WO2013038580A1 - 中空部材及び中空部材の製造方法 - Google Patents
中空部材及び中空部材の製造方法 Download PDFInfo
- Publication number
- WO2013038580A1 WO2013038580A1 PCT/JP2012/002781 JP2012002781W WO2013038580A1 WO 2013038580 A1 WO2013038580 A1 WO 2013038580A1 JP 2012002781 W JP2012002781 W JP 2012002781W WO 2013038580 A1 WO2013038580 A1 WO 2013038580A1
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- WIPO (PCT)
- Prior art keywords
- peripheral wall
- hollow member
- hardness
- torsion beam
- heat treatment
- Prior art date
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- 238000004519 manufacturing process Methods 0.000 title claims description 9
- 238000000034 method Methods 0.000 title claims description 9
- 230000002093 peripheral effect Effects 0.000 claims abstract description 75
- 238000010438 heat treatment Methods 0.000 claims abstract description 50
- 239000000463 material Substances 0.000 claims description 5
- 230000001678 irradiating effect Effects 0.000 claims description 4
- 230000000052 comparative effect Effects 0.000 description 18
- 238000010791 quenching Methods 0.000 description 14
- 230000000171 quenching effect Effects 0.000 description 14
- 239000000725 suspension Substances 0.000 description 7
- 238000009826 distribution Methods 0.000 description 6
- 230000006835 compression Effects 0.000 description 5
- 238000007906 compression Methods 0.000 description 5
- 229910000831 Steel Inorganic materials 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 230000002950 deficient Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000012447 hatching Effects 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 229910000975 Carbon steel Inorganic materials 0.000 description 1
- 238000000137 annealing Methods 0.000 description 1
- 239000010962 carbon steel Substances 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 239000003381 stabilizer Substances 0.000 description 1
- 230000008719 thickening Effects 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60G—VEHICLE SUSPENSION ARRANGEMENTS
- B60G9/00—Resilient suspensions of a rigid axle or axle housing for two or more wheels
- B60G9/04—Resilient suspensions of a rigid axle or axle housing for two or more wheels the axle or housing not being pivotally mounted on the vehicle
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60G—VEHICLE SUSPENSION ARRANGEMENTS
- B60G21/00—Interconnection systems for two or more resiliently-suspended wheels, e.g. for stabilising a vehicle body with respect to acceleration, deceleration or centrifugal forces
- B60G21/02—Interconnection systems for two or more resiliently-suspended wheels, e.g. for stabilising a vehicle body with respect to acceleration, deceleration or centrifugal forces permanently interconnected
- B60G21/04—Interconnection systems for two or more resiliently-suspended wheels, e.g. for stabilising a vehicle body with respect to acceleration, deceleration or centrifugal forces permanently interconnected mechanically
- B60G21/05—Interconnection systems for two or more resiliently-suspended wheels, e.g. for stabilising a vehicle body with respect to acceleration, deceleration or centrifugal forces permanently interconnected mechanically between wheels on the same axle but on different sides of the vehicle, i.e. the left and right wheel suspensions being interconnected
- B60G21/051—Trailing arm twist beam axles
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/06—Surface hardening
- C21D1/09—Surface hardening by direct application of electrical or wave energy; by particle radiation
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/0068—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for particular articles not mentioned below
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/08—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for tubular bodies or pipes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60G—VEHICLE SUSPENSION ARRANGEMENTS
- B60G2206/00—Indexing codes related to the manufacturing of suspensions: constructional features, the materials used, procedures or tools
- B60G2206/01—Constructional features of suspension elements, e.g. arms, dampers, springs
- B60G2206/20—Constructional features of semi-rigid axles, e.g. twist beam type axles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60G—VEHICLE SUSPENSION ARRANGEMENTS
- B60G2206/00—Indexing codes related to the manufacturing of suspensions: constructional features, the materials used, procedures or tools
- B60G2206/01—Constructional features of suspension elements, e.g. arms, dampers, springs
- B60G2206/20—Constructional features of semi-rigid axles, e.g. twist beam type axles
- B60G2206/202—Constructional features of semi-rigid axles, e.g. twist beam type axles with a radially deformed tube as a cross member
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/26—Methods of annealing
- C21D1/30—Stress-relieving
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2221/00—Treating localised areas of an article
Definitions
- the present invention relates to a hollow member that receives a torsional force such as a torsion beam used in a suspension device such as an automobile, and a method for manufacturing the hollow member.
- a hollow member called a torsion beam has been used in a suspension device for an automobile. Arms to which wheels are attached are fixed to both ends of the torsion beam, and the torsion beam repeatedly receives a torsional force by input from the traveling wheel.
- This torsion beam is required to have a high durability that hardly causes cracks or the like even if it repeatedly receives a torsional force.
- the durability of the torsion beam is improved by increasing the thickness of the material constituting the torsion beam.
- increasing the thickness of the material increases the weight of the torsion beam, which is not preferable.
- the hardness of the torsion beam increases and the toughness decreases, and for example, it may be easily damaged when subjected to an impact due to a collision of a foreign object or the like when the vehicle travels. There is. In other words, there is a limit to improving the durability by the total quenching process.
- the present invention has been made in view of such a point, and the object of the present invention is to increase the thickness of the hollow member that receives repeated torsional force and not to perform total quenching or annealing. However, it is to greatly increase the durability.
- partial heat treatment is performed on the necessary part of the hollow member to optimize the hardness distribution in the thickness direction of the peripheral wall and to reduce the residual stress.
- a hollow member that is formed in a tubular shape and receives a torsional force around a center line
- the hardness of the outer part of the peripheral wall is reduced. It is characterized by being subjected to a partial heat treatment for improving the hardness before heating and the hardness of the inner portion of the peripheral wall and reducing the residual stress of the inner portion of the peripheral wall.
- the hardness of the outer portion of the peripheral wall is improved and the strength is improved.
- the peripheral wall subjected to the partial heat treatment is not as hard as the outer part, the toughness is ensured, which makes it possible to suppress damage when subjected to impact, for example, and torsional force Durability is improved.
- the inner part of the peripheral wall that has undergone partial heat treatment has a lower hardness than the outer part as described above, but the residual stress is reduced, so the occurrence of cracks and the like is suppressed even when subjected to repeated torsional forces. Is done.
- the second invention is characterized in that, in the first invention, the hardness of the inner portion of the peripheral wall is set to be substantially the same as the hardness of the inner portion before heating.
- This configuration makes it possible to impart moderate toughness while sufficiently securing the strength of the hollow member.
- the third invention is characterized in that, in the first invention, the portion for improving the hardness on the outer side of the peripheral wall is set to 1/2 or less of the total thickness of the peripheral wall.
- This configuration makes it possible to ensure sufficient toughness of the hollow member.
- a method of manufacturing a hollow member that is formed in a tubular shape and receives a twisting force around a center line, and by heating a part of the peripheral wall of the hollow member, the hardness of the outer portion of the peripheral wall It is characterized by performing a partial heat treatment for improving the hardness of the outer portion before heating and the hardness of the inner portion of the peripheral wall and reducing the residual stress of the inner portion of the peripheral wall.
- the fifth invention is characterized in that, in the fourth invention, the partial heat treatment is performed by irradiating a laser beam from the outside of the peripheral wall of the hollow member.
- the peripheral wall of the hollow member is subjected to partial heat treatment to improve the hardness of the outer part of the peripheral wall before the heating and the hardness of the inner part of the peripheral wall, and the tension of the inner part of the peripheral wall. Residual stress is reduced. Thereby, even if the hollow member repeatedly receives a torsional force, the occurrence of cracks and the like can be suppressed, so that high durability can be obtained without increasing the thickness of the peripheral wall and without subjecting it to total quenching.
- the hardness of the inner portion of the peripheral wall is substantially the same as that before heating, high durability can be obtained while imparting appropriate toughness and making the hollow member resistant to impact.
- the portion for improving the hardness of the peripheral wall is set to 1/2 or less of the total thickness of the peripheral wall, sufficient toughness of the hollow member can be ensured and high durability can be obtained.
- a highly durable hollow member can be obtained without increasing the thickness of the peripheral wall and without subjecting it to a total quenching treatment.
- the partial heat treatment is performed by laser light irradiation, a highly durable hollow member can be efficiently obtained with a small amount of energy.
- FIG. 4 is a sectional view taken along line IV-IV in FIG. 3. It is a graph which shows the relationship between the thickness and hardness of each board
- FIG. 7 is a view corresponding to FIG. 6 when the plate thickness is 2.3 mm.
- FIG. 1 shows a part of a torsion beam type suspension apparatus having a torsion beam 1 according to an embodiment of the present invention.
- the torsion beam type suspension device is used for a rear wheel suspension device of an automobile, and includes a torsion beam 1 and arms 2 and 2 that are fixed to both ends of the torsion beam 1 and extend in the vehicle front-rear direction.
- Bushes 3, 3 are provided at the vehicle front end of each arm 2, and each arm 2 is attached to the vehicle body so as to be swingable in the vertical direction via the bushes 3, 3.
- wheel support members 4, 4 that support the wheels are attached to the rear end portions of the arms 2.
- the arms 2 and 2 are provided with spring supports 5 and 5 for receiving springs (not shown), respectively.
- the torsion beam 1 is a hollow member formed in a tubular shape extending in the vehicle width direction.
- the material of the torsion beam 1 is a general structural carbon steel pipe. The thickness of this steel pipe is 2.9 mm.
- the cross section of both ends of the torsion beam 1 is substantially circular, and both ends are welded to the arm 2 over the entire circumference.
- a concave portion 10 that is recessed upward is formed so as to extend continuously in the longitudinal direction.
- the recess 10 is formed by crushing the raw tube with a mold, and as shown in FIG. 4, the recess 10 has a substantially U-shaped or V-shaped cross section that opens downward. .
- a part of the torsion beam 1 is subjected to a partial heat treatment.
- the range in which the partial heat treatment is performed is a range indicated by hatching in FIGS. 2 and 3, and corresponds to a broken line in FIG. 4.
- the partial heat treatment is performed by irradiating a predetermined laser beam as will be described in detail later.
- the range where the partial heat treatment is performed is a place where cracks or the like are likely to occur. That is, in the present embodiment, it is not a total quenching process in which all of the torsion beam 1 is quenched, but only where cracks or the like are likely to occur. Heat treatment is performed.
- the hardness distribution of the peripheral wall of the non-heat treated member is as shown by black circles in FIG. That is, it is about 210 to 250 Hv (Vickers hardness) from the outer surface to the inner surface of the peripheral wall. Further, the residual stress of the outer surface portion of the peripheral wall of the non-heat treated member is compression of about 300 MPa, and the residual stress of the inner surface portion is tensile of about 400 MPa.
- the hardness distribution of the peripheral wall of the part subjected to partial heat treatment is shown by white circles in the figure. That is, the vicinity of A on the outer surface of the peripheral wall is 460 Hv, and the hardness gradually increases from the outer surface to near B at a depth of 0.15 mm.
- the hardness in B is about 500 Hv, which is twice or more that of the non-heat treated member.
- the hardness gradually decreases from B to C (from 0.6 mm from the outer surface), and in C, it is approximately 200 Hv, which is substantially the same as the hardness of the non-heat treated member.
- the hardness from C to D on the inner surface is substantially the same as the hardness of the non-heat treated member.
- the means for setting the hardness distribution in the thickness direction of the peripheral wall in this way is laser light irradiation.
- the residual stress on the outer surface of the peripheral wall of the heat treatment portion is about 70 MPa compression, and the inner surface residual stress is about 5 MPa tensile.
- means for significantly reducing the residual stress of the peripheral wall of the heat-treated portion than the residual stress of the peripheral wall of the non-heat-treated member is laser light irradiation.
- the manufacturing procedure of the torsion beam 1 will be described.
- a raw tube is prepared, and the recess 10 is formed by a mold (not shown).
- the torsion beam 1 is partially irradiated with laser light to be subjected to partial heat treatment.
- the energy density of the laser light at this time is such that the hardness distribution in the thickness direction of the peripheral wall is indicated by white circles in FIG. 5, the hardness in a predetermined range of the outer portion is the hardness before heating of the outer portion and the inner portion of the peripheral wall. It sets so that it may improve rather than hardness, and the residual stress of the inner part of a surrounding wall may reduce rather than a non-heat-processing member.
- the prepared torsion beam was subjected to partial heat treatment according to the present invention (the present invention), not subjected to any heat treatment (Comparative Example 1), and subjected to total quenching so that the Vickers hardness was 400 Hv ( Comparative Example 2) and a sample that was subjected to total quenching so that the Vickers hardness was 500 Hv (Comparative Example 3) were prepared.
- the hardness from the outer surface portion to the inner surface portion of the peripheral wall of the torsion beam is about 210 to 250 Hv as in the peripheral wall of the non-heat treated member of the torsion beam 1 according to the present invention.
- the residual stress of the outer surface part of the surrounding wall of the comparative example 1 is a compression of about 300 MPa, and the residual stress of the inner surface part is a tension of about 400 MPa.
- the hardness of the outer surface portion of the peripheral wall of the torsion beam is about 280 Hv, and is about 400 Hv in the vicinity of S of 0.5 mm from the outer surface portion. About 400 to 420 Hv from S to the inner surface.
- the residual stress of the outer surface part of the surrounding wall of the comparative example 2 is a compression of about 200 MPa, and the residual stress of the inner surface part is a tension of about 300 MPa.
- the cooling rate on the inner surface side is slower than that on the outer surface side, and hence a tensile residual stress is generated on the inner surface portion.
- the hardness of the outer surface portion of the peripheral wall of the torsion beam is about 380 Hv, and is about 500 Hv in the vicinity of T of 1.5 mm from the outer surface portion. About 500 to 510 Hv from T to the inner surface.
- the residual stress of the outer surface part of the surrounding wall of the comparative example 3 is a compression of about 300 MPa, and the residual stress of the inner surface part is a tension of about 200 MPa.
- Comparative Example 3 cracks occurred on the inner surface of the peripheral wall after 1.15 million times.
- Comparative Example 3 the durability is improved as compared with Comparative Examples 1 and 2, but the torsion beam 1 as a whole has a toughness of about 500 Hv.
- the torsion beam 1 is easily damaged by the impact, and is not practical.
- the hardness in a predetermined range of the outer portion of the torsion beam 1 is higher than the hardness of the outer portion before heating and the hardness of the inner portion of the peripheral wall, and the residual stress in the inner portion of the peripheral wall is non-heat treated member.
- durability of 4 times or more can be obtained only by performing the partial heat treatment so as to reduce the temperature.
- the horizontal axis represents the Q value
- the vertical axis represents the number of crack occurrences.
- the Q value is a value obtained by dividing the laser output by the scanning speed.
- the circles in the graph indicate the number of times that cracking has occurred when the laser beam is irradiated so as to obtain the Q value, and if the Q value is 1.5 or more, non-heat treatment is performed.
- the Q value is 2.8 or more and 3.1 or less, the durability is further improved.
- the upper limit of the Q value when the value is 6.0 or more, the outer surface portion of the peripheral wall becomes excessively melted, resulting in a defective product. Therefore, a value smaller than 6.0 is preferable, and preferably 5.0.
- the Q value is preferably 1.5 or more and 5.0 or less. More preferably, it is 2.8 or more and 3.1 or less. In particular, by setting the Q value in the vicinity of 3.0, the number of occurrences of cracks becomes a value close to 3 million times, and the effect of the partial heat treatment becomes more remarkable.
- the torsion beam 1 since only a part of the torsion beam 1 needs to be irradiated with laser light, less energy is consumed and the number of man-hours can be reduced as compared with the case where total quenching is performed.
- the peripheral wall of the torsion beam 1 is subjected to partial heat treatment to improve the hardness of the outer portion of the peripheral wall, compared with the hardness of the outer portion before heating and the hardness of the inner portion of the peripheral wall.
- the residual stress in the inner portion of the peripheral wall is reduced.
- the hardness of the inner portion of the peripheral wall of the torsion beam 1 is made substantially the same as the hardness before heating of the inner portion, so that the torsion beam 1 resistant to impact is imparted with appropriate toughness, High durability can be obtained.
- the portion of the torsion beam 1 that increases the hardness of the peripheral wall is set to 1/2 or less of the total thickness of the peripheral wall. Thereby, the toughness of the torsion beam 1 can be sufficiently secured and the durability can be further improved.
- a preferable range of the portion for improving the hardness of the peripheral wall of the torsion beam 1 is 1/3 or less of the total thickness of the peripheral wall.
- the torsion beam 1 having high durability can be obtained with a small amount of energy.
- the thickness of the steel pipe constituting the torsion beam 1 is 2.3 mm and the heat treatment by laser light is applied to the same portion as that having the thickness of 2.9 mm, remarkable durability as shown in FIG. An improvement is seen.
- the plate thickness is 2.3 mm
- the number of cracks can be increased in the region where the optimum energy density of the laser beam is low because the plate thickness is thinner than when the plate thickness is 2.9 mm.
- the Q value is 1.0 or more and 2.0 or less
- the Q value is 1.3 or more and 1.7 or less
- the durability is further improved.
- the upper limit of the Q value if the value is 4.0 or more, the outer surface portion of the peripheral wall is severely melted and becomes a defective product, so a value smaller than 4.0 is preferable, and preferably 3.0.
- the hollow member and the method for manufacturing the hollow member according to the present invention can be applied to, for example, parts of a suspension device for an automobile.
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- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
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- Crystallography & Structural Chemistry (AREA)
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Abstract
Description
2 アーム
3 ブッシュ
4 車輪支持部材
5 スプリングサポート
10 凹部
Claims (5)
- 管状に形成されて中心線周りの捩り力を受ける中空部材において、
上記中空部材の周壁の一部を加熱することにより、該周壁の外側部分の硬度を、該外側部分の加熱前の硬度及び該周壁の内側部分の硬度よりも向上させるとともに、該周壁の内側部分の残留応力を低減させる部分熱処理が施されていることを特徴とする中空部材。 - 請求項1に記載の中空部材において、
周壁の内側部分の硬度は、該内側部分の加熱前の硬度と略同じに設定されていることを特徴とする中空部材。 - 請求項1に記載の中空部材において、
周壁の外側の硬度を向上させる部分は、周壁の総厚さに対して1/2以下に設定されていることを特徴とする中空部材。 - 管状に形成されて中心線周りの捩り力を受ける中空部材の製造方法において、
上記中空部材の周壁の一部を加熱することにより、該周壁の外側部分の硬度を、該外側部分の加熱前の硬度及び該周壁の内側部分の硬度よりも向上させるとともに、該周壁の内側部分の残留応力を低減させる部分熱処理を施すことを特徴とする中空部材の製造方法。 - 請求項4に記載の中空部材の製造方法において、
部分熱処理は、中空部材の周壁の外側からレーザー光を照射することによって行うことを特徴とする中空部材の製造方法。
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
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MX2014000676A MX369792B (es) | 2011-09-14 | 2012-04-23 | Miembro hueco y metodo para formar el miembro hueco. |
CN201280034766.0A CN103648807B (zh) | 2011-09-14 | 2012-04-23 | 空心部件及空心部件的制造方法 |
EP12831876.3A EP2756971B1 (en) | 2011-09-14 | 2012-04-23 | Hollow member and method for manufacturing hollow member |
US14/232,867 US20140174610A1 (en) | 2011-09-14 | 2012-04-23 | Hollow member and method for forming hollow member |
BR112014001006A BR112014001006A2 (pt) | 2011-09-14 | 2012-04-23 | membro oco tubular e método para a formação de um membro oco tubular |
Applications Claiming Priority (2)
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JP2011200297 | 2011-09-14 | ||
JP2011-200297 | 2011-09-14 |
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WO2013038580A1 true WO2013038580A1 (ja) | 2013-03-21 |
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US (1) | US20140174610A1 (ja) |
EP (1) | EP2756971B1 (ja) |
JP (1) | JP6367555B2 (ja) |
CN (1) | CN103648807B (ja) |
BR (1) | BR112014001006A2 (ja) |
MX (1) | MX369792B (ja) |
WO (1) | WO2013038580A1 (ja) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2015151556A (ja) * | 2014-02-10 | 2015-08-24 | 株式会社ワイテック | 熱処理方法 |
CN106573515A (zh) * | 2014-10-03 | 2017-04-19 | 株式会社 F.泰克 | 悬架部件用端板 |
JP2019178382A (ja) * | 2018-03-30 | 2019-10-17 | 株式会社ワイテック | 鋼製曲げ成形品の製造方法 |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
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JP6090338B2 (ja) * | 2013-01-30 | 2017-03-08 | 新日鐵住金株式会社 | トーションビーム、トーションビーム組立体及びトーションビーム式サスペンション装置 |
CN105567941B (zh) * | 2016-01-20 | 2017-10-03 | 盐城高周波热炼有限公司 | 一种薄壁空芯管加热装置及其加热方法 |
CN108424998A (zh) * | 2018-04-19 | 2018-08-21 | 吉林省正轩车架有限公司 | 小型客车后副车架扭力梁冷压成型应力消除方法及设备 |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6013045B2 (ja) * | 1978-09-27 | 1985-04-04 | 株式会社日立製作所 | 炭素鋼部品の焼入れ加工方法 |
JP2003154415A (ja) * | 2001-09-04 | 2003-05-27 | Aisin Takaoka Ltd | 金属部材成形方法、金属部材及び金属部材成形装置 |
JP2007262469A (ja) * | 2006-03-28 | 2007-10-11 | Jfe Steel Kk | 鋼管およびその製造方法 |
JP2008030513A (ja) | 2006-07-26 | 2008-02-14 | Toyota Tsusho Corp | トーションビーム、トーションビーム式サスペンション並びにトーションビームの製造方法 |
JP2010242164A (ja) * | 2009-04-06 | 2010-10-28 | Jfe Steel Corp | 自動車構造部材用高強度溶接鋼管の製造方法 |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6052556B2 (ja) * | 1980-05-16 | 1985-11-20 | 高周波熱錬株式会社 | 誘導加熱による軸類の重畳熱処理方法 |
JPS58197221A (ja) * | 1982-05-13 | 1983-11-16 | Toshiba Corp | 管フランジの製造方法 |
JPS60159121A (ja) * | 1984-01-27 | 1985-08-20 | Ishikawajima Harima Heavy Ind Co Ltd | 管の残留応力改善方法 |
DE19941993C1 (de) * | 1999-09-02 | 2000-12-14 | Benteler Werke Ag | Verfahren zur Herstellung eines biegesteifen torsionsweichen Rohrprofils als Querträger für eine Verbundlenkerhinterachse eines Personenkraftwagens |
JP4317799B2 (ja) * | 2004-01-22 | 2009-08-19 | 三菱重工業株式会社 | 管体の残留応力改善方法 |
JP4209366B2 (ja) * | 2004-07-29 | 2009-01-14 | 三菱重工業株式会社 | 配管の残留応力改善装置 |
EP1982803A1 (en) * | 2007-04-16 | 2008-10-22 | Koninklijke Philips Electronics N.V. | Cutting eleemnt, electric shaver provided with a cutting element and method for producing such element |
KR100907225B1 (ko) * | 2007-05-23 | 2009-07-10 | 주식회사화신 | 열간성형장치 및 열간성형 제조방법 |
DE102007028888B4 (de) * | 2007-06-20 | 2015-07-23 | Maschinenfabrik Alfing Kessler Gmbh | Verfahren zur Erhöhung der Festigkeit eines Bauteils |
US20090321144A1 (en) * | 2008-06-30 | 2009-12-31 | Wyble Kevin J | Protecting an element from excessive surface wear by localized hardening |
JP4858624B2 (ja) * | 2009-04-01 | 2012-01-18 | Jfeスチール株式会社 | トーションビームの製造方法及びトーションビーム |
-
2012
- 2012-04-23 WO PCT/JP2012/002781 patent/WO2013038580A1/ja active Application Filing
- 2012-04-23 BR BR112014001006A patent/BR112014001006A2/pt active Search and Examination
- 2012-04-23 US US14/232,867 patent/US20140174610A1/en not_active Abandoned
- 2012-04-23 MX MX2014000676A patent/MX369792B/es active IP Right Grant
- 2012-04-23 EP EP12831876.3A patent/EP2756971B1/en active Active
- 2012-04-23 CN CN201280034766.0A patent/CN103648807B/zh active Active
- 2012-04-23 JP JP2013533458A patent/JP6367555B2/ja active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6013045B2 (ja) * | 1978-09-27 | 1985-04-04 | 株式会社日立製作所 | 炭素鋼部品の焼入れ加工方法 |
JP2003154415A (ja) * | 2001-09-04 | 2003-05-27 | Aisin Takaoka Ltd | 金属部材成形方法、金属部材及び金属部材成形装置 |
JP2007262469A (ja) * | 2006-03-28 | 2007-10-11 | Jfe Steel Kk | 鋼管およびその製造方法 |
JP2008030513A (ja) | 2006-07-26 | 2008-02-14 | Toyota Tsusho Corp | トーションビーム、トーションビーム式サスペンション並びにトーションビームの製造方法 |
JP2010242164A (ja) * | 2009-04-06 | 2010-10-28 | Jfe Steel Corp | 自動車構造部材用高強度溶接鋼管の製造方法 |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2015151556A (ja) * | 2014-02-10 | 2015-08-24 | 株式会社ワイテック | 熱処理方法 |
CN106573515A (zh) * | 2014-10-03 | 2017-04-19 | 株式会社 F.泰克 | 悬架部件用端板 |
US10543728B2 (en) | 2014-10-03 | 2020-01-28 | F-Tech Inc. | End plate of suspension member |
JP2019178382A (ja) * | 2018-03-30 | 2019-10-17 | 株式会社ワイテック | 鋼製曲げ成形品の製造方法 |
Also Published As
Publication number | Publication date |
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EP2756971A8 (en) | 2014-12-10 |
EP2756971A1 (en) | 2014-07-23 |
US20140174610A1 (en) | 2014-06-26 |
JPWO2013038580A1 (ja) | 2015-03-23 |
CN103648807B (zh) | 2017-03-29 |
JP6367555B2 (ja) | 2018-08-01 |
CN103648807A (zh) | 2014-03-19 |
MX2014000676A (es) | 2014-03-21 |
BR112014001006A2 (pt) | 2017-02-21 |
MX369792B (es) | 2019-11-21 |
EP2756971B1 (en) | 2018-07-04 |
EP2756971A4 (en) | 2015-05-27 |
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