[Technical Field]
[0001] The present invention relates to a structural member for an automotive body, and
more particularly to a structural member for an automotive body obtained by press
forming a forming material made of a steel sheet.
[Background Art]
[0002] An automotive body includes major structural members such as vehicle longitudinal
members that are disposed along a vehicle front-back direction and vehicle widthwise
members that are disposed along a vehicle widthwise direction. The vehicle longitudinal
members and the vehicle widthwise members are joined, in the way that one type of
members have flanges formed at the ends and are joined to the other type of members
via the flanges, to ensure rigidity required for the automotive body and bear the
load in case of a collision event. Such a vehicle is known from
EP 1 908 668 A1.
[0003] The structural members such as the vehicle lengthwise members and the vehicle widthwise
members are required to have properties such as high load transfer capability in the
axial direction, high flexural rigidity, and high torsional rigidity. High load transfer
capability in the axial direction means that deformation is small when the load acts
in the axial direction. High flexural rigidity means that deformation is small against
the bending moment when the longitudinal axis of the member is bent, and high torsional
rigidity means that the angle of torsion is small against the torsional moment when
the member is twisted around the longitudinal axis of the member. In recent years,
a high tension steel sheet having a tensile strength of 390 MPa or more (a high-strength
steel sheet or a high-tensile steel sheet) has tended to be used as a material for
the structural member in an aim to reduce vehicle weight and improve collision safety.
[0004] For example, a floor cross member, which is used to reinforce the floor of an automotive
body, has a cross section substantially shaped like a gutter and is joined to vehicle
longitudinal members such as side sills via outward flanges formed at both ends of
the floor cross member. It is important for the floor cross member to have an increased
joining strength to other members and an increased rigidity to ensure the rigidity
of an automotive body and better load transfer capability when an impact load is applied.
Accordingly, it is necessary not only to increase the material strength but to modify
the shape of the member so as to improve the load transfer capability and the rigidity
when an impact load is applied.
[0005] Patent Literature 1 discloses a structural member for an automotive body manufactured
by press forming. The structural member has a substantially gutter-shaped cross section
as a whole and a groove-like depression in the hat top that is a part corresponding
to the bottom in the gutter-shaped cross section.
[Prior Art Literature(s)]
[Patent Literature(s)]
[Summary of the Invention]
[Problem(s) to Be Solved by the Invention]
[0007] When a groove-like depression (hereinafter referred to as simply "groove") is provided
in the hat top as in the structural member for an automotive body disclosed in Patent
Literature 1, it is likely that the number of load-bearing ridgelines increases, and
thus the amount of energy absorption by the press-formed product is increased. However,
there have been cases in which energy absorption efficiency has not been improved
by simply forming the groove in a top plate in the structural member having a substantially
gutter-shaped cross section.
[0008] FIG. 24 shows a state in which a structural member having a substantially gutter-shaped
cross section with a groove formed in a top plate deforms by receiving an impact load
in the axial direction. FIG. 24 shows that the structural member deforms at each displacement
stroke. This structural member has the groove in the top plate but does not have an
outward flange in the region along each ridge in the longitudinal end, as illustrated
in FIG. 15 (c). As illustrated in FIG. 24, even though the structural member had the
groove, there were cases in which the structural member buckled downward, in other
words, buckled toward the opening of the substantially gutter-shaped cross section
where the rigidity of shape was relatively small, as the displacement stroke became
larger due to receiving a higher impact load. If the structural member is buckled,
the energy absorption stops increasing.
[0009] An object of the present invention is to provide a structural member for an automotive
body that is excellent in load transfer capability and rigidity by effectively enhancing
energy absorption efficiency provided by disposing a groove in a top plate in the
structural member having a substantially gutter-shaped cross section.
[Means for Solving the Problem(s)]
[0010] To solve the problem, according to an aspect of the present invention, there is
provided a structural member for an automotive body, the structural member consisting
of a press-formed product made of a steel sheet, the press-formed product extending
in a predetermined direction, including a top plate, a ridge continuing to the top
plate, and a vertical wall continuing to the ridge, and having a substantially gutter-shaped
cross section intersecting the predetermined direction, the structural member including:
at least one groove formed in the top plate, and extending in the predetermined direction;
and an outward flange formed at least in a region of the ridge in an end in the predetermined
direction. The groove having a depth set according to a width of the groove and a
sheet thickness of the steel sheet.
[0011] The depth (h) of the groove, the width (w) of the groove, and the sheet thickness
(t) of the steel sheet in the end in the predetermined direction satisfy a relation:
0.2 × H
0 ≤ h ≤ 3.0 × H
0, where H
0 = (0.037 t - 0.25) × w - 5.7 t + 29.2.
[0012] The steel sheet may be a high-tensile steel sheet having a tensile strength of 390
MPa or more.
[0013] The steel sheet may be a high-tensile steel sheet having a tensile strength of 590
MPa or more.
[0014] The steel sheet may be a high-tensile steel sheet having a tensile strength of 980
MPa or more.
[0015] The outward flange may be an outward continuous flange continuously formed in a region
over the ridge and at least a part of each of the top plate and the vertical wall,
in the end in the predetermined direction.
[0016] The structural member may include the outward flange in a region of the groove in
the end in the predetermined direction.
[0017] The structural member for an automotive body may be joined to another member via
the outward flange by resistance spot welding, penetration laser welding, arc fillet
welding, adhesion with an adhesive, or a combination thereof.
[Effect(s) of the Invention]
[0018] According to the present invention, the structural member having the outward flange
in at least the end of the ridge enhances energy absorption in the initial stage of
collision. In addition, the structural member having the groove in the top plate and
the outward flange at least in the end of the ridge restrains buckling of the structural
member in the middle and later stage of collision, and thus enhances the energy absorption
effect provided by disposing the groove.
[0019] In addition, the structural member according to the present invention having the
outward flange at least in the end of the ridge can provide a groove having an effective
depth according to the groove width and the sheet thickness. Accordingly, it becomes
easier to form a groove having a desired depth that allows the energy absorption efficiency
to improve, even in press forming the high-tensile steel sheet that is relatively
difficult for press forming. As a result, a structural member having excellent load
transfer capability and rigidity can be obtained with a high production yield.
[0020] Moreover, the structural member according to the present invention, which has the
outward flange at least in the region of the ridge in the end, enables joining to
other members via the outward flange or the flange in the vicinity thereof. Consequently,
this further improves load transfer capability and rigidity.
[Brief Description of the Drawing(s)]
[0021]
[FIG. 1] FIG. 1 is a perspective view illustrating a shape of a structural member
according to an embodiment of the present invention.
[FIG. 2] FIG. 2 (a) is a view in the axial direction illustrating a structural member
according to the present embodiment, and FIG. 2 (b) is a view illustrating another
structural example of a structural member.
[FIG. 3] FIG. 3 is a cross sectional view illustrating a press-forming apparatus for
manufacturing a structural member.
[FIG. 4] FIG. 4 (a) is a perspective view illustrating a die, and FIG. 4 (b) is a
perspective view illustrating a ridge pad. FIG. 4 (c) is a perspective view illustrating
a punch.
[FIG. 5] FIG. 5 (a) is a cross sectional view illustrating a press-forming apparatus
including a pad known in the art, and FIG. 5 (b) is a schematic view illustrating
a state in which a forming material is restrained by a pad known in the art.
[FIG. 6] FIG. 6 is a schematic view illustrating a state in which a forming material
is restrained by a ridge pad.
[FIG. 7] FIG. 7 (a) is an overall plan view illustrating a shape of a developed blank
used in Analysis 1, and FIG. 7 (b) is an enlarged plan view illustrating a longitudinal
end of a developed blank.
[FIG. 8] FIGs. 8 (a) and 8 (b) are a plan view and a view from above in the axial
direction of a structural member used in Analysis 1, respectively.
[FIG. 9] FIG. 9 is a schematic view showing dimensions of a structural member used
in Analysis 1.
[FIG. 10] FIG. 10 is a perspective view illustrating a press-forming apparatus used
in first press forming in Analysis 1.
[FIG. 11] FIG. 11 is a schematic view illustrating first press forming in Analysis
1.
[FIG. 12] FIG. 12 is a perspective view illustrating a press-forming apparatus used
in a second press forming in Analysis 1.
[FIG. 13] FIG. 13 is a schematic view illustrating second press forming in Analysis
1.
[FIG 14] FIGs. 14 (a) and 14 (b) are schematic views illustrating an intermediate
product and a structural member, respectively, which show a maximum decrease rate
of sheet thickness in the vicinity of the edge of a ridge flange and a minimum decrease
rate of sheet thickness near the base of a ridge flange.
[FIG. 15] FIG. 15 (a) is a front elevational view illustrating an analytical model
for a structural member according to the present embodiment, used in Analysis 2, and
FIG. 15 (b) is a front elevational view illustrating an analytical model for Comparative
Example 1. FIG. 15 (c) is a front elevational view illustrating an analytical model
for Comparative Example 2.
[FIG. 16] FIG. 16 is a side view illustrating a shape of each analytical model used
in Analysis 2.
[FIG. 17] FIG. 17 is a graph showing axial load vs. stroke characteristics obtained
from Analysis 2.
[FIG. 18] FIG. 18 is a graph showing amount of energy absorption vs. stroke characteristics
obtained from Analysis 2.
[FIG. 19] FIG. 19 (a) is a graph showing amount of energy absorption vs. stroke characteristics
for an analytical model of Comparative Example 2, obtained from Analysis 3 using a
steel sheet of 340HR, and FIG. 19 (b) is a graph showing amount of energy absorption
vs. stroke characteristics for an analytical model of a structural member according
to the present embodiment, obtained from Analysis 3 using a steel sheet of 340HR.
[FIG. 20] FIG. 20 is a graph showing amount of energy absorption vs. groove depth
characteristics obtained from Analysis 3 using a steel sheet of 340HR.
[FIG. 21] FIG. 21 (a) is a graph showing amount of energy absorption vs. stroke characteristics
for an analytical model of Comparative Example 2, obtained from Analysis 3 using a
steel sheet of 980Y, and FIG. 21 (b) is a graph showing amount of energy absorption
vs. stroke characteristics for an analytical model of a structural member according
to the present embodiment, obtained from Analysis 3 using a steel sheet of 980Y.
[FIG. 22] FIG. 22 is a graph showing amount of energy absorption vs. groove depth
characteristics obtained from Analysis 3 using a steel sheet of 980Y.
[FIG. 23] FIG. 23 is a graph showing normalized amount of energy absorption vs. groove
depth characteristics obtained from Analysis 3.
[FIG. 24] FIGs. 24 (a) to 24 (e) are schematic views illustrating deformation of an
analytical model of Comparative Example 2.
[FIG. 25] FIGs. 25 (a) to 25 (e) are schematic views illustrating deformation of an
analytical model of a structural member according to the present embodiment.
[Mode(s) for Carrying out the Invention]
[0022] Hereinafter, (a) preferred embodiment(s) of the present disclosure will be described
in detail with reference to the appended drawings. In this specification and the appended
drawings, structural elements that have substantially the same function and structure
are denoted with the same reference numerals, and repeated explanation of these structural
elements is omitted.
<1. Structural Member for Automotive Body>
(1-1. Structural Example)
[0023] FIG. 1 is a schematic view illustrating an exemplary structural member (first member)
2 for an automotive body according to the present embodiment. FIG. 2 (a) is a view
on the arrow A in FIG. 1, which is the view in the axial direction of the structural
member (first member) 2 according to the present embodiment.
[0024] A first member 2 is joined to a second member 3 to constitute a joined structure
1. The first member 2 is a press-formed product made of a steel sheet and extends
in a predetermined direction (or referred to as an axial direction) as designated
by the arrow X in FIG. 1. The first member 2 is joined at the axial end to, for example,
a second member 3 that is also a press-formed product made of steel sheet, via outward
continuous flanges 9a, 9b by, for example, spot welding. For example, the first member
2 is joined to the second member 3 by using resistance spot welding, penetration laser
welding, arc fillet welding, or the combination thereof. Joining the first member
1 to the second member 3 may be achieved by adhesion using an adhesive or by the combination
of welding and adhesion. The first member 2 is a long member having a longitudinal
length of, for example, 100 mm or more, preferably 200 mm or more, and more preferably
300 mm or more. The first member 2 illustrated in FIG. 1 has the predetermined direction
that corresponds to the longitudinal direction, but the predetermined direction is
not limited to the longitudinal direction of the first member 2.
[0025] As a forming material for the first member 2, a high-tensile steel sheet having,
for example, a thickness ranging from 0.5 to 6.0 mm and a tensile strength of 390
MPa or more measured by tensile testing in accordance with JIS Z 2241 can be used.
Preferably, a 2.0 mm or less thick high-tensile steel sheet having a tensile strength
of 440 MPa or more can be used as the forming material for the first member 2. Incidentally,
an upper limit of tensile strength, which is not particularly specified here, is,
for example, about 1770 MPa and typically about 1470 MPa. For a material and sheet
thickness for the second member 3, which are not particularly specified here, a steel
sheet having, for example, a thickness of 0.5 to 6.0 mm and a tensile strength of
390 MPa or more can be used.
[0026] The first member 2 illustrated in FIG. 1 can be used as a member constituting a joined
structure 1 of an automotive bodyshell. Examples of the joined structure 1 include
a floor cross member, a side sill, a front side member, and a floor tunnel brace.
When the joined structure 1 is used as the floor cross member, the side sill, the
front side member, the floor tunnel, or the like, it is preferable to use a high tensile
strength steel sheet having a tensile strength of 590 MPa or more, and more preferably
780 MPa or more as the forming material.
[0027] The first member 2 has a substantially hat-shaped cross section that includes a top
plate 4, ridges 4a, 4b continuing to the top plate 4, vertical walls 5a, 5b continuing
to the ridges 4a, 4b, curved sections 6a, 6b continuing to the vertical walls 5a,
5b, and flanges 7a, 7b continuing to the curved sections 6a, 6b. The substantially
hat-shaped cross section is one mode of a substantially gutter-shaped cross section.
It is sufficient that the structural member (first member) 2 according to the present
embodiment has the substantially gutter-shaped cross section including at least the
top plate 4, the ridges 4a, 4b, and the vertical walls 5a, 5b, so that the curved
sections 6a, 6b and the flanges 7a, 7b may be omitted. For example, a U-shaped cross
section is included in the substantially gutter-shaped cross section.
[0028] In the perimeter of an axial end of the first member 2, outward continuous flanges
9a, 9b are formed in the region along the top plate 4, the ridges 4a, 4b, and the
vertical walls 5a, 5b. The outward continuous flanges 9a, 9b are outward flanges without
having notches, which are formed continuously in the region along the part of the
top plate 4 that excludes the region along the groove 8, and in the region along the
ridges 4a, 4b and the vertical walls 5a, 5b. The first member 2 is a member that has
a ridge flange 50a or 50b at least in the region along each ridge 4a, 4b, which makes
the first member 2 different from a known structural member that does not have the
outward flange in the region along the ridges 4a, 4b in the axial end.
[0029] Thanks to the outward continuous flanges 9a, 9b of the first member 2, the ridges
4a, 4b, which receive the axial load, continues to contact surfaces with second member
3. Because of this, the load that the ridges 4a, 4b bear in the initial stage when
an impact load is applied in the axial direction (for example, an amount of displacement
stroke of 0 to 40 mm) becomes larger. Accordingly, the first member 2 is advantageous
in load transfer capability.
[0030] It is sufficient that the width of the outward continuous flange 9a or 9b is at least
1 mm or more to allow for enhancing energy absorption efficiency by forming a groove
8, which will be described later. The width of the outward continuous flange 9a or
9b, however, is preferably 3 mm or more in view of allowing for a welding margin for
laser welding, arc fillet welding, or the like, or preferably 10 mm or more in view
of allowing for a welding margin for spot welding. The width of the outward continuous
flange 9a or 9b is not necessarily constant along all the regions. In view of making
press forming easier, for example, the width of the ridge flange 50a or 50b may be
made smaller than that of the other part of the outward flange. The width of the outward
continuous flange 9a or 9b is adjustable by modifying the shape of a blank into which
the first member 2 is developed on a flat plane (a developed blank).
[0031] Incidentally, the term "outward flange" as used herein refers to a flange formed
in the way that an end of a press formed product having a substantially gutter-shaped
cross section is bent outwardly from the gutter. Further, the term "ridge flange"
as used herein refers to a flange formed along the ridge region in an end of the press-formed
product. Further, the term "outward continuous flange" refers to an outward flange
continuously formed over the ridge and at least a part of each of a gutter bottom
and the vertical wall.
[0032] Furthermore, the phrase "provide a notch in a flange" as used herein is meant to
provide a notch formed in the whole width of a flange, which makes the flange discontinuous.
The term "flange width" is used to have the same meaning as the height of a flange.
Accordingly, when the flange width is made partially small but a part of the flange
still remains, the notch is not meant to be provided in the flange.
[0033] Furthermore, the term "flange width" as used herein refers to the width of a raised
flat portion of the flange that does not include the curved rising surface that connects
the outward continuous flanges 9a, 9b to the top plate 4, the ridges 4a, 4b, and the
vertical walls 5a, 5b.
[0034] As described above, the first member 2 according to the present embodiment has the
outward continuous flanges 9a, 9b in the perimeter of the axial end thereof, or more
particularly, in the region of the top plate 4 that excludes the region along the
groove 8, and also in the region along the ridges 4a, 4b and the vertical walls 5a,
5b. It is sufficient, however, that the first member 2 has the ridge flange 50a or
50b at least in the region along each ridge 4a, 4b. In addition, the first member
2 may have an outward flange that has notches in the regions along the top plate 4
and the vertical walls 5a, 5b so that the notches make the outward flange discontinuous
from the ridge flanges 50a, 50b.
[0035] Further, as illustrated in FIG. 2 (b), the outward continuous flange 9c may be formed
including the region along the groove 8 in the top plate 4. If the outward continuous
flange 9c is also formed in the region along the groove 8, the axial load is transferred
more easily to the ridges of the groove 8 so that such ridges will be also able to
bear the load efficiently.
[0036] The top plate 4 of the first member 2 has the groove 8 disposed along the axial direction.
The shape of the groove 8 can be, for example, a substantially trapezoidal shape or
a V-letter shape. The first member 2 illustrated in FIG. 1 has the substantially-trapezoidal
groove 8. The first member 2 having the groove 8 increases the number of load-bearing
ridgelines so that the amount of impact energy absorption increases. Accordingly,
this leads to, for example, weight reduction by reducing sheet thickness without sacrificing
collision safety.
[0037] The upper width w of the groove 8 can be, for example, about 50 mm or less. In view
of formability in press forming, however, the upper width w of the groove 8 is preferably
5 mm or more. In addition, the depth h of the groove 8 is set according to the width
w of the groove 8 and also to the thickness t of the steel sheet according to the
present embodiment. More specifically, the depth h of the groove 8 is set such that
the depth h and the width w of the groove 8 and the thickness t of the steel sheet
satisfy the following relation:

[0038] The formula (2) above represents a groove depth H
0 when the amount of energy absorption per unit area (kJ/mm
2) in the cross section of the first member 2 becomes around the maximum value at a
displacement stroke of 100 mm in the case that the first member 2 has the outward
continuous flanges 9a, 9b. The cross section of the first member 2 as used above refers
to the cross section in the end of the first member 2 that includes cross sections
of the ends of the top plate 4, ridges 4a, 4b, and the vertical walls 5a, 5b, in which
the cross sections are taken along the border with the curved rising surface that
continues to the outward continuous flange 9a or 9b.
[0039] As indicated in the formula (1) above, if the groove depth h is within the range
of 20 to 300% of H
0 that is the groove depth when the amount of energy absorption per unit area becomes
around the maximum value, the energy absorption efficiency improves as compared to
the structural member that has the outward flanges but does not have the ridge flanges
50a, 50b.
[0040] For example, when the sheet thickness t is 1.4 mm and the width w of the groove 8
is 10 mm, the groove depth H
0, in which the amount of energy absorption per unit area becomes around its maximum,
is 20 mm. In this case, the depth h of the groove 8 is set from 4 mm to 60 mm. As
another example, when the sheet thickness t is 1.4 mm and the width w of the groove
8 is 40 mm, the groove depth H
0, in which the amount of energy absorption per unit area becomes around its maximum,
is 12 mm. In this case, the depth h of the groove 8 is set from 2.4 mm to 36 mm.
[0041] As still another example, when the sheet thickness t is 2.0 mm and the width w of
the groove 8 is 10 mm, the groove depth H
0, in which the amount of energy absorption per unit area becomes around its maximum,
is 17 mm. In this case, the depth h of the groove 8 is set from 3.4 mm to 51 mm. As
still another example, when the sheet thickness t is 2.0 mm and the width w of the
groove 8 is 40 mm, the groove depth H
0, in which the amount of energy absorption per unit area becomes around its maximum,
is 10 mm. In this case, the depth h of the groove 8 is set from 2.0 mm to 30 mm.
[0042] The first member 2 having the above-described structure is joined to the second member
3 by welding via the outward continuous flanges 9a, 9b that include the ridge flanges
50a, 50b. Thereby, the amount of energy absorption increases in the initial stage
of collision (at a displacement stroke of, for example, 40mm or less) after receiving
an impact load. In addition, the first member 2 has the groove 8 in the top plate
4 and the outward continuous flanges 9a, 9b that include the ridge flanges 50a, 50b
in the axial end. Thereby, the buckling behavior of the first member 2 becomes stable
in the middle and later stage of collision (at a displacement stroke of, for example,
more than 40 mm) so that the amount of energy absorption is increased.
[0043] Moreover, even if an impact load applies to the first member 2 slantwise relative
to the axial direction, for example, the buckling behavior of the first member 2 during
collision is still stable, and thus robustness against the load input is improved
for the first member 2 according to the present embodiment. Consequently, the structural
member (first member) 2 according to the present embodiment has excellent load transfer
capability.
[0044] It should be noted that the above-described first member 2 has an open cross section
but the structural member according to the present embodiment is not limited to this
mode. For example, the structural member may be shaped to have a closed cross section
in which another member is joined via flanges 7a, 7b. Moreover, the first member 2,
which has one groove 8 in the top plate 4, may have a plurality of grooves.
<2. Example of Method for Manufacturing Structural Member for Automotive Body>
[0045] An example of the method for manufacturing the structural member (first member) 2
for an automotive body according to the present embodiment will now be described.
The structural member 2 according to the present embodiment is manufactured by press
forming a high-tensile steel sheet having, for example, a sheet thickness within the
range of 0.5 mm to 6.0mm and a tensile strength of 390 MPa or more, and thus forming
defects such as wrinkling and cracking generally tend to occur.
[0046] For example, when attempting to form the outward continuous flanges 9a, 9b having
a certain degree of flange width along the whole perimeter of the axial end of the
structural member 2, forming defects such as cracking of stretched flange in the edge
of each ridge flange 50a, 50b and wrinkling near the base of each ridge flange 50a,
50b tend to occur during press forming. In general, as the material strength becomes
higher, cracking in the edge and wrinkling near the base of each ridge flange 50a,
50b are more likely to occur.
[0047] Accordingly, when using a high-tensile steel sheet as the forming material, it is
difficult for press forming methods known in the art to manufacture the structural
member having the outward continuous flanges including ridge flanges because of constraints
in press forming. Consequently, a notch has hitherto had to be provided in the region
along the ridge in the outward flange to compensate such difficulty in press forming.
Providing the notch is a cause to lower performance in terms of load transfer capability,
flexural rigidity, and torsional rigidity.
[0048] In contrast, the structural member 2 according to the present embodiment can be manufactured
by a manufacturing method as described below even though it has the outward continuous
flanges 9a, 9b that include the ridge flanges 50a, 50b. An example of the press-forming
apparatus that can be used for manufacturing the structural member 2 according to
the present embodiment will be described hereafter, and then a manufacturing method
will be explained more specifically.
(2-1. Press-forming Apparatus)
[0049] FIG. 3 and FIG. 4 are schematic views illustrating a press-forming apparatus 10 to
be used for manufacturing the structural member 2. FIG. 3 is a cross sectional view
illustrating a part of the press forming apparatus 10, which corresponds to an end
of the structural member 2. FIG. 4 (a) is a perspective view illustrating a die 12,
and FIG. 4 (b) is a perspective view illustrating a pad 13. FIG. 4 (c) is also a perspective
view illustrating a punch 11. FIG. 4 (a) to 4 (c) are respective perspective views
illustrating the die 12, the pad 13, and the punch 11, as viewed slantwise from upper
left, and the parts to form the outward continuous flanges 9a, 9b are shown on the
deep side of the paper surface.
[0050] The press-forming apparatus 10 includes the punch 11 and the die 12, and the pad
13 that presses the forming material 14 against the punch 11 and restrains the forming
material 14. The punch 11 has a groove-forming part 11b that is formed in an upper
surface 11a of the punch 11 and extends in the longitudinal direction, and has a side
wall 11c formed in the longitudinal end. The rising angle θ of the side wall 11c is,
for example, 50° to 90°.
[0051] The shape of the groove-forming part 11b corresponds to the shape of the groove 8
to be formed in the structural member 2. For example, the groove-forming part 11b
has a cross section of a trapezoidal shape or a V-letter shape (FIG. 3 (b) illustrates
the trapezoidal shape). The width in the direction perpendicular to the axial direction
in the top opening of the groove-forming part 11b is approximately 50 mm or less.
The depth of the groove-forming part 11b is designed to correspond to the shape of
the groove 8 of the structural member 2, which is determined by satisfying the above-described
formulas (1) and (2).
[0052] The pad 13 has a top plate pressing part 13b including a bump part 13a, a ridge-pressing
part 13c, and a side wall 13d. The bump part 13a faces the groove-forming part 11b
that is formed in the punch 11 and extends in the longitudinal direction. The top
plate pressing part 13b having the bump part 13a presses, and restrains, a portion
to be formed into the top plate 4 in the forming material 14 against the upper surface
11a of the punch 11. The top plate 4 having the groove 8 is formed by the pad 13 that
presses the forming material 14 against the upper surface 11a of the punch 11.
[0053] The ridge-pressing part 13c presses against the punch 11, and restrains, the ends
of portions to be formed into ridges 4a, 4b in the vicinity of portions to be formed
into outward continuous flanges 9a, 9b in the forming material 14. The pad 13 is hereinafter
referred to as the ridge pad.
[0054] More specifically, the ridge pad 13 restrains the portion to be formed into the top
plate 4 and also the end of the portion to be formed into each ridge 4a, 4b in the
vicinity of the portion to be formed into each outward continuous flange 9a, 9b in
the forming material 14. It is sufficient, however, that the ridge pad 13 restrains
at least the end of the portion to be formed into each ridge 4a, 4b. The other parts
of the portions to be formed into ridges 4a, 4b, the portion to be formed into the
top plate 4, and the portions to be formed into vertical walls 5a, 5b may leave unrestrained.
[0055] FIG. 5 is a schematic view illustrating the shape of a pad 15 known in the art. FIG.
5 (a) is a cross sectional view illustrating a press-forming apparatus 10' having
the pad 15 known in the art, and FIG. 5 (b) is a perspective view illustrating a state
in which the forming material 14 is pressed by the known pad 15. FIG. 5 (a) is a cross
sectional view illustrating the same portion of the press-forming apparatus 10 as
illustrated in FIG. 3. As illustrated, the known pad 15 restrains the portion to be
formed into the top plate 4 in the forming material 14 but does not restrain the portion
to be formed into each ridge 4a, 4b.
[0056] The press-forming apparatus 10 presses the end of the portion to be formed into each
ridge 4a, 4b using the ridge pad 13, and project outward approximately only the steel
sheet material nearby. Thereby, the ridges 4a, 4b in the vicinity of the outward continuous
flanges 9a, 9b are formed. Accordingly, this reduces the movement of the material
in the region that the ridge pad 13 contacts, and thus reduces the generation of cracking
of stretched flange in the end of the edge of each ridge flange 50a, 50b and wrinkling
near the base of each ridge flange 50a, 50b.
[0057] The ridge pad 13 is aimed at reducing the movement of the surrounding material by
projecting outward the material in the end of the portion to be formed into each ridge
4a, 4b to form the end of each ridge 4a, 4b. Accordingly, the extent of the portion
to be formed into each ridge 4a, 4b that is restrained by the ridge pad 13 in the
vicinity of the portion to be formed into each outward continuous flange 9a, 9b is
preferably at least 1/3 or more of the perimeter length of the cross section of the
portion to be formed into each ridge 4a, 4b starting from the border between each
ridge 4a, 4b and the top plate 4.
[0058] In addition, the extent in the axial direction in the portion to be formed into each
ridge 4a, 4b that is restrained by the ridge pad 13 in the vicinity of the portion
to be formed into each outward continuous flange 9a, 9b can be, for example, 5 mm
to 100 mm along the axial direction from the base of the outward continuous flanges
9a, 9b. If this restrained extent is less than 5 mm, there arises a concern that it
may become difficult to prevent distortion or scratches that may occur during press
forming. In addition, the portion to be formed into each ridge 4a, 4b may be restrained
over the whole length in the axial direction. However, if the above-described restrained
extent exceeds 100 mm, the load that the ridge pad 13 requires to press the forming
material 14 may increase.
[0059] The die 12, which has a rising surface 12a formed in the longitudinal end, is disposed
facing the punch 11. The die 12, which does not have a pressing surface corresponding
to the portion to be formed into the top plate 4 in the structural member 2, is disposed
such that it does not overlap the pad 13 in the pressing direction. The die 12 bends
the forming material 14 along the portion to be formed into each ridge 4a, 4b while
the portion to be formed into the top plate 4 and the end of the portion to be formed
into each ridge 4a, 4b in the forming material 14 are restrained by the ridge pad
13.
[0060] Incidentally, the bending of the forming material 14 by the die 12 may be bending
forming in which the die 12 presses and bends the forming material 14, or may be deep
drawing in which a blank holder (not shown) and the die 12 clamp and bend the forming
material 14.
(2-2. Manufacturing Method)
[0061] Now, a method for manufacturing the structural member 2 using the press-forming apparatus
10 will be described with reference to FIG. 6 together with FIG. 3 and FIG. 4. FIG.
6 is a perspective view illustrating a state in which the forming material 14 is restrained
by the ridge pad 13.
[0062] The forming material 14, which is a developed blank having a shape into which the
structural member 2 to be formed is developed on a flat plane, is first placed on
the punch 11 in the press-forming apparatus 10. Subsequently, the ridge pad 13 thrusts
and presses the forming material 14 against the punch 11, as illustrated in FIG. 3
and FIG. 6. At this time, a part of the portion to be formed into each outward continuous
flange 9a, 9b in the forming material 14 is bent opposite to the pressing direction
by the side wall 11c of the punch 11 and the side wall 13d of the ridge pad 13.
[0063] The end of the portion to be formed into each ridge 4a, 4b in the vicinity of the
portion to be formed into each outward continuous flange 9a, 9b in the forming material
14 is bent in the pressing direction by the ridge-pressing part 13c of the ridge pad
13, and then restrained by the ridge-pressing part 13c and the punch 11. The top plate
pressing part 13b of the ridge pad 13 subsequently presses the portion to be formed
into the top plate 4 in the forming material 14 to cause the bump part 13a to push
a part of the forming material 14 into the groove-forming part 11b of the punch 11,
and then to cause the top plate pressing part 13b and the punch 11 to restrain the
forming material 14.
[0064] While the forming material 14 is restrained by the ridge pad 13 and the punch 11
as described above, the die 12 and the punch 11 carry out first press forming. In
the first press forming, a decrease or an increase in sheet thickness is reduced,
which otherwise causes cracking in the edge of the ridge flange 50a or 50b or wrinkling
near the base of the ridge flange 50a or 50b. The first press forming provides an
intermediate product having the substantially gutter-shaped cross section and having
the ridges 4a, 4b, the vertical walls 5a, 5b, and the top plate 4 including the groove
8 that extends in the longitudinal direction. The intermediate product has the outward
continuous flanges 9a, 9b formed in the regions along the ridges 4a, 4b, a part of
the top plate 4, and the vertical walls 5a, 5b, in the longitudinal end of the intermediate
product.
[0065] Incidentally, FIG. 6 illustrates a state in which the outward continuous flanges
9a, 9b is formed in the regions along the ridges 4a, 4b, a part of the top plate 4
excluding the region along the groove 8, and the vertical walls 5a, 5b. It is sufficient,
however, that the outward flange is formed at least in the region along the ridges
4a, 4b. In addition, the outward flange may be an outward continuous flange 9c that
includes the region along the groove 8 (see FIG. 2 (b)). The shape and width of the
outward flange can be adjusted by modifying the shape of the developed blank to be
formed into the forming material 14.
[0066] In addition, press forming of the intermediate product is described in the above
example in which the end of the portion to be formed into each ridge 4a, 4b and the
end of the portion to be formed into the top plate 4, in the forming material 14,
are restrained by the ridge pad 13. However, the method for manufacturing the structural
member 2 is not limited to this example. The extent restrained by the ridge-pressing
part 13c of the ridge pad 13 may be a region of at least 1/3 or more of the perimeter
length of the cross section of each ridge 4a, 4b starting from the border between
each ridge 4a, 4b and the top plate 4, in the portion to be formed into each ridge
4a, 4b. If the extent of the forming material 14 restrained by the ridge pad 13 is
smaller than the above-described extent, the ridge pad 13 may not achieve the effect
to reduce the generation of cracking and wrinkling sufficiently.
[0067] After the first press forming is carried out as described above, the intermediate
product is then subjected to second press forming to form the parts that are left
unformed in the first press forming. The second press forming presses the portion
that has not been formed by the ridge pad 13 and the die 12 and forms the structural
member 2 having the final shape. More specifically, a part of the portion in each
vertical wall 5a, 5b, which is located underneath the ridge pad 13 in the pressing
direction, is not completely press formed by the ridge pad 13 in the first press forming.
Accordingly, the part of the portion is press formed in the second press forming by
employing a different press-forming apparatus.
[0068] Incidentally, the outward continuous flanges 9a, 9b may not be raised to the angle
in the final product in the first press forming due to the shape of the outward continuous
flanges 9a, 9b or the rising angle of flange. In this case, the outward continuous
flanges 9a, 9b may be raised approximately to a predetermined angle, for example,
to 60°, in the first press forming, and then further raised to the angle of the final
product in the second press forming or subsequent press forming.
[0069] The press-forming apparatus to be used in the second press forming may be an apparatus
that can form what is not formed in the first press forming. This press-forming apparatus
can be constituted by using a known press-forming apparatus having a die and punch.
If the second press forming does not complete forming into the final shape of the
structural member 2, another forming process may be further carried out.
[0070] Incidentally, although an example in which the groove 8 in the top plate 4 is formed
by the ridge pad 13 in the first press forming has been described as the present embodiment,
the groove 8 may be formed by die 12. In addition, although an example in which the
groove 8 is formed in the top plate 4 in the first press forming has been described
as the present embodiment, the groove 8 may be formed in the second press forming.
[0071] As described above, the structural member 2 is formed, with reduced cracking in the
edge and reduced wrinkling near the base of each ridge flange 50a, 50b, by carrying
out press forming using the ridge pad 13 including the ridge-pressing part 13c and
the top plate pressing part 13b that has the bump part 13a. The structural member
(first member) 2 is joined to the second member 3 via the outward continuous flanges
9a, 9b formed in the longitudinal end to provide the joined structure 1 including
the first member 2 and the second member 3.
[0072] It should be noted that the structural member having the outward flange formed also
in the region along the groove 8 in the longitudinal end, as illustrated in FIG. 2
(b), can be manufactured, for example, in a sequence described below. That is to say,
a pad that has the ridge-pressing part 13c but does not have the bump part 13a forms
an intermediate product having the outward continuous flange including the outward
flange formed also in the whole perimeter region along the top plate, in the first
stage. Subsequently, the intermediate product is pressed to form the groove 8 in the
top plate 4 by using a pad or a punch having the bump part 13a for forming the groove
8 in the second stage. Thereby, the structural member, which has the outward flange
in the region of the groove 8, can be obtained.
[0073] In particular, thanks to the outward continuous flanges 9a, 9b that are also formed
in the regions of the ridges 4a, 4b, the structural member according to the present
embodiment improves energy absorption efficiency even though the depth of the groove
8 is relatively small. Consequently, a desired outward flange can be provided also
in the region along the groove 8 for the structural member by the above-described
press forming in the second stage.
[0074] As described in the foregoing, the structural member 2 according to the present embodiment
is made to increase the amount of energy absorption in the initial stage of collision,
thanks to having the outward continuous flanges 9a, 9b, which include the ridge flanges
50a, 50b, in the longitudinal end of the structural member 2. Moreover, the structural
member 2 according to the present embodiment has the outward continuous flanges 9a,
9b as well as the groove 8 in the top plate 4 that is configured in a predetermined
range so that the energy absorption efficiency in the middle and later stage of collision
is increased. Consequently, the structural member 2 according to the present embodiment
is excellent in load transfer capability, flexural rigidity, and torsional rigidity,
which makes the structural member suitable for structural members for an automotive
body.
[0075] Moreover, the structural member 2 according to the present embodiment has the outward
continuous flanges 9a, 9b that include the ridge flanges 50a, 50b, which allows a
groove 8 having an effective depth h determined according to the width w of the groove
8 and the sheet thickness t to be provided in the structural member 2. Consequently,
it becomes easier to form the groove 8 having a desired depth that can improve the
energy absorption efficiency, even in press forming a high-tensile steel sheet that
is relatively difficult to form, so that the structural member having excellent load
transfer capability and rigidity can be obtained with a high production yield.
[0076] A preferable embodiment has been described so far with reference to the accompanied
drawings. The present invention, however, is not limited to the above-described example.
It will be evident that those skilled in the art to which the present invention pertains
may conceive various alternatives and modifications while remaining within the scope
of the technical idea as described in the claims. It should be understood that such
alternatives and modifications apparently fall within the technical scope of the present
invention.
[Example(s)]
[0077] Examples of the present invention will now be described.
(Analysis 1)
[0078] In Analysis 1, decrease rates of sheet thickness (or increase rates of sheet thickness)
in the edge and the base of ridge flanges 50a, 50b in a structural member 2 according
to Example was first evaluated. FIG. 7 is a plan view illustrating a shape of a developed
blank as a forming material 14 for a structural member 2 used in Analysis 1. FIG.
7 (a) is an overall plan view illustrating the shape of the forming material 14 including
an end in the longitudinal direction, and FIG. 7 (b) is an enlarged plan view illustrating
the longitudinal end.
[0079] The forming material 14 is made of a dual-phase (DP) steel sheet having a sheet thickness
of 1.4 mm and a tensile strength of 980 MPa class measured by tensile testing in accordance
with JIS Z 2241. In the forming material 14, a portion G to be formed into each ridge
flange 50a, 50b has such a shape as to intend the dispersion of deformation (a curvature
radius of 60 mm). In addition, a notch 59 is provided in the end of each ridgeline
within a region along a groove 8, while an outward flange 50c is also formed in a
region along the portion to be formed into the groove 8 in the end.
[0080] FIG. 8 and FIG. 9 illustrate a structural member (first member) 2 to be formed from
the forming material 14 that is illustrated in FIG. 7. FIG. 8 (a) is a top plan view
illustrating the structural member 2 as viewed from the top plate 4 side, and FIG.
8 (b) a diagrammatic view of the structural member 2 as viewed slantwise from above
in the longitudinal direction. In addition, FIG. 9 is a cross sectional view of the
structural member 2. The height of the structural member 2 is 100 mm. The curvature
radius of the cross section of a ridge 4a or 4b is 12mm and the depth of the groove
8 is 7.5mm. Other dimensions are as shown in FIG. 8 (b) and FIG. 9.
[0081] FIG. 10 and FIG. 11 are schematic views illustrating a press-forming apparatus 10
used in the first press forming in manufacturing the structural member 2 of Example.
FIG. 10 is a perspective view of the press-forming apparatus 10, and FIGs. 11 (a)
to 11 (c) are schematic views illustrating Cross Section 1, Cross Section 2, and Longitudinal
Section in FIG. 10, respectively. In addition, FIG. 12 and FIG. 13 are schematic views
illustrating a press-forming apparatus 20 used in the second press forming in manufacturing
the structural member 2 of Example. FIG. 12 is a perspective view of the press-forming
apparatus 20, and FIG. 13 (a) and FIG. 13 (b) are schematic views illustrating Cross
Section and Longitudinal Section in FIG. 12, respectively. Each of FIG. 10 and FIG.
12 illustrates only a part for forming one end of the structural member 2.
[0082] When the structural member 2 was press formed from the forming material 14 by using
the first and second press-forming apparatuses 10, 20, the deformation behavior of
the forming material 14 was analyzed by the finite element method. In the first press
forming, a ridge pad 13 according to Example was used to form an intermediate product
with the intention to reduce cracking in the edge and wrinkling near the base of ridge
flanges 50a or 50b to be formed in the region along ridges 4a, 4b in the longitudinal
end. In the first press forming, a descending die 12 and a punch 11 carried out press
forming after the forming material 14 was pressed by the ridge pad 13.
[0083] The first press forming does not form the shape of a portion located, in the pressing
direction, under the region in each ridge 4a, 4b that is pressed by the ridge pad
13, as illustrated in FIG. 11 (a). Accordingly, the portion that was not formed in
the first press forming was formed by the second press forming. In the second press
forming, re-striking was carried out using bending forming, while forming what was
not formed in the first press forming. In the second press forming, a top portion
41 of an intermediate product 40 was first restrained by a pad 23 that had a bump
part 23a corresponding to the groove 8 in shape. Subsequently, bending forming was
carried out by lowering a die 22 toward a punch 21 to form the structural member 2.
[0084] FIGs. 14 (a) and 14 (b) respectively illustrate the obtained intermediate product
40 and structural member 2 in which the analytical results on decrease rates of sheet
thickness in the edge and near the base of each ridge flange 50a, 50b are shown. FIG.
14 shows a maximum decrease rate of sheet thickness in the vicinity of a region A,
which is vulnerable to cracking in the edge of the ridge flange 50a or 50b, and a
minimum decrease rate of sheet thickness in the vicinity of a region B, which is vulnerable
to wrinkling near the base of the ridge flange 50a or 50b. A negative value in decrease
rate of sheet thickness means increase rate of sheet thickness.
[0085] As the press forming proceeds from the first press forming to the second, the decrease
rate of sheet thickness becomes larger in the region vulnerable to cracking, in other
words, in the vicinity of the edge of each ridge flange 50a, 50b (region A), as shown
in FIG. 14. It should be noted that, in the obtained structural member 2, the decrease
rate of sheet thickness, in the region vulnerable to cracking, in other words, in
the vicinity of the edge of each ridge flange 50a, 50b (region A), was about 14%,
with which cracking is avoidable.
[0086] As the press forming proceeds from the first press forming to the second, the increase
rate of sheet thickness becomes larger in the region vulnerable to wrinkling, in other
words, in the vicinity of the base of each ridge flange 50a, 50b (region B), as shown
in FIG. 14. It should be noted that, in the obtained structural member 2, the increase
rate of sheet thickness, in the region vulnerable to wrinkling or near the base of
each ridge flange 50a, 50b (region B), was about 12%, with which wrinkling is reduced.
(Analysis 2)
[0087] Subsequently, energy absorption efficiency for the structural member 2 according
to Example, which had both the outward continuous flanges 9a, 9b including the ridge
flanges and the groove 8 in the top plate 4, was evaluated in Analysis 2. In Analysis
2, the joined structure 1 in which the structural member (first member) 2 was joined
to a second member 3 by spot welding was assumed (see FIG. 1), and the axial load
and the amount of energy absorption were evaluated when the structural member 2 was
pressed along the axial direction from the side where the second member 3 was joined.
In Analysis 2, the displacement stroke was set up to 40 mm, which corresponded to
the initial stage of collision, with the intention to evaluate collision-safety capability
from a deformation prevention point of view.
[0088] FIG. 15 is schematic views illustrating analytical models used in Analysis 2. FIG.
15 (a) illustrates an analytical model 30 of the structural member 2 according to
Example, and FIG. 15 (b) illustrates an analytical model 31 of Comparative Example
1, which does not have either the ridge flanges or the groove. FIG. 15 (c) illustrates
an analytical model 32 of Comparative Example 2, which has the groove 8 but does not
have the ridge flanges. FIG. 15 (a) to 15 (c) are diagrammatic views of each analytical
model 30, 31, 32 as viewed slantwise from above in the longitudinal direction. In
addition, FIG. 16 is an overall view of the analytical models 30, 31, 32 as viewed
from the lateral direction relative to the longitudinal direction.
[0089] The analytical model 31 of Comparative Example 1 has the same shape as the analytical
model 30 of the structural member 2 according to Example, except that a groove is
not provided in the top plate 4 of the first member 2, and a notch 55 is provided
in the outward flange in the longitudinal end of each ridge 4a, 4b in the analytical
model 31. In addition, the analytical model 32 of Comparative Example 2 has the same
shape as the analytical model 30 of the structural member 2 according to Example,
except that a notch 55 is provided in the outward flange in the longitudinal end of
each ridge 4a, 4b in the analytical model 32.
[0090] In Analysis 2, each analytical model 30, 31, 32 was spot welded, via flanges 7a,
7b, to a closing plate 45 made of a 0.6 mm thick steel sheet having a tensile strength
of 270 MPa class. Each analytical model 30, 31, 32 had the same shape as the above
described structural member 2 illustrated in FIG. 8 and FIG. 9, except for the presence
of the closing plate 45 joined thereto and the presence or non-presence of the groove
or the ridge flange. Each analytical model 30, 31, 32 used the same forming material
14 as in Analysis 1, which was a 1.4 mm thick steel sheet having a tensile strength
of 980 MPa class. This analysis assumed the second member 3 as a rigid-body wall with
the intention to study the influence of the shape of the joint portion and the influence
of the structure of the structural member 2 on collision-safety capability.
[0091] FIG. 17 is a graph showing the analytical results on axial load vs. stroke characteristics,
and FIG. 18 is a graph showing the analytical results on amount of energy absorption
vs. stroke characteristics. As shown in FIG. 17, the analytical model 30 of the structural
member 2 according to Example exhibits a higher peak value in the axial load (kN)
as compared to the analytical model 31 of Comparative Example 1. In addition, in the
analytical model 30 of the structural member 2 according to Example, a peak value
in the axial load (kN) in the initial stage of collision has appeared on the smaller-stroke
side of the graph, in other words, in an earlier timing, as compared to the analytical
model 31, 32 of Comparative Examples 1,2.
[0092] Moreover, in association with the peak difference in the axial load, the amount of
energy absorption (kJ) is also higher for the analytical model 30 of the structural
member 2 according to Example than that for the analytical model 31 of Comparative
Example 1. The structural member 2 according to Example also exhibits a higher amount
of energy absorption (kJ) than that of the analytical model 32 of Comparative Example
2 that has the groove 8 and the notches formed in the outward flange.
[0093] These results are likely due to the fact that the analytical model 30 of the structural
member 2 according to Example has more ridges that serve to transfer the load than
those of the analytical model 31 of Comparative Example 1. It is also likely that,
in the analytical model 30 of the structural member 2 according to Example, the outward
continuous flanges 9a, 9b that include the ridge flanges 50a, 50b cause the ridges
to produce a high axial stress from the initial stage of collision and to be able
to make the axial load confined and transferable with a high efficiency. The above-described
results from Analysis 2 show that the structural member 2 according to Example has
an excellent ability as a deformation prevention member as compared to Comparative
Examples 1, 2.
(Analysis 3)
[0094] In Analysis 3, the energy absorption efficiency of the structural member 2 according
to Example was evaluated in the middle and later stage of collision. In Analysis 3,
the analytical model 30 of the structural member 2 according to Example illustrated
in FIG. 15 (a) and the analytical model 32 according to Comparative Example 2 illustrated
in FIG. 15 (c) were used among the analytical models used in Analysis 2. In particular,
the only difference between the shapes of two analytical models 30, 32 is whether
or not the notches 55 are provided in the outward flange. The basic features of the
shape and structure of the analytical models 30 and 32, including having the closing
plate 45 joined, are the same as in Analysis 2.
[0095] In Analysis 3, however, each type of the analytical models 30, 32 was formed using
two different types of steel sheets, in other words, a 1.4 mm thick steel sheet of
340 MPa class in tensile strength and a 1.4 mm thick steel sheet of 980 MPa class
in tensile strength. Further in Analysis 3, four different type of depths of the groove
8, such as depths of 7.5mm, 15mm, 30mm, and 40mm, were provided and then analyzed
per each type of the steel sheet per each analytical model 30, 32. The displacement
stroke for Analysis 3 was set up to 100 mm to cover the middle and later stage of
collision.
[0096] FIG. 19 and FIG. 20 show the analytical results for the analytical models 30, 32
in which the 1.4 mm thick steel sheet of 340 MPa class in tensile strength was used.
FIG. 19 (a) is a graph showing the analytical results on amount of energy absorption
vs. stroke characteristics for the analytical model 32 according to Comparative Example
2, and FIG. 19 (b) is a graph showing the analytical results on amount of energy absorption
vs. stroke characteristics for the analytical model 30 of the structural member 2
according to Example. In addition, FIG. 20 is a graph showing the analytical results
on amount of energy absorption vs. groove depth characteristics at a displacement
stroke of 100 mm for each of the analytical model 30 of the structural member 2 according
to Example and the analytical model 32 of Comparative Example 2.
[0097] As shown in FIG. 19, when the 1.4 mm thick steel sheet of 340 MPa class in tensile
strength is used, the analytical model 30 of the structural member 2 according to
Example exhibits higher amounts of energy absorption (kJ) than those of the analytical
model 32 of Comparative Example 2 over the period until the displacement stroke reaches
100mm. However, an increase effect on the amount of energy absorption is limited.
In addition, as shown in FIG. 20, the analytical model 30 of the structural member
2 according to Example exhibits a higher amount of energy absorption for every groove
depth h at a displacement stroke of 100 mm (kJ) than that of the analytical model
32 of Comparative Example 2.
[0098] FIGs. 21 to 23 show the analytical results on the analytical models 30, 32 in which
the 1.4 mm thick steel sheet of 980 MPa class in tensile strength was used. FIG. 21
(a) is a graph showing the analytical results on amount of energy absorption vs. stroke
characteristics for the analytical model 32 according to Comparative Example 2, and
FIG. 21 (b) is a graph showing the analytical results on amount of energy absorption
vs. stroke characteristics for the analytical model 30 of the structural member 2
according to Example. In addition, FIG. 22 is a graph showing the analytical results
on amount of energy absorption vs. groove depth characteristics at a displacement
stroke of 100 mm for each of the analytical model 30 of the structural member 2 according
to Example and the analytical model 32 of Comparative Example 2.
[0099] In addition, FIG. 23 is a graph showing the analytical results on normalized amount
of energy absorption per unit cross sectional area vs. groove depth characteristics
at a displacement stroke of 100 mm for each of the analytical model 30 of the structural
member 2 according to Example and the analytical model 32 of Comparative Example 2.
The normalized amount of energy absorption per unit cross sectional area represents
the value that is obtained as follows: an amount of energy absorption per unit cross
sectional area at a displacement stroke of 100 mm is divided by the amount of energy
absorption per unit cross sectional area for the analytical model 32 of Comparative
Example 2 at a groove depth of 7.5 mm and at a displacement stroke of 100 mm, and
then the obtained result is multiplied by 100. Further, FIG. 24 and FIG. 25 are schematic
views showing deformation, with respect to displacement stroke (10 to 50mm), of the
analytical model 32 of Comparative Example 2 and the analytical model 30 of the structural
member 2 according to Example.
[0100] As shown in FIG. 21, when the 1.4 mm thick steel sheet of 980 MPa class in tensile
strength is used, the analytical model 30 of the structural member 2 according to
Example also exhibits higher amounts of energy absorption (kJ) than those of the analytical
model 32 of Comparative Example 2 over the period until the displacement stroke reaches
100mm. Moreover, an increase effect on the amount of energy absorption is conspicuously
shown as compared to the case using the 1.4 mm thick steel sheet of 340 MPa class
in tensile strength. Consequently, the structural member 2 according to Example provides
a higher improvement effect on the energy absorption efficiency as the strength of
the forming material 14 increase.
[0101] In addition, as shown in FIG. 22, the analytical model 30 of the structural member
2 according to Example exhibits a higher amount of energy absorption (kJ) at every
groove depth h at a displacement stroke of 100 mm than that of the analytical model
32 of Comparative Example 2. Further, the analytical model 30 of the structural member
2 according to Example exhibits higher amounts of energy absorption at a displacement
stroke of 100 mm (kJ) from the state in which the groove depth h is smaller.
[0102] Moreover, as shown in the graph in FIG. 23 in which the influence of the perimeter
length of each analytical model 30, 32 is eliminated, the analytical model 32 of Comparative
Example 2 does not exhibit an increase in the energy absorption efficiency (%) at
a displacement stroke of 100 mm when the depth h of the groove 8 is small. Furthermore,
the analytical model 32 of Comparative Example 2 does not show a marked increase in
the energy absorption efficiency when the depth h of the groove 8 is made larger.
This is due to the fact that the analytical model 32 of Comparative Example 2 does
not have the ridge flanges 50a, 50b so that when the ridges of the groove 8 is stressed
hard in the middle stage of collision in which the displacement stroke exceeds 40
mm, the restraint at the ridge ends becomes loose and the structural member buckles,
as shown in FIG. 24.
[0103] In contrast, the energy absorption efficiency (%) at a displacement stroke of 100
mm is increased, regardless of the groove depth h, in the analytical model 30 of the
structural member 2 according to Example. In addition, when the energy absorption
efficiency at a displacement stroke of 100 mm is a maximum, the groove depth h is
smaller for the analytical model 30 of the structural member 2 according to Example
than that for the analytical model 32 of Comparative Example 2. This is due to the
fact that the analytical model 30 of the structural member 2 according to Example
has the ridge flanges 50a, 50b so that the buckling behavior of the structural member
2 becomes stable in the middle stage of collision in which the displacement stroke
exceeds 40 mm, as shown in FIG. 25.
[0104] Incidentally, the groove depth H
0 in FIG. 23, with which the energy absorption efficiency at a displacement stroke
of 100 mm becomes a maximum, can be expressed in the above described formula (2).
In addition, when the groove depth h is in the range of 0.2 × H
0 to 3.0 × H
0 in terms of above H
0 as shown in the above described formula (1), the energy absorption efficiency at
a displacement stroke of 100 mm becomes large as compared to the analytical model
32 according to Comparative Example 2.
[Reference Signs List]
[0105]
1 joined structure
2 structural member (first member)
3 second member
4 top plate
4a, 4b ridge
5a, 5b vertical wall
6a, 6b curved section
7a, 7b flange
8 groove
9a, 9b, 9c outward continuous flange
10 press-forming apparatus
11 punch
11b groove-forming part
12 die
13 pad (ridge pad)
13a bump part
13b top plate pressing part
13c ridge-pressing part
14 forming material
15 pad known in the art
20 press-forming apparatus
30, 31, 32 analytical model
40 intermediate product
45 closing plate
50a, 50b ridge flange
50c outward flange (groove bottom flange)
55 notch
h groove depth
w groove width