Welded Structure And Method For Manufacturing Welded Structure
Abstract:
ngavengave1/2aveavengave The purpose of the present invention is to provide a welded structure capable of reducing fractures of a welded section. According to the present invention there is provided a welded structure in which two or three steel plates (11 12) are bonded by spot welding in a plurality of locations in a stacked section where the steel plates are stacked. In this welded structure with the diameter of a nugget (14) denoted by d(mm) the tip diameter of an electrode used in spot welding denoted by d(mm) and the average thickness per steel plate in the stacked section denoted by t(mm) the spot welded section satisfies the relationship d > d(t) in accordance with the average thickness t(mm) when 0.5 mm = t < 1.1 mm and satisfies the relationship d > 1.05 d when 1.1 mm = t = 2.6 mm.
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Notices, Deadlines & Correspondence
c/o NIPPON STEEL & SUMITOMO METAL CORPORATION 6 1 Marunouchi 2 chome Chiyoda ku Tokyo
1008071
2. OKADA Tohru
c/o NIPPON STEEL & SUMITOMO METAL CORPORATION 6 1 Marunouchi 2 chome Chiyoda ku Tokyo
1008071
3. ITO Yasuhiro
c/o NIPPON STEEL & SUMITOMO METAL CORPORATION 6 1 Marunouchi 2 chome Chiyoda ku Tokyo
1008071
4. YASUYAMA Masanori
c/o NIPPON STEEL & SUMITOMO METAL CORPORATION 6 1 Marunouchi 2 chome Chiyoda ku Tokyo
1008071
5. SAWA Yasunori
c/o NIPPON STEEL & SUMITOMO METAL CORPORATION 6 1 Marunouchi 2 chome Chiyoda ku Tokyo
1008071
Specification
Description
Title of Invention
WELDED STRUCTURE AND METHOD FOR MANUFACTURING THE SAME
5
Technical Field
[OOOl]
The present invention relates to a welded structure including n~ultiples teel
sheets that are joined by using resistance spot welding (hereinafter simply referred to
10 as "spot welding") at multiple locatiot~si n lapped portions in which multiple steel
sheets are overlapped, and also relates to a method for manufacturing the welded
structure. In particular, the present invention relates to a welded structure that
il~cludes an expected deformation region that is expected to be deformed by
receiving a load, and also relates to a method for manufacturing the welded structure.
15
Background Art
[0002]
FIG. 1 is a perspective view illustrating a structure of an autonlobile
showing framework ~nembers. A front side menlbcr 2, a rear side member 3, and a
20 side sill 7 are ar~anged on a side of the autonlobile. Each of these members is
disposed along a vehicle front-back direction (hereinafter simply referred to as
"fiont-back direction"). The front side member 2 and the rear side member 3 are
disposed in the front and back portions, respectively, and the side sill 7 is disposed in
tlie intermediate portion in the front-back direction.
25 [OOO3]
Floor cross members :4 atid 4', which are disposed in the intertilediate t ' ,
portion in the front-back direction, extend in a vehicle widthwise direction along the
floor surface. A center pillar 6 extending in a vertical direction is disposed on a side
in tlie iutermediate portion in the fiont-back direction. A bumper reinforcement 5
30 extendit~g in a vehicle widthwise direction is disposed at the front end of the
automobile. The above tllet~tioned members are fiatnework members that foml the
PCT Application No.: PCT/JP2015/057G56
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franlework of the auto~nobile.
[0004]
The fian~eworkm embers and crash-boxes la and lb are welded structures
including multiple steel sheets. The welded struch~reh as lapped portions in wllich
5 multiple steel sheets are overlapped, and these steel sheets are joined by spot welding
at multiple locations. W11en a spot weld portion (hereinafter simply referred to as
"weld portion") fractures (shear fractures) in the case of automobile collision, the
fra~nework member camiot generate a desired deformation, and thus cannot
sufficie~~tlayb sorb the collision energy. Thus, the welded structure that can
10 suppress the shear fracture is desired.
[OOOS]
Patent Literature 1 describes a method for allowing a base steel sheet to
fracture by reducing the width of a heat-influenced portion generated by welding in
the case of using a high-tensile steel sheet having a tensile strength of 440 MPa.
15 Patent Literature 2 describes a method for widely softening the outer sides of a weld
nugget, and for providing equiaxial martensite structure inside the nugget, to obtain a
resistance spot weld joint of the high-tensile steel sheet that is excellent both in
tensile shear resistance and in cross tension prope~ties. Patent Literatures 3 and 4
describe that the nugget diameter d is made to satisfy 3 x t, ID 5 d 5 6 x t,,ln (t,,, is
20 the sheet thickness (mm) of the thinnest sheet) by controlling weld current conditions
in multiple steps. Patent Literature 3 insists that the method can restrain initial
expulsion and expulsion at the faying surface, arid Patent Literature 4 insists that the
method can achieve a high joint strength.
25 Citation List
Patent Literature
[0006]
Patent Lite~ature1 : JP 2001-9573A
Patent Literature 2: JP 2013-78782A
Patent Literatu~e3 : JP 5359571B
Patent Literature 4: JP5333560B
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Snmmaiy of Invention
Technical Problem
[0007]
5 However, the methods of Patent Literatures 1 to 4 presupposes that the
nugget diameters cannot be made to be larger than a certain diametel; which inlposes
limitations on fracture suppressioti at weld portions. In particular, as the tensile
strength of a steel sheet becomes larger, the electric resistance becomes larger
accordingly, which generates expulsion due to heat generation during welding and
10 makes the nugget diameter smaller. This has led to a problem that the weld strength
cannot be stably obtained.
[0008]
The present invention is conceived in view of the above-described problem,
and is directed to provide a welded structure and a method for tnanufact~~rintghe
15 welded structure, which are new and improved and can reduce the fiacture of the
weld portions.
Solution to Problem
[0009]
20 According to an etnbodiment of the present invention, there is provided a
welded structure including two or three steel sheets and a lapped portion in which the
steel sheets are overlapped and joined by spot welding at a plurality of locations, the
welded structure including a spot weld portion, and, ~vliena diameter of a nugget is
d,, (nun), a tip diameter of an electrode used by the spot welding is d (mtn), and an
25 average thickness per steel sheet of the steel sheets at the lapped portion is t,,,, (mmn),
the spot \veld portion satisfies a condition (a) or a condition (b) below in accordance
wit11 the average thickness t,,,, (rnm).
(a) d,, > d(ta,,)" when 0.5 nun it,,., < 1.1 nnn (1)
(b) d,,, > 1.05d when 1.1 lmn < t,,, < 2.6 mtn (2)
30 [OOlO]
The xvelded structure may include an cxpected deformation region to be
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subjected to plastic deformation when a load is applied, and the spot welding may be
cal+ied out at least within the expected deformation region.
[OOll]
The expected deformation region may be free from spatter adhesion.
5 [0012]
The steel sheets may have a tensile strength of 980 MPa or more.
[OO 1 31
The electrode may be a combined electrode having an electrode body to be
pressed against the steel sheets at the lapped portion and a ring-shaped member to be
10 pr~sseda gainst the steel sheets around the electrode body.
[OO 141
The movable electrode may include a first ring-shaped member and a
second ring-shaped member to be pressed against the steel sheets at the lapped
portion with the first ring-shaped member and the second ring-shaped member facing
15 each other, and a first electrode body and a second electrode body, each being
inserted in a through hole disposed each of the first ring-shaped member and the
second ring-shaped member, to be pressed against the steel sheets at the lapped
portion with the first electrode body and the second electrode body facing each other,
and an electric current may flow through the steel sheets behveen the first electrode
20 body and the second electrode body.
[0015]
The spot weld portion satisfying the condition (a) or the condition (b) may
be present in a 20 to 60% extent on the welded structure.
[0016]
25 The spot weld portion preferably has an equivalelit carbon content (Ceq) of
0.13 mass% oE: more, the equivalent carbon content (Ceq) being defined by an
equation (3) below:
Ceq = [C] + 1/90 [Si] + Ill00 ([Mn] + [Cr])(3)
wvllere
30 [C]: an average C content (mass%) of the spot weld portion;
[Si]: an average Si content (mass%) of the spot weld portion;
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[Mn]: an average Mn content (mass%) of the spot weld portion; and
[Cr]: an average Cr content (mass%) of the spot \veld portion.
[0017]
The welded stmcture tnay be a rnember to be used for an automobile, for
5 example, atid in this case, the expected defornlation region may be a region to be
subjected to at least one of an axial conlpression load and a bending load.
[OO 1 81
According to an embodiment of the present invention, there is provided a
tilethod for manufacturing a welded structure including two or three steel sheets and
10 a lapped portion in which the steel sheets are overlapped and joined by spot welding
at a plurality of locations, the method includitig carrying out spot welding, the
carrying out spot welding including a first step in which a first rod-shaped electrode
body arid a second rod-shaped electrode body are arranged facing each other with the
lapped portion being sandwiched therebetween, and a first ring-shaped member and a
15 second ring-shaped member are arranged facing each other, the first ring-shaped
member having a though hole through which the first electrode body is inserted and
a back end to which a first elastic body is connected and the second ring-shaped
member having a through hole through which the second electrode body is inserted
and a back end to which a second elastic body is connected, and a second step in
20 which the lapped portioti is pressurized by pressing a tip face of each of the first
electrode body and the second electrode body against the lapped portion, and by
pressing a--tip face of each of the first ring-shaped member and the second ringshaped
nietiiber against the lapped portion while the first elastic body exerts a
pressing pressure on the first ring-shaped member and the second elastic body exerts
25 a pressing pressure on the second ring-shaped menibel; and then an electric current is
applied between the first electrode body and the second electrode.body. The first
step and the second step cause a spot \veld portion to satisfy a conditioti (c) or a
condition (d) below in accordance with an average thickness t,,., (mtn):
(c) d,, > d(ta,te)'nx vhen 0.5 mtn 5 t,,,, < 1.1 mil (4)
30 (d) d,, > 1.05d wvl~en 1.1 mm 5 t,,, 5 2.6 mm (5)
whexe d,, (nun) is a nugget diameter, d (nun) is a tip diameter of an
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electrode used by the spot welding, and t,,., (mtn) is an average thickness per steel
sheet of the steel sheets at the lapped portion.
Advantageous Effects of Invention
5 [0019]
The welded structure and the method for manufacturing the same according
to the present invention can reduce the fracture of the weld portion, as compared to
known welded structures, and thus the welded structure exhibits an excellent
collision energy absorbing capability. In particulal; applying this invention to
10 welded structures made of high-tensile steel sheets can provide such effects
appreciably, thereby eliminating the necessity of thickening the steel sheets.
Consequently, this enables the steel sheets to be thinner so that the weight of the
welded structures can be further reduced.
15 Brief Description of Drawings
[0020]
[FIG. 11 FIG. 1 is a perspective view illustrating an automobile st~ucture showing
framework members.
[FIG. 2 4 FIG. 2A is a right side view schematically illustrating a configuration
20 exaniple A of a welded structure according to the second embodiment.
[FIG. 2B] FIG. 2B is a right side view schematically illustrating a configuration
exan~pleB of the welded structure according to the second embodiment.
[FIG. 2C] FIG. 2C is a right side view schematically illustrating a configuration
exalnple C of the welded structure according to the second embodiment.
25 [FIG. 2D] FIG. 2D is a sight side view schematically illustrating a configuration
example D of the welded structure according to the second einbodiment.
[FIG. 3A] FIG. 3A is a side view illustrating a fiont side menlbel; in which expected
deformation regions are indicated.
[FIG. 3B] FIG. 3B is a side view illustrating a center pillar, in which expected
30 deformation regions are indicated.
[FIG. 3C] FIG. 3C is a side view illustrating a rear side member, in which expected
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defor~nationrc gions are indicated.
[FIG. 3D] FIG. 3D is a perspective view illustrating a side sill, in which expected
deformation rcgions are indicated.
[FIG. 4A] FIG. 4A is a cross-sectional view illustrating a vicinity of a spot weld
5 portion in a welded structure wvhen curvature changing regions are observed near
both ends of an indentation.
[FIG. 4B] FIG. 4B is a cross-sectional view illustrating the vicinity of a spot weld
portion it1 a welded structure when curvature changing regions are not obse~~endea r
both ends of an indentation, but a depressed amount of the indentation can be
10 identified.
[FIG. 4C] FIG. 4C is a photograph showing a cut surface of the vicinity of a spot
weld portion of a welded structure when a depressed amount of an indentation cannot
be identified.
[FIG. 5A] FIG. 5A is a schematic diagram illustrating an example of a resistance spot
15 welding apparatus that can be used in the method for manufacturing welded
structures according to the present invention, showing a state of the apparatus before
welding starts.
FIG. 5B] FIG. 5B is a schematic diagram illustrating an example of a resistance spot
. .welding apparatus that can be used in the method for manufacturing welded
20 structures according to the present invention, showing a state of the apparatus during
welding.
-[FIG. 6A] FIG. 6A is a schematic diagram illustrating a situation in which a weld
.. nugget is formed by spot welding using the resistance spot welding apparatus
illustrated in FIGS. 5A and 5B when a ring-shaped r~lelilber is not electrically
25 conductive.
?%[FIG. 6B] FIG. 6B is a schematic diagram illustrati~~ag situation in which a \veld
nugget is formed by spot wvelding using the resistance spot welding apparatus
illustrated in FIGS. 5A and 5B ~vliena ring-shaped member is electrically conductive.
[FIG. 71 FIG. 7 is a diagram showing a relation bet\veen nugget diameters and cross
30 tension loads.
[FIG. 81 FIG. 8 is an illustration including a front vie\\( and a right side view showing
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shapes and din~e~~soifo a~ h~ast- chantlel member and a closillg plate included in a
welded structure that is used in crushing tests by bending defonnation.
[FIG. 91 FIG. 9 is a diagram showing relatious between nugget diameters and
absorbed energy in bending defomlation.
5 [FIG. 101 FIG. 10 is an illustration including a front view and a right side view
showing shapes and dimensions of a hat-channel member and a closing plate
included in a welded structure that is used in axial crushing tests.
[FIG. 111 FIG. 11 is a diagram showing a relatiall between nugget diameters and
absorbed energy in axial crush deformation.
[FIG 121 FIG. 12 is a characteristic diagram showing a relation between nugget
diameters d,, (mm) and an average thickness per material steel sheet t,, (tnm) when
a welded structure is obtained by the method according to present embodiment.
[FIG. 13A] FIG. 13A is a right side view schelnatically illustrating a configuration
example E of a welded structure according to a first embodiment.
[FIG. 13B] FIG. 13B is a right side view schematically illustrating a cotlfiguration
example F of a welded structure according tothe second embodiment.
[FIG. 14A] FIG. 14A is a right side view schematically illustrating a configuration
example G of the welded st~ucturea ccording to the first embodiment.
[FIG. 14B] FIG. 14B is a right side view schematically illustrating a configuration
example H of the welded stt~~chtarcec ording to the second embodiment.
[FIG. 151 FIG. 15 is a right side view schelnatically illustrating a configuration
example I of the welded structure according to the first embodiment.
[FIG. 161 FIG. 16 is a right side view schematically illustrating a configuration
exanlple J of the welded structure according to the first embodiment.
[FIG. 171 FIG. 17 is a right side view schematically illustrating a configuration
example K of the welded structure according to the first embodiment.
. .
Description of Embodiments
[0021]
Hereinafter, prefe~ved embodiments of the present invention will be
described in detail with refcrellce to the appended drawings. Note that, in this
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specification and the appended drawings, structural elements that liave substantially
the same function and structure are denoted with the same reference numerals, and
repeated explanation of these structural elements is omitted.
roo221
5 Now, the welded stlucture and the method for niant~facturing the welded
structure according to the present invention will be described in detail.
As described above, there is provided a welded structure including two or
thee steel sheets and a lapped portion in ~vliicht he steel sheets are overlapped and
10 joined by spot welding at a plurality of locations, the welded stn~cturei ncluding a
spot weld portion, and, wlien a diameter of a nugget is d,,, (nm), a tip diameter of an
electrode used by the spot welding is d (mm), and an average thickness per steel
sheet of the steel sheets at the lapped portion is t, (mnl), the spot weld portion
satisfies a condition (a) or a condition (b) below in accordance with the average
15 thickness t,,, (mm).
(a) d., > d(t,,,,)ln when 0.5 mm 5 ta,, < 1.1 mm (1)
(b) d,,, > 1.05d when 1.1 mm 5 ta,, < 2.6 mm (2)
[0023]
The welded structure according to the embodiment of the present invention
20 may have a configuration in which two steel sheets are included and overlapped at
the lapped portion (hereinafter referred to as "first embodimetlt"). When two steel
sheets are a first and a second steel sheet;- the first steel sheet can serve as a hatchannel
member, and the second steel sheet can serve as a closing plate member, for
exanlple, as described later with reference to FIG. 8.
25 [0024]
The welded structore according to'the embodimetit of the present invention
may liave a configuration including three steel sheets (hereinafter referred to as
"second embodiment"). In this case, two sheets out of the thee may be overlapped
at the lapped portion, or all of the t l ~ e esh eets may be overlapped at the lapped
30 portion. The welded st~ucture of the second embodinlent, for example, may be
formed of a tube-shaped body and an intermediate plate that partitions tl~e inner
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space of the body. More specifically, configuration exa~llples illustrated in FIGS.
2A to 2D may be adopted when the three steel sheets sen7e as the first, the secoad,
and the third steel sheet.
[0025]
5 FIGS. 2A to 2D are right side views sche~naticallyil lustrating configuratio~i
exanlples of the welded structure according to the second embodiment. FIGS. 2A,
2B, 2C and 2D illustrate a configuration example A, a configuration example B, a
configuration exanlple C, and a configuration example D, respectively. A \velded
structure 43 illustrated in FIG. 2A has the body formed of a first steel sheet 53 and a
10 second steel sheet 63, and the intermediate plate formed of a third steel sheet 73.
The first steel sheet 53 is the hat-channel member and the second steel sheet 63 is the
closing plate member. The welded structure in the configuration example A has
four lapped portions, and two out of the three steel sheets are overlapped at each
lapped portion.
15 [0026]
Welded structures (44 to 46) illustrated in FIGS. 2B to 2D each have the
body formed of a first steel sheet (54 to 56) and a second steel sheet (64 to 66). The
intermediate plate is formed of a third steel sheet (74 to 76). The first steel sheet
(54 to 56) and the second steel sheet (64 to 66) each have two bent portions with a
20 predetermined angle (90' in these figures). The welded strncture of the
configuration examples B to D has two lapped portions, at each of which all of the
three steel sheets are overlapped. ..
[0027] -. -
FIGS. 13A and 13B illustrate a configuration example E and a configuration
25 exanlple F, FIGS. 14A and 14B illustrate a configuration example G and a
configuration example 13, and FIGS. 15, 16, and 17 illustrate a configuration ...*. ..
exanlplc I, a configuration exanlple J, and a configuration example K, respectively. , .
A welded st~ucture 80 illustrated in FIG. 13A has the body fornled of a first steel
sheet 83 and a second steel sheet 93. A welded structure 82 illustrated in FIG. 13B
30 has the body formed of the first steel sheet 83 and the second steel sheet 93, and the
internlediate plate is formed of a third steel sheet 84. The first steel sheet 83 is the
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hat-channel inember, and the second steel sheet 93 is the closing plate inember. The
welded structure in the configuration example E has two lapped portions, and two
steel sheets are overlapped at each lapped portion. The welded structure in the
configuration example F has four lapped portions, and two out of tlie three steel
5 sheets are overlapped at each lapped portion.
[0028]
A welded structure 100 illustrated in FIG. 14A has the body formed of a first
steel sheet 103 and a second steel sheet 113. A welded structure 101 illustrated in
FIG. 14B has the body formed of the first steel sheet 103 and the second steel sheet
10 113, and the intermediate plate is formed of a third steel sheet 114. The first steel
sheet 103 is the hat-channel member, and the second steel sheet 113 is the closing
plate member. Tlie welded structure in the configuration example G has two lapped
portions, and two steel sheets are overlapped at each lapped portion. The welded
structure in the configuration example H has four lapped portions, and two out of the
15 three steel sheets are overlapped at three lapped portions. Three steel sheets are
overlapped at the remaining one lapped portion.
[0029]
A welded structure 120 illustrated in FIG. 15 has the body formed of a first
steel sheet 123 and a second steel sheet 133. The first steel sheet 123 is the hat-
20 channel member, and the second steel sheet 133 is the closing plate member. Tlie
welded stl-ucture in the configuration example I has three lapped portions, and two
steel slieets are overlapped at each lapped portion.
[0030]
A welded stl-ucture 140 illustrated in FIG. 16 has the body formed of a first
25 steel sheet 143 and a second steel slieet 153. The first steel sheet 143 is the hatchannel
member, and the secotid steel sheet 153 is tlie clositig plate menlibel: The ;'
welded structure in the configuration example J has two lapped portions, and t\vo
steel sheets are overlapped at each lapped portion.
[003 I]
30 . A welded stl-i~cture1 50 illustrated in FIG. 17 has the body forn~edo f a first
steel shcet 153 and a second steel sheet 163. The first steel sheet 153 is the hatPCT
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channel membel; and the second steel sheet 163 is the closing plate menibel: The
welded stn~cturein the configrtration example K has two lapped portions, and two
steel sheets are overlapped at each lapped portion.
[0032]
5 With reference to FIG. 1, such welded structures of the present embodiment
can be applied, for example, to any one of crash-boxes la and lb, a front side
member 2,, a rear side member 3, floor cross members 4 and 4', a bumper
reinforcement 5, a center pillar 6, and a side sill 7.
[0033]
10 In most cases, collision against the automobile nlay occur fsotn ahead, from
behind, and from side (respectively represented by "Fr. inlpact", "Rr. impact", and
"Side impact" with an accompanying thick arrow in FIG. 1). In such a case, a
member near a collided portion in the automobile deforms. The above-described
members each have a shape extending in the longitudinal direction. When a load is
15 applied in the collision along the longitudirial direction (that is, the axial direction) to
the vicinity of an end of the member, there occurs axial crush deformation
(progressive plastic buckling deformation) in which the member contracts like
bellows (or is folded in pleats) in the longitudinal direction. 111 addition, when the
member has a bent portion and a load is applied in the collision in a direction along
20 the longitudinal direction, there occurs bending deformation followed by buckling at
the bent portion. When a load is applied in the collision to a central portion of the
member in a direction pe~pendicular or oblique to the longitndinal direction of the
member, there occurs bending deformation. When a load is applied to the ~netnber
in a cross-sectional direction of the member, there occurs the collapse of the cross
25 section acco~npanied by bending deformation, resulting in the overall bending
deformation of the tnembec
[0034] , .
Table 1 shows examples of the regions in u~llicll plastic defornlation is
expected by receiving a load (hereinafter referred to as "expected defornlation
30 region") for each of the memnbe~s. FIGS. 3A to FIG. 3D are diagrams each
illustrating the.expected deformation regions of the front side member 2, the center
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pillar 6, the rear side nleniber 3, and the side sill 7.
[Table 11
Welded
structure
(niember
name)
Front side
member
Expected
deformation
region ratio
(%I
Approx. 30
to 60
Expected deformation region
Axial crush deformation: region between the front end
and approx. 250 mm fiorn the fiont end
Bending deformation: apmox. 300 mm long I the midportion in the longitudinal directiloonn -g re-ei on in
Center I Approx. 20 1 Bending deformation: region between the top end and
5 corresponding members that are niounted on an automobile.
[0036]
pillar
Rear side
member
Side sill
In these members that are the welded stmctore, multiple weld portions
created by spot welding are fornled, for example, at equal intervals along the
longitudinal directioii of each ~l~etnbeeT he \veld portions present in the 'expected
10 defonnation region satisfy either the above-mentioned condition (a) or (b). .
[0037]
In examples in Table 1 and FIGS. 3A to 3D, the length of the expected
deformation r~ionSivit11re spect to the longitudinal direction of the weldeit'structure
is approximately 20 to 60% of the whole length of the ivelded structure. Thus, in
Note that "front end", "rear end", "top end", and "bottom end" are with respect to
to-50
Approx. 35
to 60
Approx. 30
to 60
15 the ease that the spot \veld portions are present approximately at equal intervals over
approx.-150 mm from thetop end
Collapse of the cross section: region between the
bottonl end and approx. 300 mm froni the bottom end
Axial crush deformation: region between the rear end
and approx. 300 mm from the rear end
Bending deformation: approx. 300 mm long region in
the mid portion in the longitudinal direction
Axial crush deformation: region behveen the front end
and approx. 100 mm fiom the front end
Bending deformation: approx. 300 mm long region in
the mid portion in the longitudinal direction
the whole \velded structure in the longitudinal direction thereof, approximately 20 to
60% spot weld portions of all the spot weld portions are present in the expected
deforn~ationr egion. In this ease, the reniaining spot \veld portions do not have to
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satisfy either of the condition (a) or (b).
[0038]
Regarding the crash-boxes la and lb and the bumper reinforcement 5 (sce
FIG. l), the expected deformation region covers the whole region of each membel;
5 and all of the weld portions of each member needs to satisfy either of the condition
(a) or (b).
[0039]
The diameter of the weld nugget defined in the conditions (a) and (b) is
larger than tlie nugget diameter that can be fortned by known spot welding witl~out
10 generating expulsion.
[0040]
The expulsion is generated due to the fact that spot welding locally creates a
region of high electric current density within an expected weld region of a base steel
sheet, and sudden heating and melting of the region causes the melt of the base metal
15 to spatter. Consequently, when the spatters are adhered to the welded structure, the
shape of the nugget in terms of size and thickness distribution, and the like does not
become uniform even if the conditions of the spot welding remains the same. As a
result, the welded structure having the weld poriions that satisfy the conditions (a)
and (b) cannot he obtained in all of the expected deformation regions. Moreover,
20 this does not stably provide the nuggets having a high strength, and thus causes shear
fracture to occur frequently even if the conditions (a) and (b) are satisfied.
[0041]
The welded structure of the present embodiment does .not. cause the
generation of the expulsion and adhesion of the spatters, and the melt of the heated
25 and melted base metal has not been observed to spatter out of the melted portions
during n~anu@iqt,tul.in. g....T ,. hus, unifornl heating is achieved within the.-expected weld
region, which causes the size and shape of the nuggets to be substantially uniform
wlien the conditions of spot welding remain the same. In the welded structure of
the present embodiment, satisfying either of the condition (a) or (h) makes the nugget
30 strength stably high, and the shear fracture is not likely to occur.
PCT Application No.: PCT/JP2015/057G5G
15/48
In the present embodiment, wvl~en the tip diameter of an electrode used in the
spot welding is uuknoww~n, the diameter of a11 indentation formed on the surface of the
steel sheet of the welded structure can be regarded as the tip diameter of the electrode.
The indentation is formed by the tip of the electrode being pressed on the surface of
.5 the steel sheet during spot welding. Now, tile structure of the welded structure and
a method for determining the diameter of the indentation will be described with
, reference to a case in which two steel sheets (the first and the second steel sheets) are
joined.
[0043]
10 FIG. 4A is a cross-sectional view illustrating the vicinity of a spot weld
portion in the welded structure.
This welded structure 10 includes a first steel sheet 11 atid a second steel
sheet 12. The welded structure 10 has a lapped portion in which the first and tlie
second steel sheets 11 and 12 are overlapped. The first steel sheet 11 and the
15 second steel sheet 12 are joined at ~nultiplel ocations in this lapped portion by spot
welding. Only one spot \veld portion 13 is shown in FIG. 4A.
[0044]
An indentation 15, which corresponds to the tip of an electrode used for spot
welding, is formed on the surface of each of the first and the second steel sheets 11
20 and 12. In FIG. 4A, a depressed portion is the indentation 15. A nugget 14 is
formed inside tlie weld portion 13. In FIG. 4A, the weld portion 13 is substantially
symmetrical with respect to the plane between the first steel sheet 11 and the second
steel sheet 12, and t1111s reference ~lo~lleraflosr , and related to, the i~identatioti1 5 are
provided only for one of the first and the second steel sheets 1 I and 12.
25 [0045]
&In. the present embodimnent, the diameter of a wel&ptigget (hereinafter
referred to as-"nugget diameter") d,, is defined as the maximum length of the nugget
14 in a direction parallel to the steel sheets (11 and 12) near the nugget 14. FIG. 4A
is a cross sectio~pi erpendicular to the first and the second steel sheets, illustrating the
30 cross section of the illdentation 15 including. the lllaximum diameter portion
(hereinafter referred t o as "maximum diameter cross section"). The ~naximutn
PCT Application No.: PCT/JP2015/057G5G
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lengtli of the nugget 14 in a direction parallel to the first and the second steel sheets
11 and 12 in this cross section can be regarded as tlie nugget diameter. I11 a cut face
of the weld portion 13, tlie nugget 14 displays a different color (brightness), and
thereby the length of the nugget 14 in a direction parallel to tlie first arid the second
5 steel sheets I1 and 12 can be determined easily.
[0046]
The indentation 15 corresponds to a region that is pressed by the tip of the
electrode when spot welding is carried out. When the type and thickness of the
steel sheets (the first steel sheet 11 and the second steel sheet 12 in the figure) that
10 are pressed by the electrodes are the same, there is a tendency it1 which the
indentation 15 becomes deeper as the nugget diameter d,,g becomes larger.
[0047]
The diameter d of the indentation 15 (that is, the tip diameter of the
electrode used for spot welding) in the present embodiment is defined as below.
15 In FIG. 4A, regions where the cuwature changes can be identified near both
ends of the indentation 15. The inside surfaces of the indentation 15 include a
bottom surface that is curved with a large curvature radius (or a flat surface), and
inclined surfaces that are formed on the periphety of the bottom surface and are
inclinedas a whole with respect the bottom surface and that have a curvature radius
20 smaller than that of the bottom surface. In the cross sectiot~ in FIG. 4A, the
curvature of the contour of the indentation 15 changes between the bottom surface
andthe inclined surfaces. In this case, the diameter d of the indentation 15 is a
distance- between two points l6a and 16b where the curvature changes (or tlie
curvature change becomes maximum) in this cross section (~iiaximum diameter cross
25 section).
[OW481 * , .*. >.>-,
. .. FIG. 48 illustrates the vicinity of the weld po~tion 13, showing the
maximum diameter cross section of a portion it1 whicli a region where the curvature
changes in the indentation 15 is not observed but a depressed aniount D of tlie
30 indentation 15 is identifiable. In FIG. 4B, the same reference numerals are used for
cotnpotients similar to those in FIG. 4A, thereby omitting the description thereof.
PCT Al~pLication No.: PCT/JP2015/057656
17/48
In this case (including the case in which the region \vliere the curvature
changes are observable near only one end of the indentation 15), the length of the
indentation 15 (depressed region) in the direction parallel to the steel sheets (I 1 and
5 12) in this cross section is regarded as the diatneter d of the indentation 15.
[0050]
FIG. 4C is a photograph showing a cut face of a portion near the weld
portion'l3 that is cut at the maximum diameter cross section. In this portion, the
depressed atiiount of the indentation 15 is not identifiable. In FIG. 4C, the same
10 reference numerals are used for components similar to those in FIG. 4A, thereby
omitting the description thereof. A hardened portion 17 generated by heat influence
is present around the nugget 14. The hardened portion 17 is formed by the fist and
the second steel sheet 11 and 12 as base metals being heated to the austenite region
and then being quenched during spot welding.
15 [0051]
When the depressed amount of the indentation 15 is not identifiable, the
diameter of the hardened portion 17 generated by heat influence in the maximum
diameter cross section of the first or tlie second steel sheet 11 or 12 is regarded as the
diatneter d of the indentation 15. In the cross. section, the brightness of the
20 hardened portion 17 generated by heat influence is different from that of another
portion, and thus tlie diameter of the hardened portion 17 generated by heat influence
I can be determined easily.
[0052] ..~
M~liilet lie tip diameter of the electrode used for spot welding is determined
25 . from tlie diameter of the indentation by the method described with reference to FIGS.
3*,:4A to 4C, the tip diameter may instead be deter~ilined-firomth e liiaximum diatneter of
.a region having a high Cu (copper) concentration on the surface of the steel sheet.
The electrodes to be used for spot welding contain Cu, and CLI is transferred to the
surface of the steel sheet dnring spot welding. Thus, the region having a high Cu
30 concentration on the smface of the steel sheet corresponds to the tip of the electrode.
[0053]
PCT Application No.: PCT/JP2015/057G56
1 8/48
In either case of determining tlie diameter of the indentation by using tlic
method described with reference to FIGS. 4A to 4C or by using the region having a
high Cu concentration, when the diameter d of the indentation 15 of one steel sheet
11 cannot be regarded identical to the diameter d of the indentation 15 of tlie otlier
5 steel sheet 12, an average of the diameters d of the indentations 15 of both steel
sheets 11 and 12 is regarded as the diameter d of the indentation 15.
[0054]
In the present embodiment, whcn the lapped portion in which two steel
sheets are overlapped is joined by spot welding, the average thickness t,, (mm) per
10 steel sheet at the lapped portion is (tl+t2)/2, where tl (mm) and t2 (mm) represent the
individual thicknesses of the two steel sheets, respectively. The average thickness
t,,, is 0.5 mm or more and 2.6 mn or less. Wfien the average thickness t,,, is in this
range, it is possible to form the weld pol-ti011 that satisfies the Formula (1) or (2)
without generating expulsion by using a preferred method for manufacturing the
15 welded structure of tlie present embodiment (see later description).
[0055]
In the present embodiment, when the lapped portion in which three steel
sheets are overlapped is joined by spot welding, tlie average thickness per steel sheet
_ t,,., (mm) at the lapped portion is (t,+td+ts)/3, where t3 (mm), 4 (tnm), and tS (mm)
20 represent the individual thicknesses of the three steel sheets, respectively. The
average thickness t,, is 0.5 mm or more and 2.6 mm or less, which is the same as in
the case that the lapped portion in which two steel sheets are overlapped is joined by
spot welding. When the average thickness t,.,.is in this range, it is possible to form
the weld portion that satisfies Fornlula (1) or (2) without generating expulsion by
25 using the preferred method for manufacturing tlie- welded structure of the present
?.- enlbodiment (see later description). ~?fi... .
. . [0056] .: .
In the present embodiment, the amount of energy that can be absorbed when
the wvelded structure receives impact becomes larger as the intel-val between weld
30 portions is smaller, in other words, the number of weld portions in a given unit length
of the welded structure is larger. However, if the interval between \veld portions is
PCT Application No.: PCT/JP2015/057666
19/48
made too small, adjacent nuggets may be overlapped with each other. This causes a
sliu~lct urrent to flow in a direction toward an adjacent nugget, thereby prevetiting the
nugget from being formed to have a predetermined diameter. Thus, the interval
bet\veen weld portions is preferably 17 mm or more.
5 [0057]
Tlie present embodiment is preferably applied to welded structures having
weld portions in which Ceq, that is, an equivalent C (carbon) content, defined in
Formula (3) below is 0.13 mass% or more.
Ceq = [C] + 1/90 [Si] + 11100 ([Mn] + [Cr]) . (3)
10 where
[C]: average C content (mass%) of weld portion;
[Si]: average Si content (mass%) of weld portion;
[Mn]: average Mn content (mass%) of weld portion; and
[Cr]: average Cr content (mass%) of weld portion.
15 [0058]
In general, as the equivaletlt carbon content in steel sheets to be welded
becomes larger, the electric resistance becomes higher and spot welding becomes
more difficult to carry out without generating expulsion. When the equivalent
carbon content (Ceq) of the weld portion is-0.13 mass% or more, it is extremely
20 difficult to carry out spot welding without generating expulsion by using known
manufacturing methods. On the other hand, it can be achieved by using the
preferred method for manufacturing the welded structure of the present embodiment
(see later description).
[0059]
25 The equivalent carbon content (Ceq) of the weld portion is approximately
r,_ equal to an equivalent carbon content based on an average chemical composition of
multiple steel sheets. When two steel sheets (the first and the second steel sheets)
are joined by spot welding at the lapped portion in which the two sheets are
overlapped, aud when the thicknesses of the two steel sheets are different, the
30 average chemical cornposition of the two steel sheets is calculated as a. weighted
average bet\veen the average chemical composition of the first steel sheet and the
PCT Application No.: PCT/JP2015/057656
20148
average chenlical composition of the second steel sheet \\lit11 respect to the
thicknesses tl and t2. More specificall>: the equivalent carbon content (Ceqplateo)f
the first and the second steel sheets based on their average chemical coltlpositions is
given in Formula (6) belo~v.
5 Ceq,late = RI[C]I + R2[C]2 + 1/90 (Rl[Si]l + R2[Si]2) + 11100 (Rl[Mn]l +
R2[M1112 + RI [Crl I + R2[Crl2) (6)
where
[C]I: average C content (mass%) of tile first steel sheet;
[CI2: average C content (mass%) of the second steel sheet;
[Sill: average Si content (mass%) of the first steel sheet;
[Si]2: average Si content (mass%) of the second steel sheet;
[Mnll: average Mn content (mass%) of the first steel sheet;
[Mnlz: average Mn content (mass%) of the second steel sheet;
[CrIl: average Cr content (mass%) of the first steel sheet;
[Cr]2: average Cr content (mass%) of tlie second steel sheet;
RI = tl/(tl+ t2); and
R2 = t2l(tl + t2).
[0060]
When three steel sheets (the first, the second, and the third steel sheets) are
20 joined by spot welding at the lapped portion in which the three sheets are overlapped,
and when the thicknesses of the three steel sheets are different, the average chemical
composition of the three steel sheets is calculated as a weighted average among the
average chemical composition of the first steel sheet, the average chemical
composition of the second steel sheet, arid the average chemical composition of the
25 third steel sheet with respect to tlie tl~icknesses t3, t4 and ts. More specifically, the
equivalent carbon content (Ceqplalc)tfotrh e first, the second, and the third steel sheets
based on their average chemical compositions is given in Formula (7) below.
Ceq,~,,, = R3[Cl3 + &LC14 + Rs[CIS + 1/90 (R3[Si13 + R4[Sil4 + Rs[Sil~) +
11100 (R3[Mn]3 + &[Mn]4 + Rs[Mn]s + R3[Cr]3 + R.I[Cr]4 + Rs[Cr]s) (7)
30 where
[C]3: average C content (mass%) the first steel sheet;
PCT Application No.: PCT/JP2015/067656
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[C]4: average C content (mass%) of the second steel sheet;
[CIS: average C content (mass%) of the third steel sheet;
[Si]3: average Si content (mass%) of the first steel sheet;
[%I4: average Si content (mass%) of the second steel sheet;
[Sils: average Si content (mass%) of the third steel sheet;
[MnI3: average Mn content (mass%) of the first steel sheet;
[Mnl~a:v erage Mn content (mass%) of the second steel sheet;
[Mnls: average Mn content (mass%) of the third steel sheet;
[Cr]3: average Cr content (mass%) of the first steel sheet;
10 [Crld: average Cr content (mass%) of the second steel sheet;
[Crls: average Cr content (mass%) of the third steel sheet;
R ~ t d ( t 3+ t4 + 1s);
%=t4/(t3 + 4 + tS); and
Rs=ts/(t3 + 4 + ts).
15 [0061]
Now, a chemical eonlposition of a high-tensile steel sheet, which is a
dificult material for welding and which can be used for the present embodiment,
will be described below by way of example. It is assumed that a chemical
composition example below~is used to form a streel structure that mainly contains
20 bainite and mal-tensite as main phases, and also contains ferrite and residual austenite
partially. The steel sheet containing such a structure exhibits a high strength and
also a ductility to a level in which the base metal does not fracture in a collision
event. The steel sheet according to the present ernbodinlent is not limited to the
above-described structure or the steel sheet containing the ehetnieal composition
25 described below. In terms of the content of each element, " % means "mass% in
the example below.
[0062]
(i) C: 0.06% to 0.35%
30 C has an effect of pronloting the generation of bainite or martensite as a
main phase and also the gelleiation of residual austenite. C also has an effect of
PCT Application No.: PCTlJP2015105765G
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enhancing the tensile strength of a steel sheet by improving the strength of the
martensite. In addition, C strengthens steel by way of solid solution hardening and
provides an effect of improving the yield strength and tensile strength of the steel
sheet.
5 100631
A C content of less than 0.06% may make it difficult to obtain the abovedescribed
effects. Thus, the C content is set preferably at 0.06% or more, more
preferably at more than 0.12%, and still more preferably at more than 0.14%. In
contrast, if the C content exceeds 0.35%, the hardness of the martensite may become
10 excessively high, or the stability of the residual austenite may become excessively
increased, to cause work-induced transformation to be less likely to occur. This
may result in a substantial decrease in local ductility of the steel sheet. Moreover,
weldability deteriorates considerably. Therefore, it is preferable to set the C content
at an amount of 0.35% or less.
15 [0064]
(ii) Mn: 1.0% to 3.5%
Mn has an effect of promoting the generation of bainite or martensite as a
main phase, and also the generation of residual austenite. Mn also strengthens steel
by way of solid solution hardening and provides an effect of improving the yield
20 strength and tensile strength of a steel sheet. Moreover, Mn enhances bainite
strength by way of solid solution hardening so as to provide an effect of improving
local ductility of the steel sheet by improving the bainite hardness under high-strain
loading conditions.
[0065]
25 A Mn content of less than 1.0% may make it difficult to obtain the abovedescribed
effects. Tlms, the Mn content is set preferably at 1.0% or more;more
preferably at more than 1.5%, still more preferably at more than 1.8%, and especially
preferably at more than 2.0%. In contrast, a Mn content of tnore than 3.5%
excessively retards bainite transfornation, which fails to stabilize the residual
30 austenite so as to make it difficult to obtain a predetermined amount of residual
austenite. Therefore, the Mti content is preferably set at 3.5% or less.
PCT Al)plication No.: PCT/JP2015/057656
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[0066]
(iii) Si+Al: 0.20% to 3.0%
Si and A1 have an effect of promoting the generation of residual austenite by
reducing the generation of carbides in bainite to improve the uniform ductility and
5 local ductility of the steel sheet. Si aud A1 also strengthen steel by way of solid
solutio~hi ardening and provides an effect of improving the yield strength and tensile
strength of a steel sheet. Moreover, Si and A1 enhance bainite strength by way of
solid solution hardening so as to provide an effect of improving local ductility of the
steel sheet by improwring the bainite hardness under high-strain loading conditions.
10 [0067]
A total content of Si and Al (hereinafter referred to as "(Si+AI) content") of
less than 0.20% makes it dificult to obtain such effects. Consequently, the (Si+Al)
content is set preferably at 0.20% or more, more preferably at 0.5% or more, and still
more preferably at 0.8% or more. h~ contrast, a (Si+AI) content of more than 3.0%
15 will only result in saturating the above-described effects, which leads to cost
disadvantage. This also results in rising the transformation temperature and thus in
hampering productivity. Therefore, the (Si+Al) content is preferably set at 3.0% or
less.
[0068]
20 Si has an excellent solid solution hardening capability. Thus, the Si
content is set preferably at 0.20% or more, and more preferably at 0.8% or more. In
contrast, Si has an.effect of deteriorating the chemical conversion treatability and the
weldability of the. steel sheet, and thus the Si content is set preferably at less than
1.9%, more preferably at less than 1.7%, and still more preferably at less than 1.5%.
25 [0069]
(iv) P: 0.10% or less I"
In ge11era1,~P is contained as an impurity. P is segregated ~ i t i grain
boundaries to make steel brittle, thereby aggravating crack generation when an
impact load is applied. A P content of more than 0.10% noticeably etnbrittles steel
30 due to the above-described effect, making it difficult to suppress the crack generation
when an impact load is applied. The P content is preferably less than 0.020%, and
PCT 11l)plication No.: PCT/JP2015/05765G
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more preferably less than 0.015%.
[0070]
(v) S: 0.0 10% or less
In general, S is contained as an inlpuritj: aud S has an effect of deteriorating
5 formability by forniing sulfide-base inclusions. The above-described effects
becomes evident at a S content of more than 0.010%. The S content is preferably
, 0.005% or less, more preferably less than 0.003%, and especially preferably 0.001%
or less.
[0071]
10 (vi) N: 0.010% or less
In general, N is contained in steel as an impurity, and N has an effect of
deteriorating the ductility of the steel sheet. The deterioration of the ductility
becomes evident at an N content of more than 0.010%. The N content is preferably
0.0050% or less.
15 100721
As described above, the steel co~itains C: 0.06% to 0.35%, Mn: 1.0% to
3.5%, (Si+Al): 0.20% to 3.0%, P: 0.10% or less, S: 0.010% or less, N: 0.010% or
less, and the balance: Fe and impurities. Here, the impurities means what comes to
be mixed in from law materials such as ore and scrap, fiom manufacturing
20 environment, and so on, in the industrial steel manufacturing. The impurities are
allowed as far as they do not negatively influence the steel of concern to the present
embodiment.
100731
Elements that will be described hereafter are optional, and can be contained,
25 ~vhen necessary as a substitute of a portion of Fe, in the steel having the abovedescribed
cbetnical conlposition.
[0074] . ..
(vii) One or more elements selected fsom the group consisting of Cr: 0.5% or less,
Mo: 0.5% or less, and B: 0.01% or less.
30 Cr, Mo, and B have an effect of improving hardenabilitj~a tid promoting
bainite generation. In addition, these eletnents have an effect of promoting the
PCT Al)plicatioii No.: PCT/JP2015/057656
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generation of martensite and residual austenite, and also liavc an effect of
strengthening the steel by solid solution hardening to improve the yield strength and
tensile strength of the steel sheet. Therefore, one or more elements selected from
the group consisting of Cr, Ma, and B may be contained. To make sure of obtaining
5 the above-described effect, it is preferable to satisfy any one of Cr: 0.1% or more,
Mo: 0.1% or more, and B: 0.0010% or more.
[0075]
Howevel; if the Cr content exceeds 0.5%, the Mo content exceeds 0.5%, or
the B content exceeds 0.01%, noticeable deterioration in the uniform elongation and
10 local ductility of the steel sheet may be resulted. Thus, when one species or more
of Cr, Mo, and B are contained, it is preferable to have each content within the
above-described content range.
[0076]
pLication No.: PCT/JP2015/05765G
30148
tlie second ring-shaped member 32 first comes into contact with and presses the
surface of the first steel sheet 11, which prevents the further tnoving of the second
ring-shaped tnenlber 32.
[0091]
5 Subsequently, at the first combined electrode 20, the first electmde body 21
continues moving toward the second steel sheet 12. At this time, the distance
between the first ring-shaped member 22 and the retainer plate 25 becomes gradually
smaller, which causes the first elastic body 23 (compression coil spring 23A) to
defo'onn by compression. Simultaneously, at the second combined electrode 30, the
10 second electrode body 3 1 continues moving toward the first steel sheet 11. At this
time, the distance between the second ring-shaped member 32 and the retainer plate
35 becomes gradually small, which causes the second elastic body 33 (compression
coil spring 33A) to deform by compression.
[0092]
15 Subsequently, as illustrated in FIG. SB, at the first combined electrode 20,
the tip portion of the electrode tip 21a comes into contact with and presses the
suiface of the second steel sheet 12, which prevents the further inoving of the first
electrode body 21. Simultaneously, at the second combined electrode 30, the tip
portion of the electrode tip 31a comes.into contact with and presses the surface of the
20 first steel sheet 11, which prevents the further tiloving of the second electrode body
31.
[0093]
By pressing the tip portions of the electrode tips 31a and 21a against the
respective surfaces of the first and the second steel sheets 11 and 12 (or by flowing
25 an electric current between the first and the second electrode bodies 21 and 31 in this
state), the indentations 15 (see FIGS. 4A to 4C) are fonned. %:A
[0094]
In FIG. 4A, the bottoni surfaces of tlie indentations 15, which are formed as
depressed poitions, correspond to the portions that have come into contact with the
30 tip faces 21aa and 31aa of the first and the second electrode bodies 21 and 31
illustrated in FIGS. 5A and 5B. The iriclincd surfaces of the indentations 15 in FIG.
PCT Application No.: PCT/JP2015/067G56
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4A correspond to the inclined surfaces formed on the peripheries of the tip faces 21aa
and 3 1 aa and inclined with respect to the tip faces 2 1 aa and 3 1 aa in the electrode tips
21a and 31a illustrated in FIGS. 5Aand 5B.
[0095]
5 The portions corresponding to the inclined surfaces of the electrode tips 21a
and 31a are not clearly exhibited in the indentations 15 illustrated in FIGS. 4B and
4C.
[0096]
The diameters d of the indentations, which have been described with
10 reference to FIGS. 4A to 4C, correspond to the diameters of the tip faces 21aa and
3 laa of the electrode tips 21 a and 3 1 a.
[0097]
As described above, the lapped portion of the steel sheet set is sandwiched
by the first electrode body 21 and the second electrode body 31 that are facing each
15 other. At the same time, the lapped portion is also sandwiched by the first ringshaped
member 22 and the second ring-shaped member 32 that are facing each other.
At this time, the pressure from the first electrode body 21 and the second electrode
body 31 is applied onto the lapped portion, and the pressure from the first ringshaped
member 22 and the second ring-shaped member 32 is also applied onto the
20 lapped portion.
[0098]
Here, the repulsive force of the first elastic body 23 that is in compressive
defornlation is acting on the first ring-shaped nlember 22, and the repulsive force of
the second elastic body 33 that is also in compressive deformation is acting on the
25 second ring-shaped member 32. Thereby, the first and the second steel sheets 11 .
and 12 are in close contactbwith each other over a wide area due to the fact that ~iot
only the region in contact with the first electrode body 21 and the second electrode
body 3 1 is pressed, but also the peripheral region therearound (the region in contact
with the first ring-shaped member 22 and the second ring-shaped member 32) is also
30 pressed, Thereby, the generation of sheet separation (the first steel sheet 11 is
separated from the second steel sheet 12 near the portion pressed by the electrode
PCT Application No.: PCT/JP2015/057G56
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tips 21a and 22a) is restrained.
[0099]
With this state being achieved, an electric cmrent is applied between the
first electrode body 11 and the second electrode body 21 by operating the power
5 supply to weld the first steel sheet 11 and the second steel sheet 12.
[O 1001
, FIGS. 6A and 6B are schematic diagrams for describing the situatioa in
which a \veld nugget is formed by spot welding using the resistance spot welding
apparatus illustrated in FIGS. 5A and 5B. FIG. 6A illustrates the case in which the
10 first ring-shaped member 22 and the second ring-shaped member 32 are not
electrically conductive, while FIG. 6B illustrates the case in which the first ringshaped
member 22 and the second ring-shaped member 32 are electrically
conductive. In FIGS. 6A and 6B, dotted arrows represent the flow of welding
current.
15 [OlOl]
As illustrated in FIG. 6A, the contact region between the first and the second
steel sheets 11 and 12 extends in a wide area, encompassing not only the contact
region with the first electrode body 21 and the second electrode body 3 1, but also the
surrounding contact .region with the first ring-shaped member 22 and the second
20 ring-shaped member 32. Thereby noticeable sheet separation does not occur.
Thus, when an electric cu~~eins ta pplied between the first electrode body 21 and the
second electrode body 31, the electric current flows it1 a wider area as compared to
known spot welding. . . .
[O 1021
25 Especially \~11e1l the first ring-shaped member 22 and the second ringshaped
nlember 32 are electrically conductive, the flow of the electric currenb'spreads
to an even wider area in the first and the second steel sheets 11 and 12 as illustrated
in FIG. 6B. More specifically, the electric current not only spreads in a central area
and flows from the first electrode body 21 to the second electrode body 31, but also
. 30 is drawn from first electrode body 21 toward the first ring-shaped member 22, and
then drawn toward the second ring-shaped nletllber 32, and finally towvard the second
PCT Apl~lication No.: PCTIJP2015/057656
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clectrode body 31. This is because both of the first ring-shaped nle~nber2 2 aud the
second ring-shaped member 32 have a high electric conductivity while the first and
the second steel sheets 11 and 12 are in close contact with each other in the region
~vl~etrhee first ring-shaped member 22 and the second ring-shaped member 32 are
5 facing each other due to a strong pressure exerted by the first ring-shaped member 22
and the second ring-shaped tnetnber 32.
[0.103]
In general, expulsion (expulsion at the faying sorface) is generated between
metal sheets. However, a large amount of electric current applying to electrodes
10 may cause the contact portion between the metal sheet and the electrode to be
overheated to generate expulsion (expulsion at the outside surface) from the outer
surface of the metal sheet. The embodiment illustrated in FIG. 6B, in which the
first and the second ring-shaped members 22 and 32 are made electrically conductive,
provides another advantage that the electric current makes a detour from the first and
15 the second electrode bodies 21 and 31 to the first and the second ring-shaped
nlembers 22 and 32 which are electrically-conductive, which can suppress the heat
generation at the contact portion between the electrodes and the metal sheet, and
thereby can suppress the expulsion generation from the outer surface of the metal
sheet.
20 [0104]
Thus, the first and the second steel sheets 11 and 12 are pressed firmly by
the first ring-shaped member 22 and the second ring-shaped member 32 so that the
contact region between the first and the second steel sheets 11 and 12 melts over a
wide area to form the nugget 14 having a large nugget diameter. In addition,
25 according to this spot welding, the appropriate welding current range can be
expanded with the nugget diameter being larger. .I
[0 1051
As described above, the nlethod for manufacturing the welded structure
according to the present etnbodiment provides effects of suppressing the sheet
30. separation, suppressing the expulsion generation, expanding the nugget diameter, and
cxpanding the appropriate welding current range. These effects have been
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described by using the exen~plaryc asc with the steel sheet set illcludillg the first and
the second steel sheets. These effects are not limited to the case of the steel sheet
set including two steel sheets, but can be produced in the case includillg thee steel
sheets. Consequently, not only the welded st~ucture according to the first
5 enlbodiment but also the welded structure according to the second embodiment can
be obtained by the method for lnanufacturing the.welded structure of the present
embodiment.
[0106]
Note that, when the steel sheet set includes thee steel sheets, the exerted
10 pressure, the current value, and the welding current pattern will be properly adjusted
as the need arises. Thereby, nuggets having a large diameter can be formed as is the
case of the steel sheet set having two steel sheets, which will be described in
Example later.
[0107]
15 In order to suppress the sheet separation sufficiently, what is impostant are
the distance between the peripheral edge of the tip face 21aa of the first electrode
body 21 and the inner peripheral edge of the tip face 22a of the first ring-shaped
member 22, and the distance between the peripheral edge of the tip face 3laa of the
second. electrode body 31 and the inner peripheral edge of the tip face 32a of the
20 second ring-shaped me~ilber 32, wvhen the electrode tips 21a and 31a are in contact
with the steel sheet set. These distances are preferably as small as possible as far as
no interference occurs during welding. If these distances are too large, the
suppressing effect of the sheet separation becomes small, and also the electric current
does not easily spread in the case that the first ring-shaped member 22 and the
25 seco~td ring-shaped member 32 are electrically conductive. These distances are
preferablj+.7 tnm or less, Inore preferably 5 nlln or less, and stilk Illore preferably 3
mm or less.
[0108]
One elnbodinlent of the present invention has been described so far, but the
30 present invention can also be i~ilplelnented in other modes. For example, the
welded structure may be a housing of an electric appliance (for example, a copying
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machine) that is manufactured by using a thin steel sheet. In this case, tlic welded
structure according to tlie present invention, for esaniple, may sufficiently absorb an
impact shock so as to protect the inside of tlie appliance when the appliance falls.
5 [Esaniples]
[OI 091
The tests as described below were conducted to coilfir111 tlie effects of the
present invention.
One of the steel sheets A to C (Mat. A to Mat. C) in Table 2 was used in the
10 tests. Table 2 shows the chemical coniposition and the properties of the steel sheet
including thickness, yield strength (YS), tensile strength (TS), and breaking
elongation (El) for each of the steel sheets A to C. All of the steel sheets A to C are
those generally used for the framework members of autotnobiles. As shown in
Table 2, the equivalent carbon content (Ceq) of each of the steel sheets A to C
15 exceeds 0.15 mass%, which has been difficult to be welded without generating
expulsion when known welding methods are used.
20 A*. J
[Table 21
By using tlie resistance spot welding apparatus illustrated in FIGS. 5A and
5B and a known resistance spot welding apparatus, two steel sheets were spot welded
to manufacture corresponding welded structures, and then cross tension tests were
Steel
sheet
conducted on these welded structures.
25 [0112]
Chemical composition (mass%) Properties
(TS is measuredafter buenchinrr
Retnark
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As described above, the resistance spot welding apparatus illustrated in
FIGS. 5A and 5B, wliicli had the first and the second combined electrodes 20 and 30
(hereinafter referred to as "rnovable electrodes"), was configured to sandwich the
material with tlie first and tlie second electrode bodies 21 and 31 and with the first
5 and the second ring-shaped members 22 and 32, to apply an electric current. The
known spot welding apparatus was the one that corresponded to the resistance spot
welding apparatus illustrated in FIGS. 5A and 5B, but excluded the first and the
second ring-shaped members 12 and 22 and the first and the second elastic bodies 23
and 33, and the electrodes corresponding to the first and the second electrode bodies
10 21 and 31 (hereinafter referred to as "normal electrodes") were configured to
sandwich the material to apply an electric cul'rent.
[0113]
In either case, the steel sheets C (2.0 mm in thicktiess) in Table 2 were used
as the two steel sheets. The average thickness per steel sheet t,,,, was 2.0 mn at the
15 lapped portion, and thus the thickness fell in a range from 1.1025 to 2.6 rnm. Spot
welding was carried out with the electric currelit value being varied. The cross
tension tests were condncled in accordance with the method stipulated in Japanese
Industrial Standards (JIS) Z 3137.
[0114]
20 FIG. 12 is a cha~acteristic diagram showing a relation between obtained
nugget diameters d,,, (mm) and average thicknesses la,-,( mm) per material steel sheet
.-when the welded structures are obtained by the method according to present
embodiment. In the welded structure in which two-steel sheets are joined by spot
welding at a plurality of locations, the average thickness on the transverse axis of FIG.
25 . 12-is t,, = (tl + 12) 12, where the thicknesses of the steel sheets at the lapped portion
!;+.in \vliich two steel slieets are overlapped are represent6d by tl and tz.
[01 151
According to the tnatiufacturing method of the present e~nbodiment, the
relation between the nugget diameter d,, (mnl) and the average thickness t a , (mrn)
30 were obtained in the range indicated by hatching in FIG. 12. More specificallj: it
was found that different characteristics in the relation among the nugget diameter d,,
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(nnn), the average thickless t,,, (~rnn)a, nd the tip diameter d (111111) of the electrode
used for spot welding could be obtained 011 the two sides of the boundary of the
average thickness t,,., = 1.1 (mm).
[0116]
5 More spccifically, when 0.5 mm i t,,, < 1.1 mm, the condition (a) below
was obtained.
(a) dng > d(tave)ln (1)
[0117]
In addition, when 1.1 mm i t,, 5 2.6 tntn, the condition (b) below was
10 obtained.
(b) d,, > 1.05d (2)
[0118]
A thin joint in which the average thickness t,., per ~nateriasl teel sheet is less
than 1.1 mm is susceptible to the generation of peel stress at a weld portion because
15 the flexural rigidity is low. To suppress the interfacial peeling caused by the peel
stress at the weld portion, the nugget diameter d,, (mm) needs to be controlled to
satisfy the condition (a). In contrast, when the average thickness t,,, per material
steel sheet is 1.1 mtn or more, the flexural rigidity is high, and thus the interfacial
peeling at a weld portiot~c an be suppressed by providing a nugget diameter d,,, (mm)
20 of more than 1.05d as indicated in the condition (b). Therefore, by satisfying the
conditiot~ (a) or (b), the manufactured welded structure can provide desired
deformation behavior .. . -
[0119]
The welded structures manufactured using the movable electrodes did not
25 - have spatters adhering thereto, but the welded structures manufactured using the
,.{ I . nornlal electrodes had spatters adhering theretb'. ..~FI G. 7 shows a relation between
, the nugget diameter d,,, and the cross tension load P. In FIG. 7, the dotted line
indicates that the nugget diameter equals to 1.05d (d is the tip diameter of the
electrodes used in spot welding). In FIG. 7, the \velded structures according to the
30 present it~ventioat~re those using the tnovable electrodes that satisfy d,, > 1.05d.
[O 1201
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Either case of using the movable electrodes or using the normal electrodes
exhibits a tendency in which the cross teusion load P becomes larger as the nugget
diameter d,,, becomes larger. II-Iowevel; the case of using the tiormal electrodes
exhibits a large dispersion in tlie cross tension load P with the same nugget diameter
d,,,, as conlpared to the case of using the ~novablee lectrodes, and has not necessarily
provided a level of the cross tension load P equivalent to the case of using the
movable electrodes even when d,, > 1.05d is satisfied (for welded structures having
no spatter adhesion). Welded structures without spatter adhesion have stably
exhibited high cross tension loads P as compared to those with spatter adhesion. In
the case of using the movable electrodes, both the spot weld portions that satisfy d,,,
> 1.05d and the spot weld portions that satisfy d,,, i 1.05d have been obtained.
However, the welded structure that satisfies d,, > 1.05d can be stably obtained by
properly setting welding conditions.
(01211
When the nugget diameter d,, cannot be made larger than a certain size,
there arises a limitation in suppressing fiacture at the weld portion. Especially as
the tensile strength of the steel sheet becomes larger, the stress expected at the weld
portion becomes larger. Thus, it is necessary to form strong welds by obtaining a
large nugget diameter d,,. Moreover, as the steel sheet becomes thicker, the stress
expected at the weld potlion becomes larger. Thus, it is also necessary to form
strong welds by obtaining a large nugget diameter dng
[O 1221
In contrast, as tlie tensile strength of the steel sheet becomes larger, the
electric resistance becomes larger accordingly, causing expulsio~tlo occur due to heat
generation during welding. The generation of expulsion causes the nugget diameter
to be smaller and the steel sheet thickness to be smaller, and also makes it difficult to
carry out stable welding. As a result, the welded steel sheets are vulnerable to
peeling. Thus, it is desirable to obtain a larger nugget diameter d,,, while
suppressing the expulsion generation. According to the present embodiment, the
30 steel sheets to be welded are in contact with each other firnlly and securely by
pressing, against the steel sheet, tlie first ring-shaped member 22 included in the first
PCT Al~plication No.: PCTIJP20151057G5G
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combined electrode 20 and the second ring-shaped nlenlber 32 included in the
second combined electrode 30. Thereby, the nugget diameter dng can be reliably
made larger, which causes the strength of the weld portion to be substantially higher.
In addition, when the first ring-shaped nlcnlber 22 and the second ring-shaped
5 member are made electrically conductive, tlie electric current flows in a wide area as
illustrated in FIG. 6B.. This lowers the electric current density, which enables the
generation of expulsion to be securely prevented. Consequently, even if the steel
sheets having a tensile strength of 980 MPa or more are used, the nugget diameter d,,,
that satisfies the condition (a) or (b) can be obtained, and the generation of expulsion
10 can be suppressed, according to the present embodiment. Thereby, the joining
strength of the weld portion can be made considerably larger and tlie peeling at the
weld poaion can be reliably prevented. In other words, when known manufacturing
methods are used, it is difficult to obtain the nugget diameter d,, that satisfies the
condition (a) or (b) especially for the steel sleet having a tensile strength of 980 MPa
15 or more.
[0123]
Moreover, if the movable electrodes according to the present embodiment
are not used, there are not many solutions to enlarge the nugget diameter except for
increasing tlie pressure exerted by the electrodes so as to flow a large amount of the
20 electric current. On the other hand, when the movable electrodes according to the
present embodiment are used, the first ring-shaped member 22 and the second ringshaped
member 32 are pressed against the steel sheet in the peripheries of the first
electrode body 21 and the second electrode body 31, which enables tlie nugget
diameter to be larger while suppressing sheet separation. Thus, while known
25 electrodes exerts a large pressure to cause the gap between the steel sheets to be
wider, the rliovable electrodes according to the present embodiment enables the sheet 2'. .
gap to be sufficiently small by suppressing the sheet separation. Consequently, in
the deformation process in a collision event, the joint forrned of the \veld portion
xvith the larger sheet gap by the knowvn method tends to enter a stress state of peeling
30 tlie weld portion, thns-causing the weld portion to be peeled.off. On the other hand,
the joints having large diameter nuggets formed by tlie ~novablee lectrodes according
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to the present etnbodiment have a sheet gap smaller than that fornied by the known
clcctrodes, thereby securely suppressing the peeling off during deformation in a
collision event.
[0 1241
5
Crushing tests (what is called "dynamic defornlation impact .testsn) were
conducted on the welded structures with the procedure as described below. The
crushing tests were conducted in two different conditions, in other words, bending
deformation conditions and axial crush deformation conditions, which are basic
10 testing modes related to actual automobile collisions.
[0125]
1. Bending Deformation
Hat-channel members and closing plate members formed of the steel sheets
A and B were prepared. FIG. 8 illustrates the shapes and dimensions of the hat-
15 channel member and the closing plate member. As illustrated in FIG. 8, the hatchannel
member, which was 120 tnm in width, 60 lntn in height, and 600 mtn in
length, had 20 mm wide protruding portions (bent portions and flanges) at both sides
in the widthwise direction. The flanges were overlapped and were spot welded with
the closing plate member having the same length and width with the hat-channel .
20 member.
[0 1261
Spot welding was conducted by using the movable electrodes, and also -
using the normal electrodes. The intel-val between weld portions were set at 17.5
mm and 3 5 nun.
25 [0127]
This welded structure was placed on two se~nicylindricajli gs (the curvature-'
radius of the cylindrical portion: 30 mm) with the closing plate menlber facing
upward. At this time, two jigs were positioned in parallel with each other with a
440 nnn spacing therebetween and with each cylindrical portion facing upward.
30 .[0128]
Using a hydraulic compression tester, the se~nicylindrical impactor (the
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curvature radius of the cylindrical portion: 150 mm) was collided f~omab ove against
the mid postion in the longitudinal direction of the welded structure in this state, at a
velocity of 8.6 km/h with the cylindrical portion facing downward.
[0129]
5 On this occasion, the displacement of the inlpactor was measured, and also
the defornlation resistance following the bending defor~nation -was measured by
using piezoelectric load cells built in the impactor. The test displacement, which is
an amount of the impactor movement, was set at 60 nun. Based on the curve of the
deformation resistance against the test displacement, the deformation resistance was
10 integrated with respect to the test displacement (from the point the impactor collided
with the welded stn~cture to the point the impactor moved 45 t m ) to obtain an
absorbed energy U when the welded stri~cturew as subjected to bending deformation.
[0130]
FIG. 9 shows a relation between the nugget diameter d,, and the absorbed
15 energy U. As shown in FIG. 9, in either case of using the steel sheet A (Mat. A) or
of using the steel sheet B (Mat. B), the absorbed energy U generally becomes larger
as the nugget diameter d,, becomes larger. When the steel sheet A is used and the
nugget diameter dng exceeds 1.05d, the absorbed energy U stably exhibits high values.
[0131]
20 When the steel sheet A is used, the difference in the interval between the
weld portions does not cause the absorbed energy U to become largely different. In
the case of using the steel sheet B, when the welded structures using the movable
electrodes are compared with each other, the welded structures having an interval of
17.5 nnn tend to exhibit higher absorbed energies as compared to the nrelded
25 structures having an interval.of 35n1m. As shown in Table 2, the steel sheet B has
an equivalent carbon co~ltent higher than that of the steel sheet A. When a\,.steel
sheet ivith a high equiva1ent:carbon content (for exatnple, a steel sheet with Ceq >
0.3) is used, it is preferable to make the interval smaller to obtain a suficiently high
absorbed energy.
30 [0132]
2. Axial Crush Deformation
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Hat-channel members aud closing plate members formed of the steel sheets
C (having a thicluiess of 1.6 mm) were prepared. FIG. 10 illustrates the shapes and
dimensions of the hat-channel member and the closing plate member. As illustrated
in FIG. 10, the hat-channel member, which was 120 mnl or 126 in width, 60 mm iu
5 height, and 300 nlm in length, had 20 mm or 23 nnn wide protruding portions @ent
portions and flanges) at both sides in the widtl~wise direction. The length of each
bent portion in the widthwise direction of the hat-channel member is 5 nnn, and thus
the width of the flauge is 15 nlm or 18 mm. The flanges were overlapped and were
spot welded wit11 the closing plate member having the same letlgth and width with
10 the fiat-channel member.
[0133]
Spot welding was conducted by using the tnovable electrodes, and also
using the normal electrodes. The interval between weld portions were set at 35 mnl.
[0134]
15 The axial direction of the welded structure was aligned to a vertical
direction, and then the falling weight having a mass of 850 kg was fallen freely from
a height of 4.83 111 and was collided from above against the welded structure in the
axial direction thereof at a velocity of 35 kmlh. On this occasion, the displacement
of the falling weight was measured, and the deformation resistance of the welded
20 sttucture was also measured by using piezoelectric load cells. Based on the curve
of the deformation resistance against the displacement of the falling weight, the
deformation resistance was integrated with respect to the displacement of the falling
weight (from the point the falling weight collided with the welded structure to the
' point the falling weight moved 200 mnl) to obtain an absorbed energy U when the
25 welded structure was subjected to axial crush deformation.
[0135] I , _ *'-
FLG. 11 sho\vs a relation between the nugget diameter d,, and the absolbed
energy U. In the legend in FIG. 11, "If = 20 mm" represents the case where a flange
width is 20 tnm, and "lf= 23 n1111' represents the case where a flange width is 23 mm.
30 .As illustrated in FIG. 11, the absorbed energy U generally becomes larger as the
nugget diameter d,, becomes largel; and the absorbed energy U stably exhibits high
PCT Al~plication No.: PCT/JP2015/067G56
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values xvllen the ilugget diameter dng exceeds 1.05d.
[0136]
Incidentally, while the welding using the movable electrodes described
above is used as a main joining method, laser welding or adhesion may be used
5 together as an auxiliaty joining method. In this case, an adhesive such as an
electrically conductive weldbond, etc., can be used.
[0137]
It should be understood by those skilled in the art that various tnodificatiotls,
conlbinations, sub-combinations and alterations may occur depending on design
10 requirements and other factors insofar as they are within the scope of the appended
claims or the equivalents thereof.
Reference Signs List
welded structure
first steel sheet
second steel sheet
third steel sheet
.spot weld portion
nugget
indentation
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CLAIMS
Claim 1
A welded structure including two or three steel sheets and a lapped portion
in wllich the steel sheets are overlapped and joined by spot welding at a plurality of
5 locations, the welded structure connprising:
a spot weld portion, and, when a diameter of a nugget is d,,, (mm), a tip
diameter of an electrode used by the spot welding is d (mm), and an average
thickness per steel sheet of the steel sheets at the lapped portion is t,., (mm), the spot
weld portion satisfies a condition (a) or a condition (b) below in accordance with the
10 average thickness t,, (mnl).
(a) d,, > d(t,,,)ln when 0.5 lmn 5 ta,-, < 1.1 nlm (1)
(b) d,, > 1.05d when 1.1 lnnl 5 t,,, 5 2.6 mm (2)
Claim 2
15 The welded structure according to claim 1,
wherein the welded structure includes an expected deformation region to be
subjected to plastic deformation wl~ehen a load is applied, and the spot welding is
carried out at least within the expected deformation region.
20 Clairn 3
T11e welded structure according to claim 1 or 2,
wherein the expected deformation region is free from spatter adhesion.
Claim 4
25 The welded structure according to any one of clai~ns1 to 3,
.:, \vherein the steel sheets ha\7e a tensile strength of 980 MPa or more
, .
Claim 5
The welded structure according to any one of claims 1 to 4,
30 \\herein the electrode is a combined electrode having an electrode body to
be pressed against the steel sheets at the lapped portion and a ring-shaped lne~nbetro
PCT Application No.: PCTlJP20151057G5G
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be pressed against the steel sheets around the electrode body.
Claitn 6
The welded structure according to claim 5,
wherein the movable electrode includes:
a first ring-shaped nlember and a second ring-shaped member to be
pressed against the steel sheets at the lapped pol-tion with the first ring-shaped
member and the second ring-shaped member facing each other; and
a first electrode body and a second electrode body, each being
10 inserted in a though hole disposed each of the first ring-shaped member and the
seco~ld ring-shaped member, to be pressed against the steel sheets at the lapped
portion with the first electrode body and the second electrode body facing each other,
and
wherein an electric current flows through the steel sheets between the first
15 electrode body and the second electrode body.
Claim 7
The welded structure according to any one of claitns 1 to 6,
wherein the spot weld portion satisfying the condition (a) or the condition
20 (b) is present in a 20 to 60% extent on the welded structure.
Claim 8
The welded structure according to any one of claims 1 to 7,
wherein the spot weld portion has an equivalent carbon content (Ceq) of
25 0.13 mass% or more, the equivalent carbon content (Ceq) being defined by an
equation (3) below: . .
Ceq = [C] + 1/90 [Si] + 1/100 ([Mn] + [Cr])(3)
wl~ere
[C]: an average C content (mass%) of the spot weld portion;
[Si]: an average Si content (mass%) of the spot weld portion;
MI^]: an average Mn conte~l(tm ass%) of the spot weld portion; and
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[Cr]: an average Cr content (mass%) of tllc spot \veld portion.
Claim 9
The welded structure according to any one of clai~lls2 to 8,
wherein the welded structure is a member to be used for an automobile, and
the expected deformation region is to be subjected to an axial compression load..
Claim 10
The welded structure according to any one of claims 2 to 9,
10 wherein the welded structure is a member to be used for an automobile, and
the expected deformation region is to be subjected to a bending load.
Claim 11
A method for manufacturing a welded structure including two or three steel
15 sheets and a lapped portion in which tlie steel sheets are overlapped and joined by
spot welding at a plurality of locations, the method comprising:
carrying out spot welding, the carrying out spot welding including
a first step in which a first rod-shaped electrode body and a second
rod-shaped electrode body are arranged facing each other with the lapped portion
20 being sandwiched therebetween, and a first ring-shaped member and a second ringshaped
member are arranged facing each other, the first ring-shaped member having
. . a tlnough hole through ~vllicht he first electrode body is inserted and a back end to
which a first elastic body is co~ulecteda nd the second ring-shaped member having a
through hole through \vhich the second electrode body is inserted and a back end to
25 which a second elastic body is conllected, and
.,. a second step in which the lapped portion is pressurized by pressing +.
a tip face of each of the first electrode body and the second electrode body against
the lapped portion, and by pressing a tip face of each of the first ring-shaped member
and the second ring-shaped member against the lapped po~tionw hile the first elastic
30 body exerts a pressing.pressure on the first ring-shaped member and .the second
elastic body exerts a pressing pressure on the second ring-shaped member, and then
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. an electric current is applied between the first electrode body and the second
.. .
electrode body, -2
' wherein the first step and the second step cause a spot weld portion to
satisfy a condition (c) or a condition (d) below in accordance with an average
5 thickness t,,, (mm):
(c) dng > d(tnve)'" when 0.5 mrn 5 t,,, < 1.1 - mm (4); (d)dn,>1.O5dwhen 1.1 mm_