JPH032220B2 - - Google Patents
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- Publication number
- JPH032220B2 JPH032220B2 JP22468284A JP22468284A JPH032220B2 JP H032220 B2 JPH032220 B2 JP H032220B2 JP 22468284 A JP22468284 A JP 22468284A JP 22468284 A JP22468284 A JP 22468284A JP H032220 B2 JPH032220 B2 JP H032220B2
- Authority
- JP
- Japan
- Prior art keywords
- temperature
- cooling
- eutectic
- sintering
- experimental example
- 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
- 238000001816 cooling Methods 0.000 claims description 48
- 230000005496 eutectics Effects 0.000 claims description 30
- 239000000463 material Substances 0.000 claims description 28
- 238000005245 sintering Methods 0.000 claims description 18
- 238000010791 quenching Methods 0.000 claims description 17
- 230000000171 quenching effect Effects 0.000 claims description 16
- 238000000034 method Methods 0.000 claims description 15
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 12
- 238000004519 manufacturing process Methods 0.000 claims description 8
- 238000010438 heat treatment Methods 0.000 claims description 6
- 229910052742 iron Inorganic materials 0.000 claims description 6
- 238000007711 solidification Methods 0.000 claims description 6
- 230000008023 solidification Effects 0.000 claims description 6
- 239000011261 inert gas Substances 0.000 claims description 3
- 229910000734 martensite Inorganic materials 0.000 claims 1
- 239000000843 powder Substances 0.000 description 12
- 239000007789 gas Substances 0.000 description 10
- 229910001566 austenite Inorganic materials 0.000 description 8
- 230000007423 decrease Effects 0.000 description 7
- 238000002347 injection Methods 0.000 description 7
- 239000007924 injection Substances 0.000 description 7
- 238000012360 testing method Methods 0.000 description 6
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 5
- 230000000694 effects Effects 0.000 description 5
- 239000007791 liquid phase Substances 0.000 description 5
- 150000001247 metal acetylides Chemical class 0.000 description 5
- 229910001315 Tool steel Inorganic materials 0.000 description 4
- 229910052799 carbon Inorganic materials 0.000 description 4
- 239000013078 crystal Substances 0.000 description 4
- 238000005496 tempering Methods 0.000 description 4
- 238000000137 annealing Methods 0.000 description 3
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 3
- 238000005452 bending Methods 0.000 description 3
- 230000003247 decreasing effect Effects 0.000 description 3
- 238000007542 hardness measurement Methods 0.000 description 3
- 230000000977 initiatory effect Effects 0.000 description 3
- 238000005259 measurement Methods 0.000 description 3
- 229910052750 molybdenum Inorganic materials 0.000 description 3
- 238000000465 moulding Methods 0.000 description 3
- 229910052760 oxygen Inorganic materials 0.000 description 3
- 239000001301 oxygen Substances 0.000 description 3
- 229910052720 vanadium Inorganic materials 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 2
- 238000007796 conventional method Methods 0.000 description 2
- 238000000280 densification Methods 0.000 description 2
- 230000008034 disappearance Effects 0.000 description 2
- 238000002474 experimental method Methods 0.000 description 2
- 239000012467 final product Substances 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 239000011159 matrix material Substances 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 239000011148 porous material Substances 0.000 description 2
- 239000000047 product Substances 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 229910000997 High-speed steel Inorganic materials 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- 230000008033 biological extinction Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 238000001739 density measurement Methods 0.000 description 1
- 238000004455 differential thermal analysis Methods 0.000 description 1
- 238000007580 dry-mixing Methods 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 239000012768 molten material Substances 0.000 description 1
- 239000012071 phase Substances 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 230000002250 progressing effect Effects 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 238000004904 shortening Methods 0.000 description 1
- 239000007858 starting material Substances 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 238000009692 water atomization Methods 0.000 description 1
- XOOUIPVCVHRTMJ-UHFFFAOYSA-L zinc stearate Chemical compound [Zn+2].CCCCCCCCCCCCCCCCCC([O-])=O.CCCCCCCCCCCCCCCCCC([O-])=O XOOUIPVCVHRTMJ-UHFFFAOYSA-L 0.000 description 1
Landscapes
- Powder Metallurgy (AREA)
Description
産業上の利用分野
本発明は工具材料等特に高強度、耐摩耗性が要
求される鉄基焼結材料の製造方法に関する。
従来技術
近年、高速度工具鋼、冷間・工具鋼等の焼結法
による製造が普及しつつある。これらは水アトマ
イズ法による予備合金粉末をプレス成形後焼結す
るものである。すなわち、比較的酸素量が多いが
成形性の優れた水アトマイズ粉末を出発原料と
し、この表面酸化物を、該粉末に黒鉛粉末を添加
して還元すること、及び粉末材中の共晶炭化物が
溶融する温度域の真空又は不活性ガス中で焼結す
ることにより真密度に近く高密度化することの二
条件の併合によるものである。
これらは高速度工具鋼では、エンドミル、ドリ
ル、タツプ、バイトチツプ等、自動車関係では、
ロツカーアーム、カムシヤフトリング等に応用さ
れている。
この焼結材料は、圧延材等の溶製材に比し、焼
結完了時点の形状を最終製品に近く設定すること
により、高材料歩留かつ省工数に製造できる特長
がある。
しかし、従来の焼結製品は、性能的に十分満足
できないものであつた。次に、実験例1により従
来法の性能上の問題点を具体例をもつて示す。
まず、JIS SKH9相当の重量比で、C0.91%、
Si0.23%、Mn0.20%、Cr4.10%、W5.95%、
Mo5.02%、V1.89%、Fe Bal、および不可避的
不純物からなる100メツシユの乾燥状態でO2含有
量3200PPmの水アトマイズ粉末を準備した。
この粉末にその酸素分をCOガスとして還元す
るための化学量論的炭素量として、黒鉛粉末を
0.24%添加し、真空中で1000℃×3hrの還元処理
を施した。還元後の酸素量は960ppm、炭素量は
0.83%であつた。以下に述べる実験にはこの還元
粉末を使用した。
実験例 1
この還元粉末に潤滑剤としてステアリン酸亜鉛
を0.7%添加し、乾式混合後、通常のプレスによ
り6tonf/cm2の圧力で成形し、10-2Torrの真空中
で昇温速度200℃/hrで1255℃まで昇温し、この
温度で1hr保持後炉冷することにより焼結した。
この時の半冷時間は2hrでこの処理は従来の製造
方法に従つたものである。半冷時間とは、焼入温
度をt℃とするとt/2℃まで冷却した時に要し
た時間を示す。
この焼結試料の密度は8.06g/cm3であり、400
倍で検鏡の結果、残存空孔は存在せず実質的に真
密度と判断され、またオーステナイト結晶粒度は
JIS法で9.0であつた。
次にこの焼結材を、比較材として溶製法による
ほゞ同成分のSKH9の30mmφ棒鋼から削出した試
験片とともに、完全焼なまし、焼入れ、焼もどし
処理した後、寸法5.0w×3.0t×40の試片による
抗折試験、硬さ測定、検鏡を行つた。処理条件は
溶製材の標準的条件である焼なましは860℃×3hr
加熱保持後20℃/hr冷却、焼入れは真空炉中で
1200℃×20min加熱保持後3barのN2ガス噴射冷
却(半冷時間3min)、焼もどしは大気中560℃×
1hr×2回である。焼結材及び溶製材の硬さ、抗
折力はそれぞれHRC63.1,270Kgf/mm2及び
HRC66.1,410Kgf/mm2であつた。
この結果から焼結材は溶製材に比し、硬さ、抗
折力ともに格段に低いことが伴る。この原因は第
1図に焼結材のミクロ組織を示すように、溶製材
の標準的組織に比し、共晶炭化物が粗大化し、形
状的に不安定で応力集中し易いこと及びオーステ
ナイト結晶粒が粗いことに起因すると推定され
る。
高速度工具鋼の共晶炭化物の共晶開始温度は実
験式として次式で示されることが報告されてい
る。
Te(〓)=2310−200(%C)+40(%V)+8(%
W)+5(%Mo)
本式に実験例の成分を代入すると、Te=2292
(〓)=1256(℃)となる。一方前記の原料粉末を
示差熱分析計で200℃/hrの昇温速度で1300℃ま
で加熱し、共晶開始温度を測定した結果は1256℃
で、ほゞ上式の結果と一致し、上式は焼結温度の
選択に利用できることが判つた。前記実験例の焼
結温度もこの温度にゞ近く、高速度工具鋼の焼結
による高密度化が、共晶による部分液相の生成で
進行していると考えられる。材料のち密化が、液
相が共存する状態で進行することは、共晶炭化物
が粗大化し、炭化物形状が不定形化することにつ
ながる。また、共晶炭化物の粗大化は当然オース
テナイト結晶粒度を粗大化するとともに、粗大化
過程で基質中のC、W、Mo、V等の合金元素が
炭化物に吸収されて、基地中のCと合金量が減少
し、焼もどし硬さを低下させることになる。
したがつて、結論的には炭化物の粗大化が焼結
材料の強度低下と硬さ低下の原因となる。換言す
ると、従来技術の範ちゆうでの焼結高速度鋼は、
溶製材に対比して性能的には満足すべきものは得
られないことを示している。
発明が解決しようとする問題点
本発明は、従来の製造方法を改良することによ
り、性能を改善した鉄基焼結材料を提供すること
を目的とする。
問題点を解決するための手段
本発明は、昇温過程における共晶炭化物の共晶
開始温度以上で焼結し、この温度から6℃/min
以上64℃/min以下の冷却速度で事実上降温過程
の共晶炭化物凝固終了温度以下まで冷却後その
まゝ不活性ガス噴射により半冷時間10min以上の
冷却速度で焼入れすることを特徴とする鉄基焼結
材料の製造方法である。
作用及び実施例
以下、実験例により、本発明の作用、効果を述
べる。
実験例 2
前記実験例1と同条件で成形後これと同様に、
真空炉中で1255℃で1hr保持することにより焼結
を完了した試料を、この温度で上部から3barの
N2ガスを吹きつけて強制冷却した。半冷時間は
約3minであつた。室温まで冷却後、焼なまし及
び焼入れの処理をすることなく、560℃×1hr×2
回の焼もどし処理を行つた。この試料のミクロ組
織を第2図に示す。実験例1での組織と比較し
て、共晶炭化物の粒径がやや微細化しており、オ
ーステナイト結晶粒度もJIS9.5でやはり微細化の
傾向が認められた。また密度測定結果は8.08g/
cm3で残留空孔は認められず、実質的に真密度であ
つた。実験例1と同様の試片による抗折力は370
Kgf/mm2、硬さはHRC65.5であり、実験例1に
比し、焼結温度から直ちに急冷焼入れすることに
より、組織が微細化し、これにより機械的強度及
び硬さが大幅に改善されることが判明した。しか
し、試料には大きな歪が発生しており、実用化上
重大な障害となることが予想された。恐らく共晶
反応による部分液相が存在している状態から、焼
入を行うことは、大きな歪発生を伴うものと推定
される。
実験例 3
実験例1と同条件で成形後これと同様に、真空
炉中で1255℃×1hr保持後それぞれ約8℃/min
の冷却速度で1245℃,1235℃,1225℃及び1215℃
まで降温し、それぞれの温度から実験例2と同様
N2ガス冷却した。このときの半冷時間は約3min
であつた。この焼入れ試料と実験例1と同条件で
焼もどし処理した後、歪測定、オーステナイト結
晶粒度測定、抗折試験及び硬さ測定を行つた。第
1表のその結果を実験例1で行つた焼結材及び溶
製材並びに実験例2で行つた焼結材の結果と併せ
て示す。
INDUSTRIAL APPLICATION FIELD The present invention relates to a method for producing iron-based sintered materials, such as tool materials, which particularly require high strength and wear resistance. BACKGROUND OF THE INVENTION In recent years, the production of high-speed tool steel, cold-worked tool steel, etc. by the sintering method has become popular. These are prepared by press-forming pre-alloyed powder using a water atomization method and then sintering it. That is, a water atomized powder with a relatively large amount of oxygen but excellent moldability is used as a starting material, and this surface oxide is reduced by adding graphite powder to the powder, and the eutectic carbide in the powder material is reduced. This is due to the combination of two conditions: sintering in a vacuum or inert gas in a melting temperature range to achieve high density close to true density. These are high-speed tool steels such as end mills, drills, taps, bit tips, etc., and automobile-related products.
It is applied to Rotscar arms, camshaft rings, etc. Compared to ingot materials such as rolled materials, this sintered material has the advantage that it can be manufactured with a high material yield and reduced man-hours by setting the shape at the time of completion of sintering close to that of the final product. However, conventional sintered products have not been fully satisfactory in terms of performance. Next, using Experimental Example 1, problems with the performance of the conventional method will be illustrated with a concrete example. First, the weight ratio equivalent to JIS SKH9 is C0.91%,
Si0.23%, Mn0.20%, Cr4.10%, W5.95%,
A 100 mesh dry water atomized powder with an O 2 content of 3200 PPm was prepared consisting of 5.02% Mo, 1.89% V, Fe Bal, and unavoidable impurities. Graphite powder is added to this powder as the stoichiometric amount of carbon to reduce the oxygen content to CO gas.
0.24% was added and subjected to reduction treatment in vacuum at 1000°C for 3 hours. The amount of oxygen after reduction is 960ppm, and the amount of carbon is
It was 0.83%. This reduced powder was used in the experiments described below. Experimental example 1 0.7% zinc stearate was added as a lubricant to this reduced powder, and after dry mixing, it was molded with a normal press at a pressure of 6 tonf/cm 2 and heated at a temperature increase rate of 200°C in a vacuum of 10 -2 Torr. The temperature was increased to 1255°C at a rate of 1255°C at a rate of 1255°C, maintained at this temperature for 1 hour, and then cooled in the furnace for sintering.
The half-cooling time at this time was 2 hours, and this treatment followed the conventional manufacturing method. The half-cooling time refers to the time required for cooling to t/2°C, where the quenching temperature is t°C. The density of this sintered sample is 8.06 g/ cm3 , which is 400 g/cm3.
As a result of the microscopic examination at double magnification, it was determined that there were no residual pores and that the density was substantially true, and the austenite grain size was
It was 9.0 according to JIS method. Next, this sintered material was completely annealed, quenched, and tempered, along with a test piece cut from a 30mmφ steel bar of SKH9 with almost the same composition by the melting method as a comparison material. A bending test using a 40× specimen, hardness measurement, and microscopic examination were performed. The processing conditions are standard conditions for ingot lumber, annealing is 860℃ x 3 hours.
After heating and holding, cooling at 20℃/hr and quenching in a vacuum furnace.
After heating and holding at 1200°C for 20 min, cooling with 3 bar N2 gas injection (half-cooling time 3 min), tempering at 560°C in the air
1hr x 2 times. The hardness and transverse rupture strength of the sintered material and ingot material are HRC63.1, 270Kgf/mm 2 and
HRC66.1, 410Kgf/ mm2 . This result shows that the sintered material has significantly lower hardness and transverse rupture strength than the ingot material. The reason for this is that, as shown in the microstructure of the sintered material in Figure 1, the eutectic carbides are coarser than the standard structure of the sintered material, making it unstable in shape and prone to stress concentration, and the austenite crystal grains. This is presumed to be due to the roughness of the surface. It has been reported that the eutectic initiation temperature of eutectic carbides in high-speed tool steel is expressed by the following empirical formula: Te(〓)=2310−200(%C)+40(%V)+8(%
W) + 5 (%Mo) Substituting the components of the experimental example into this formula, Te = 2292
(〓) = 1256 (℃). On the other hand, the above raw material powder was heated to 1300°C at a heating rate of 200°C/hr using a differential thermal analyzer, and the eutectic initiation temperature was measured to be 1256°C.
The result almost coincides with the result of the above equation, and it was found that the above equation can be used to select the sintering temperature. The sintering temperature in the above-mentioned experimental example was also close to this temperature, and it is thought that the densification of the high-speed tool steel by sintering is progressing due to the formation of a partial liquid phase due to eutectic. When the densification of the material progresses in the presence of a liquid phase, the eutectic carbide becomes coarser and the shape of the carbide becomes amorphous. In addition, the coarsening of the eutectic carbide naturally coarsens the austenite grain size, and during the coarsening process, alloying elements such as C, W, Mo, and V in the matrix are absorbed by the carbide and alloyed with C in the matrix. The amount will decrease and the tempering hardness will decrease. Therefore, the conclusion is that the coarsening of carbides causes a decrease in strength and hardness of the sintered material. In other words, sintered high speed steel within the scope of the prior art is
This shows that it is not possible to obtain satisfactory performance compared to ingot lumber. Problems to be Solved by the Invention The present invention aims to provide an iron-based sintered material with improved performance by improving the conventional manufacturing method. Means for Solving the Problems The present invention sinters the eutectic carbide at a temperature higher than the eutectic start temperature in the temperature raising process, and from this temperature the eutectic carbide is sintered at a rate of 6°C/min from this temperature.
Iron characterized by being cooled to below the temperature at which eutectic carbide solidification ends in the cooling process at a cooling rate of 64°C/min or less, and then quenched by inert gas injection at a cooling rate of 10 min or more for half-cooling time. This is a method for producing a base sintered material. Effects and Examples The effects and effects of the present invention will be described below using experimental examples. Experimental Example 2 After molding under the same conditions as Experimental Example 1, similarly,
The sample, which has been sintered by holding it at 1255℃ for 1 hour in a vacuum furnace, is heated at 3bar from the top at this temperature.
Forced cooling was performed by blowing N 2 gas. The half-cooling time was about 3 minutes. After cooling to room temperature, 560℃×1hr×2 without annealing or quenching.
A second tempering process was performed. The microstructure of this sample is shown in FIG. Compared to the structure in Experimental Example 1, the grain size of the eutectic carbide was slightly refined, and the austenite crystal grain size also showed a tendency to become finer in JIS9.5. Also, the density measurement result is 8.08g/
No residual pores were observed at cm 3 and the density was substantially the same. The transverse rupture strength of the same specimen as in Experimental Example 1 was 370.
Kgf/mm 2 , hardness is HRC65.5, and compared to Experimental Example 1, by rapidly cooling and quenching immediately from the sintering temperature, the structure becomes finer and the mechanical strength and hardness are significantly improved. It turned out that. However, large distortions had occurred in the sample, which was expected to pose a serious obstacle to practical application. Since a partial liquid phase is present, probably due to a eutectic reaction, quenching is presumed to be accompanied by large strain. Experimental Example 3 After molding under the same conditions as Experimental Example 1, in the same way, after holding in a vacuum furnace at 1255°C for 1 hour, each was heated at approximately 8°C/min.
1245℃, 1235℃, 1225℃ and 1215℃ with cooling rate of
Same as Experimental Example 2 from each temperature.
Cooled with N2 gas. The half-cooling time at this time is approximately 3 minutes.
It was hot. After this hardened sample was tempered under the same conditions as in Experimental Example 1, strain measurements, austenite grain size measurements, bending tests, and hardness measurements were performed. The results in Table 1 are shown together with the results for the sintered material and ingot material conducted in Experimental Example 1 and the sintered material conducted in Experimental Example 2.
【表】
本表から、歪は焼入れ冷却開始温度を焼結温度
より20〜30℃低温とすることにより、急激に低下
することが判る。昇温過程の共晶開始温度に対
し、降温過程の共晶凝固終了温度は低温であるか
ら、実験例2並びに実験例3のD及びEでは、相
液が存在する状態から急冷したため大きい焼入れ
歪が発生したものと思われる。
実験例 4
次に、焼結温度から共晶消出温度までの冷却速
度の影響を調べる実験を行つた。実験例1と同条
件で成形後これと同様に、1255℃×1hr保持後
1225℃まで、それぞれ2,4,16,32及び64℃/
minの冷却速度で降温後、3barのN2ガスを噴射
して焼入れし、実験例1と同条件の焼もどし処理
し、実験例3と同条件で特性を調査した。なお焼
入れの半冷時間はそれぞれ3minであつた。この
結果を第2表に、冷却速度8℃/minのものは第
1表のFと併せて示す。[Table] From this table, it can be seen that strain decreases rapidly by setting the quenching cooling start temperature to 20 to 30°C lower than the sintering temperature. Since the eutectic solidification end temperature in the temperature decreasing process is lower than the eutectic start temperature in the temperature increasing process, in Experimental Examples 2 and 3, D and E, there was a large quenching strain because the phase liquid was rapidly cooled. seems to have occurred. Experimental Example 4 Next, an experiment was conducted to investigate the influence of the cooling rate from the sintering temperature to the eutectic extinction temperature. After molding under the same conditions as Experimental Example 1, after holding at 1255℃ for 1 hour.
Up to 1225℃, 2, 4, 16, 32 and 64℃/
After cooling at a cooling rate of min, quenching was performed by injecting N 2 gas at 3 bar, tempering was performed under the same conditions as in Experimental Example 1, and the characteristics were investigated under the same conditions as in Experimental Example 3. The half-cooling time of each quenching was 3 min. The results are shown in Table 2, and the cooling rate of 8° C./min is shown together with F in Table 1.
【表】【table】
【表】
本表から、1225℃つまり、共晶消失温度までの
降温速度が低くなるに従つてオーステナイト結晶
粒度がやや粗く、硬さ、抗折力もやや低下し、ま
た焼入歪が増加することが判る。ミクロ組織の観
察結果では、この冷却速度の低下とともに共晶炭
化物がやや粗大化し、不定形化することが確認さ
れた。第3図に試料Jのミクロ組織を示す。1225
℃までの冷却速度を16℃/minと比較的速くする
ことで、共晶炭化物のミクロ組織がきわめて微細
化できる。
実験例3の結果を併せて考察すると、液相の存
在下で極めて速い速度で冷却すると焼入れ歪が発
生し、逆に冷却速度を極度に低下すると組織の粗
大化及び歪の増加が起り、その中間の4〜64℃/
min程度に適正な冷却速度が存在することが判
る。したがつて本発明ではこの冷却速度の下限を
6℃/minとする。
実験例 5
重量比で、C1.6%、Si0.6%、Mn0.5%、Cr12.6
%、Mo1.0%、V0.4%、Fe BaからなるJIS
SKD11相当の−100メツシユの水アトマイズ粉末
に黒鉛粉末を添加し、1000℃×3hrの真空中で還
元処理した。残存O2量は820ppm、C量は1.5%で
あつた。本粉末の示差熱分析による昇温過程の共
晶炭化物の共晶開始温度は、1235℃、降温中の液
相消失温度は1202℃であつた。同粉末を6tonf/
cm2で冷間成形後昇温速度200℃/hrで1235℃まで
昇温し、1hr温度保持した後、それぞれ下記の条
件で焼入れ処理し、550℃×1hr×2回の焼もどし
を行つて、オーステナイト結晶粒度、抗折試験、
硬さの測定及び検鏡を行つた。
(M) 温度保持後常温まで半冷時間約2hrの炉
冷、850℃×3hrの焼なまし及び1050℃×1hr保
持後3barのN2ガス噴射による半冷時間約3min
の焼入れ処理
(N) 温度保持直後3barのN2ガス噴射により
半冷時間約3minで常温まで強制冷却
(O) 温度保持後1200℃まで8℃/minで降温
し、この温度から(N)と同様N2ガス噴射に
より、半冷時間約3minで常温まで強制冷却
(P) 温度保持後1050℃まで8℃/minで降温
し、この温度から(N)と同様N2ガス噴射に
より、半冷時間約3minで常温まで強制冷却
第3表にこの結果を示す。なお本表には併せて
作製した、ほゞ同成分の溶製材を1050℃×1hr保
持後3barのN2ガス噴射により半冷時間約3minの
焼入れを行い前記と同条件の焼もどし処理を行つ
たものの測定結果(Q)も併記した。[Table] From this table, it can be seen that as the temperature decreases to 1225℃, that is, the eutectic disappearance temperature, the austenite crystal grain size becomes slightly coarser, the hardness and transverse rupture strength decrease slightly, and the quenching strain increases. I understand. The microstructure observation results confirmed that as the cooling rate decreased, the eutectic carbides became somewhat coarser and became amorphous. FIG. 3 shows the microstructure of sample J. 1225
By setting the cooling rate to 16°C/min relatively fast, the microstructure of the eutectic carbide can be made extremely fine. Considering the results of Experimental Example 3 as well, it can be seen that cooling at an extremely high rate in the presence of a liquid phase causes quenching distortion, and conversely, when the cooling rate is extremely reduced, the structure becomes coarser and distortion increases. Intermediate 4-64℃/
It can be seen that there is an appropriate cooling rate around min. Therefore, in the present invention, the lower limit of this cooling rate is set to 6° C./min. Experimental example 5 Weight ratio: C1.6%, Si0.6%, Mn0.5%, Cr12.6
%, Mo1.0%, V0.4%, JIS consisting of Fe Ba
Graphite powder was added to -100 mesh water atomized powder equivalent to SKD11, and reduced in vacuum at 1000°C for 3 hours. The amount of residual O 2 was 820 ppm, and the amount of C was 1.5%. Differential thermal analysis of this powder revealed that the eutectic initiation temperature of the eutectic carbide during the heating process was 1235°C, and the liquid phase disappearance temperature during the cooling process was 1202°C. 6tonf of the same powder/
After cold forming at cm2 , the temperature was raised to 1235℃ at a temperature increase rate of 200℃/hr, and after holding the temperature for 1 hour, it was quenched under the following conditions and tempered twice at 550℃ x 1hr. , austenite grain size, bending test,
Hardness measurements and microscopic examination were performed. (M) After temperature maintenance, half-cooling time to room temperature: Furnace cooling for about 2 hours, annealing at 850℃ x 3 hours, and after holding at 1050℃ x 1 hour, half-cooling time by 3 bar N2 gas injection for about 3 minutes.
Quenching treatment (N) Immediately after holding the temperature, forced cooling to room temperature with a half-cooling time of approximately 3 minutes using N2 gas injection at 3 bar (O) After holding the temperature, the temperature is lowered at a rate of 8°C/min to 1200°C, and from this temperature (N) Similarly, by N2 gas injection, forced cooling to room temperature in about 3 minutes (P) After temperature maintenance, the temperature is lowered at 8℃/min to 1050℃, and from this temperature, by N2 gas injection, like (N), it is half cooled. Forced cooling to room temperature in about 3 minutes Table 3 shows the results. This table also shows melted materials with almost the same composition that were held at 1050°C for 1 hour, then quenched with N2 gas injection at 3 bar for a half-cooling time of about 3 minutes, and then tempered under the same conditions as above. The measurement results (Q) of the vines are also listed.
【表】
本表及び検鏡結果によると、前記実験例1〜4
で得られたSKH9の場合と全く同様の現象が見ら
れることが判る。すなわち、従来法である焼結後
炉冷し再焼入れする方法では、真密度化は達成で
きるが、共晶炭化物の粗大化、オーステナイト結
晶粒の粗大化、抗折力及び熱処理硬が低下する
(M)、これに対し焼結温度から直接焼入れするも
のでは、硬さ、抗折力は増加するが、歪が大きい
(N)、焼結温度から適度の降温速度で共晶炭化物
凝固完了温度(この成分では1202℃)以下まで冷
却し、この状態から焼入れすることにより、溶製
材に匹敵する硬さ及び抗折力が得られる(O,
P)ことが判る。
発明の効果
以上に述べたように本発明は、最終製品形状に
近い形状に焼でき、歩留り、仕上加工能率等で有
利な面を有するが、従来、性能面では溶製材に比
して劣つていた鉄基の焼結材を、焼結後適当な降
温速度で共晶凝固完了温度以下に降温後焼入れす
ることにより、過大な歪の発生を防止してその性
能を溶製材に匹敵するまで高めるものであり、特
に工具用途に対し大きな効果を有するものであ
る。また本発明は、焼結の降温過程を焼入れ冷却
に利用するものであり、省エネルギ、工程短縮の
効果の効果も有する。[Table] According to this table and the microscopic results, the above experimental examples 1 to 4
It can be seen that exactly the same phenomenon as in the case of SKH9 obtained in . In other words, the conventional method of furnace cooling and re-quenching after sintering can achieve true density, but it results in coarsening of eutectic carbides, coarsening of austenite crystal grains, and a decrease in transverse rupture strength and heat treatment hardness ( On the other hand, when quenching directly from the sintering temperature, the hardness and transverse rupture strength increase, but the strain is large (N), and the eutectic carbide solidification completion temperature ( With this component, by cooling to below 1202℃ and quenching from this state, hardness and transverse rupture strength comparable to that of ingot material can be obtained (O,
P) It turns out that. Effects of the Invention As described above, the present invention can be fired into a shape close to the final product shape, and has advantages in terms of yield, finishing efficiency, etc. However, in terms of performance, it has traditionally been inferior to ingot material. After sintering, iron-based sintered material is cooled to below the eutectic solidification completion temperature at an appropriate temperature cooling rate and then quenched to prevent excessive distortion and improve its performance to match that of molten material. This is particularly effective for tool applications. Further, the present invention utilizes the temperature decreasing process of sintering for quenching cooling, and has the effects of energy saving and process shortening.
第1図及び第2図は、それぞれ従来の製造方法
によつて作製し、焼入れ焼もどし処理した試験片
及び焼結温度から直接焼入れした後焼もどし処理
した試験片のそれぞれミクロ金属組織写真であ
る。第3図は本願発明手法によるもので、共晶炭
化物の凝固終了温度まで16℃/minの冷却速度で
冷却後、半冷時間10minで焼入し、焼もどした試
料のミクロ金属組織写真である。
Figures 1 and 2 are photographs of the micrometallic structure of a test piece produced by a conventional manufacturing method and quenched and tempered, and a test piece that was quenched directly from the sintering temperature and then tempered, respectively. . Figure 3 is a photograph of the micrometallic structure of a sample obtained by the method of the present invention, which was cooled at a cooling rate of 16°C/min to the solidification end temperature of the eutectic carbide, then quenched for a half-cooling time of 10 min, and then tempered. .
Claims (1)
より強度と耐摩耗性を与える鉄基焼結材料の製造
方法において、昇温過程における共晶炭化物の共
晶開始温度以上で焼結し、この焼結温度から6
℃/min以上64℃/min以下の冷却速度で事実上
降温過程の共晶炭化物凝固完了温度以下まで冷却
後、そのまゝ不活性ガスを噴射し、半冷時間10mm
以上の速度で冷却し、焼入れすることを特徴とす
る鉄基焼結材料の製造方法。1. In a method for producing an iron-based sintered material containing eutectic carbide and imparting strength and wear resistance through martensitic hardening, sintering is performed at a temperature higher than the eutectic start temperature of the eutectic carbide in the heating process, and this sintering 6 from temperature
After cooling at a cooling rate of ℃/min to 64℃/min to below the temperature at which eutectic carbide solidification is completed in the cooling process, inert gas is directly injected and half-cooling time is 10 mm.
A method for producing an iron-based sintered material, characterized by cooling and quenching at a rate equal to or higher than the above.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP22468284A JPS61104046A (en) | 1984-10-25 | 1984-10-25 | Manufacture of iron-base sintered material |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP22468284A JPS61104046A (en) | 1984-10-25 | 1984-10-25 | Manufacture of iron-base sintered material |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS61104046A JPS61104046A (en) | 1986-05-22 |
| JPH032220B2 true JPH032220B2 (en) | 1991-01-14 |
Family
ID=16817570
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP22468284A Granted JPS61104046A (en) | 1984-10-25 | 1984-10-25 | Manufacture of iron-base sintered material |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS61104046A (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP4783032B2 (en) * | 2004-02-18 | 2011-09-28 | 住友電工焼結合金株式会社 | Sintered high speed steel, its manufacturing method and sliding parts made of the sintered high speed steel |
-
1984
- 1984-10-25 JP JP22468284A patent/JPS61104046A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS61104046A (en) | 1986-05-22 |
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