DESCRIPTION
Title of Invention: Lap Welding Method, Lap Joint,
Production Method of Lap Joint, and an Automobile Part
5
Technical Field
[OOOl] The present invention relates to lap welding of
a plurality of steel sheets, a lap joint formed by that
lap welding and a method of production of the same, and
10 an automobile part having that lap weld joint.
Background Art
[0002] Up until now, in structures formed using a
plurality of steel sheet members, resistance spot welding
has been used to join superposed steel sheet members in
15 accordance with the function and usage environment.
Forming spot welds having nuggets so as to form a lap
welded member comprised of a plurality of steel sheet
members has been a common practice. For example, in an
automobile body having a monocoque structure, to improve
20 impact safety and fuel efficiency, the general practice
has been to superpose high strength steel sheets and join
the flanges (superposed parts) by resistance spot
welding.
[0003] In recent years, in the assembly of car bodies,
25 remote laser welding has come to be used instead of the
conventionally used resistance spot welding. Remote laser
welding drives a galvanomirror to enable freedom of
welding within a predetermined three-dimensional area.
With remote laser welding, the galvanomirror attached to
30 the front end of a robot arm can be moved quickly between
welding points, so the welding tact time can be greatly
shortened. Further, with remote laser welding, there is
no shunting of welding current to existing welds such as
with resistance spot welding, so it is possible to
35 shorten the pitch between welds. The rigidity of the car
body is also improved due to multipoint welding.
[0004] Remote laser welding is used in place of
resistance spot welding, so usually a substantially
circular laser weld, that is, a circular shape, oval
shape, circular ring shape, oval ring shape, C-shape,
long C-shape, multiple circular ring shape, or other
5 welding shape, is used.
[0005] On the other hand, as the material forming a
car body, in recent years, high strength steel sheet has
been increasingly used. Cold pressed parts and hot
pressed parts (hot stamped parts) of tensile strength
10 1500 MPa or other 1180 MPa or higher class high strength
steel sheets have also come into use. For this reason, in
the future, application of remote laser welding to 1180
MPa or higher class high strength steel sheet will be
sought.
15 [0006] However, such high strength steel sheet has a
metal structure mainly comprised of hardened martensite,
so the surroundings of a laser weld are tempered,
tempered martensite is formed, and the hardness falls.
For example, in the case of 1500 MPa class high strength
20 steel sheet, the hardness of the matrix material is Hv460
or so, but the hardness of the heat affected zone around
a laser weld (hereinafter called "HAZ") locally falls to
Hv300 or so and that part softens. This locally softened
part is called a "HAZ softened part".
25 [00071 Such a HAZ softened part sometimes becomes the
starting point of break of a steel sheet forming the car
body at the time of impact of the vehicle. For example,
in the case of a center pillar obtained by laser welding
1500 MPa class steel sheet to a flange as a reinforcement
30 , member, in a side collision test, sometimes a crack
*starts from the HAZ softened part of,the flange and the
center pillar breaks.
[OOOE] The phenomenon of breakage starting from the
HAZ softened part formed by this laser welding remarkably
35 occurs in a high strength steel sheet with a tensile
strength of over 1180 MPa. In particular, it is
remarkable in a laser weld of a tensile strength 1180 MPa
or more high strength steel sheet formed with a hardened
structure by a continuous annealing facility having a
water cooling function or a high strength steel sheet
formed by hot stamping (hot pressing). Remote laser
welding enables the pitch between welds to be shortened
so forms a large number of welds at a flange. However, if
forming a large number of laser welds, a large number of
HAZ softened parts are also formed, so that risk of break
rises.
[0009] No countermeasures against break due to a HAZ
softened part formed in a high strength steel sheet have
been reported up to now. However, it has been reported
that a similar phenomenon also occurs in the case of
resistance spot welding.
[OOlO] NPLT 1 discloses treating a part in an A-pillar
formed by hot stamping where there is a risk of break
upon impact by heat treating it at the time of hot
stamping so as to lower the strength of the matrix
material and thereby inhibit HAZ softening resulting from
resistance spot welding. Due to this, it is possible to
prevent break of a structural member starting from the
HAZ softened part.
[OOll] NPLT 2 discloses the method of tempering the
flange part of a B-pillar formed by hot stamping by high
frequency heating so as to lower the strength of the
matrix material so that HAZ softening does not occur even
if performing resistance spot welding and thereby
preventing break of the structural member starting from
the HAZ softened part.
[0012] Further, as similar art, for example, PLT 1
discloses the art of combining laser welding and spot
welding to ease the stress of a weld and suppress delayed
break when welding high strength steel sheets to form a
structural member for an automobile. PLT 2 discloses the
art of laser welding a metal material to form a
continuous weld along spot welds as art for improving the
joint by welds. Furthermore, PLT 3 discloses the art of
laser welding a spot weld or the surroundings of a spot
weld as art for improving the joint strength of a weld.
Citation List
Patent Literature
[0013] PLT 1. Japanese Patent Publication No. 2008-
178905A
PLT 2. Japanese Patent Publication No. 2009-241116A
PLT 3. Japanese Patent Publication No. 2010-264503A
Nonpatent Literature
[0014] NPLT 1. Tailored Properties for Press-Hardened
Body Parts, Dr. Camilla Wastlund, Automotive Circle
International, Insight edition 2011, Ultra-high strength
steels in car body lightweight design - current
challenges and future potential
NPLT 2. Tempering of hot-formed steel using induction
heating, Olof Hedegard, Martin Aslund, Diploma work No.
54/2011 Chalmers University of Technology, Gothenburg,
Sweden (URL:
http://publications.lib.chalmers.se/records/fulltext/
144308.pdf) )
Summary of Invention
Solution to Problem
[00151 With the method of adjusting the strength for
each portion of an A-pillar as disclosed in NPLT 1, low
strength parts are unavoidably formed over a relatively
wide range of the A-pillar. For this reason, the effect
of hot stamping of imparting a high strength cannot be
sufficiently enjoyed and the effect of lightening the
weight also becomes limited. In addition, with this
method, there are wide transitional regions between the
hardened regions and nonhardened regions, the strength
characteristics become uneven, and the impact performance
of the A-pillar can become spotty.
[0016] With the method of tempering by high frequency
heating after hot stamping as disclosed in NPLT 2, the
thermal strain caused by the high frequency heating may
cause the B-pillar to deform and the dimensional
precision to drop. This is not limited to a B-pillar.
Dimensional precision also has to be secured for
structural members arranged around the door opening such
as A-pillars and roof rails so that the clearances with
5 for example the door panels become uniform over the
entire circumferences of the door panels. If the
dimensional precision of structural members arranged
around the door openings falls, the quality of appearance
of the vehicle can no longer be secured. For this reason,
10 it is difficult to apply the art disclosed in NPLT 2 to
the structural members around door openings.
[0017] Note that, it may be considered to design the
B-pillar and other structural members so that the HAZ
softened parts of the spot welds will not reach the
15 breakage strain at the time of impact. However, such
design will lead to an increase of thickness of the steel
sheets forming the structural members and addition of
reinforcement members and therefore will increase the
cost and weight of the car body.
20 [0018] The art disclosed in PLT 1 is the art of
inhibiting delayed break due to hydrogen embrittlement
occurring right after continuous laser welding for
joining superposed steel sheets. Hydrogen embrittlement
is caused by the residual stress or strain accompanying
25 welding concentrating at the starting and terminal ends
of laser welding and the dissolved hydrogen in the steel
concentrating there. Therefore, to prevent deformation of
the steel sheets and ease the residual stress or strain,
it is proposed to tack weld the sheets etc. at the
3 0 scheduled positions for laser welding to suppress
deformation of the steel sheets. That is, this art
relates to suppressing deformation of the steel sheets
arising in continuous laser welding and dealing with
delayed break caused by hydrogen embrittlement and does
3 5 not relate to replacing resistance spot welding and
dealing with breakage due to the HAZ softened parts
around substantially circular laser welds for joining
superposed steel sheets.
[0019] The art disclosed in PLT 2 also performs
resistance spot welding before performing continuous
laser welding to thereby function as fastening means for
5 joining superposed parts. That is, this art is also art
for suppressing deformation of the steel sheets arising
in continuous laser welding and does not relate to
replacing resistance spot welding and dealing with break
caused by the HAZ softened parts around substantially
10 circular laser welds for joining superposed steel sheets.
[0020] The art disclosed in PLT 3 successively
performs spot welding and laser welding so that even when
a spot weld cannot be formed between a thick steel sheet
adjoining a surface side steel sheet and that surface
15 side steel sheet among two or more steel sheets, the
laser welding enables the surface side steel sheet and
this thick steel sheet to be welded for reliable lap
welding. That is, this art also does not relate to
replacing resistance spot welding and dealing with break
20 caused by the HAZ softened parts around substantially
circular laser welds for superposing steel sheets.
[0021] In the above way, as the joint for superposing
steel sheets including a high strength steel sheet (in
particular, 1180 MPa or higher class steel sheet),
25 application of laser welding has been sought for
replacing resistance spot welding. Despite this, no
effective measure has been devised for dealing with
breaks caused at the HAZ softened parts. The present
invention was made in consideration of such a situation
30 and has as its object to inhibit breaks due to fractures
arising at HAZ softened parts even when performing laser
welding for joining a plurality of superposed steel
sheets including a high strength steel sheet. In
particular, it has as an urgent object to devise
35 effective measures inhibiting break at low strain at the
time of application to pillars and other impact resistant
structural members of automobiles. Below, in this
Description, laser welding for joining superposed steel
sheets will be called "laser lap welding" and the welded
parts will be called "laser lap welds". Further, in this
Description, unless particularly indicated otherwise,
5 1180 MPa or higher class steel sheet will be called "high
strength steel sheetN.
Solution to Problem
[00221 The inventors etc. engaged in in-depth studies
for solving the above problems and as a result discovered
10 that by firing a laser beam cutting across a
substantially circular laser lap weld up to the outside
of the HAZ softened part and forming a rehardened part,
it is possible to inhibit concentration of strain at the
HAZ softened part and inhibit break at the HAZ softened
15 part. The inventors etc. engaged in further studies and
obtained the following findings.
[0023] (a) They discovered that by firing a laser to
reheat and harden a HAZ softened part formed by laser lap
welding, it is possible to raise the once softened part
20 in hardness, eliminate the softened part, and thereby
inhibit break starting from this HAZ softened part. They
also discovered that it is sufficient to harden the HAZ
softened part by reheating by firing a laser. That is, it
is possible to fire a laser to melt and solidify that
25 part, but melting and solidification are not necessarily
required. In this Description, hardening by firing a
laser will be called "laser hardening" and the hardened
part will be called the "laser hardened part".
[0024] (b) They discovered that hardening by reheating
30 should be performed in a substantially straight line in
the principal stress direction. In this Description, the
maximum stress direction will be called the "principal
stress direction". The strain at this time will be called
the "main strain". Usually, an impact resistant member
35 using high strength steel sheet as a reinforcement member
is determined by the direction in which the impact stress
is applied. In a pillar and other members of an
automobile, the long direction of the flange becomes the
principal stress direction. Therefore, it is sufficient
to take measures to inhibit fracture.in this direction.
[0025] (c) They discovered that a softened part is
5 also formed around a laser hardened part and that the
terminal end (ending end) becomes a starting point of new
fracture, but the curvature of this terminal end is
smaller compared with the HAZ softened part of the laser
lap weld, so fracture can be remarkably suppressed. That
10 is, since the laser is fired in the principal stress
direction in a straight line, the part becoming the
starting point of fracture becomes a softened part formed
at the terminal end of the laser hardened part. The
inventors etc. conducted experiments and confirmed that a
15 softened part is formed at the outside from the laser
hardened part by 1 mm or so. That is, the radius of
curvature of the softened part of the terminal end
depends on the laser scan width. Compared with the circle
equivalent diameter (radius of curvature) of a
20 substantially circular shape laser lap weld, the radius
of curvature of the terminal end of the laser hardened
part (laser scan width) is small. The length of an arc
when viewed by a certain center angle is proportional to
the radius of curvature. Therefore, the length of the arc
2 5 at the terminal end of the laser hardened part when
making the center angle the same as the center angle of
the part of the HAZ softened part restored in hardness
due to the laser lap welding becomes remarkably shorter
compared with the length of the part of the tJAZ softened
30 part restored in hardness. For this reason, by performing
straight'line laser hardening in the principal stress
direction, it is possible to greatly suppress the
occurrence of fracture. Usually, the diameter of a laser
lap weld made in a substantially circular shape is 2 to
35 15 mm or so. On the other hand, the laser scan width at
reheating (same as beam diameter) is 0.15 to 0.9 mm or
so. Therefore, if the laser scan width at the time of
reheating is smaller than the diameter of the laser lap
welding (radius of curvature of part through which
hardened part runs), it is possible to obtain a fracture
inhibiting effect. In particular, if the laser scan width
5 is 50% or less of the diameter of the laser lap weld
(radius of curvature), fracture due to the softened part
can be remarkably suppressed. More preferably, the width
should be made 40% or less, still more preferably 30% or
less. On the other hand, if making the laser scan width
10 too narrow, the effect of inhibiting fracture at the HAZ
softened part falls. For this reason, the laser scan
width should be at least 10% of the diameter of the laser
lap welding (radius of curvature of part through which
hardened part passes). More preferably, it should be 20%
15 or more.
[0026] (d) The most softened part of laser lap welding
is formed at 1 to 2 mm or so at the outside of the melted
part. For this reason, the length of the laser hardened
part must be made 3 mm or more from the outer edge of the
20 laser lap weld. Preferably, the length of the laser
hardened part may be made 5 mm or more from the outer
edge of the laser lap weld, if possible 6 mm or more.
[0027] (e) The reheating temperature by the laser
firing action (hardening temperature) may be the A3 point
25 of the steel sheets or more. When firing a laser for
heating, if stopping the operation, the sheets are
rapidly cooled, so once reaching a temperature of the A3
point or more, hardening occurs. Further, there is no
problem even if once making the material melt. If making
3 0 it melt once, the chemical components of the assembled
steel sheets become diluted, but stress concentrates at
the most softened part formed at the outer circumference
and the problem remains of forming the starting point of
fracture .
35 [00281 (f) Based on the above findings, the inventors
etc. prepared test pieces where a laser was fired in a
straight line in the principal stress direction cutting
across.the HAZ softened part of the laser lap welding and
ran tensile tests, whereupon they confirmed that the
elongation at break became greater compared with the case
of just la,ser lap welding (FIG. 4). That is, they
5 confirmed that the problem of low strain breakage could
be resolved.
[0029] The present invention was made based on the
above findings and has as its gist the following:
[0030] (1) Lap welding method comprising superposing a
10 plurality of steel sheets and firing a laser to form a
substantially circular laser weld, which lap welding
method firing the laser in a straight line through an
outer edge of the substantially circular laser weld so as
to form a hardened part at the steel sheets.
15 (2) The lap welding method according to (1) wherein the
straight line laser firing operation fires the laser in a
principal stress direction found in advance.
(3) The lap welding method according to (1) or (2)
wherein the straight line laser firing operation fires
20 'the laser over at least 3 mm from an outer edge of the
substantially circular laser weld.
(4) The lap welding method according to any one of (1) to
(3) wherein the "substantially circular" is a circular
shape, oval shape, circular ring shape, oval ring shape,
25 'c-shape, long C-shape, or multiple circular ring shape.
(5) The lap welding method according to any one of (1) to
(4) wherein a fired width of the straight line laser
fired part is smaller than a curvature diameter of the
part of the outer edge of the substantially circular
3 0 1ase.r weld through rsrhich the laser is fired in a straight
line:. ---
(6) The lap welding method according to any one of (1) to
(5) wherein at least one steel sheet among the plurality
of steel sheets is a steel sheet having a martensite
3 5 structure.
(7) The lap welding method according to (6) wherein the
steel sheet having a martensite structure is a steel
sheet having a tensile strength of 1180 MPa or more.
(8) A lap joint obtained by superposing a plurality of
steel sheets and firing a laser to form substantially
circular laser weld so as to join the plurality of steel
5 sheets, which lap joint provided with a hardened part
formed in a straight line by firing the laser through an
outer edge of the substantially circular laser weld.
(9) The lap joint according to ( 8 ) , wherein the straight
line hardened part is formed in a principal stress
10 direction found in advance.
(10) The lap joint according to (8) or (9) wherein the
straight line hardened part is formed over at least 3 mm
from an outer edge of the substantially circular laser
weld.
15 (11) The lap joint according to any one of (8) to (10)
wherein the "substantially circular" is a circular shape,
oval shape, circular ring shape, oval ring shape, Cshape,
long C-shape, or multiple circular ring shape.
(12) The lap joint according to any one of (8) to (11)
20 wherein a fired width of the straight line hardened part
is smaller than a curvature diameter of the part of the
outer edge of the substantially circular laser weld
through which the straight line hardened part crosses or
contacts.
25 (13) The lap joint according to any one of (8) to (12)
wherein at least one steel sheet among the steel sheets
is a steel sheet having a martensite structure.
(14) The lap joint according to (13) wherein the steel
sheet having a martensite structure is a steel sheet
30 having a tensile strength of 1180 MPa or more.
--i15) A method of production of a lap'3oint produced by
superposing a plurality of steel sheets and firing a
laser to form a substantially circular laser weld, which
method of production of a lap joint fires the laser in a
35 straight line through the outer edge of the substantially
circular laser weld so as to form a hardened part at the
steel sheets.
(16) An automobile part provided with a lap joint
according to any one of (8) to (14).
[0031] Note that, the shape of the laser lap welding
according to the present invention is not particularly an
issue. However, the shape of laser lap welding for
replacing the usual resistance spot welding is
substantially circular. The "substantially circular"
referred to here is a circular shape, oval shape,
circular ring shape, oval ring shape, C-shape, long Cshape,
or other combination of arcs or further a multiple
circular ring shape or multiple combination of arcs.
Further, the present invention can also be applied to
laser welding for filling in the insides of these.
Furthermore, while not generally used, the present
invention can also be applied to a shape not
substantially circular. For example, it may also be a
triangular shape, rectangular shape, or other polygonal
shape.
Advantageous Effects of Invention
[0032] According to the present invention, even when
superposing a plurality of steel sheet members and
joining them by laser lap welding, no starting points of
fracture will be formed at the HAZ softened parts around
the laser lap welds and the members can be kept from
breaking at a low strain. For this reason, for example,
it is possible to provide' a high strength automobile part
which has impact resistance excellent for performance in
protecting passengers at the time of impact.
Brief Description of Drawings
[0033] [FIGS. 11 FIGS. 1 show a tensile test piece,
wherein FIG. 1A shows the piece as a whole and FIG. 1B
shows a cross-section along a centerline of the test
piece.
[FIGS. 21 FIG. 2A is a view showing a position for
investigation of hardness in a circular shape laser weld
at a 1310 MPa class steel sheet, while FIG. 2B is a view
showing a hardness distribution of a circular shape laser
weld.
[FIG. 31 FIG. 3 is a view showing a break at a HAZ
softened part of a circular shape laser weld.
[FIGS. 41 FIG. 4A is a view showing a laser weld joint of
a comparative example in a tensile test, FIG. 4B is a
view showing a laser weld joint of Invention Example 1,
FIG. 4C is a view showing a laser weld joint of Invention
Example 2, and FIG. 4D is a graph of load-elongation of
the comparative example, Invention Example 1, and
Invention Example 2 in a tensile test.
[FIGS. 51 FIG. 5A is a view showing a break position in a
tensile test of Invention Example 1, while FIG. 58 is a
view showing a break position in a tensile test of
Invention Example 2.
[FIGS. 61 FIG. 6A to FIG. 6G are views showing examples
of an embodiment of the present invention.
[FIGS. 71 FIG. 7A to FIG. 75 are also views showing
examples of an embodiment of the present invention.
[FIG. 81 FIG. 8 is a view showing an example of
application of the present invention to a center pillar.
[FIG. 91 FIG. 9 is a view showing an example of
application of the present invention to a side sill.
[FIG. 101 FIG. 10 is a view showing an example of
application of the present invention to an A-pillar and
roof rail.
[FIGS. 111 FIG. 11A is a view showing a tensile test
piece obtained by C-shape laser lap welding, FIG. llB is
a viexd shoriing a laser lap weld of a comparative example,
FIG. 11C is a view showing a laser lap weld according to
an invention example, and FIG. 11D is a graph showing
results of a tensile test.
[FIGS. 121 FIG. 12A is a view showing a break position of
a comparative example, while FIG. 12B is a view showing a
break position of an invention example.
[FIGS. 131 FIGS. 13 are views showing the hardness
distribution of a C-shape laser lap joint in an invention
example, wherein FIG. 13A is a view showing a position of
measurement of the hardness distribution of the lap joint
according to the present invention, F I G . 138 is a view
showing the hardness distribution of a terminal end of a
straight line laser scanned part, F I G . 13C is a view
showing a hardness distribution of an intermediate part
of the straight line laser scanned part, and F I G . 13D is
a view showing a hardness distribution of a substantially
circular laser lap weld.
Description of Embodiments
[0034] First, a welding method using a laser beam
according to the present invention will be explained.
[0035] The laser welder is not particularly limited.
As examples, a disk laser, fiber laser, YAG laser, and COz
gas laser can be used. A beam diameter of 0.15 to 0.9 mm
in range, an output of 1 to 10 kW in range, and a welding
speed of 1 to 25 m/min in range can be illustrated. The
conditions for laser welding are suitably determined by
the types of the steel sheets, the thicknesses of the
steel sheets, etc. and are not limited to the above
illustrations.
[0036] The welding may be general welding by a torch
carried by a robot, but is preferably remote laser
welding using a galvanomirror. "Remote laser welding" is
the art of combining a long focal point focus lens with a
specialized scanning mirror and firing the laser beam
through space to make the laser spot scan the surface at
a high speed to perform welding. Compared with the robot
or NC device used for conventional laser welding, the
beam travel time becomes substantially zero, so high
efficiency welding becomes possible. This system has the
merit of not requiring almost any travel time of the . .
laser spot from a weid location being worked to the next
weld location.
[0037] At the step of forming the hardened part, a
laser beam is fired at the lap part to form a
substantially circular laser weld, then is run across the
HAZ softened part formed around the substantially
circular laser weld (outer circumference) to form a
straight line hardened part and thereby make the HAZ
softened part around the substantially circular laser
weld harden. Therefore, by firing a laser through the
5 outer edge of the laser lap weld in a straight line, it
is possible to form a hardened part so as to split the
HAZ softened part. Here, "through the outer edge of the
laser lap weld" indicates the state of crossing the outer
edge of the laser lap weld or contacting it.
10 [0038] A laser lap weld is a melted and solidified
part shown as shown in F I G . 2B. Therefore, the outer edge
of the laser lap weld indicates the boundary between the
melted and solidified part and the matrix metal. F I G . 2
shows an example where the center part of the circular
15 shape is also made to melt and solidify. F I G . 13 shows a
C-shape, but in this case as well, the laser lap weld is
a melted and solidified part. The thinking is the same.
[0039] F I G . 13A shows an example of laser hardening so
as to cut across a C-shape laser lap weld. This shows the
20 hardness distribution of the surface of a steel sheet in
the direction shown by the dotted line in F I G . 13A. F I G S .
13B, 13C, and 13D show the hardness distributions of the
surface of a steel sheet at the laser hardened part
terminal end (ending end), laser hardened part, and laser
25 lap weld.
[0040] The "hardened part", as shown in F I G . 13C,
indicates the region sandwiched between the local maximum
points of hardness appearing sandwiching a laser scanned
part when measuring the hardness distribution across the
30 laser hardened part. Around a hardened part, a softened
part can be formed due to the heat input at the time of
hardening. In F I G . 13C, there is a part showing the local
minimum value of hardness at the outside of the peak of
hardness. This is the part softened by laser hardening.
35 [00411 The state of hardness of the terminal end
(ending end) of the laser hardened part is shown in F I G .
13B. F I G . 13B is a view showing the hardness distribution
in the laser firing direction. The local maximum point of
the hardness in FIG. 13B is the terminal end (ending end)
of the hardened part. The right side becomes the hardened
part. As will be understood from FIG. 13B there is a part
5 showing the local minimum point immediately to the
outside of the local maximum point of hardness. This is
the part softened by laser hardening.
[0042] Further, the hardened part is preferably formed
at 50% or more of the thickness of the high strength
10 steel sheet (in particular, steel sheet including
martensite structure).
[0043] Further, the straight line hardened part may be
positioned in the principal stress direction envisioned
at the time of impact. Alternatively, when laser welding
15 flange shaped steel sheet members, the direction of
extension of this flange may be made the principal stress
direction. Even if off from the principal stress
direction due to the precision of the laser welding etc.,
the angle of that deviation is preferably as small as
2 0 possible. Therefore, the straight line hardened part is
preferably formed in a range of within f30° with respect
to the principal stress direction. If the hardened part
is formed in a range of within f30° with respect to the
principal stress direction, it can be deemed to have been
2 5 formed in the principal stress direction. More
preferably, the range may be within f15O with respect to
the principal stress direction. Still more preferably,
the range may be within flOo with respect to the principal
stress direction.
3 0 [0044] Note that, the principal stress direction can
be found in advahce at the design stage. The method 0;-
finding the principal stress direction in advance is not
limited. For example, the finite element method (FEM) or
other simulation can be used to find it. Alternatively, a
3 5 model or actual shape test member can be used for testing
to find it. There may also be a plurality of principal
stress directions. In this case, it is sufficient to fire
the laser in a straight line matching each principal
stress direction so as to form hardened parts.
[0045] By firing a laser for reheating so as to form a
5 straight line hardened part, the HAZ softened part around
the substantially circular laser lap weld is split and a
drop in strength in the principal stress direction due to
the HAZ softened part is suppressed. Note that, the
straight line hardened part need only split the HAZ
10 softened part of the laser lap weld, so need not
necessarily be continuously formed in a straight line
inside the laser lap weld.
[0046] The steel sheet to which the present invention
can be applied is not limited. However, HAZ softening
15 remarkably occurs at steel having a martensite structure.
If applying the present invention to such a steel sheet,
the effect is large. As steel sheet having a martensite
structure, there is high strength steel having a 1180 MPa
.or more tensile stress. Such high strength steel is often
20 used for hot stamping (hot press forming) and is
sometimes called "hot stamp-use steel". Further, the
presence or absence of plating is not an issue.
[0047] The lap joint according to the present
invention may be applied to any steel member. In
2 5 particular, the obtained effect is large by application
to an automobile member in which impact resistance is
sought.
[0048] The present invention will be explained based
on specific examples. For example, if the center pillar
30 of an automobile is impacted, a tensile load will be
applied to the flange part where the inner member panel
and outer member panel are lap welded. For this reason,
strain will concentrate at the HAZ softened part of the
circular shape laser lap welded formed at the flange
35 causing it to break. The inventors etc. ran tests
envisioning such a case.
[0049] FIG. 1 is an explanatory view showing a tensile
test piece. A 440 MPa class steel sheet (thickness 1.2
mrn), a 1310 MPa class steel sheet (thickness 1.4 mm), and
a 270 MPa class hot dipped galvannealed steel sheet
(thickness 0.7 mm) were superposed and fastened by
5 resistance spot welding at the gripping parts of the test
piece. Circular shape laser lap welding was performed at
the center part of the test piece. A fiber laser was used
for laser welding under conditions of a beam diameter of
0.6 mm, an output of 2.0 kW, and a welding speed of 2.0
10 m/min so as to form a test piece having a laser lap weld
shown in FIG. 4A of a circular shape of a diameter of
about 7 mm welded inside the circle as well.
[OOSO] FIG. 2A is an explanatory view showing the
position for investigation of hardness of a circular
15 shape laser weld in a 1310 MPa class steel sheet, while
FIG. 2B is an explanatory view showing the hardness
distribution of a circular shape laser weld.
[OOSl] As shown in FIG. 2A and FIG. 2B, in circular
shape laser welding of 1310 MPa class steel sheet, the
20 HAZ around the hardened part was tempered and softened.
[0052] FIG. 3 is an explanatory view showing a break
position of a circular shape laser lap welded joint. When
performing a tensile test, as shown in FIG. 3, it was
learned that strain concentrated at the HAZ softened part
25 around the laser weld of the 1310 MPa class steel sheet
causing it to break.
[00531 FIGS. 4 show a comparative example in the
tensrle test (FIG. 4A), Invention Example 1 (FIG. 4B),
Invention Example 2 (FIG. 4C), and a load-elongation
3 0 graph of the same (FIG. 4D). The comparative example
(FIG. 4A), shows the case of only laser lap rielding.
Invention Example 1 (FIG. 4B) shows the case of firing a
laser in a straight line from an outer edge of the laser
lap welding along the axial direction of the test piece
35 (principal stress direction) to form a hardened part. The
laser was fired from a point 12mm separated from the lap
weld edge and cut across the laser lap weld so as to
extend in a straight line in a length from the point 12
mm separated from the lap weld edge of 31 mm. Invention
Example 2 (FIG. 4C) is the case of forming the laser
hardened part up to the gripping parts of the test piece.
5 It is a test piece designed so that the terminal end of
the laser hardened part does not form a starting point of
fracture. A tensile test was run with a distance between
prepared welds evaluated of 50 mm and a tensile speed of
3 mm/min. FIGS. 5 are explanatory views showing break
10 positions of Invention Example 1 (FIG. 5A) and Invention
Example 2 (FIG. 5B).
[0054] The results of measurement of the elongation at
break are shown in FIG. 4D. It will be understood that
the "comparative example" had an elongation at break of a
15 small one of 2.3% or so and that low strain breakage
occurred. Invention Example 1 had an elongation at break
of 4.3%. Even compared with the comparative example, the
elongation at break was improved over the comparative
example by about 87%. Further, it could be confirmed that
20 the location of break was the terminal end of the laser
hardened part (FIG. 5A). As a result, it could be
confirmed that Invention Example 1 solved the problem of
low strain breakage compared with the comparative
example. Note that, the melted metal part of the lap weld
25 softens due to being mixed with elements of the steel
sheets, but this part is comprised of three steel sheets
superposed and is large in thickness, so does not break
at the me'1te.d metal part.
[0055] For Invention Example 2, the elongation at
30 break was 7.3% or so. Compared with the comparative
exampLe, it was improved about 317%. It cauld be
confirmed that the location of break was the middle of
the laser hardened part (FIG. 5 B ) . That is, it could be
confirmed that the example did not break at the HAZ
3 5 softened part of the lap welding. As a result, it could
be confirmed that Invention Example 2 solved the problem
of low strain breakage compared with the comparative
example and Invention Example 1. Note that, for
observation of the broken surface, the broken surface of
the high strength steel sheet in the test piece (in the
above test piece, the 1310 MPa class steel sheet) was
5 observed.
[0056] FIG. 6A to FIG. 6G are explanatory views
showing various substantially circular laser lap welds 1
to 7 assuming flanges. In this case, the principal stress
direction is the long direction of the flange (left-right
10 direction in the figure). The present invention, as shown
in FIG. 6A to FIG. 6G, can be applied to laser lap
welding of a circular shape 1, oval shape 2, C-shape 3,
long C-shape 4, circular ring shape 5, oval ring shape 6,
and double circular ring shape 7.
15 100571 FIG. 7A to FIG. 7J are explanatory views
showing straight line laser hardened parts 8 formed
cutting across HAZ softened parts formed around circular
shape laser lap welds 1. FIGS. 7 also assume a flange. In
the same way as FIGS. 6, the principal stress direction
2 0 is the long direction of the flange (left-right direction
in the figure).
[0058] As shown in FIG. 7A, the straight line laser
hardened part 8 need not necessarily run through the
center of the circular shape laser weld 1. '
25 [0059] As shown in FIG. 7B, the direction of formation
of the straight line laser hardened part 8 may be within
30° of the assumed principal stress direction.
[0060] As shown in FIG. 7C, the left and right lengths
of the straight line laser hardened part 8 need not
3 0 necessarily be the same, but the laser hardened part 8
has to be formed up to a position sepdrated by at least 3
mm outward from the end of the substantially circular
laser weld 1.
[0061] As shown in FIG. 7D, the end of the straight
3 5 line laser hardened part 8 may be made broader so as to
suppress stress concentration. However, the size has to
be smaller than the circular shape laser weld 1.
[0062] As shown in F I G . 7E, the straight line laser
hardened part 8 may be bent if within f 3 O o of the assumed
principal stress direction.
roo631 As shown in F I G . 7F, a plurality of circular
shaped laser hardened parts 1, 1 were continuously
connected by a single straight line laser weld 8.
[0064] As shown in F I G . 7 G and F I G . 7H, the straight
line laser hardened part 8 need not run through the
inside of the circular shape laser lap weld 1.
[0065] As shown in F I G . 71, there may be a plurality
of laser hardened parts 8. If there are a plurality of
principal stress directions, the laser hardened parts may
be formed in those directions.
[0066] As shown in F I G . 75, the width of the laser
hardened part may also be changed. In particular, as
shown in F I G . 71, the width of the laser hardened part
should be broader than the outer edge of the laser lap
weld and narrower at the terminal end.
[0067] The state of application of the present
invention to an automobile part will be explained next.
F I G . 8 is an explanatory view showing the state of
application of the present invention to a center pillar
9.
[0068] In the process of production of a side panel, a
side panel outer member (not shown) comprised of a 2 7 0
MPa class hot dipped galvannealed steel sheet, a center
pillar reinforcement member 10 comprised of a hot stamped
member, and a center pillar inner member (not shown)
comprised of a 590 MPa class steel sheet are superposed
at flanges formed at their edge parts and resistance spot
welded to tack them by spot welds'~.ll.
[0069] The assembled side panel is assembled with the
under body at the main body line, is tack welded, then is
further welded by remote laser welding.
[0070] At this time, as shown in F I G . 8, circular
shape laser lap welding is performed to form the laser
lap weld 1, then the HAZ softened part around the
circular shape laser lap weld 1 s split by firing a laser
in a straight line to form the laser hardened part 8.
[0071] Note that, as shown in FIG. 8, the operation of
firing a laser for splitting the HAZ softened part around
the circular shape laser lap weld 1 does not have to be
performed for all of the laser lap welds 1. It need only
be performed for a laser lap weld 1 with a possibility of
break at the HAZ softened part.
[0072] FIG. 9 is an explanatory view showing the state
of application of the present invention to a side sill
12. The side sill 12 also, in the same way as the center
pillar 9, is assembled with the under body at the main
body line, tack welded, then increased in welds by remote
laser welding. The side sill 12 is comprised of a sill
inner member panel comprised of a 590 MPa class hot
dipped galvannealed steel sheet, a sill inner member
reinforcement member comprised of a 1180 MPa class hot
dipped galvannealed steel sheet, and a sill outer member
panel comprised of a 270 MPa class hot dipped
galvannealed steel sheet superposed by flanges formed at
their edge parts. At this time, circular shape laser
welding is performed to form the laser lap welds 1, then
a laser is fired to split the HAZ softened parts and form
the laser hardened parts 8.
[0073] FIG. 10 is an explanatory view showing the
state of application of the present invention to an Apillar
13 and roof rail 14.
[0074] As shown in FIG. 10, with the A-pillar 13 and
roof rail 14 as well, like the center pillar 9, a side
panel including the A-pillar 13 and roof rail 14 is
assembled with the under body..by the main body line and
then further welded by remote laser welding. The A-pillar
13 and the roof rail 14 are respectively comprised of
shaped panels comprised of two hot stamped members and a
270 MPa class hot dipped galvannealed steel sheet
superposed. At this time, circular shape laser welding is
performed to form the laser lap welds 1, then a laser is
fired to split the HAZ softened parts around the circular
shape laser lap welds 1 and form the laser hardened parts
8.
[0075] Above, the present invention was explained
based on the example of automobile parts having a
circular shape laser lap welds. As mentioned above, the
embodiments of the present invention are not limited to
the above examples. The effects of the present invention
are exhibited so long as including the requirements of
the present invention. These are included in the scope of
the present invention. Below, examples of embodiments
different from the above will be explained.
Example 1
[0076] Example 1 is an example of application of the
present invention to C-shape laser lap welding. FIG. 11A
is an explanatory view showing a tensile test piece, FIG.
11B is an explanatory view showing a laser weld of a
comparative example, FIG. 11C is an explanatory view
showing a laser weld of an invention example, and FIG.
11D is a graph showing the results of a tensile test.
[00771 For the tensile test piece, three sheets of a
thickness 0.7 mm 270 MPa class hot dipped galvannealed
steel sheet, a thickness 1.4 mm 1310 MPa class steel
sheet, and a thickness 1.2 mm 440 MPa class steel sheet
were stacked in that order and the gripping parts of the
test piece were welded by resistance spot welding to
prepare the tensile test piece shown in FIG. 11A.
[0078] Next, using a fiber laser under conditions of a
beam diameter of 0.6 mm, output of 2.7 kW, and welding
speed of 2.0 m/min and use of a galvanomirror, a test
piece formed with a diameter approximately 7 mm C-shape
laser weld shown in FIG. llB (comparative example) and a
test piece formed with a C-shape weld shown in FIG. 11C,
then fired upon by laser in a straight line (invention
example) were prepared.
[0079] The tensile test was conducted at a tensile
speed of 3 mm/min with the prepared welds at the
evaluation distance 50 mm.
[0080] FIG. 12A is an explanatory view showing a break
position of the comparative example, while FIG. 12B is an
explanatory view showing a break position of an invention
5 example.
[0081] As shown in FIG. 11D, in laser welding a Cshape
of the comparative example, the elongation at break
was 2.7%. Further, as shown in FIG. 12A, the sample broke
along the outer circumference of the C-shape.
10 [0082] As opposed to this, in the invention examples,
as shown in FIG. 11D, the elongation at break was 4.3%.
Further, as shown in FIG. 12B, the break position was at
the front end (terminal end) of the laser hardened part.
[0083] In this way, the invention examples are
*
15 improved in elongation at break compared with the
comparative example.
Industrial Applicability
[0084] The present invention can be utilized for a lap
joint joining steel sheets including a high strength
20 steel sheet. In particular, it can be utilized for
automobile parts and other machine structure parts.
Reference Signs List
[0085] 1. substantially circular (circular shape)
laser weld
2 5 2. substantially circular (oval shape) laser weld
3. substantially circular (C-shape) laser weld
4. substantially circular (long C-shape) laser weld
5. substantially circular (circular ring shape) laser
weld
30 6. substantially circular (oval ring shape) laser weld
7. substantially circular (double circular ring shape) -
laser weld
8. straight line hardened part
9. center pillar
35 10. center pillar reinforcement member
11. spot weld
12. side sill
13. A-pillar
14. roof rail
- 26 -
CLAIMS
Claim 1.
Lap welding method comprising superposing a
plurality of steel sheets and firing a laser to form a
5 substantially circular laser weld, which lap welding
method firing the laser in a straight line through an
outer edge of said substantially circular laser weld so
as to form a hardened part at the steel sheets.
Claim 2.
10 The lap welding method according to claim 1 wherein
said straight line laser firing operation fires the laser
in a principal stress direction found in advance.
Claim 3.
The lap welding method according to claim 1 or 2
15 wherein said straight line laser firing operation fires
the laser over at least 3 mm from an outer edge of said
substantially circular laser weld.
Claim 4.
The lap welding method according to any one of
20 claims 1 to 3 wherein said "substantially circular" is a
circular shape, oval shape, circular ring shape, oval
ring shape, C-shape, long C-shape, or multiple circular
ring shape.
Claim 5.
25 The lap welding method according to any one of
claims 1 to 4 wherein a fired width of said straight line
laser fired part is smaller than a curvature diameter of
the part of the outer edge of said substantially circular
laser weld through which said laser is fired in a
30 straight line.
Claim 6.
The lap welding method according to any one of
claims 1 to 5 wherein at least one steel sheet among said
plurality of steel sheets is a steel sheet having a
35 martensite structure.
Claim 7.
The lap welding method according to claim 6 wherein
said steel sheet having a martensite structure is a steel
sheet having a tensile strength of 1180 MPa or more.
Claim 8.
A lap joint obtained by superposing a plurality of
5 steel sheets and firing a laser to form substantially
circular laser weld so as to join said plurality of steel
sheets, which lap joint provided with a hardened part
formed in a straight line by firing the laser through an
outer edge of said substantially circular laser weld.
10 Claim 9.
The lap joint according to claim 8, wherein said
straight line hardened part is formed in a principal
stress direction found in advance.
Claim 10.
15 The lap joint according to claim 8 or 9 wherein said
straight line hardened part is formed over at least 3 mm
from an outer edge of said substantially circular laser
weld.
Claim 11.
20 The lap joint according to any one of claims 8 to 10
wherein said "substantially circular" is a circular
shape, oval shape, circular ring shape, oval ring shape,
C-shape, long C-shape, or multiple circular ring shape.
Claim 12.
25 The lap joint according to any one of claims 8 to 11
wherein a width of said straight line hardened part is
smaller than a curvature diameter of the part of the
outer edge of said substantially circular laser weld
through which said straight line hardened part crosses or
30 contacts.
Claim 13.
The lap joint according to any one of claims 8 to 12
wherein at least one steel sheet among said steel sheets
is a steel sheet having a martensite structure.
3 5 Claim 14.
The lap joint according to claim 13 wherein said
steel sheet having a martensite structure is a steel
sheet having a tensile strength of 1180 MPa or more.
Claim 15.
A method of production of a lap joint produced by
superposing a plurality of steel sheets and firiny a
5 laser- to form a substantially circular laser weld, which
method of production of a lap joint firing the laser in a
straight line through the outer edge of said
substantially circular laser weld so as to form a
hardened part at the steel sheets.
10 Claim 16.
An automobile part provided with a lap joint
according to any one of claims 8 to 14.