fractured portion to diameter of fused portion is 115% or more. B: In 5 to 9 out of 10 samples, ratio of diameter of fractured portion to diameter of fused portion is 115% or more. C: In 1 to 4 out of 10 samples, ratio of diameter of fractured portion to diameter of fused portion is 115% or more. (*5) B value: B = 1 + 0.1 .Math. Tc C value: C = 1 + 0.2 .Math. Tc (*6) Preferred lower limit of Ip/Im: when 0 < A < 3, (22 + A) .Math. B/80; when 3 ≤ A < 7, (17 + A) .Math. B/64; and when 7 ≤ A < 15, (11 + A) .Math. B/48. Preferred upper limit of Ip/Im: 1 + 0.15 .Math. Tc when 0 < A < 3, 3 ≤ A < 7, and 7 ≤ A < 15.
(62) TABLE-US-00004 TABLE 2-3 Non- Number of energizing repetitions Electrode Tip Primary energizing step Secondary of non- Total misalign- diameter step Energization energizing step energizing sheet ment of Current suspension Current and Steel Steel Steel thickness angle electrode Electrode value Energizing time value Energizing secondary B sheet sheet sheet t A D force Im time Tc Ip time energizing value No. 1 2 3 (mm) (degrees) (mm) (kN) (kA) (cyc) (cyc) (kA) (cyc) steps Ip/Im (*5) Formula (I) applied 61 h h — 4.0 8 6 7 7.0 24 5 12.5 3 1 1.79 1.5 (11 + A) .Math. B/60 < Ip/Im < C 62 h h — 4.0 8 6 7 7.0 24 5 14.2 3 1 2.03 1.5 (11 + A) .Math. B/60 < Ip/Im < C 63 h h — 4.0 8 6 7 7.0 24 5 4.0 10 1 0.57 1.5 (11 + A) .Math. B/60 < Ip/Im < C 64 h h — 4.0 8 6 7 7.0 24 5 3.4 10 1 0.49 1.5 (11 + A) .Math. B/60 < Ip/Im < C 65 h h — 4.0 8 6 7 7.0 24 5 2.0 10 1 0.29 1.5 (11 + A) .Math. B/60 < Ip/Im < C 66 h h i 6.0 5 6 5.5 6.0 30 8 8.0 3 1 1.33 1.8 (17 + A) .Math. B/80 < Ip/Im < C 67 h h i 6.0 5 6 5.5 6.0 30 8 8.0 3 2 1.33 1.8 (17 + A) .Math. B/80 < Ip/Im < C 68 h h i 6.0 5 6 5.5 6.0 30 — — — 1 — — (17 + A) .Math. B/80 < Ip/Im < C 69 b b b 4.2 14 6 6.3 6.0 40 4 6.5 3 1 1.08 1.4 (11 + A) .Math. B/60 < Ip/Im < C 70 b b b 4.2 14 6 6.3 6.0 40 6 8.0 3 1 1.33 1.6 (11 + A) .Math. B/60 < Ip/Im < C 71 b b b 4.2 14 6 6.3 6.0 40 6 8.0 3 2 1.33 1.6 (11 + A) .Math. B/60 < Ip/Im < C 72 b b b 4.2 14 6 6.3 6.0 40 — — — 1 — — (11 + A) .Math. B/60 < Ip/Im < C 73 i i — 3.2 10 6 6 7.0 14 6 10.5 3 2 1.50 1.6 (11 + A) .Math. B/60 < Ip/Im < C 74 i i — 3.2 10 6 6 7.0 14 6 4.0 3 2 0.57 1.6 (11 + A) .Math. B/60 < Ip/Im < C 75 i i — 3.2 10 6 6 7.0 14 6 16 3 2 2.29 1.6 (11 + A) .Math. B/60 < Ip/Im < C 76 k k — 3.0 6 6 6 5.3 14 4 6.5 3 1 1.23 1.4 (17 + A) .Math. B/80 < Ip/Im < C 77 k k — 3.0 6 6 6 5.3 14 4 6.5 3 3 1.23 1.4 (17 + A) .Math. B/80 < Ip/Im < C 78 k k — 3.0 6 6 6 5.3 14 4 6.5 3 5 1.23 1.4 (17 + A) .Math. B/80 < Ip/Im < C 79 k k — 3.0 6 6 6 5.3 14 4 6.5 3 9 1.23 1.4 (17 + A) .Math. B/80 < Ip/Im < C 80 k k — 3.0 6 6 6 5.3 14 4 2.0 3 1 0.38 1.4 (17 + A) .Math. B/80 < Ip/Im < C 81 k k — 3.0 6 6 6 5.3 14 4 12.5 3 1 2.36 1.4 (17 + A) .Math. B/80 < Ip/Im < C 82 l l — 3.6 9 6 6 6.2 30 4 7.4 3 1 1.19 1.4 (11 + A) .Math. B/60 < Ip/Im < C 83 l l — 3.6 9 6 6 6.2 30 4 7.4 3 3 1.19 1.4 (11 + A) .Math. B/60 < Ip/Im < C 84 l l — 3.6 9 6 6 6.2 30 4 7.4 3 5 1.19 1.4 (11 + A) .Math. B/60 < Ip/Im < C 85 l l — 3.6 9 6 6 6.2 30 4 7.4 3 9 1.19 1.4 (11 + A) .Math. B/60 < Ip/Im < C 86 l l — 3.6 9 6 6 6.2 30 4 2.0 3 1 0.32 1.4 (11 + A) .Math. B/60 < Ip/Im < C 87 l l — 3.6 9 6 6 6.2 30 4 12.5 3 1 2.02 1.4 (11 + A) .Math. B/60 < Ip/Im < C 88 b c — 2.8 7 6 4 5.6 18 5 6 3 1 1.07 1.5 (11 + A) .Math. B/60 < Ip/Im < C 89 b c — 2.8 7 6 4 5.6 18 5 8 3 1 1.43 1.5 (11 + A) .Math. B/60 < Ip/Im < C 90 b c — 2.8 7 6 4 5.6 18 5 8.0 3 3 1.43 1.5 (11 + A) .Math. B/60 < Ip/Im < C 91 b c — 2.8 7 6 4 5.6 18 5 8.0 3 5 1.43 1.5 (11 + A) .Math. B/60 < Ip/Im < C 92 b c — 2.8 7 6 4 5.6 18 5 10 3 1 1.79 1.5 (11 + A) .Math. B/60 < Ip/Im < C 93 b c — 2.8 7 6 4 5.6 18 5 12.0 3 1 2.14 1.5 (11 + A) .Math. B/60 < Ip/Im < C 94 b c — 2.8 7 6 4 5.6 18 — — — — — — (11 + A) .Math. B/60 < Ip/Im < C Upper Preferred Preferred limit of lower upper Right- Fracture Lower Ip/Im in limit of limit of hand mode limit of formula Ip/Im in Ip/Im in side of Preferred during Stability Ip/Im in (I) formula formula formula range of Presence cross of formula applied (I) (I) (II) Formula formula Formula of tension fracture (I) (C value) applied applied applied (I) (I) (II) cracking test mode No. applied (*5) (*6) (*6) Formula (II) applied (cyc) (*1) (*1) (*1) (*2) (*3) (*4) Remarks 61 0.475 2 0.5938 1.75 0 < Tc < 8 .Math. (17 − A) .Math. t/D 48.0 ◯ X ◯ ◯ ⊚ C Inventive Example 62 0.475 2 0.5938 1.75 0 < Tc < 8 .Math. (17 − A) .Math. t/D 48.0 X X ◯ X X — Comparative Example 63 0.475 2 0.5938 1.75 0 < Tc < 8 .Math. (17 − A) .Math. t/D 48.0 ◯ X ◯ ◯ ⊚ C Inventive Example 64 0.475 2 0.5938 1.75 0 < Tc < 8 .Math. (17 − A) .Math. t/D 48.0 ◯ X ◯ ◯ ◯ — Inventive Example 65 0.475 2 0.5938 1.75 0 < Tc < 8 .Math. (17 − A) .Math. t/D 48.0 X X ◯ ◯ X — Comparative Example 66 0.495 2.6 0.6188 2.2 0 < Tc < 5 .Math. (23 − A) .Math. t/D 90.0 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 67 0.495 2.6 0.6188 2.2 0 < Tc < 5 .Math. (23 − A) .Math. t/D 90.0 ◯ ◯ ◯ ◯ ⊚ A Inventive Example 68 N/A N/A N/A N/A 0 < Tc < 5 .Math. (23 − A) .Math. t/D 90.0 X X X X X — Comparative Example 69 0.5833 1.8 0.7292 1.6 0 < Tc < 8 .Math. (17 − A) .Math. t/D 16.8 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 70 0.6667 2.2 0.8333 1.9 0 < Tc < 8 .Math. (17 − A) .Math. t/D 16.8 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 71 0.6667 2.2 0.8333 1.9 0 < Tc < 8 .Math. (17 − A) .Math. t/D 16.8 ◯ ◯ ◯ ◯ ⊚ A Inventive Example 72 N/A N/A N/A N/A 0 < Tc < 8 .Math. (17 − A) .Math. t/D 16.8 X X X X X — Comparative Example 73 0.56 2.2 0.7 1.9 0 < Tc < 8 .Math. (17 − A) .Math. t/D 29.9 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 74 0.56 2.2 0.7 1.9 0 < Tc < 8 .Math. (17 − A) .Math. t/D 29.9 ◯ X ◯ ◯ ◯ — Inventive Example 75 0.56 2.2 0.7 1.9 0 < Tc < 8 .Math. (17 − A) .Math. t/D 29.9 X X ◯ X ◯ — Comparative Example 76 0.4025 1.8 0.5031 1.6 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.5 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 77 0.4025 1.8 0.5031 1.6 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.5 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 78 0.4025 1.8 0.5031 1.6 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.5 ◯ ◯ ◯ ◯ ⊚ A Inventive Example 79 0.4025 1.8 0.5031 1.6 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.5 ◯ ◯ ◯ ◯ ⊚ A Inventive Example 80 0.4025 1.8 0.5031 1.6 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.5 X X ◯ ◯ X — Comparative Example 81 0.4025 1.8 0.5031 1.6 0 < Tc < 5 .Math. (23 − A) .Math. t/D 42.5 X X ◯ X ◯ — Comparative Example 82 0.4667 1.8 0.5833 1.6 0 < Tc < 8 .Math. (17 − A) .Math. t/D 38.4 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 83 0.4667 1.8 0.5833 1.6 0 < Tc < 8 .Math. (17 − A) .Math. t/D 38.4 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 84 0.4667 1.8 0.5833 1.6 0 < Tc < 8 .Math. (17 − A) .Math. t/D 38.4 ◯ ◯ ◯ ◯ ⊚ A Inventive Example 85 0.4667 1.8 0.5833 1.6 0 < Tc < 8 .Math. (17 − A) .Math. t/D 38.4 ◯ ◯ ◯ ◯ ⊚ A Inventive Example 86 0.4667 1.8 0.5833 1.6 0 < Tc < 8 .Math. (17 − A) .Math. t/D 38.4 X X ◯ ◯ X — Comparative Example 87 0.4667 1.8 0.5833 1.6 0 < Tc < 8 .Math. (17 − A) .Math. t/D 38.4 X X ◯ X ◯ — Comparative Example 88 0.45 2 0.5625 1.75 0 < Tc < 8 .Math. (17 − A) .Math. t/D 37.3 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 89 0.45 2 0.5625 1.75 0 < Tc < 8 .Math. (17 − A) .Math. t/D 37.3 ◯ ◯ ◯ ◯ ⊚ B Inventive Example 90 0.45 2 0.5625 1.75 0 < Tc < 8 .Math. (17 − A) .Math. t/D 37.3 ◯ ◯ ◯ ◯ ⊚ A Inventive Example 91 0.45 2 0.5625 1.75 0 < Tc < 8 .Math. (17 − A) .Math. t/D 37.3 ◯ ◯ ◯ ◯ ⊚ A Inventive Example 92 0.45 2 0.5625 1.75 0 < Tc < 8 .Math. (17 − A) .Math. t/D 37.3 ◯ X ◯ ◯ ◯ — Inventive Example 93 0.45 2 0.5625 1.75 0 < Tc < 8 .Math. (17 − A) .Math. t/D 37.3 X X ◯ X X — Comparative Example 94 N/A N/A N/A N/A 0 < Tc < 8 .Math. (17 − A) .Math. t/D 37.3 X X X X X — Comparative Example (*1) ◯: Satisfying the formula. X: Not satisfying the formula. (*2) ◯: No cracking is found in weld. X: Cracking is found in weld. (*3) ⊚: Diameter of fractured portion is 110% or more of diameter of fused portion. ◯: Diameter of fractured portion is 100% or more and less than 110% of diameter of fused portion. X: Diameter of fractured portion is less than 100% of diameter of fused portion, or interfacial fracture. (*4) A: In 10 out of 10 samples, ratio of diameter of fractured portion to diameter of fused portion is 115% or more. B: In 5 to 9 out of 10 samples, ratio of diameter of fractured portion to diameter of fused portion is 115% or more. C: In 1 to 4 out of 10 samples, ratio of diameter of fractured portion to diameter of fused portion is 115% or more. (*5) B value: B = 1 + 0.1 .Math. Tc C value: C = 1 + 0.2 .Math. Tc (*6) Preferred lower limit of Ip/Im: when 0 < A < 3, (22 + A) .Math. B/80; when 3 ≤ A < 7, (17 + A) .Math. B/64; and when 7 ≤ A < 15, (11 + A) .Math. B/48. Preferred upper limit of Ip/Im: 1 + 0.15 .Math. Tc when 0 < A < 3, 3 ≤ A < 7, and 7 ≤ A < 15.
REFERENCE SIGNS LIST
(63) 1, 2 steel sheet 3, 4 electrode 5 weld (nugget)