JP2003260531A - Method for manufacturing strong structural member, and strong structural member - Google Patents

Method for manufacturing strong structural member, and strong structural member

Info

Publication number
JP2003260531A
JP2003260531A JP2002064047A JP2002064047A JP2003260531A JP 2003260531 A JP2003260531 A JP 2003260531A JP 2002064047 A JP2002064047 A JP 2002064047A JP 2002064047 A JP2002064047 A JP 2002064047A JP 2003260531 A JP2003260531 A JP 2003260531A
Authority
JP
Japan
Prior art keywords
structural member
strength
diameter side
manufacturing
hollow tube
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP2002064047A
Other languages
Japanese (ja)
Other versions
JP3811947B2 (en
Inventor
Hiroshi Sakurai
寛 桜井
Hideji Saeki
秀司 佐伯
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Nissan Motor Co Ltd
Original Assignee
Nissan Motor Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Nissan Motor Co Ltd filed Critical Nissan Motor Co Ltd
Priority to JP2002064047A priority Critical patent/JP3811947B2/en
Publication of JP2003260531A publication Critical patent/JP2003260531A/en
Application granted granted Critical
Publication of JP3811947B2 publication Critical patent/JP3811947B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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  • Shaping Metal By Deep-Drawing, Or The Like (AREA)

Abstract

<P>PROBLEM TO BE SOLVED: To provide a method for manufacturing a strong structural member which can manufacture a strong structural member without the need to provide a number of welding equipment, can simplify the behavior of springback at the time of press molding and, at the same time, can ensure the accuracy of a component in a short time. <P>SOLUTION: A tapered hollow tube 1, which has been integrally formed from a steel sheet S having strain aging properties, is subjected to contracting for reducing the taper, by spinning or swaging, to provide a strain gradient from one end 2a (1a) located on a smaller-diameter side of the hollow tube 2 (1) toward the other end 2b (1b) located on a larger-diameter side. Thereafter, this hollow tube 2 is molded into a component shape followed by heat treatment to manufacture a strong structural member 4 having a strength gradient from one end 4a toward the other end 4b. <P>COPYRIGHT: (C)2003,JPO

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【発明の属する技術分野】本発明は、例えば、自動車の
構造部材として用いられて、衝突時の衝撃エネルギを吸
収して衝撃を和らげるのに利用される強度構造部材の製
造方法および強度構造部材に関するものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a method of manufacturing a strong structural member used as a structural member of an automobile, for example, for absorbing impact energy at the time of collision and softening the impact, and a strong structural member. It is a thing.

【0002】[0002]

【発明が解決しようとする課題】上記したような強度構
造部材において、その素材となるブランク材は、板厚や
強度が異なる板材同士をレーザ溶接やシーム溶接によっ
て接合することによって形成される都合上、このブラン
ク材に対してよりきめ細かな板厚分布と強度分布を与え
ようとする場合には、溶接する板の枚数を増やす必要が
ある。つまり、後の行程でプレス成形される1個のブラ
ンク材を形成するためには、何枚もの板材を溶接しなく
てはならず、その分だけ、多くの溶接設備が必要になる
という問題があった。
In the above-described strength structural member, the blank material used as the material is conveniently formed by joining plate materials having different plate thicknesses and strengths by laser welding or seam welding. In order to give a finer plate thickness distribution and strength distribution to this blank material, it is necessary to increase the number of plates to be welded. That is, in order to form one blank material that is press-molded in the subsequent process, many plate materials must be welded, and accordingly, a lot of welding equipment is required. there were.

【0003】また、このような板厚や強度が異なる板材
同士を接合してなるブランク材に対してプレス加工を施
す場合には、1枚の板材にプレス加工を施す場合と比較
してスプリングバックの挙動が複雑になるうえ、とく
に、強度の高い板材あるいはヤング率の低い軽合金を使
用する場合には、より大きなスプリングバックが発生す
るため、短時間に部品精度を確保することが困難である
という問題があり、これらの問題を解決することが従来
の課題であった。
Further, in the case where the blank material formed by joining the plate materials having different plate thicknesses and strengths is subjected to the press working, compared with the case where the press working is performed on one plate material, the spring back is performed. Behavior becomes complicated, and especially when using a plate material with high strength or a light alloy with a low Young's modulus, larger springback occurs, so it is difficult to secure component accuracy in a short time. Therefore, it has been a conventional problem to solve these problems.

【0004】[0004]

【発明の目的】本発明は、上記した従来の課題に着目し
てなされたもので、多くの溶接設備を必要とすることな
く強度構造部材を製造することができ、加えて、プレス
成形時のスプリングバックの挙動が単純でかつ短時間の
うちに部品精度を確保することが可能である強度構造部
材の製造方法および強度構造部材を提供することを目的
としている。
SUMMARY OF THE INVENTION The present invention has been made in view of the above-mentioned problems of the prior art, and it is possible to manufacture a strong structural member without requiring a lot of welding equipment. It is an object of the present invention to provide a method for manufacturing a strength structural member and a strength structural member that have a simple springback behavior and can secure component accuracy in a short time.

【0005】[0005]

【課題を解決するための手段】本発明の請求項1に係わ
る強度構造部材の製造方法は、ひずみ時効性を有する鋼
板から一体に形成されてなるテーパ状の中空管にスピニ
ングあるいはスウェージングによるテーパを減らす縮管
成形を施して、中空管の小径側に位置する一方の端部か
ら大径側に位置する他方の端部にかけてひずみ勾配をも
たせた後、この中空管を部品形状に成形するのに続いて
熱処理を行って、上記一方の端部から上記他方の端部に
かけて強度勾配を有する強度構造部材を製造する構成と
したことを特徴としており、この強度構造部材の製造方
法の構成を前述した従来の課題を解決するための手段と
している。
According to a first aspect of the present invention, there is provided a method for manufacturing a strength structural member by spinning or swaging a tapered hollow tube integrally formed from a steel plate having strain aging. After performing shrinkage tube molding to reduce the taper and giving a strain gradient from one end located on the small diameter side of the hollow tube to the other end located on the large diameter side, this hollow tube is formed into a part shape. After molding, heat treatment is performed, and the structure is characterized in that a strength structural member having a strength gradient from the one end to the other end is manufactured. The configuration is a means for solving the above-mentioned conventional problems.

【0006】本発明の請求項2に係わる強度構造部材の
製造方法において、ひずみ時効性を有する鋼板から一体
に形成されてなるテーパ状の中空管に小径側に位置する
一方の端部の直径および板厚を維持したままスピニング
あるいはスウェージングによるテーパを減らす縮管成形
を施して、中空管の小径側に位置する一方の端部から大
径側に位置する他方の端部にかけて漸次板厚が増加する
板厚勾配をもたせた後、この中空管を部品形状に成形す
るのに続いて熱処理を行って、上記一方の端部から上記
他方の端部にかけて板厚勾配および強度勾配を有する強
度構造部材を製造する構成としたことを特徴としてお
り、この強度構造部材の製造方法の構成を前述した従来
の課題を解決するための手段としている。
In the method of manufacturing a strength structural member according to claim 2 of the present invention, the diameter of one end located on the small diameter side in a tapered hollow tube integrally formed from a steel sheet having strain aging. And while reducing the taper due to spinning or swaging while maintaining the plate thickness, the plate thickness is gradually increased from one end located on the small diameter side of the hollow pipe to the other end located on the large diameter side. Of the hollow tube is formed, and then the hollow tube is formed into a shape of a part and then heat-treated to have a thickness gradient and a strength gradient from the one end to the other end. The present invention is characterized in that it is configured to manufacture a strength structural member, and the structure of the method for manufacturing the strength structural member is used as means for solving the above-mentioned conventional problems.

【0007】本発明の請求項3に係わる強度構造部材の
製造方法において、大径側の他方の端部の縮管率を8〜
25%とした構成とし、本発明の請求項4に係わる強度
構造部材の製造方法において、小径側の一方の端部の縮
管率を0〜2%とした構成としている。
In the method for manufacturing a strength structural member according to claim 3 of the present invention, the contraction rate of the other end portion on the large diameter side is 8 to 8.
25%, and in the method for manufacturing a strength structural member according to claim 4 of the present invention, the shrinkage rate at one end on the small diameter side is set to 0 to 2%.

【0008】本発明の請求項5に係わる強度構造部材の
製造方法において、小径側の一方の端部の相当ひずみを
0.035以下とし、大径側の他方の端部の相当ひずみ
を0.09以上とした構成とし、本発明の請求項6に係
わる強度構造部材の製造方法において、大径側の他方の
端部における縮管成形前の板厚に対する板厚増加率を5
%以上とした構成としている。
In the method for manufacturing a strength structural member according to claim 5 of the present invention, the equivalent strain at one end on the small diameter side is 0.035 or less, and the equivalent strain at the other end on the large diameter side is 0. In the method for manufacturing a strength structural member according to claim 6 of the present invention, the plate thickness increase rate with respect to the plate thickness before contraction molding at the other end on the large diameter side is 5 or more.
% And above.

【0009】一方、本発明の請求項7に係わる発明は、
ひずみ時効性を有する鋼板から一体に形成された中空状
の強度構造材において、一方の端部から他方に端部にか
けて強度勾配をもたせてある構成としたことを特徴とし
ており、この強度構造部材の構成を前述した従来の課題
を解決するための手段としている。
On the other hand, the invention according to claim 7 of the present invention is
A hollow strength structural material integrally formed from a steel sheet having strain aging is characterized in that a strength gradient is provided from one end to the other end. The configuration is a means for solving the above-mentioned conventional problems.

【0010】本発明の請求項8に係わる強度構造部材に
おいて、一方の端部から他方に端部にかけて漸次板厚が
増加する板厚勾配をもたせてある構成としている。
According to the eighth aspect of the present invention, the strength structural member has a plate thickness gradient in which the plate thickness gradually increases from one end to the other end.

【0011】[0011]

【発明の実施の形態】本発明に係わる強度構造部材の製
造方法において、引張り強度が上昇するひずみ時効型の
鋼板によってテーパ状の中空管を形成し、スピニングあ
るいはスウェージングによってこの中空管のテーパを減
らす縮管成形を行うことにより、中空管の長手方向にひ
ずみ分布と板厚分布を付与した後、このひずみ分布を有
する中空管を部品形状に成形するのに続いて熱処理を行
うことによって、小径側の一方の端部から大径側の他方
の端部に向けて強度勾配および板厚分布を与えることが
可能となる。
BEST MODE FOR CARRYING OUT THE INVENTION In the method for manufacturing a strength structural member according to the present invention, a tapered hollow tube is formed by a strain aging type steel plate having an increased tensile strength, and the hollow tube is formed by spinning or swaging. Strain distribution and plate thickness distribution are given in the longitudinal direction of the hollow tube by reducing the taper to reduce the taper, and then the hollow tube having this strain distribution is formed into a part shape and then heat treatment is performed. This makes it possible to provide a strength gradient and a plate thickness distribution from one end on the small diameter side to the other end on the large diameter side.

【0012】より詳しく述べると、例えば、小径側の一
方の端部は強度が低く、縮管された大径側の他方の端部
に向けて強度を大きくしたり、あるいは、強度に加えて
板厚を大径側の他方の端部に向けて厚くした中空管を成
形することができ、これによって、多数の板材を溶接す
ることなく、ひずみ時効性を有する鋼板から一体に形成
されてなる部材に板圧分布と強度分布を与えることが可
能となる。
More specifically, for example, one end portion on the small diameter side has low strength, and the strength is increased toward the other end portion on the large diameter side which is contracted, or the plate is added to the strength in addition to the strength. It is possible to form a hollow tube whose thickness is increased toward the other end on the large diameter side, and thereby it is integrally formed from a steel plate having strain aging without welding many plate materials. It is possible to give the plate pressure distribution and strength distribution to the member.

【0013】上記スピニングによって中空管の長手方向
にひずみ分布を与えることは可能であるが、断面の大き
さが変化する中空管の断面が大きな箇所に対して、より
大きなひずみを与えたり、板厚の増肉を行ったりするこ
とは、スピニング加工の性質上困難である。そこで、本
発明に係わる強度構造部材の製造方法では、素材とする
中空管にテーパを与えて、小さい断面の部分については
絞り成形を行わず、大きな断面の部分を縮管して断面が
大きい部分に大きなひずみと板厚増肉を形成する。
Although it is possible to give a strain distribution in the longitudinal direction of the hollow tube by the above spinning, a larger strain is given to a portion having a large cross section of the hollow tube in which the size of the cross section changes, It is difficult to increase the plate thickness due to the nature of the spinning process. Therefore, in the method of manufacturing a strength structural member according to the present invention, the hollow tube used as a material is tapered, and a portion having a small cross section is not drawn, and a portion having a large cross section is contracted to have a large cross section. Large strain and thickening are formed in the part.

【0014】ここで、使用する鋼板としてひずみ時効性
をほとんど持たない鋼板を用いると、加工硬化によって
耐力は増加するが、強度が大きく上昇することは望めな
い。そこで、例えば、耐力のみならず強度も増加するひ
ずみ時効性を有する材料を使用して、自動車の焼きつけ
塗装工程における典型的な熱処理である170℃で20
分間の熱処理を行うことによって、より大きな耐力およ
びより大きな強度を大きなひずみを加えた部位に付与す
ることが可能となり、したがって、異なる板厚および異
なる強度レベルの材料同士を溶接等によって接合するこ
となく、ひずみ時効性を有する鋼板から一体に形成され
てなる1つの中空管に強度勾配、さらには板厚分布を与
えることができる。
When a steel sheet having almost no strain aging is used as the steel sheet to be used, the yield strength increases due to work hardening, but the strength cannot be expected to increase significantly. Therefore, for example, a material having a strain aging property that increases not only the proof stress but also the strength is used, and at a temperature of 170 ° C., which is a typical heat treatment in the baking and painting process of automobiles,
By performing the heat treatment for a minute, it becomes possible to give greater yield strength and greater strength to a portion to which a large strain is applied, and therefore, it is possible to weld materials having different plate thicknesses and different strength levels without welding. It is possible to give a strength gradient and further a plate thickness distribution to one hollow tube integrally formed from a steel plate having strain aging.

【0015】このようにして、テーパ付きの中空管をス
ピニング加工によって、断面の大きな箇所により大きな
縮管成形を行い、この中空管に使用する鋼板に自動車の
焼き付け塗装工程等において耐力および強度が上昇する
鋼板を用いることで、長手方向に強度勾配を有する強度
構造部材を得ることができる。
In this manner, a tapered hollow tube is subjected to spinning to form a large shrink tube at a portion having a large cross section, and a steel sheet used for the hollow tube is subjected to a proof stress and a strength in a baking process of an automobile or the like. By using a steel plate having an increased strength, a strength structural member having a strength gradient in the longitudinal direction can be obtained.

【0016】[0016]

【発明の効果】本発明に係わる強度構造部材の製造方法
によれば、上記した構成としているので、多くの溶接設
備を用いることなく、一方の端部から他方の端部に向け
て強度勾配を有する強度構造部材を製造することができ
るのに加えて、プレス成形時のスプリングバックの挙動
を単純なものとすることができると共に、部品精度を短
時間のうちに確保することが可能であるという非常に優
れた効果がもたらされる。
According to the method of manufacturing a strength structural member according to the present invention, since it has the above-mentioned structure, the strength gradient is increased from one end to the other end without using a lot of welding equipment. In addition to being able to manufacture a strong structural member having, it is possible to simplify the behavior of springback at the time of press molding and to ensure the accuracy of parts in a short time. Very good effect.

【0017】本発明に係わる強度構造部材によれば、上
記した構成としたから、溶接設備をほとんど不要なもの
とすることができるうえ、プレス成形時におけるスプリ
ングバックの挙動が単純化すると共に、部品精度が短時
間のうちに確保されるという非常に優れた効果がもたら
される。
Since the strength structural member according to the present invention has the above-mentioned structure, the welding equipment can be almost unnecessary, and the behavior of the spring back at the time of press molding can be simplified and the parts can be easily manufactured. This has an extremely excellent effect of ensuring accuracy in a short time.

【0018】[0018]

【実施例】以下、本発明を図面に基づいて説明する。DESCRIPTION OF THE PREFERRED EMBODIMENTS The present invention will be described below with reference to the drawings.

【0019】[実施例1]図1は、本発明に係わる強度
構造部材の製造方法の一実施例による製造工程を示して
いる。
[Embodiment 1] FIG. 1 shows a manufacturing process according to an embodiment of a method for manufacturing a strength structural member according to the present invention.

【0020】この実施例による強度構造部材の製造方法
では、まず、図1(a)に示すように、引張り強度が4
60MPaでかつ板厚が1.8mmのひずみ時効性を有
する鋼板Sを丸めて長さ500mmのテーパ管状に成形
し、鋼板Sの端縁同士をシーム溶接で接合することによ
って、小径側の一方の端部1aにおける直径が100m
mで大径側の他方の端部1bにおける直径が150mm
のテーパ状の中空管1を形成する。
In the method of manufacturing a strength structural member according to this embodiment, first, as shown in FIG.
A steel plate S having a strain aging property of 60 MPa and a plate thickness of 1.8 mm is rolled into a tapered tubular shape having a length of 500 mm, and the edges of the steel plate S are joined by seam welding to obtain one of the smaller diameter sides. The diameter at the end 1a is 100 m
m, the diameter at the other end 1b on the large diameter side is 150 mm
The tapered hollow tube 1 is formed.

【0021】次に、図1(b)に示すように、スピニン
グローラR,Rを使用してこの中空管1にスピニング加
工を行うことによって、図1(c)に示すように、小径
側の一方の端部2aにおける直径が100mmで大径側
の他方の端部2bにおける直径が120mmのテーパ状
の中空管2とする。
Next, as shown in FIG. 1 (b), by spinning the hollow tube 1 using spinning rollers R, R, as shown in FIG. 1 (c), the small diameter side The tapered hollow tube 2 has a diameter of 100 mm at one end 2a and a diameter of 120 mm at the other end 2b on the large diameter side.

【0022】このとき、中空管2の板厚は、全長にわた
って1.8mmになった。また、中空管2の全長は、中
空管1よりも長くなったが、素材としての鋼板Sの長さ
に比較すると、全長に対する縮管率、すなわち、各部位
の直径とこれに対応する縮管前の各部位との直径の比
が、図1(d)のグラフに示すように、直線的に変化す
るように成形することができた。
At this time, the plate thickness of the hollow tube 2 was 1.8 mm over the entire length. Further, although the total length of the hollow tube 2 is longer than that of the hollow tube 1, compared with the length of the steel plate S as a raw material, the contracted tube ratio to the total length, that is, the diameter of each portion and the corresponding It was possible to mold such that the ratio of the diameter of each part before the contraction was linearly changed as shown in the graph of FIG.

【0023】なお、このときの縮管率は、30%を超え
るようにすることも可能であるが、ひずみ分布を与えた
テーパ状の中空管2に対して後工程においてさらに成形
加工を施すためには、縮管率を25%以下に留めること
が望ましい。さらに、ひずみ時効型の鋼板Sを用いてい
る場合には、焼付け硬化処理後の強度の上昇は、縮管率
で8%以上で最も効果的である。
The shrinkage rate at this time can be set to exceed 30%, but the tapered hollow tube 2 having the strain distribution is further subjected to a forming process in a later step. Therefore, it is desirable to keep the shrinkage rate at 25% or less. Further, when the strain-aged steel sheet S is used, the increase in strength after the bake hardening treatment is most effective when the shrinkage ratio is 8% or more.

【0024】従って、自動車のフロントサイドメンバの
ように前端部(図示左側の小径側端部)から優先的に変
形させようとする強度構造部材では、最も変形を抑制し
たい後端部(図示右側の大径側端部)の縮管率は、8%
から25%の間が望ましい。相当ひずみとして表現する
ならば、0.09以上とすることによって焼き付け硬化
処理後の強度上昇が効果的となる。
Therefore, in the case of a strength structural member that is preferentially deformed from the front end (the small diameter side end on the left side in the figure) like the front side member of an automobile, the rear end (the right side in the figure on the right side) in which the deformation is desired to be suppressed most. The contraction rate of the large diameter end) is 8%
Between 25% and 25% is desirable. Expressed as equivalent strain, a strength increase after bake hardening treatment is effective when it is 0.09 or more.

【0025】変形が生じた場合に最も優先的に変形させ
たい前端部では、ひずみ硬化性材料を用いる特徴上、不
必要に大きなひずみを加えることは好ましくない。相当
ひずみ量として0.035以下に留めることによって、
強度の大幅上昇を抑制することができる。また、前端部
の縮管率は、0%〜2%とすることが好ましい。
When deformation occurs, it is not preferable to apply an unnecessarily large strain to the front end portion which is to be deformed most preferentially because of the characteristic of using the strain hardening material. By keeping the equivalent strain amount to 0.035 or less,
A large increase in strength can be suppressed. Further, the shrinkage rate of the front end portion is preferably 0% to 2%.

【0026】次いで、液圧成形型により、初期液圧を1
0MPaとして、中空管2が液圧で拡管しないようにそ
の後の液圧増加を20MPa以下に制御しつつ中空管2
のプレス成形を行って、図1(e)に示すように、部品
形状をなす中空角管3を得た、すなわち、一方の端部3
aの断面が60mm×90mmの小さい四角形状をなし
ていると共に他方の端部3bの断面が80mm×100
mmの大きい四角形状をなす中空角管3を得た。
Then, the initial hydraulic pressure is set to 1 by a hydraulic forming die.
The hollow tube 2 is controlled to 0 MPa while controlling the subsequent increase in hydraulic pressure to 20 MPa or less so that the hollow tube 2 is not expanded by hydraulic pressure.
1 (e), a hollow rectangular tube 3 having a component shape was obtained, that is, one end 3 was formed.
The cross section of a has a small square shape of 60 mm × 90 mm, and the cross section of the other end 3 b is 80 mm × 100.
A rectangular hollow tube 3 having a large mm shape was obtained.

【0027】そして、図1(f)に示すように、この中
空角管3に対して170℃のオーブンで20分間の熱処
理を行った。このようにして製造した強度構造部材4に
おいて、一方の端部4a(図示左端部)のビッカース硬
度はHv=200であり、他方の端部4b(図示右端
部)のビッカース硬度はHv=250であって、全長に
わたって強度分布を有しており、これにより、この実施
例による強度構造部材の製造方法によって、一方の端部
4aから他方の端部4bに向けて強度勾配を有する強度
構造部材4を製造可能であることが実証できた。
Then, as shown in FIG. 1 (f), the hollow rectangular tube 3 was heat-treated in an oven at 170 ° C. for 20 minutes. In the strength structural member 4 thus manufactured, the Vickers hardness of one end 4a (left end in the drawing) is Hv = 200, and the Vickers hardness of the other end 4b (right end in the drawing) is Hv = 250. Therefore, the strength structural member 4 has a strength distribution over the entire length, and thus the strength structural member 4 having a strength gradient from one end 4a to the other end 4b is manufactured by the method for manufacturing a strength structural member according to this embodiment. It has been proved that can be manufactured.

【0028】[実施例2]図2は、本発明に係わる強度
構造部材の製造方法の他の実施例による製造工程を示し
ている。
[Embodiment 2] FIG. 2 shows a manufacturing process according to another embodiment of the method for manufacturing a strength structural member according to the present invention.

【0029】この実施例による強度構造部材の製造方法
では、まず、図2(a)に示すように、引張り強度が4
60MPaでかつ板厚が1.8mmのひずみ時効性を有
する鋼板Sを丸めてテーパ管状に成形し、鋼板Sの端縁
同士をシーム溶接で接合することによって、小径側の一
方の端部21aにおける直径が100mmで大径側の他
方の端部21bにおける直径が125mmのテーパ状の
中空管21を形成する。
In the method of manufacturing a strength structural member according to this embodiment, first, as shown in FIG.
A steel plate S having a strain aging property of 60 MPa and a plate thickness of 1.8 mm is rolled into a tapered tubular shape, and the edges of the steel plate S are joined by seam welding, whereby one end 21a on the small diameter side is joined. A tapered hollow tube 21 having a diameter of 100 mm and a diameter of 125 mm at the other end 21b on the large diameter side is formed.

【0030】次に、図2(b)に示すように、スピニン
グローラR,Rを使用してこの中空管21にスピニング
加工を行うことによって、図2(c)に示すように、小
径側の一方の端部22aから大径側の他方の端部22b
にかけて直径を100mmで一定させた長さ400mm
のストレート状の中空管22とする。
Next, as shown in FIG. 2 (b), by spinning the hollow tube 21 using spinning rollers R, R, as shown in FIG. 2 (c), on the small diameter side. From one end 22a to the other end 22b on the large diameter side
400mm in length with a constant diameter of 100mm
The straight hollow tube 22 of FIG.

【0031】このとき、中空管22の一方の端部22a
における板厚を1.8mmとし、他方の端部22bに向
けて漸次板厚を増して他方の端部22bの板厚が2.0
mmとなるように成形した。また、中空管22の全長は
伸びているが、素材としての鋼板Sの長さに比較する
と、全長に対する板厚分布は、図2(d)のグラフに示
すように、直線的に変化するように成形することができ
た。
At this time, one end 22a of the hollow tube 22 is
And the plate thickness at the other end 22b is 2.0 mm.
It was molded to have a size of mm. Further, although the entire length of the hollow tube 22 is extended, compared with the length of the steel plate S as a material, the plate thickness distribution with respect to the entire length changes linearly as shown in the graph of FIG. Could be molded as.

【0032】次いで、液圧成形型により、初期液圧を1
0MPaとして、中空管22が液圧で拡管しないように
その後の液圧増加を20MPa以下に制御しつつ中空管
22のプレス成形を行って、図2(e)に示すように、
部品形状をなす中空角管23を得た、すなわち、断面が
75mm×75mmの四角形状をなしている中空角管2
3を得た。
Then, the initial hydraulic pressure is set to 1 by a hydraulic forming die.
The pressure is set to 0 MPa, and the hollow pipe 22 is press-molded while controlling the subsequent increase in hydraulic pressure to 20 MPa or less so that the hollow pipe 22 is not expanded by hydraulic pressure, and as shown in FIG.
A hollow square tube 23 having a component shape was obtained, that is, a hollow square tube 2 having a rectangular cross section of 75 mm × 75 mm.
Got 3.

【0033】そして、図2(f)に示すように、この中
空角管23に対して170℃のオーブンで20分間の熱
処理を行った。このようにして製造した強度構造部材2
4において、一方の端部24a(図示左端部)のビッカ
ース硬度はHv=200であり、他方の端部24b(図
示右端部)のビッカース硬度はHv=250であって、
全長にわたって強度分布および板厚分布を有しており、
これにより、この実施例による強度構造部材の製造方法
により、一方の端部24aから他方の端部24bに向け
て強度勾配および板厚勾配を有する強度構造部材24を
製造可能であることが実証できた。
Then, as shown in FIG. 2F, the hollow rectangular tube 23 was heat-treated in an oven at 170 ° C. for 20 minutes. Strength structural member 2 manufactured in this manner
4, the Vickers hardness of one end 24a (left end in the drawing) is Hv = 200, and the Vickers hardness of the other end 24b (right end in the drawing) is Hv = 250.
Has strength distribution and plate thickness distribution over the entire length,
From this, it can be demonstrated that the method for manufacturing a strength structural member according to this example can manufacture a strength structural member 24 having a strength gradient and a plate thickness gradient from one end 24a to the other end 24b. It was

【0034】[実施例3]図3は、本発明に係わる強度
構造部材の製造方法のさらに他の実施例による製造工程
を示している。
[Embodiment 3] FIG. 3 shows a manufacturing process according to still another embodiment of the method for manufacturing a strength structural member according to the present invention.

【0035】この実施例による強度構造部材の製造方法
では、まず、図3(a)に示すように、引張り強度が4
60MPaでかつ板厚が1.8mmのひずみ時効性を有
する鋼板Sを丸めて長さ500mmのテーパ管状に成形
し、鋼板Sの端縁同士をシーム溶接で接合することによ
って、小径側の一方の端部31aにおける直径が100
mmで大径側の他方の端部31bにおける直径が150
mmのテーパ状の中空管31を形成する。
In the method of manufacturing a strength structural member according to this embodiment, first, as shown in FIG.
A steel plate S having a strain aging property of 60 MPa and a plate thickness of 1.8 mm is rounded to form a taper tube having a length of 500 mm, and the edges of the steel plate S are joined by seam welding. The diameter at the end 31a is 100
mm, the diameter at the other end 31b on the large diameter side is 150
A mm-shaped tapered hollow tube 31 is formed.

【0036】次に、図3(b)に示すように、スピニン
グローラR,Rを使用してこの中空管31にスピニング
加工を行うことによって、図3(c)に示すように、小
径側の一方の端部32aにおける直径が100mmで大
径側の他方の端部32bにおける直径が120mmのテ
ーパ状の中空管32とする。
Next, as shown in FIG. 3B, the hollow tube 31 is subjected to a spinning process by using spinning rollers R, R, and as shown in FIG. The tapered hollow tube 32 has a diameter of 100 mm at one end 32a and a diameter of 120 mm at the other end 32b on the large diameter side.

【0037】このとき、中空管32の一方の端部32a
における板厚を1.8mmとし、他方の端部32bに向
けて漸次板厚を増して他方の端部32bの板厚が2.0
mmとなるように成形した。また、素材の長さに対する
中空管32の全長の板厚分布は、図3(d)のグラフに
示すように、直線的に変化するように成形することがで
きた。
At this time, one end 32a of the hollow tube 32
And the plate thickness at the other end 32b is 2.0 mm.
It was molded to have a size of mm. Further, the plate thickness distribution of the entire length of the hollow tube 32 with respect to the length of the material could be molded so as to change linearly as shown in the graph of FIG.

【0038】次いで、液圧成形型により、初期液圧を1
0MPaとして、中空管32が液圧で拡管しないように
その後の液圧増加を20MPa以下に制御しつつ中空管
32のプレス成形を行って、図3(e)に示すように、
部品形状をなす中空角管33を得た、すなわち、すなわ
ち、一方の端部33aの断面が60mm×90mmの小
さい四角形状をなしていると共に他方の端部33bの断
面が80mm×100mmの大きい四角形状をなす中空
角管33を得た。
Next, the initial hydraulic pressure is set to 1 by a hydraulic forming die.
As shown in FIG. 3 (e), the hollow pipe 32 is press-molded while controlling the hydraulic pressure to 20 MPa or less so that the hollow pipe 32 is not expanded by hydraulic pressure.
A hollow rectangular tube 33 having a component shape was obtained, that is, a cross section of one end 33a had a small square shape of 60 mm × 90 mm, and a cross section of the other end 33b had a large square of 80 mm × 100 mm. A hollow rectangular tube 33 having a shape was obtained.

【0039】そして、図3(f)に示すように、この中
空角管33に対して170℃のオーブンで20分間の熱
処理を行った。このようにして製造した強度構造部材3
4において、一方の端部34a(図示左端部)のビッカ
ース硬度はHv=200であり、他方の端部34b(図
示右端部)のビッカース硬度はHv=255であって、
全長にわたって強度分布および板厚分布を有しており、
これにより、この実施例による強度構造部材の製造方法
により、一方の端部34aから他方の端部34bに向け
て強度勾配および板厚勾配を有する強度構造部材34を
製造可能であることが実証できた。
Then, as shown in FIG. 3F, the hollow rectangular tube 33 was heat-treated in an oven at 170 ° C. for 20 minutes. Strength structural member 3 manufactured in this manner
4, the Vickers hardness of one end 34a (left end in the drawing) is Hv = 200, and the Vickers hardness of the other end 34b (right end in the drawing) is Hv = 255.
Has strength distribution and plate thickness distribution over the entire length,
From this, it can be demonstrated that it is possible to manufacture a strength structural member 34 having a strength gradient and a plate thickness gradient from one end 34a to the other end 34b by the method for manufacturing a strength structural member according to this example. It was

【図面の簡単な説明】[Brief description of drawings]

【図1】本発明に係わる強度構造部材の製造方法の一実
施例による製造工程説明図(a)〜(f)である。
FIG. 1 is a manufacturing process explanatory view (a) to (f) according to an embodiment of a method for manufacturing a strength structural member according to the present invention.

【図2】本発明に係わる強度構造部材の製造方法の他の
実施例による製造工程説明図(a)〜(f)である。
2A to 2F are manufacturing process explanatory diagrams according to another embodiment of the method for manufacturing a strength structural member according to the present invention.

【図3】本発明に係わる強度構造部材の製造方法のさら
に他の実施例による製造工程説明図(a)〜(f)であ
る。
FIG. 3 is manufacturing process explanatory diagrams (a) to (f) according to still another embodiment of the method for manufacturing a strength structural member according to the present invention.

【符号の説明】[Explanation of symbols]

1,21,31 テーパ状の中空管 2,22,32 縮管成形後の中空管 2a,22a,32a 縮管成形後の中空管の小径側に
位置する一方の端部 2b,22b,32b 縮管成形後の中空管の大径側に
位置する一方の端部 3,23,33 部品形状に成形した中空角管 4,24,34 強度構造部材 4a,24a,34a 強度構造部材の一方の端部 4b,24b,34b 強度構造部材の他方の端部
1, 21, 31 Tapered hollow tube 2, 22, 32 Hollow tube 2a, 22a, 32a after contracted tube One end 2b, 22b located on the small diameter side of the hollow tube after contracted tube , 32b One end 3,23,33 located on the large diameter side of the hollow tube after the contraction molding Hollow square tube 4,24,34 molded into a component shape Strength structural members 4a, 24a, 34a Strength structural member One end 4b, 24b, 34b The other end of the strength structural member

Claims (8)

【特許請求の範囲】[Claims] 【請求項1】 ひずみ時効性を有する鋼板から一体に形
成されてなるテーパ状の中空管にスピニングあるいはス
ウェージングによるテーパを減らす縮管成形を施して、
中空管の小径側に位置する一方の端部から大径側に位置
する他方の端部にかけてひずみ勾配をもたせた後、この
中空管を部品形状に成形するのに続いて熱処理を行っ
て、上記一方の端部から上記他方の端部にかけて強度勾
配を有する強度構造部材を製造することを特徴とする強
度構造部材の製造方法。
1. A tapered hollow tube integrally formed from a steel plate having strain aging is subjected to a shrink tube forming for reducing a taper due to spinning or swaging,
After applying a strain gradient from one end located on the small diameter side of the hollow tube to the other end located on the large diameter side, heat treatment is subsequently performed after forming this hollow tube into a component shape. A method for manufacturing a strength structural member, comprising manufacturing a strength structural member having a strength gradient from the one end to the other end.
【請求項2】 ひずみ時効性を有する鋼板から一体に形
成されてなるテーパ状の中空管に小径側に位置する一方
の端部の直径および板厚を維持したままスピニングある
いはスウェージングによるテーパを減らす縮管成形を施
して、中空管の小径側に位置する一方の端部から大径側
に位置する他方の端部にかけて漸次板厚が増加する板厚
勾配をもたせた後、この中空管を部品形状に成形するの
に続いて熱処理を行って、上記一方の端部から上記他方
の端部にかけて板厚勾配および強度勾配を有する強度構
造部材を製造することを特徴とする強度構造部材の製造
方法。
2. A taper hollow tube integrally formed of a steel plate having strain aging, which is formed by spinning or swaging while maintaining the diameter and plate thickness of one end located on the small diameter side. After reducing the diameter of the hollow pipe, the hollow pipe has a thickness gradient that gradually increases from one end located on the small diameter side to the other end located on the large diameter side. A strength structural member characterized by producing a strength structural member having a plate thickness gradient and a strength gradient from the one end to the other end by performing heat treatment after forming the pipe into a component shape. Manufacturing method.
【請求項3】 大径側の他方の端部の縮管率を8〜25
%とした請求項1または2に記載の強度構造部材の製造
方法。
3. The contraction rate of the other end on the large diameter side is 8 to 25.
%, The method for manufacturing a strong structural member according to claim 1 or 2.
【請求項4】 小径側の一方の端部の縮管率を0〜2%
とした請求項3に記載の強度構造部材の製造方法。
4. The shrinkage ratio of one end on the small diameter side is 0 to 2%.
The method for manufacturing a strong structural member according to claim 3.
【請求項5】 小径側の一方の端部の相当ひずみを0.
035以下とし、大径側の他方の端部の相当ひずみを
0.09以上とした請求項1ないし4のいずれかに記載
の強度構造部材の製造方法。
5. The equivalent strain of one end on the small diameter side is set to 0.
5. The method for manufacturing a strong structural member according to claim 1, wherein the strain is 035 or less and the equivalent strain of the other end on the large diameter side is 0.09 or more.
【請求項6】 大径側の他方の端部における縮管成形前
の板厚に対する板厚増加率を5%以上とした請求項5に
記載の強度構造部材の製造方法。
6. The method for manufacturing a strength structural member according to claim 5, wherein the plate thickness increase rate with respect to the plate thickness before contraction molding at the other end on the larger diameter side is 5% or more.
【請求項7】 ひずみ時効性を有する鋼板から一体に形
成された中空状の強度構造材において、一方の端部から
他方に端部にかけて強度勾配をもたせてあることを特徴
とする強度構造部材。
7. A strength structural member which is a hollow strength structural member formed integrally from a steel plate having strain aging, wherein a strength gradient is provided from one end to the other end.
【請求項8】 一方の端部から他方の端部にかけて漸次
板厚が増加する板厚勾配をもたせてある請求項7に記載
の強度構造部材。
8. The strength structural member according to claim 7, wherein the strength structural member has a plate thickness gradient in which the plate thickness gradually increases from one end to the other end.
JP2002064047A 2002-03-08 2002-03-08 Manufacturing method of strength structural member Expired - Fee Related JP3811947B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
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Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2002064047A JP3811947B2 (en) 2002-03-08 2002-03-08 Manufacturing method of strength structural member

Publications (2)

Publication Number Publication Date
JP2003260531A true JP2003260531A (en) 2003-09-16
JP3811947B2 JP3811947B2 (en) 2006-08-23

Family

ID=28670981

Family Applications (1)

Application Number Title Priority Date Filing Date
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Country Status (1)

Country Link
JP (1) JP3811947B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108127014A (en) * 2017-12-06 2018-06-08 西安航天动力机械有限公司 A kind of method away from reversed spinning wrong to wheel

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108127014A (en) * 2017-12-06 2018-06-08 西安航天动力机械有限公司 A kind of method away from reversed spinning wrong to wheel
CN108127014B (en) * 2017-12-06 2019-05-31 西安航天动力机械有限公司 The wrong method away from reversed spinning of a kind of pair of wheel

Also Published As

Publication number Publication date
JP3811947B2 (en) 2006-08-23

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