JPS63491B2 - - Google Patents
Info
- Publication number
- JPS63491B2 JPS63491B2 JP10426883A JP10426883A JPS63491B2 JP S63491 B2 JPS63491 B2 JP S63491B2 JP 10426883 A JP10426883 A JP 10426883A JP 10426883 A JP10426883 A JP 10426883A JP S63491 B2 JPS63491 B2 JP S63491B2
- Authority
- JP
- Japan
- Prior art keywords
- strength
- tempering
- cold
- coil spring
- stage
- 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.)
- Expired
Links
- 238000010438 heat treatment Methods 0.000 claims description 27
- 239000000463 material Substances 0.000 claims description 21
- 238000001816 cooling Methods 0.000 claims description 6
- 230000006698 induction Effects 0.000 claims description 6
- 229910000734 martensite Inorganic materials 0.000 claims description 4
- 238000005496 tempering Methods 0.000 description 26
- 238000000034 method Methods 0.000 description 9
- 238000010791 quenching Methods 0.000 description 7
- 230000000171 quenching effect Effects 0.000 description 7
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 5
- 229910052799 carbon Inorganic materials 0.000 description 5
- 230000000694 effects Effects 0.000 description 4
- 150000001247 metal acetylides Chemical class 0.000 description 4
- 239000000203 mixture Substances 0.000 description 4
- 239000000126 substance Substances 0.000 description 4
- 229910000975 Carbon steel Inorganic materials 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 3
- 239000010962 carbon steel Substances 0.000 description 3
- 238000002474 experimental method Methods 0.000 description 3
- 239000010959 steel Substances 0.000 description 3
- 230000003746 surface roughness Effects 0.000 description 3
- 238000007796 conventional method Methods 0.000 description 2
- 238000005262 decarbonization Methods 0.000 description 2
- 238000000354 decomposition reaction Methods 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 238000009826 distribution Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000001556 precipitation Methods 0.000 description 2
- 230000035882 stress Effects 0.000 description 2
- 230000003679 aging effect Effects 0.000 description 1
- 229910001566 austenite Inorganic materials 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
- 239000002436 steel type Substances 0.000 description 1
- 238000005482 strain hardening Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- 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
- C21D9/02—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for springs
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Springs (AREA)
- Heat Treatment Of Articles (AREA)
Description
本発明は冷間成形コイルばねに関するものであ
る。
従来、コイルばねは大別して冷間成形法か熱間
成形法かによつて成形されている。細径のばねは
主として冷間成形法によつて、又10mmφ以上の大
径のばねは主として熱間成形法によつて成形され
ている。素材の径が太くなると強度の高いものほ
ど、冷間成形が困難となるためである。この間の
事情をさらに詳細に述べれば、従来10mmφ以上の
大径のコイルばねは、素材を熱間でコイルばね形
状に成形した後、焼入焼戻処理により所要の高強
度を付与するという方法で製造されている。
熱間成形法によれば、コイルの成形は容易であ
るが、反面、加熱時に生ずるばね表面の脱減炭、
熱間ゆえの材料強度の低下により表面キズがつき
やすいことやコイルばね形状での熱処理であるた
め強度のバラツキが生じやすいこと、さらには熱
処理時に表面肌荒れ、変形等が生ずる等、仕上品
は品質的には冷間成形品と比較して欠陥が生じや
すい。
所定の強度を有する、比較的細径のオイルテン
パー線等の線材を冷間成形してコイルばねを製造
する冷間成形法によれば、成形時に線材を加熱し
ないため、線材の強度はそのまゝ保有され、表面
肌荒れも生じないので、その点では熱間成形法よ
り優れているが、素材が高強度線材であると、線
径が太くなるに従い成形が困難となるという問題
点がある。
本発明は上述した熱間成形法および冷間成形法
によつて得られる従来のコイルばねがそれぞれ有
する長所は兼ね具え、しかもそれぞれの有する欠
陥を除去した優れた冷間成形コイルばねを提供し
ようとするものである。
さらに具体的には本発明は誘導加熱による急速
加熱、急速冷却からなる熱処理で母材が結晶粒度
ASTM番号9以上の細粒組織を有し、引張強さ
150Kgf/mm2以上、伸び9%以上、絞り49%以上
の高強度と延性・靭性を兼備した機械的性質を有
する、線径10mmφ以上の、200万回での疲労限が
ねじり剪断応力τw=60±45Kgf/mm2以上で、か
つ、へたりのきわめて少ない冷間成形コイルばね
を提供しようとするものである。
本発明を第1図〜第3図に従つて以下詳細に説
明する。
炭素鋼からなる線材を、たとえば引抜後、高周
波誘導加熱等による急速加熱後、1000℃以下のオ
ーステナイト領域に、当該線材の化学成分に応じ
て設定できる極小時間保持し、水焼入れすること
によつて当該鋼材の結晶粒がASTM no.9〜12と
非常に微細になり、かつミクロ組織的に炭素濃度
の不均一な組織が生ずることによつて焼入れ段階
で通常の熱処理に比べて高強靭性の線材を製造し
うることは高周波誘導加熱等の急速加熱焼入の特
徴として既に知られている処であるが、本発明者
は、炭素含有量0.3%以上の線材に上記の焼入を
施してえた高強度線材を、従来の焼戻温度よりも
比較的に高温の300゜〜600℃に加熱した後、当該
加熱を停止し、しかる後、従来法における炉加熱
焼戻しでは考えられないような、60秒以下という
きわめて短時間(従来法では30〜60分程度)、当
該温度に保持し、冷却することによつて引張強さ
150Kgf/mm2以上の強度を有し、しかも靭性が高
く、きわめて冷間加工性に富んだ線材を得られる
ことを見出した。
これは前述したごとく、従来の焼戻しの概念を
離脱して比較的高温かつ極小時間の急速加熱によ
り、過飽和に炭素等の侵入型原子を固溶したマル
テンサイトの分解および炭化物の析出が徐々に加
熱する場合と比べて急速に起り、かつ、短時間保
持後、急冷するという第一段階の焼戻しによつ
て、当該温度において一般的に考えられる十分な
焼戻し状態に達するには不十分な熱エネルギー供
給により、炭化物の分布、形状をも含めて、いわ
ば焼戻し不十分な状態で反応を一応停止させてし
まうことによるものと推定される。
換言すれば、急速加熱、短時間保持、急速冷却
による焼入れにより鋼材を微細粒をもつマルテン
サイト組織とし、それによつて鋼材に高強度と高
延性を有するのに必要なベースを与えた上で、第
一段階の高温かつ短時間保持の焼戻しを行なうこ
とによつて150Kgf/mm2以上の強度を与え、なお
かつ総じて転位密度は高いが、降伏点を比較的低
く押さえ、降伏してから十分な伸びを得るのに必
要な動転位の比率が高い状態、すなわち、得られ
る特性として延性が高く、具体的には加工性の高
い状態とするのである。もちろん、この段階では
焼戻し不十分の状態であるので耐へたり性につい
ては好ましくないと云える。
このことを証明するための実験結果の一部を次
表に示す。
実験例 1
(1) 供試体
材 質 SAE 1552
化学成分 C=0.51、Mn=1.56
径 12mm
焼入硬さ Hv=800
(2) 焼戻し条件と機械的性質の関係
The present invention relates to cold-formed coil springs. Conventionally, coil springs are formed by either cold forming or hot forming. Small diameter springs are mainly formed by cold forming, and large diameter springs of 10 mmφ or more are mainly formed by hot forming. This is because the thicker the diameter of the material and the higher the strength, the more difficult it becomes to cold form the material. To explain the situation in more detail, conventionally, large-diameter coil springs of 10 mmφ or more are produced by hot forming a material into a coil spring shape, and then applying quenching and tempering to give the required high strength. Manufactured. According to the hot forming method, it is easy to form a coil, but on the other hand, the decarbonization of the spring surface that occurs during heating,
The quality of the finished product may deteriorate due to the fact that the strength of the material decreases due to hot treatment, which tends to cause surface scratches, and because the heat treatment is performed on coiled springs, the strength tends to vary, and the surface roughness and deformation occur during heat treatment. Specifically, defects are more likely to occur compared to cold-formed products. According to the cold forming method, which manufactures coil springs by cold forming wire rods such as oil-tempered wires with a predetermined strength and a relatively small diameter, the strength of the wire rods remains the same because the wire rods are not heated during forming. In this respect, it is superior to the hot forming method because it retains its properties and does not cause surface roughness. However, if the material is a high-strength wire rod, there is a problem that forming becomes difficult as the wire diameter increases. The present invention aims to provide an excellent cold-formed coil spring that combines the advantages of the conventional coil springs obtained by the above-mentioned hot forming method and cold forming method, and eliminates the defects of each. It is something to do. More specifically, the present invention uses heat treatment consisting of rapid heating by induction heating and rapid cooling to improve the crystal grain size of the base material.
Has a fine grain structure with ASTM number 9 or higher, and has tensile strength
It has mechanical properties that combine high strength, ductility and toughness of 150Kgf/ mm2 or more, elongation of 9% or more, and reduction of area of 49% or more, and the fatigue limit after 2 million cycles is the torsional shear stress τw = wire diameter of 10mmφ or more. It is an object of the present invention to provide a cold-formed coil spring that has a strength of 60±45 Kgf/mm 2 or more and has very little set. The present invention will be explained in detail below with reference to FIGS. 1 to 3. For example, after drawing a wire rod made of carbon steel, it is rapidly heated by high-frequency induction heating, etc., and then kept in the austenite region at 1000℃ or less for a minimum time that can be set depending on the chemical composition of the wire rod, and then water quenched. The grains of the steel are extremely fine, ASTM no. 9 to 12, and the microstructure has a non-uniform carbon concentration, which results in higher strength and toughness during the quenching stage compared to normal heat treatment. The ability to manufacture wire rods is already known as a feature of rapid heating quenching such as high-frequency induction heating, but the present inventor has demonstrated that wire rods with a carbon content of 0.3% or more are subjected to the above quenching process. After heating the obtained high-strength wire rod to a temperature of 300° to 600°C, which is relatively higher than the conventional tempering temperature, the heating is stopped. Tensile strength can be improved by maintaining the temperature for an extremely short period of 60 seconds or less (compared to 30 to 60 minutes with conventional methods) and cooling.
It has been found that a wire rod having a strength of 150 Kgf/mm 2 or more, high toughness, and excellent cold workability can be obtained. As mentioned above, this method departs from the conventional concept of tempering and uses rapid heating at a relatively high temperature and for an extremely short period of time to gradually heat up the decomposition of martensite containing supersaturated interstitial atoms such as carbon and the precipitation of carbides. The first stage of tempering, which occurs more rapidly than when the tempering is carried out and is held for a short time and then rapidly cooled, provides insufficient thermal energy to reach the generally considered sufficient tempering state at that temperature. This is presumed to be due to the fact that the reaction is temporarily stopped in a state where the tempering is insufficient, including the distribution and shape of the carbides. In other words, by quenching by rapid heating, short-time holding, and rapid cooling, the steel material is made into a martensitic structure with fine grains, thereby giving the steel material the base necessary for having high strength and high ductility. The first stage of high-temperature and short-time tempering provides a strength of over 150Kgf/ mm2 , and although the dislocation density is generally high, the yield point is kept relatively low and sufficient elongation is achieved after yielding. A state in which the ratio of dynamic dislocations necessary to obtain the following properties is high, that is, a state in which the resulting properties are high in ductility, and specifically, in a state in which workability is high. Of course, at this stage, the tempering is insufficient, so it can be said that the resistance to settling is not favorable. Some of the experimental results to prove this are shown in the table below. Experimental example 1 (1) Specimen material SAE 1552 Chemical composition C=0.51, Mn=1.56 Diameter 12mm Quenching hardness Hv=800 (2) Relationship between tempering conditions and mechanical properties
【表】
(3) 実験結果
上記実験結果によれば、急速加熱、短時間保
持、急速冷却による焼入れを行ない、しかる後
300〜600℃に急速加熱し、60秒以下という短時
間の保持時間の後、急冷して焼戻しをすると、
引張強さ150Kgf/mm2以上、伸び9%以上、絞
り49%以上の高強度、かつ高加工性の線材をえ
られることが判明する。
なお、第1図は本実験例における供試体の焼
戻し時間と温度との関係を示し、第2図は焼戻
温度500℃における保持時間と線材の硬さ、靭
性との関係を示す。第1図において縦軸は焼戻
温度、横軸は焼戻し時間(対数(尺))を、第
2図において横軸は焼戻時間(対数(尺))を、
又曲線a,bおよびcはそれぞれ引張強さ、絞
りおよび伸びの変化を示す。
上述の第一段階階の焼戻し処理によつて上記実
験例から明らかなように炭素含有量0.51%の炭素
鋼を素材として用いると150Kgf/mm2以上の高強
度で、かつ加工性のすぐれた線材がえられる。さ
らに本発明者の他の実験例によれば、たとえば
JIS SWRH 62B、SAE9254、SUP6、7、9に
化学組成が示されているごとき炭素含有量0.3%
以上の炭素鋼を素材として用いれば上記同様150
Kgf/mm2以上、鋼種或は成分系によつては220Kg
f/mm2程度の高強度で加工性に優れた線材がえら
れることも判明している。
上述の線材は高強度で、かつ高加工性が付与さ
れているので、たとえば10〜16mmφの如き従来の
冷間成形対象の線径のものより直径において5、
6割方太い大径のコイルばねを容易に冷間成形可
能である。すなわち、高強度で大径のコイルばね
を公知の成形機をもつて容易に冷間成形すること
が可能である。
上述した線材をコイルばねに冷間成形後、これ
を300〜500℃に30〜60分加熱する、第二段階の低
温焼戻しにより当該コイルばねに優れた耐クリー
プ性が付与され、きわめてヘタリの少ないばねを
得ることができる。換言すれば、急速加熱、短時
間保持を特徴とする第一段階の焼戻しにより、き
わめて高い転位密度を維持した線材が冷間成形に
よる塑性加工をうけることによつて、更にその転
位が増殖され、これに加えて第一段階の焼戻しで
得られた高強度を低下させない、上記第一段階の
焼戻し温度より上限の低い、300〜500℃の温度範
囲で30〜60分という一定時間、一般に行なわれて
いる電気炉等で第二段階の焼戻しを行なうことに
より、転位と溶質原子や炭化物の間で固着現象が
生じて転位を動けなくし、いわゆる不動転位を形
成させることによつて一種の歪時効効果が得ら
れ、その結果冷間成形コイルばねの弾性限、降伏
点およびリラクゼーシヨン特性が向上し、又線材
の冷間成形前の熱処理の段階でのマルテンサイト
の分解、炭化物の析出、分布、形状等の焼戻し現
象が前述のように十分でなかつたものが安定化
し、最終的にはコイルばねに高強度を維持しなが
ら、高い耐クリープ性が付与されるものと推定さ
れる。
なお、上記第二段階の低温焼戻しにより、冷間
加工による残留応力の除去という一般的な効果が
付加されることはもちろんである。
本発明者は上記第二段階の安定化焼戻しによる
効果を確認するために実験を行なつた。その実験
結果の一部を示すと第3図のとおりである。
実験例 2
(1) 実験条件
(1) 供試体
実験例1におけるものと同じ。
(2) 熱処理条件
実験例1におけると同一条件で熱処理を行
なつた。
(3) 熱処理した供試体の1部はねじりによる塑
性変形を加え(加工材)、1部はねじりによ
る塑性を加えず(非加工材)、両者に同一条
件(前述)の第二段階の安定化焼戻し処理を
施した。
(2) 実験結果
第3図に示すとおりで、縦軸は引張荷重P
を、横軸はひずみεを示し、mは加工材の、n
は非加工材の引張荷重−ひずみ曲線を示す。第
3図から加工材は非加工材に比し弾性限が上昇
しており、耐クリープ性が高いことが明白とな
つた。
本発明者は、更に本発明にかゝるコイルばね
の具体的な機械的性質と、従来の熱間成形によ
つて得たコイルばねのそれとを比較するため次
の実験を行なつた。
実験例 3
(1) 供試体
原材料 線径14mmφ
材質
A:本発明を実施したものSAE
1552
B:従来方法を実施したものSUP
6
製造工程[Table] (3) Experimental results According to the experimental results above, quenching by rapid heating, short-term holding, and rapid cooling was performed, and after
When rapidly heated to 300-600℃, held for a short time of less than 60 seconds, and then rapidly cooled and tempered,
It has been found that a wire rod with high strength and high workability, with a tensile strength of 150 Kgf/mm 2 or more, an elongation of 9% or more, and a reduction of area of 49% or more, can be obtained. Note that FIG. 1 shows the relationship between the tempering time and temperature of the specimen in this experimental example, and FIG. 2 shows the relationship between the holding time and the hardness and toughness of the wire at a tempering temperature of 500°C. In Figure 1, the vertical axis is the tempering temperature, the horizontal axis is the tempering time (logarithm), and in Figure 2 the horizontal axis is the tempering time (logarithm).
Curves a, b and c show changes in tensile strength, area of area and elongation, respectively. As is clear from the above experimental example, when carbon steel with a carbon content of 0.51% is used as a material by the above-mentioned first-stage tempering process, a wire rod with high strength of 150 Kgf/mm 2 or more and excellent workability can be obtained. It can be grown. Furthermore, according to other experimental examples of the present inventor, for example,
Carbon content 0.3% as chemical composition shown in JIS SWRH 62B, SAE9254, SUP6, 7, 9
If the above carbon steel is used as the material, 150
Kgf/mm 2 or more, 220Kg depending on steel type or composition system
It has also been found that a wire rod with high strength of about f/mm 2 and excellent workability can be obtained. The above-mentioned wire rod has high strength and high workability, so it has a diameter of 5 mm compared to the conventional wire diameter for cold forming, such as 10 to 16 mmφ.
A large diameter coil spring that is 60% thicker can be easily cold-formed. That is, it is possible to easily cold-form a high-strength, large-diameter coil spring using a known molding machine. After cold-forming the above-mentioned wire rod into a coil spring, the second stage of low-temperature tempering, in which the wire is heated to 300-500℃ for 30-60 minutes, gives the coil spring excellent creep resistance and extremely little set-up. You can get a spring. In other words, the wire rod that maintains an extremely high dislocation density through the first stage of tempering, which is characterized by rapid heating and short-time holding, undergoes plastic processing through cold forming, thereby further multiplying its dislocations. In addition to this, tempering is generally performed at a temperature range of 300 to 500°C for a certain period of time of 30 to 60 minutes, with an upper limit lower than the above-mentioned first stage tempering temperature, so as not to reduce the high strength obtained in the first stage tempering. By performing the second stage of tempering in an electric furnace, etc., a sticking phenomenon occurs between dislocations and solute atoms or carbides, making the dislocations immobile and forming so-called immobile dislocations, resulting in a type of strain aging effect. As a result, the elastic limit, yield point, and relaxation characteristics of the cold-formed coil spring are improved, and the decomposition of martensite, precipitation, distribution, and shape of carbides during the heat treatment stage before cold forming of the wire rod are improved. It is presumed that the insufficient tempering phenomenon described above will be stabilized, and that the coil spring will ultimately be given high creep resistance while maintaining high strength. It goes without saying that the second stage of low-temperature tempering adds the general effect of removing residual stress due to cold working. The inventor conducted an experiment to confirm the effect of the second stage of stabilizing tempering. Figure 3 shows part of the experimental results. Experimental Example 2 (1) Experimental Conditions (1) Specimen Same as in Experimental Example 1. (2) Heat treatment conditions Heat treatment was performed under the same conditions as in Experimental Example 1. (3) One part of the heat-treated specimen underwent plastic deformation due to torsion (processed material), and the other part did not undergo plastic deformation due to torsion (unprocessed material), and both were subjected to the second stage of stability under the same conditions (described above). A chemical tempering treatment was applied. (2) Experimental results As shown in Figure 3, the vertical axis is the tensile load P.
, the horizontal axis shows the strain ε, m is the processed material, n
shows the tensile load-strain curve of the unprocessed material. From FIG. 3, it is clear that the processed material has a higher elastic limit than the unprocessed material, and has higher creep resistance. The inventor further conducted the following experiment to compare the specific mechanical properties of the coil spring according to the present invention with those of a coil spring obtained by conventional hot forming. Experimental example 3 (1) Specimen Raw material Wire diameter 14mmφ Material A: SAE in which the present invention was implemented
1552 B: SUP using conventional method
6 Manufacturing process
【表】【table】
【表】
↓
[Table] ↓
【表】
A、B両者ともに160Kgf/mm2強度レベルと
し、下記の如き圧縮コイルばね完製品とする。
D/d ………6
有効巻数Na ………5巻
総巻数Nt ………7巻
自由高さH ………220mm
(2) 実験方法
A、Bともに定歪型疲労試験機にかけ、200
万回での疲労限を求めた。
(3) 実験結果
下記のとおりであつた。[Table] Both A and B have a strength level of 160Kgf/ mm2 , and are completed compression coil spring products as shown below. D/d......6 Effective number of turns Na...5 turns Total number of turns Nt...7 turns Free height H...220 mm (2) Experimental method Both A and B were subjected to a constant strain fatigue tester and 200
The fatigue limit after 10,000 repetitions was determined. (3) Experimental results The results were as follows.
【表】
すなわち、本発明にかゝる冷間成形コイルば
ねは従来の熱間成形によるコイルばねの疲労限
が60±38Kgf/mm2であつてのに対し、60±45Kg
f/mm2以上の疲労限を示した。
上記実施例においては急速加熱手段として主と
して高周波誘導加熱を用いる場合について述べた
が、それに代えて直接通電方式等を用いてもほゞ
同様の効果がえられる。
本発明によれば、誘導加熱による急速加熱、急
速冷却からなる熱処理で母材の引張強さが150Kg
f/mm2以上の高強度でありながら、伸び9%以
上、絞り49%以上という高加工性が付与されてい
るので、従来、熱間成形せざるを得なかつた、線
径が10mmφ以上の大径の高強度線材からなる冷間
成形コイルばねを容易に提供することができ、そ
の結果、従来の熱間成形コイルばねにとつて避け
られなかつた、ばね表面の脱減炭、材料強度の低
下、強度のバラツキ、表面肌荒れ、変形等の生ず
ることのない、大径かつ高強度のコイルばねを実
現することができる。さらに製品は定歪型疲労試
験機による200万回での疲労限が60±45Kgf/mm2
以上という高耐久性で、かつ低へたり性を有する
ので、上述の効果と併せて従来のものに比し、き
わめて優れたばね特性を有するコイルばねを提供
することができる。[Table] In other words, the fatigue limit of the cold-formed coil spring according to the present invention is 60±45Kg, whereas that of the conventional hot-formed coil spring is 60±38Kgf/ mm2 .
It showed a fatigue limit of f/mm 2 or more. In the above embodiments, the case where high frequency induction heating is mainly used as the rapid heating means has been described, but substantially the same effect can be obtained even if a direct energization method or the like is used instead. According to the present invention, the tensile strength of the base material can be increased to 150 kg by heat treatment consisting of rapid heating and rapid cooling by induction heating.
Although it has high strength of f/mm 2 or more, it has high workability of elongation of 9% or more and reduction of area of 49% or more, so it can be used for wires with a diameter of 10 mmφ or more, which conventionally had to be hot formed. It is possible to easily provide cold-formed coil springs made of large-diameter, high-strength wire rods, and as a result, the decarbonization of the spring surface and material strength, which were unavoidable with conventional hot-formed coil springs, can be easily provided. It is possible to realize a large-diameter, high-strength coil spring that does not suffer from deterioration, strength variations, surface roughness, deformation, etc. Furthermore, the product has a fatigue limit of 60±45Kgf/mm 2 after 2 million cycles using a constant strain fatigue tester.
Since it has the above-mentioned high durability and low flattening property, it is possible to provide a coil spring which has the above-mentioned effects and extremely superior spring characteristics compared to conventional ones.
第1図〜第3図は本発明の実験結果を示す、そ
れぞれ線図である。
FIGS. 1 to 3 are diagrams showing experimental results of the present invention, respectively.
Claims (1)
熱処理で母材が結晶粒度ASTM番号9以上の細
粒マルテンサイト組織を有し、引張強さ150Kg
f/mm2以上、伸び9%以上、絞り49%以上の高強
度と延性・靭性を兼備した機械的性質を有する、
線径10mmφ以上の、200万回での疲労限が、ねじ
り剪断応力τw=60±45Kgf/mm2以上で、かつ、
へたりのきわめて少ない冷間成形コイルばね。1 Through heat treatment consisting of rapid heating and rapid cooling by induction heating, the base material has a fine martensitic structure with a grain size of ASTM number 9 or higher, and a tensile strength of 150 kg.
It has mechanical properties that combine high strength with f/mm 2 or more, elongation of 9% or more, and reduction of area of 49% or more, as well as ductility and toughness.
Wire diameter 10mmφ or more, fatigue limit after 2 million cycles is torsional shear stress τw=60±45Kgf/mm2 or more , and
Cold-formed coil spring with extremely low settling.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP10426883A JPS5964717A (en) | 1983-06-13 | 1983-06-13 | Cold-formed coil spring |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP10426883A JPS5964717A (en) | 1983-06-13 | 1983-06-13 | Cold-formed coil spring |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP4993078A Division JPS5913568B2 (en) | 1978-04-28 | 1978-04-28 | Manufacturing method for cold-formed coil springs |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5964717A JPS5964717A (en) | 1984-04-12 |
| JPS63491B2 true JPS63491B2 (en) | 1988-01-07 |
Family
ID=14376174
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP10426883A Granted JPS5964717A (en) | 1983-06-13 | 1983-06-13 | Cold-formed coil spring |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5964717A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2006111980A3 (en) * | 2005-04-20 | 2009-04-09 | Ideal Cures Pvt Ltd | Pva based film coating and film coating compositions |
-
1983
- 1983-06-13 JP JP10426883A patent/JPS5964717A/en active Granted
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2006111980A3 (en) * | 2005-04-20 | 2009-04-09 | Ideal Cures Pvt Ltd | Pva based film coating and film coating compositions |
Also Published As
| Publication number | Publication date |
|---|---|
| JPS5964717A (en) | 1984-04-12 |
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