Specification
Title of invention: Structural member
Technical field
[0001]
　The present invention relates to structural members, and more specifically to structural members of automobiles.
Background technology
[0002]
　Suspension parts, which are structural members of automobiles, are important parts that affect the steering stability of automobiles. For example, the front lower arm (hereinafter, also referred to as "lower arm") holds the position and orientation of the tire, holds the lateral force when the vehicle turns, blocks the impact transmission to the body side when an impact is input, and maintains the strength when riding on a curb. It plays a role such as. Various studies have been made to achieve high performance in these roles.
[0003]
　For example, in Patent Document 1, as a technique for blocking impact transmission to the body side at the time of impact input, a hollow substantially rectangular closed cross-sectional area is formed by an upper member and a lower member, and the cross-sectional area of ​​the rear upper corner portion is determined. A shock absorbing structure of an automobile lower arm that reduces and increases the cross-sectional area of ​​the rear lower corner portion is disclosed. With such a configuration, the input of the collision load from the wheel is absorbed without securing the deformation allowance on the suspension member side.
[0004]
　In Patent Document 2, three support portions are connected by a main frame to form a substantially triangular hollow suspension arm main body, and a plurality of subframes are arranged along the principal stress direction in the hollow portion of the suspension arm main body. A suspension arm configured in the above is disclosed. With this configuration, weight reduction is achieved while ensuring sufficient strength against stress transmitted from the suspension.
[0005]
　Patent Document 3 describes a first horizontal portion that extends substantially horizontally when attached to a vehicle body, a vertical portion in which the peripheral edge of the first horizontal portion is bent downward, and a reverse portion in which the lower edge of the vertical portion is bent inward. A suspension arm for an automobile in which a metal plate is pressed is disclosed, which includes a flange and a second horizontal portion protruding upward from the first horizontal portion. By providing a second horizontal portion that protrudes upward from the first horizontal portion, the height of the bending center with respect to the bending load in the vertical direction is increased to increase the distance from the bending center to the reverse flange, and the reverse flange is formed. The acting tensile load and compressive load are reduced.
[0006]
　Patent Document 4 includes a plate-shaped main body portion that is arranged substantially parallel to a load input surface, and a substantially pipe-shaped reinforcing portion that is continuously provided along at least one side edge of the main body portion. Suspension arm for use is disclosed. With such a configuration, the bending rigidity of the suspension arm is increased, and sufficient rigidity that can withstand a large load input due to unevenness of the road surface, turning of the vehicle, braking of the wheels, etc. is secured.
[0007]
　Patent Document 5 describes a suspension arm formed by press-molding a single plate material into an open cross-sectional shape, wherein the inner terminal portion and the outer terminal portion of the first arm portion and the inner terminal portion of the second arm portion are formed. And a configuration in which the outer terminal portion is bent in a direction approaching each other are disclosed. With such a configuration, sufficient rigidity is ensured without increasing the weight.
[0008]
　Patent Document 6 provides a suspension arm made of a metal plate, provided with a reinforcing portion formed in a pipe shape by folding back the end portion of the metal plate at at least a part of a side forming the outer periphery of the metal plate, and the end of the metal plate. A configuration is disclosed in which the portion is caught inside the reinforcing portion and is overlapped with a metal plate. Since the reinforcing portion has a winding portion having a double plate structure, it is sufficient without welding as compared with the case where the end portion of the metal plate is simply folded back to form a reinforcing portion having no winding portion. High rigidity can be achieved.
Prior art literature
Patent documents
[0009]
Patent Document 1: Japanese Patent Application Laid-Open No. 2016-124320
Patent Document 2: Japanese Patent Application Laid-Open No. 9-315123
Patent Document 3
: Japanese Patent Application Laid-Open No. 3725031 Patent Document 4: Japanese Patent Application Laid-Open No. 8-188022
Patent Document 5: Japanese Patent Application Laid-Open No. 8-188022 318722
Japanese Patent Document 6: Japanese Patent Application Laid-Open No. 10-264624
Outline of the invention
Problems to be solved by the invention
[0010]
　In recent years, there has been an increasing demand for weight reduction of automobile bodies, and structural members of automobiles are required not only to fulfill their role but also to achieve both weight reduction of automobile bodies. However, in general, these are contradictory, and for example, in a structural member having a curved shape such as a lower arm of a suspension component, if the thickness of the structural member is reduced in order to reduce the weight of the automobile body, the structural member is deformed out of plane. Is likely to occur. The occurrence of this out-of-plane deformation causes a shortage of vehicle body front-rear bending strength (hereinafter, also referred to as "front-rear bending strength") for maintaining the positional relationship between the tire and the body. If the front-rear bending strength is insufficient, the force generated by the wheels when the vehicle body rides on the curb cannot be resisted, and the positional relationship between the tire and the body is broken.
[0011]
　As shown in Patent Documents 1 to 6, various studies have been made on suspension parts having a curved shape in order to maintain the role required of the parts, but the front-rear bending strength has hardly been studied. .. This is because, in the past, where it was possible to sufficiently increase the plate thickness of structural members of automobiles, out-of-plane deformation hardly occurred and it was not necessary to consider the influence thereof.
[0012]
　However, in recent years, due to the thinning of steel plates due to the weight reduction of automobile bodies, out-of-plane deformation of structural members is likely to occur. Further, for example, a structural member having an open cross section when cut along a line connecting the inside and the outside of a curved shape as in Patent Document 3 is a structural member having a closed cross section as in Patent Document 1. Compared to, the weight of parts can be reduced. However, a structural member having an open cross section tends to undergo out-of-plane deformation when the compressive stress is locally increased inside the curved shape, particularly in the curved portion.
[0013]
　Furthermore, from the viewpoint of reducing the weight of automobile bodies and improving collision safety, high-strength steel plates have come to be used as materials for structural members, but the higher the strength of the material, the longer the elastic range and the more likely it is to undergo out-of-plane deformation. ..
[0014]
　Therefore, the present invention has been made in view of the above problems, and an object of the present invention is to reduce the weight of the structural member and suppress out-of-plane deformation in the structural member having a curved shape. It is to provide possible new and improved automotive structural members.
Means to solve problems
[0015]
　In order to solve the above problems, according to a certain viewpoint of the present invention, the structural member is a top plate having a first edge portion and a second edge portion facing the first edge portion. It has a portion, a wall portion extending from the second edge portion in a direction intersecting the top plate portion, and a closed cross-sectional portion provided on the first edge portion, and the first edge portion relates to the top plate portion. When the structural member width is defined as the distance from the first edge portion to the second edge portion of the structural member when the top plate portion is curved inward in a plan view, the closed cross-sectional portion is along the direction of the structural member width. A closed cross section is formed on the vertical cut surface of the structural member, the vertical cut surface of the structural member along the direction of the width of the structural member has an open cross section, and the shape of the vertical cut surface of the structural member including the closed cross section is A structural member is provided that is asymmetric with respect to the length center of the structural member width.
[0016]
　The structural member has a first region on the first edge side from the center of the length of the structural member width and a second region on the second edge side from the center of the structural member width on the vertical cut surface. However, in the vertical cut surface including the closed cross-sectional area , the cross-sectional area ratio S in / S out of the cross- sectional area S in the first region to the cross- sectional area S out in the second region satisfies the following relational expression. Good. 1.15 ≤ S in / S out ≤ 2.65
[0017]
　The top plate portion, the wall portion, and the closed cross-section portion of the structural member may be formed from one member.
[0018]
　Further, the closed cross-sectional portion of the structural member may be formed of one member different from the member forming the top plate portion.
[0019]
　The closed cross-section portion may be provided adjacent to the top plate portion.
[0020]
　Alternatively, the closed cross-section may be formed from a plurality of members.
[0021]
　The structural member is formed of a top plate portion, a wall portion, a first member forming a part of the closed cross-section portion, and a second member forming the closed cross-section portion together with the first member. Both ends of the second member may be welded to the first member.
[0022]
　In the vertical cut surface, α / β is The relational expression of may be satisfied.
3/7 ≤ α / β ≤ 7/3
[0023]
　The cross-sectional shape of the closed cross-sectional portion may be rectangular.
[0024]
　The closed cross section may be formed from a hollow member.
[0025]
　The hollow portion of the closed cross section may be filled with a resin filler.
[0026]
　The closed cross section may be formed from a solid member.
[0027]
　The structural member may be, for example, a structural member of an automobile.
[0028]
　Alternatively, the structural member may be an automobile suspension component.
[0029]
　The tensile strength of the structural member may be 780 MPa or more.
[0030]
　The plate thickness of the structural member may be 2.9 mm or less.
[0031]
　The arm length of the structural member may be 350 mm or more.
[0032]
　The width of the structural member of the structural member may be 70 mm or more.
Effect of the invention
[0033]
　As described above, according to the present invention, in a structural member having a curved shape, it is possible to reduce the weight of the structural member and suppress out-of-plane deformation.
A brief description of the drawing
[0034]
FIG. 1 is a perspective view showing an outline of the shape of a structural member of an automobile according to an embodiment of the present invention.
FIG. 2 is a schematic view of a cut surface in the AA cutting line of FIG. 1, showing a configuration example of a structural member of an automobile.
FIG. 3 is a schematic view of a cut surface in the AA cutting line of FIG. 1, showing another configuration example of a structural member of an automobile.
FIG. 4 is a schematic view of a cut surface in the AA cutting line of FIG. 1, showing another configuration example of a structural member of an automobile.
FIG. 5 is a schematic view of a cut surface in the AA cutting line of FIG. 1, showing another configuration example of a structural member of an automobile.
6 is a schematic view of a cut surface in the AA cutting line of FIG. 1, showing another configuration example of a structural member of an automobile.
[Fig. 7] Fig. 7 is an explanatory view showing an example of an aspect ratio of a closed cross section.
FIG. 8 is an explanatory view showing another example of the aspect ratio of the closed cross section.
[Fig. 9] Fig. 9 is an explanatory view showing a welded portion of a steel plate by arc welding.
FIG. 10 is an explanatory view showing an arm length W and a structural member width Wp of a structural member having a curved shape according to the same embodiment.
[Fig. 11] Fig. 11 is a graph showing the relationship between the weight of the lower arm and the proportional limit strength.
FIG. 12 is a schematic cross-sectional view showing a structural member having a substantially U-shaped cross section in the width direction of the structural member.
FIG. 13 is an explanatory diagram schematically showing the susceptibility to out-of-plane deformation in the case where the cross section in the width direction of the structural member is a closed cross section and the case where the cross section is an open cross section.
FIG. 14 is a schematic perspective view showing a modified example of the shape of a structural member of an automobile according to the same embodiment.
FIG. 15 is a schematic plan view showing an example of a structural member having a curved shape according to the same embodiment.
16 is a schematic cross-sectional view taken along the BB cutting line of FIG.
FIG. 17 is a graph showing the relationship between the plate thickness of structural members and the performance improvement ratio of proportional limit strength.
FIG. 18 is a graph showing the relationship between the tensile strength TS and the proportional limit strength per unit component weight.
Mode for carrying out the invention
[0035]
　Preferred embodiments of the present invention will be described in detail below with reference to the accompanying drawings. In the present specification and the drawings, components having substantially the same functional configuration are designated by the same reference numerals to omit duplicate description.
[0036]
　<1. Structural members of automobiles>
　First, structural members of automobiles according to an embodiment of the present invention will be described with reference to FIGS. 1 to 6. FIG. 1 is a perspective view showing an outline of the shape of a structural member of an automobile according to the present embodiment. 2 to 6 are schematic views of a cut surface in the AA cutting line of FIG. 1, and show a configuration example of a structural member of an automobile.
[0037]
　[1-1. Overall configuration]
　The structural member 100 of the automobile according to the present embodiment has a curved shape as shown in FIG. Examples of such a structural member 100 include chassis parts. Examples of the chassis parts include arm or link part of the suspension part, and specifically, there are a lower arm, a front upper arm, a rear upper arm, a trailing arm and the like. The shape of the structural member 100 according to the present embodiment is not limited to suspension parts, but can also be applied to body parts. Specifically, vehicle skeletons of body parts include roof side rails, B-pillars, A-pillar lowers, A-pillar uppers, kick-clean forces, and the like. Further, examples of the shock absorbing skeleton of the body parts include a rear side member and a front side member. In particular, by applying the shape of the structural member 100 according to the present embodiment to a component having a curved shape having a thick plate thickness and a small cross-sectional size as compared with a general body component, the weight of the component can be reduced. And the effect of suppressing out-of-plane deformation can be effectively exhibited.
[0038]
　Such a structural member 100 has a top plate portion 101, a wall portion 103 extending in a direction intersecting the top plate portion 101, and a closed cross-section portion 105. In particular, the structural member 100 includes a curved top plate portion 101, a wall portion 103 provided along the curved outer side of the top plate portion 101, and a closure provided at least a part of the curved inner side of the top plate portion 101. It has a cross section 105. Regarding the structural member 100, the side having a large radius of curvature of the curved shape is defined as the outside of the curve, and the side of the curved shape having a small radius of curvature is defined as the inside of the curve.
[0039]
　The top plate portion 101 is a surface having a first edge portion 101a and a second edge portion 101b facing the first edge portion 101a. The first edge portion 101a is curved toward the inside of the top plate portion 101 in a plan view with respect to the top plate portion 101. In particular, the top plate portion 101 is a surface that is curved in one direction in a plane orthogonal to the plate thickness direction of the steel plate constituting the top plate portion 101. That is, the top plate portion 101 has a curved shape in a plan view with respect to the top plate portion 101. The surface shape of the top plate portion 101 does not have to be flat, and may be uneven as shown in FIG. Further, a through hole (not shown) or the like may be formed in the surface of the top plate portion 101.
[0040]
　The wall portion 103 is a surface formed so as to extend in a direction intersecting the top plate portion 101 from the edge portion on the second edge portion 101b side (curved outer side) of the top plate portion 101. For example, the wall portion 103 is formed so as to extend in a direction substantially orthogonal to the top plate portion 101.
[0041]
　The closed cross-section portion 105 is on the first edge portion 101a side (curved inner side) of the top plate portion 101, and is relative to the top plate portion 101 so as to form an open cross section together with the top plate portion 101 and the wall portion 103. It is provided. The closed cross section 105 is formed by one or a plurality of members to form a closed cross section. Further, the closed cross-section portion 105 may independently form a closed cross-section, or the closed cross-section portion 105 may form a closed cross-section together with the top plate portion 101.
[0042]
　The closed cross-section portion 105 may be provided adjacent to the top plate portion 101. Here, the fact that the closed cross-section portion 105 is adjacent to the top plate portion 101 means a state in which the portion forming the closed cross-section portion 105 is directly or indirectly connected to the top plate portion 101.
[0043]
　Specifically, the fact that the closed cross-section portion 105 is directly adjacent to the top plate portion 101 means that the closed cross-section portion 105 is the top plate portion as shown in the configuration examples D and D'of FIGS. Refers to the state of being attached to the lower surface 101d of 101. The fact that the closed cross-section portion 105 is directly adjacent to the top plate portion 101 includes a state in which the closed cross-section portion 105 is attached to the curved inner end surface of the top plate portion 101. Alternatively, the fact that the closed cross-section portion 105 is directly adjacent to the top plate portion 101 means that a part or all of the closed cross-section portion 105 is heavenly, as shown in the configuration examples A to C of FIGS. It is formed by using the member forming the plate portion 101, and includes a state in which the top plate portion 101 and the closed cross-section portion 105 are continuous.
[0044]
　Further, the fact that the closed cross-section portion 105 is indirectly adjacent to the top plate portion 101 means that a member is provided between the closed cross-section portion 105 and the top plate portion 101, and the closed cross-section portion 105 and the ceiling are provided via the member. Refers to a state in which the plate portion 101 is connected.
[0045]
　The closed cross-section portion 105 may be provided inside the curved surface of the structural member 100 in a manner capable of exerting a reinforcing effect, and a part of the closed cross-section portion 105 is above the upper surface 101c of the top plate portion 101. It may exist.
[0046]
　When such a structural member 100 is cut along a straight line connecting the curved outer side and the curved inner side, which is orthogonal to the neutral line of the top plate portion 101 (that is, cut at the AA cutting line of FIG. 1). The cross section (vertical cut surface) is an open cross section in which the lower surface side of the top plate portion 101 opens. On the other hand, in the cross section, the closed cross section 105 of the structural member 100 is closed. That is, the structural member 100 has an open cross-sectional shape as a whole, but there is a portion having a closed cross-section inside the curve. As described above, in the structural member 100 according to the present embodiment, by providing the closed cross-sectional portion 105 only on the curved inner side, the curved inner side is reinforced while suppressing the weight increase of the structural member 100, and the front-rear bending strength is increased. .. Further, since the closed cross-section portion 105 is provided adjacent to the top plate portion 101, the reinforcing effect of the curved inner side by the closed cross-section portion 105 is further improved. A more detailed geometric shape of the structural member 100 will be described later.
[0047]
　Here, the open cross section of the vertical cut surface of the structural member 100 means an open cross section formed integrally by the top plate portion 101, the wall portion 103, and the closed cross section portion 105. That is, although the vertical cut surface includes the closed cross section partially formed by the closed cross section 105, the structural member 100 as a whole has an open cross section because it is open to the lower surface side of the top plate 101.
[0048]
　[1-2. Configuration Example]
　Specific configuration examples of the structural member 100 are shown in FIGS. 2 to 6.
[0049]
(Structure Example A) In the
　structural member 100A shown in FIG. 2, a top plate portion 101, a wall portion 103, and a closed cross-section portion 105 are formed from one steel plate. The wall portion 103 extends from the one end side, which is the curved outer edge of the top plate portion 101, to the lower surface 101d side of the top plate portion 101. That is, the wall portion 103 extends in the plate thickness direction of the top plate portion 101 (the direction from the upper surface 101c side to the lower surface 101d side of the top plate portion 101) by bending the top plate portion 101. On the other end side of the top plate portion 101, which is the curved inner edge portion, the closed cross-sectional portion 105 is formed so as to project toward the lower surface 101d side of the top plate portion 101. The closed cross-section portion 105 is, for example, a rectangular closed portion formed by four surfaces 105a to 105d formed by bending a steel plate. At this time, the surface 105d including the end portion of the steel plate is welded and fixed to the upper surface 101c of the top plate portion 101. By welding the surface 105d and the upper surface 101c of the top plate portion 101, the welded portion Pw is provided, and the internal space of the closed cross-section portion 105 is completely closed.
[0050]
(Structure Example B) The
　structural member 100B shown in FIG. 3 is formed of two steel plates. Specifically, a part of the top plate portion 101, the wall portion 103, and the closed cross-sectional portion 105 is formed by the first steel plate 110B as the first member, and is closed by the second steel plate 120B as the second member. A part of the cross section 105 is formed. Similar to the configuration example A in FIG. 2, the wall portion 103 is formed by bending the first steel plate 110B so as to extend from one end side, which is the curved outer edge of the top plate portion 101, to the lower surface 101d side of the top plate portion 101. Will be done. On the other hand, on the other end side of the top plate portion 101, which is the curved inner edge portion, the first steel plate 110B is bent to form two surfaces, a surface 105e and a surface 105f. The surface 105e is a surface extending toward the lower surface 101d of the top plate portion 101. The surface 105f is a surface extending from the surface 105e to the side opposite to the wall portion 103 (that is, inside the curve). Further, the side of the surface 105f opposite to the wall portion 103 (that is, the inside of the curve) is bent to the outside of the bent portion between the surface 105e and the surface 105f (the side opposite to the top plate portion 101) to form a welded surface 105 g. ..
[0051]
　Further, the second steel plate 120B is bent along the curved inner edge of the top plate portion 101 of the structural member 100B. As a result, two surfaces 105h and 105i forming the closed cross-section portion 105 are formed. As described above, in the second steel plate 120B having an L-shaped cross section, the end portion of the surface 105h is welded to the welded surface 105g, and the end portion of the surface 105i is welded to the upper surface 101c of the top plate portion 101. That is, both ends of the second steel plate 120B are welded to the first steel plate 110B. As a result, the closed cross-sectional portion 105 of the structural member 100B is formed by the four surfaces 105e, 105f, 105h, and 105i.
[0052]
(Structure Example C) The
　structural member 100C shown in FIG. 4 is formed of two steel plates. Specifically, a part of the top plate portion 101, the wall portion 103, and the closed cross-sectional portion 105 is formed by the first steel plate 110C as the first member, and is closed by the second steel plate 120C as the second member. A part of the cross section 105 is formed. Similar to the configuration example A in FIG. 2, the wall portion 103 is formed by bending the first steel plate 110C so as to extend from one end side, which is the curved outer edge of the top plate portion 101, to the lower surface 101d side of the top plate portion 101. It is formed. On the other hand, on the other end side of the top plate portion 101, which is the curved inner edge portion, the first steel plate 110C is bent to form a surface 105l extending toward the lower surface 101d side of the top plate portion 101.
[0053]
　Further, the second steel plate 120C is bent along the curved inner edge of the top plate portion 101 of the structural member 100C. As a result, two surfaces 105j and 105k forming the closed cross-section portion 105 are formed. Further, in the second steel plate 120C having an L-shaped cross section, the ends of the surfaces 105j and 105k are bent in the bending outer direction of the second steel plate 120C, respectively, so that the welded surfaces 105n and 105p are formed. Will be done. The welded surface 105n is welded to the lower surface 101d of the top plate portion 101, and the welded surface 105p is welded to the surface 105l. That is, both ends of the second steel plate 120C are welded to the first steel plate 110C. As a result, the closed cross-sectional portion 105 of the structural member 100C is formed by the four surfaces 105j, 105k, 105l, and 105m.
[0054]
　In the configuration example B and the configuration example C, both ends of the second steel plates 120B and 120C are welded to the first steel plates 110B and 110C to form the closed cross-section portion 105. By such a relatively simple method, the closed cross-section portion 105 having various configurations is formed. Therefore, various closed cross-section portions 105 are provided depending on the strength and shape required for the structural portion 100. Further, the first steel plates 110B and 110C and the second steel plates 120B and 120C are welded in a state of surface contact. As a result, the joint strength can be further increased, and the reinforcing effect on the curved inner side by the closed cross-section portion 105 is further improved.
[0055]
(Structure Example D) The
　structural member 100D shown in FIG. 5 is also formed of two steel plates. Specifically, the top plate portion 101 and the wall portion 103 are formed by the first steel plate 110D, and the closed cross-section portion 105 is formed by the second steel plate 120D. That is, the first steel plate 110D is bent along a line that becomes the curved outer edge of the top plate 101 of the structural member 100D to form the top plate 101 and the wall 103. Further, the closed cross section 105 may be formed of, for example, a hollow member having a rectangular cross section. The closed cross-section portion 105 is fixed by welding the outer surface 105q to the lower surface 101d of the top plate portion 101 in the vicinity of the curved inner edge portion of the top plate portion 101. In this way, the structural member 100D having the closed cross-section portion 105 inside the curve can also be formed.
[0056]
　As a modification of the structural member 100, for example, the closed cross-sectional portion 105 of the structural member 100 does not necessarily have to be hollow as shown in FIGS. 2 to 5, and may be solid. For example, FIG. 6 shows a structural member 100D'with a closed cross-sectional portion 105'as a solid, as a modification of the structural member 100D shown in FIG. The closed cross-section portion 105'of the structural member 100D'is filled with the resin filler 130 in the hollow portion of the closed cross-section portion 105 of FIG. Further, the closed cross-section portion 105'may be formed of a solid prism member or the like, although the weight increases. As described above, even if the closed cross-section portion 105 is solid, the reinforcing function for increasing the front-rear bending strength can be achieved. Similarly, in the configuration example A of FIG. 2, the configuration example B of FIG. 3, and the configuration example C of FIG. 4, the closed cross-section portion 105 may be solid.
[0057]
　Further, the cross-sectional shape of the closed cross-sectional portion 105 is not limited to a rectangle. For example, the cross-sectional shape of the closed cross-sectional portion 105 may be polygonal, circular, elliptical, or the like. That is, the shape of the closed space is not particularly limited as long as it is formed by the closed cross-sectional portion 105. These closed cross-sections 105 can be realized, for example, by a square cylinder or a cylinder.
[0058]
　Further, as shown in FIG. 7, the cross-sectional shape of the closed cross-sectional portion 105 has the longest length in the structural member width direction (horizontal direction) of the closed cross-sectional portion 105 as α, and is perpendicular to the structural member width direction of the closed cross-sectional portion 105. When the longest length in the above direction (vertical direction) is β, α / β may satisfy the relational expression of 3/7 ≦ α / β ≦ 7/3. FIG. 7 is the same as that of FIG. 3, and shows the vertical cutting surface of the configuration example C (that is, the cross section when cut along the AA cutting line of FIG. 1). By having a relationship in which the aspect ratio α / β of the closed cross-sectional portion 105 is applied, it is possible to prevent the cross-sectional shape of the closed cross-sectional portion 105 from becoming a vertically long or horizontally long flat shape and becoming equivalent to a flat surface. As a result, the closed cross-section portion 105 can sufficiently exert the reinforcing effect on the curved inner side of the structural member 100.
[0059]
　Further, the aspect ratio α / β of the cross-sectional shape of the closed cross-sectional portion 105 may be set to be 2/3 or more and 3/4 or less. As a result, the closed cross-section portion 105 can further exert the reinforcing effect on the curved inner side of the structural member 100.
[0060]
　When the cross-sectional shape of the closed cross-sectional portion 105 is a polygonal shape, as shown in FIG. 8, the longest length in the width direction (horizontal direction) of the structural member 100 in the polygon is defined as α, and the closed cross-sectional portion The longest length in the direction perpendicular to the width direction (vertical direction) in 105 may be β. The same applies when the cross-sectional shape of the closed cross-sectional portion 105 is circular, elliptical, or the like.
[0061]
　Further, the structural members 100A to 100D'shown in FIGS. 2 to 6 and the welded portion Pw in FIG. 16 to be described later schematically show the welded portion. The actual welding is performed by, for example, arc welding. When performing the arc welding, the steel plate S 1 and the steel plate S 2 weld Pw and has a shape as shown in FIG. 9, for example. Further, the welded portions of the configuration examples A to D'may be joined portions by a joining method other than welding.
[0062]
　In this embodiment, the material of each member constituting the structural member 100 is not particularly limited. The top plate portion 101, the wall portion 103, and the closed cross-section portion 105 constituting the structural member 100 according to the present embodiment are formed of a metal material such as steel, an aluminum alloy, or a magnesium alloy, or a resin material such as glass fiber or carbon fiber. May be done. Further, the member may be formed of a composite material of a metal material and a resin material.
[0063]
　<2. Shape of Structural Member> As
　shown in FIGS. 2 to 6, the structural member 100 of the automobile according to the present embodiment is a straight line connecting the curved outer side and the curved inner side, which is orthogonal to the neutral line of the top plate portion 101. The cross section when cut along the line is an open cross section as a whole, but there is a portion which becomes a closed cross section inside the curve. Such a shape is determined based on the relationship between the shape of the structural member 100 and the occurrence of out-of-plane deformation. Hereinafter, the configuration of the structural member 100 according to the present embodiment will be described in detail.
[0064]
　[2-1. Relationship with Out-of-plane Deformation]
　First, the relationship between the shape of the structural member 100 having a curved shape and the out-of-plane deformation will be described with reference to FIGS. 10 to 12. FIG. 10 is an explanatory view showing an arm length W and a structural member width Wp of the structural member 100 having a curved shape according to the present embodiment.
[0065]
　As an example of the structural member 100, FIG. 10 shows a front lower arm. The front lower arm is a suspension component for connecting the lower part of the knuckle that rotatably supports the wheel to the vehicle body. A point P1 on one end side of the curved top plate portion 101 of the structural member 100 indicates a ball joint installation position for suspending the wheel. Further, the point P of the curved portion of the top plate 101 2 and the point P at the other end of the top plate 101 3 are located which is connected to the body parts. Structural member 100, the point P 2 and the point P 3 is fixed to the body part, for example, via a bush joint provided.
[0066]
　For example, the point P of the structural member 100 2 site is the body mounting portion 107. The vehicle body mounting portion 107 projects from the top plate portion 101 and the wall portion 103 in a direction orthogonal to the front-rear direction of the automobile vehicle body on the curved outer side of the structural member 100. The vehicle body mounting portion 107 has a substantially U-shaped cross section. The vehicle body mounting portion 107 has a top wall portion 107a extending from the top plate portion 101 and a pair of vertical wall portions 107b and 107c extending from the wall portion 103.
[0067]
　As shown in FIG. 10, the arm length W and the structural member width Wp are defined for the structural member 100. The arm length W is the length of the structural member 100 in the direction orthogonal to the front-rear direction of the vehicle body. In other words, the arm length W is the length of the structural member 100 in the direction orthogonal to the direction in which the load is applied to the curved structural member 100. The structural member width Wp is the distance from the curved inner side to the curved outer side of the structural member 100 in the direction orthogonal to the neutral line Lc of the top plate portion 101.
[0068]
　As a result of examination of such a structural member 100, the inventor of the present application has found that the rigidity of the top plate portion 101 decreases as the area of ​​the top plate portion 101 of the structural member 100 increases. In other words, the larger the area of ​​the top plate portion 101 of the structural member 100, the more easily out-of-plane deformation occurs. As shown in FIG. 10, the point P of the structural member 100 1 a load F is applied in the longitudinal direction of the automobile body in, the structural member 100 of a curved shape, the point P in the curved portion is curved outer 2 point P from 1 and point P 3 while tensile stress is generated toward the point P at the curved inner 1 and the point P 3 compressive stress is generated toward the curved portion from the side. Out-of-plane deformation occurs due to the compressive stress inside the curve. Then, as the area of ​​the top plate portion 101 becomes larger, the structural member 100 is more likely to be out-of-plane deformed under the influence of the compressive stress generated inside the curvature. In general, an automobile having a large body weight has a larger area of ​​the top plate portion 101 of the structural member 100 than an automobile having a small body weight, and out-of-plane deformation is likely to occur.
[0069]
　The occurrence of out-of-plane deformation of the structural member 100 causes insufficient front-rear bending strength. The front-back bending strength is evaluated by the proportional limit strength. The proportional limit strength indicates the presence or absence of permanent strain, and is used as an index indicating the influence on the alignment performance that maintains the positional relationship between the tire and the body. Specifically, the proportional limit strength, for example a point P of the structural member 100 as shown in FIG. 11 1 when a load is applied F, the relationship between the load F and the displacement amount by the load F (stroke) The strength at the limit point that maintains the alignment.
[0070]
　Here, FIG. 11 shows a graph showing an example of the relationship between the weight of the lower arm and the proportional limit strength. In FIG. 11, for the sake of simplicity, the relationship between the weight of the structural member and the proportional limit strength is shown for the structural member 10 having a substantially U-shaped cross section in the width direction of the structural member as shown in FIG. The structural member 10 having a substantially U-shaped cross section shown in FIG. 12 has a curved shape as shown in FIG. 1 in the same manner as the structural member 100 according to the present embodiment, and has a curved top plate portion 10a. It is composed of an outer wall portion 10b on the outer side of the curve and an inner wall portion 10c on the inner side of the curve. Compared with the cross section in the width direction of the structural member shown in FIGS. 2 to 6, such a structural member 10 does not have a closed cross section 105 inside the curve, but has a common open cross section as a whole.
[0071]
　In FIG. 11, as an example, the proportional limit strength of the lower arm was examined when the steel plate had a tensile strength of 980 MPa and the plate thickness was 2.3 mm and 3.6 mm. As a result, as shown in FIG. 11, the smaller the plate thickness and the smaller the weight of the lower arm (that is, the weight of the parts), the smaller the proportional limit strength.
[0072]
　[2-2. Structural member having cross-sectional asymmetry]
　Based on the above finding, the inventor of the present application is more likely to deform the structural member 100 out of the plane due to the influence of the compressive stress generated inside the curvature as the area of ​​the top plate portion 101 increases. The structure of the structural member 100 capable of reducing out-of-plane deformation was examined. As a result, as shown in FIGS. 2 to 6, a curved structural member 100 having an open cross section in the width direction of the structural member and a closed cross section 105 provided inside the curved surface was conceived. The cross section of the structural member 100 in the width direction of the structural member is asymmetric. Hereinafter, the cross-sectional asymmetry of the structural member 100, which is a structural feature of the structural member 100 according to the present embodiment, will be described.
[0073]
(1) Shape Comparison
　The structural member 100 according to the present embodiment has a shape in which the cross section in the width direction of the structural member is an open cross section and has a closed cross section 105 inside the curve. Such a configuration is characterized in that out-of-plane deformation is unlikely to occur and the weight of parts can be reduced. Here, FIG. 13 schematically shows the susceptibility to out-of-plane deformation in the case where the cross section in the width direction of the structural member is a closed cross section and the case where the cross section is an open cross section. When the cross section in the width direction of the structural member is an open cross section, the structural member having a symmetrical cross section such as the structural member 10 having a substantially U-shaped cross section in the width direction of the structural member shown in FIG. 12 and the present embodiment. The structural member 100 has an asymmetric cross section. For generating the ease of out-of-plane deformation, as described with reference to FIG. 10, one end side of the point of the top plate portion 10a, 101 to the curvature of the structural member 10, 100 (in FIG. 10 the point P 1 a load to) Consider the state when it is added.
[0074]
　First, when the cross section in the width direction of the structural member is a closed cross section, the cross section shape does not easily collapse even when a load is applied, but the weight of the component increases. On the other hand, when the cross section in the width direction of the structural member is an open cross section, the weight of the part can be reduced as compared with the case of a closed cross section, but when the cross section is symmetric, the inner wall portion inside the curve opens when a load is applied. , The cross-sectional shape is liable to collapse. Therefore, if the cross section in the width direction of the structural member is an open cross section symmetrical with respect to the center of the length in the width direction, out-of-plane deformation is likely to occur.
[0075]
　Therefore, like the structural member 100 according to the present embodiment, the cross section in the width direction of the structural member is reduced in weight as an open cross section, and a closed cross section 105 is provided inside the curve so as to withstand the compressive stress generated inside the curve. .. By providing the closed cross section 105 inside the curvature of the structural member, the cross section in the width direction of the structural member becomes an asymmetric open cross section at the center of the length in the width direction, and the compressive stress generated asymmetrically can be effectively suppressed. It will be possible.
[0076]
　In the present embodiment, as in the structural member 100 of FIG. 1, the closed cross-section portion 105 is formed in the entire region inside the curve of the structural member 100, but the closed cross section is formed inside the curve of the structural member 100. The region forming the portion 105 is not limited to such an example. For example, the closed cross-section portion 105 may be formed in a part of the curved inner side of the structural member 100. FIG. 14 is a schematic perspective view showing a modified example of the shape of the structural member 100 of the automobile according to the present embodiment. As shown in FIG. 14, the closed cross-sectional portion 105E of the structural member 100E according to the present modification may be formed in a part of the curved inner side of the structural member 100E. The structural member 100E includes a curved top plate portion 101E, a wall portion 103E provided along the curved outer side of the top plate portion 101E, and a closed cross-sectional portion 105E provided on a part of the curved inner side of the top plate portion 101E. And have. It is also possible to suppress the occurrence of out-of-plane deformation by partially forming the closed cross-section portion 105E in the structural member 100E in this way. In particular, as shown in FIG. 14, of the curved inner side of the structural member 100E, the portion recessed toward the curved outer side of the intermediate portion in the bending direction is a portion where the influence of the out-of-plane deformation is relatively larger than the other portions. is there. Therefore, by forming the closed cross-section portion 105E in such a region, it is possible to more reliably suppress the occurrence of out-of-plane deformation. Further, when the closed cross-section portion 105E is formed by using other members as shown in FIGS. 3 to 5, the amount of other members required to form the closed cross-section portion 105E can be reduced. Therefore, it is possible to suppress an increase in the weight of the structural member 100E.
[0077]
(2) Specific Configuration
　Hereinafter, details of the structural member according to the present embodiment will be described with reference to FIGS. 15 to 18.
[0078]
(Definition of cross-sectional asymmetry by cross-sectional area)
　First, the cross-sectional asymmetry in the width direction of the structural member according to the present embodiment will be described with reference to FIGS. 15 and 16. The asymmetry of the cross section in the width direction of the structural member is defined based on the cross-sectional area of ​​the cross section. FIG. 15 is a schematic plan view showing an example of the structural member 200 having a curved shape according to the present embodiment. FIG. 16 is a schematic cross-sectional view taken along the BB cutting line of FIG.
[0079]
　As shown in FIGS. 15 and 16, the structural member 200 is provided on the curved top plate portion 201, the wall portion 203 provided along the curved outer side of the top plate portion 201, and the curved inner side of the top plate portion 201. It is composed of a closed cross-sectional portion 205 provided. The structural member 200 has the structure of the structural member 100D shown in FIG. That is, the top plate portion 201 and the wall portion 203 are composed of the first steel plate 210, and the closed cross-section portion 205 is composed of the second steel plate 220. The closed cross-section portion 205 has a rectangular cross-section, and a part of the outer surface thereof is fixed to the lower surface 201d of the top plate portion 201 by welding. In this example, it is assumed that the first steel plate 210 and the second steel plate 220 have the same plate thickness t.
[0080]
　In such a structural member 200, the cross-sectional area of ​​the cross section in the width direction of the structural member is represented by the product of the plate thickness t of the steel plate and the total line length L. The total line length L is the sum of the line length L 1 of the top plate portion 201 constituting the structural member 200, the line length L 2 of the wall portion 203, and the line length L 3 of the closed cross-section portion 205 . Further, the structural member 200 has a first region Z1 on the first edge portion 201a side (inside the curve) from the center of the structural member width Wp on the vertical cut surface (BB cut surface) along the structural member width direction. And a second region Z2 on the second edge portion 201b side (curved outer side) from the center of the structural member width Wp. The fact that the cross section in the width direction of the structural member is asymmetric means that the ratio S in / S out of the cross-sectional area S in of the first region Z1 to the cross- sectional area S out of the second region Z2 is the following equation (1). Suppose it is time to meet. At this time, the cross-sectional area S in and the cross-sectional area S out are represented by the following equations (1-1) and (1-2). Incidentally, L 1in the line length L of the top plate portion 201 1 of the shows the line length of the curved inside the center of the structural member width Wp, L 1out is line length of the top plate portion 201 L 1Of these, the line length on the curved outer side from the center of the structural member width Wp is shown.
[0081]
　1.15 ≤ S in / S out ≤ 2.65 ... (1)
　　　S in = (L 1 in + L 3 ) x t ... (1-1)
　　　S out = (L 1 out + L 2 ) x t ... ・ ・ (1-2)
[0082]
　As shown in FIG. 16, in a curved structural member 200 having an open cross section in the width direction of the structural member and a closed cross section 205 provided inside the curvature, the cross section asymmetry satisfying the above equation (1). By giving the property, a large amount of mass is arranged on the inside of the curve from the neutral line Lc as compared with the outside of the curve from the neutral line Lc (see FIG. 10). As a result, the occurrence of out-of-plane deformation of the structural member 200 can be suppressed, and the front-rear bending strength can be increased. Further, the structural member 200 is provided with a cross-sectional asymmetry satisfying the above formula (1) so that too much mass is not arranged inside the curve as compared with the outside of the curve, and the neutral line Lc is placed inside the curve. It is possible to prevent the movement from decreasing in weight efficiency.
[0083]
　Further, preferably, the cross section in the width direction of the structural member is asymmetric, and the ratio S in / S out of the cross-sectional area S in of the first region Z1 to the cross- sectional area S out of the second region Z2 is expressed by the following formula. It is time to satisfy (1').
[0084]
　1.15 ≤ S in / S out ≤ 2.35 ... (1')
[0085]
　As shown in FIG. 16, a cross section satisfying the above formula (1') in a curved structural member 200 having an open cross section in the width direction of the structural member and a closed cross section 205 provided inside the curve. By providing the asymmetry, not only the same effect as in the case of satisfying the above equation (1) can be obtained, but also the mass of the structural member 200 is further reduced. As a result, the structural member 200 is further reduced in weight.
[0086]
　Regarding the cross-sectional area, when the closed cross-sectional portion 205 of the structural member 200 is filled with resin or when the closed cross-sectional portion 205 is made of a solid member, that portion is also included in the cross-sectional area in the above formula (1-). 1) is calculated. Further, in the above description, the first steel plate 210 and the second steel plate 220 have the same plate thickness t, but the plate thicknesses of the first steel plate 210 and the second steel plate 220 may be different. .. For example, in the structural member 200 of FIG. 16, when the plate thickness of the first steel plate 210 is t 1 and the plate thickness of the second steel plate 220 is t 2 , the following equations (2-1) and (2-2) ), The cross-sectional area S in and the cross-sectional area S out may be calculated, and the cross-sectional area ratio S in / S out may be calculated based on the above formula (1) or (1') .
[0087]
　　　S in = (L 1in x t 1 ) + (L 3 x t 2 ) ... (2-1)
　　　S out = (L 1out + L 2 ) x t 1　　　　　　... (2-2)
[0088]
　When the closed cross-section portion 105 is formed of the same steel plate as the steel plate forming the top plate portion 101 as in the configuration example A of FIG. 2, the cross-sectional area ratio S in / S out is set in the same manner as described above. Can be sought. Specifically, the total line length L is the line length L of the top plate 101 constituting the structural member 100A 1 line length L of the wall portion 103 2 line length L and of closed-section portion 105 3 is the sum of. Furthermore, L 1in the line length L of the top plate portion 101 1 of the shows the line length of the curved inside the center of the structural member width, L 1out is line length L of the top plate portion 101 1 of the structural member The line length outside the curve from the center of the width is shown. At this time, the cross-sectional area S in and the cross-sectional area S out are expressed by using the above formulas (1-1) and (1-2), and the cross- sectional area ratio S in / S out is further expressed in the above formula (1). Alternatively, the cross section of the structural member 100A in the width direction of the structural member is asymmetric so as to satisfy (1'). Further, when the closed cross-section portion 105 is formed of a plurality of members as in the configuration examples B and C of FIGS. 3 and 4, the cross-sectional area ratio S is the same as described above. The cross sections of the structural members 100B and C in the width direction of the structural members are asymmetric so that in / S out satisfies the above formula (1) or (1').
[0089]
　Further, in the description of the above configuration examples B and C, it is assumed that the first steel plates 110B and C and the second steel plates 120B and C have the same plate thickness t, but the first steel plates 110B and C and the second steel plates have the same thickness t. The thickness of the steel plates 120B and C may be different. For example, in the structural member 100B of FIG. 3, when the plate thickness of the first steel plate 110B is t 1 and the plate thickness of the second steel plate 120B is t 2 , the following equations (2-3) and (2-4) ), The cross-sectional area S in and the cross-sectional area S out may be calculated, and the cross-sectional area ratio S in / S out may be calculated based on the above formula (1) or (1') . The line length L 3-1 is the line length of the portion of the line length L 3 of the closed cross section 105 along the first steel plate 110B, and the line length L 3-2 is the line length L 3-2 of the closed cross section 105. This is the line length of the portion of the line length L 3 along the second steel plate 120B.
[0090]
　　　S in = (L 1 in x t 1 ) + (L 3-1 x t 1 ) + (L 3-2 x t 2 ) ... (2-3)
　　　S out = (L 1 out + L 2 ) x t 1　　　　　　... (2-4)
[0091]
(Structural member that effectively suppresses out-of-plane deformation)
　The structural member 200 according to the present embodiment is particularly effective in suppressing out-of-plane deformation when it has a shape in which out-of-plane deformation is likely to occur. Specifically, when the plate thickness, component size, and strength of the steel plate constituting the structural member 200 are within the following ranges, the cross section in the width direction of the structural member is an open cross section and a closed cross section inside the curve. It is preferable to use a curved structural member shape provided with the portion 205.
[0092]
　When the plate thickness of the structural member 200 is t ≦ 2.9 mm, it is desirable to have the structural member shape according to the present embodiment. The reason for this is that, as shown in FIG. 11, when the plate thickness is thin and out-of-plane deformation is likely to occur, the value of the proportional limit strength becomes small.
[0093]
　FIG. 17 shows the relationship between the plate thickness of the structural member 200 and the performance improvement ratio of the proportional limit strength. In the same thickness, the proportional limit strength in the case of a structural example B showing the shape of the structural member 200 in FIG. 3 P 1 proportional when the, was substantially U-shaped cross-section showing the shape of the structural member 200 in FIG. 12 When the limit strength is P 2 , the performance improvement ratio of the proportional limit strength is obtained by (P 1 − P 2 ) / P 2 . The larger the value of the performance improvement ratio of the proportional limit strength, the higher the effect of increasing the proportional limit strength when the structural member shape according to the present embodiment is applied.
[0094]
　As shown in FIG. 17, it can be seen that the higher the plate thickness, the smaller the performance improvement ratio of the proportional limit, and even if the cross-sectional shape of the structural member 200 is the cross-sectional shape of the structural example B, the proportional limit is not so improved. Specifically, when the plate thickness was 3.6 mm, the performance improvement ratio of the proportional limit strength was 0.63. On the other hand, the thinner the plate thickness, the larger the performance improvement ratio of the proportional limit, and the proportional limit is improved by changing the cross-sectional shape of the structural member 200 to the cross-sectional shape of the structural example B. In particular, when the plate thickness of the thin-walled material is 2.9 mm or less, the performance improvement ratio of the proportional limit becomes large. Specifically, when the plate thickness was 2.9 mm, the performance improvement ratio of the proportional limit strength was 0.96. Further, when the plate thickness was 2.3 mm, the performance improvement ratio of the proportional limit strength was 1.58. Therefore, when the plate thickness t of the structural member 200 is 2.9 mm or less, it is desirable to use the structural member shape according to the present embodiment.
[0095]
　Further, in order to secure the proportional limit strength required for the structural member 200, it is necessary to increase the plate thickness, but if the plate thickness is increased, the weight of the component also increases. If the plate thickness t can be set to 2.9 mm or less, the weight of the component can be reduced by 20% or more. Therefore, when the plate thickness t of the structural member 200 is 2.9 mm or less, the structural member shape according to the present embodiment is used. Is desirable. As the plate thickness of the structural member 200 here, the maximum plate thickness of each member constituting the structural member 200 may be considered.
[0096]
　The larger the area of ​​the top plate 201 of the structural member 200, the greater the out-of-plane deformation. The area of ​​the top plate portion 201 can be calculated from the arm length W of the structural member 200 and the structural member width Wp. That is, the larger the arm length W and the larger the structural member width Wp, the more effectively the occurrence of out-of-plane deformation in the structural member 200 can be suppressed by adopting the structural member shape according to the present embodiment.
[0097]
　Here, FIG. 18 shows one relationship between the tensile strength and the proportional limit strength per unit component weight for the structural members A and B having two different component dimensions. The structural member A has an arm length W320 mm and a structural member width Wp60 mm, and the structural member B has an arm length W350 mm and a structural member width Wp70 mm. The plate thickness is 3.6 mm for both structural members A and B. That is, the area of ​​the top plate portion 201 is larger in the structural member B than in the structural member A, and out-of-plane deformation is likely to occur.
[0098]
　Looking at FIG. 18, with respect to the structural member A, the proportional limit strength per unit component weight also increases as the tensile strength increases. On the other hand, for the structural member B, which has a larger area of ​​the top plate 201 than the structural member A, the value of the proportional limit strength per unit component weight does not exceed even if the tensile strength increases, and shows a constant value. There is. That is, in a structural member having a large area of ​​the top plate portion 201 and a large out-of-plane deformation, it can be said that the proportional limit strength does not increase even if the strength of the steel plate is increased. Therefore, for a structural member such as the structural member B, which is prone to out-of-plane deformation, the occurrence of out-of-plane deformation in the structural member can be effectively suppressed by adopting the structural member shape according to the present embodiment. For example, when the arm length W is W ≧ 350 mm, particularly W ≧ 370 mm, it is desirable to have the structural member shape according to the present embodiment. Further, regarding the structural member width Wp, when Wp ≧ 70 mm, particularly Wp ≧ 75 mm, it is desirable to have the structural member shape according to the present embodiment.
[0099]
　Further, the structural member 200 has a longer elastic region and is more likely to be out-of-plane deformation as the steel plate forming the structural member 200 is made of a high-strength material. From FIG. 18, it can be seen that as the tensile strength of both the structural members A and B increases, the proportional limit strength per unit component weight increases. Therefore, when the steel plate forming the structural member 200 is a high-strength material, the occurrence of out-of-plane deformation in the structural member 200 can be effectively suppressed by adopting the structural member shape according to the present embodiment. For example, as shown in FIG. 18, for the structural member B in which out-of-plane deformation is likely to occur, the tensile strength Ts is set to the present embodiment when the proportional limit strength does not increase even if the strength of the steel plate is increased, that is, when Ts ≧ 780 MPa. It is desirable to have such a structural member shape.
Example
[0100]
　Regarding the structural member 100 according to the present invention, the mass (part mass) of the structural member required to secure the performance of the proportional limit strength of 25 kN was investigated. Regarding the structural member 100 of the present invention, the structural member 100D of the configuration example D shown in FIG. 5 is shown in Examples 1, 2, 5 to 7, and the structural member 100A of the configuration example A shown in FIG. 2 is shown in the third embodiment. Taking the structural member 100B of the configuration example B shown in 3 as the fourth embodiment, the mass (part mass) of the structural member 100 required to secure the performance of the proportional limit strength of 25 kN was calculated. Further, as Comparative Example 1, in order to secure the performance of the proportional limit strength of 25 kN as an example of the value required for the automobile in the configuration of the closed cross-sectional shape having the wall portion on the curved outer side and the curved inner side shown in FIG. The required mass of structural members (part mass) was calculated. The results are shown in Table 1 below. Table 1 shows the cross-sectional areas calculated based on the above formulas (1), (1-1) and (1-2) or the above formulas (1), (2-1) and (2-2). The cross-sectional area ratio S in / S out of S out and cross-sectional area S in is also shown.
[0101]
[table 1]

[0102]
　From Table 1, the mass (part mass) of the structural member 100 required to secure the performance of the proportional limit strength of 25 kN by adopting the shapes of the structural members of Examples 1 to 7 is 20 with respect to Comparative Example 1. It was reduced by about 30%. Further, as shown in Examples 1 to 6, when the cross-sectional area ratio is 2.65 or less, the mass of the parts is smaller than 2.0 kg, and the weight reduction effect is obtained. Further, as shown in Examples 1 to 5, when the cross-sectional area ratio is 2.35 or less, the mass of the parts is smaller than 1.9 kg, and a higher weight reduction effect is obtained. From this, it was shown that the required proportional limit strength can be achieved while ensuring the weight efficiency of the structural member 100 by adopting the configuration of the structural member 100 of the present invention.
[0103]
　Further, regarding the structural member 100 according to the present embodiment, the relationship between the aspect ratio α / β of the closed cross-section portion 105 and the amount of out-of-plane deformation was investigated. Specifically, the point P in FIG. 10 of the structural member 100 1 giving load to examined the plane deformation amount when is 10mm deformed in the longitudinal direction of the automobile body. In Table 2, the longest length in the structural member width direction (horizontal direction) of the structural member 100 closed cross-section portion 105 is α, and the longest length in the direction perpendicular to the structural member width direction (longitudinal direction) of the structural member 100 closed cross-section portion 105 is set. The relationship between the aspect ratio α / β value when β is set and the amount of out-of-plane deformation is summarized.
[0104]
[Table 2]

[0105]
　From Table 2, by setting the aspect ratio of the closed cross-section portion 105 of Examples 8 to 12 to α / β, the amount of out-of-plane deformation becomes 7.0 mm or less, which is within a predetermined reference range, and the closed cross-section portion 105 is reinforced. It was shown that the effect was fully exerted. On the other hand, in the aspect ratios α / β of Comparative Examples 2 and 3, as a result of the closed cross-section portion 105 having a vertically long or horizontally long flat shape, the amount of out-of-plane deformation exceeds a predetermined reference range, and the closed cross-section portion 105 It was shown that the reinforcing effect was not sufficiently obtained. From this, it was shown that a sufficient reinforcing effect is exhibited by setting the closed cross-sectional portion 105 of the structural member 100 of the present invention to a predetermined aspect ratio.
[0106]
　Although the preferred embodiments of the present invention have been described in detail with reference to the accompanying drawings, the present invention is not limited to such examples. It is clear that a person having ordinary knowledge in the field of technology to which the present invention belongs can come up with various modifications or modifications within the scope of the technical ideas described in the claims. , These are also naturally understood to belong to the technical scope of the present invention.
Code description
[0107]
　100, 100A-100D', 200 Structural members
　101, 201 Top plate
　101a, 201a First edge
　101b, 201b Second edge
　101c Top
　101d Bottom
　103, 203 Wall
　105, 105', 205 Closed cross section
　110B, 110C, 110D, 210 First steel plate
　120B, 120C, 120D, 220 Second steel plate
　130 Resin filler
　Z1 First region
　Z2 Second region
The scope of the claims
[Claim 1]
　A structural member,
　the structural member,
　a top plate portion having a second edge portion opposite the first edge and the first edge,
　and the top plate portion from said second edge a wall portion extending in a direction intersecting,
　and the closed cross-section portion provided on the first edge
has a
　first edge, an inner side of the top plate portion in plan view with respect to the top plate portion When
　the distance from the first edge portion of the structural member to the second edge portion of the structural member
　is defined as the structural member width, the closed cross-sectional portion is provided inside the curvature of the top plate portion. A closed cross section is formed at
　the vertical cut surface of the structural member along the direction of the structural member width, and the vertical cut surface of the structural member along the direction of the structural member width has an open cross section, and the
　closed cross section portion. The structural member, wherein the shape of the vertical cross-section of the structural member is asymmetric with respect to the center of the width of the structural member.
[Claim 2]
　In the vertical cut surface, the structural member has a first region on the first edge side from the center of the length of the structural member width and a second region on the second edge side from the center of the structural member width. In the
　vertical cut surface having two regions and including the closed cross-sectional portion, the cross-sectional area ratio S in / S out of the cross- sectional area S in of the first region to the cross- sectional area S out of the second region. Is the structural member according to claim 1, which satisfies the following relational expression. 1.15 ≤ S in / S out ≤ 2.65
[Claim 3]
　The structural member according to claim 1 or 2, wherein the top plate portion, the wall portion, and the closed cross-section portion are formed of one member.
[Claim 4]
　The structural member according to claim 1 or 2, wherein the closed cross-section portion is formed of one member different from the member forming the top plate portion.
[Claim 5]
　The structural member according to claim 1 or 2, wherein the closed cross-section portion is provided adjacent to the top plate portion.
[Claim 6]
　The structural member according to claim 1 or 2, wherein the closed cross-section portion is formed of a plurality of members.
[Claim 7]
　The structural member includes a
　first member forming the top plate portion, the wall portion, and a part of the closed cross-section portion, and
　a second member forming the closed cross-section portion together with the first member. When,
is formed by,
　the ends of the second member, said first welded to the member, the structural member according to claim 6.
[Claim 8]
　In the vertical cut surface, when the longest length in the direction of the structural member width in the closed cross section is α, and the longest length in the direction perpendicular to the direction of the structural member width in the closed cross section is β. The structural member according to any one of claims 1 to 7, wherein α / β satisfies the following relational expression.
3/7 ≤ α / β ≤ 7/3
[Claim 9]
　The structural member according to any one of claims 1 to 8, wherein the cross-sectional shape of the closed cross-sectional portion is rectangular.
[Claim 10]
　The structural member according to any one of claims 1 to 9, wherein the closed cross-section portion is made of a hollow member.
[Claim 11]
　The structural member according to claim 10, wherein the hollow portion of the closed cross section is filled with a resin filler.
[Claim 12]
　The structural member according to any one of claims 1 to 9, wherein the closed cross-section portion is made of a solid member.
[Claim 13]
　The structural member according to any one of claims 1 to 12, wherein the structural member is a structural member of an automobile.
[Claim 14]
　The structural member according to any one of claims 1 to 12, wherein the structural member is an automobile suspension component.
[Claim 15]
　The structural member according to any one of claims 1 to 14, wherein the tensile strength of the structural member is 780 MPa or more.
[Claim 16]
　The structural member according to any one of claims 1 to 15, wherein the plate thickness of the structural member is 2.9 mm or less.
[Claim 17]
　The structural member according to any one of claims 1 to 16, wherein the arm length of the structural member is 350 mm or more.
[Claim 18]
　The structural member according to any one of claims 1 to 17, wherein the structural member width of the structural member is 70 mm or more.