WO1995010637A1 - Acier de forgeage a chaud sans traitement thermique, presentant d'excellentes caracteristiques de resistance a la traction et a la fatigue et une tres bonne aptitude a l'usinage - Google Patents
Acier de forgeage a chaud sans traitement thermique, presentant d'excellentes caracteristiques de resistance a la traction et a la fatigue et une tres bonne aptitude a l'usinage Download PDFInfo
- Publication number
- WO1995010637A1 WO1995010637A1 PCT/JP1994/001693 JP9401693W WO9510637A1 WO 1995010637 A1 WO1995010637 A1 WO 1995010637A1 JP 9401693 W JP9401693 W JP 9401693W WO 9510637 A1 WO9510637 A1 WO 9510637A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- machinability
- ratio
- steel
- tensile strength
- bainite
- Prior art date
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Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/14—Ferrous alloys, e.g. steel alloys containing titanium or zirconium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/001—Ferrous alloys, e.g. steel alloys containing N
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/28—Ferrous alloys, e.g. steel alloys containing chromium with titanium or zirconium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/60—Ferrous alloys, e.g. steel alloys containing lead, selenium, tellurium, or antimony, or more than 0.04% by weight of sulfur
Definitions
- Non-heat treated steel for hot forging with excellent tensile strength, fatigue strength and machinability
- the present invention relates to a non-heat treated steel used as hot forged having excellent tensile strength, fatigue strength and machinability at the same time without performing a tempering treatment such as quenching and tempering after hot forging.
- non-heat treated steel has become widespread for use in parts for machine structures such as automobiles from the viewpoint of omitting processes and reducing manufacturing costs.
- non-heat treated steels have been developed mainly for their high tensile strength (or hardness), yield strength and toughness. Therefore, as shown in, for example, Japanese Patent Application Laid-Open No. 62-205245, non-heat treated steels using V, which is a typical element of precipitation strengthening, have been proposed.
- V which is a typical element of precipitation strengthening
- the machinability is extremely deteriorated by increasing the tensile strength, and if the tensile strength exceeds 120 kgf / mm 2 , production can no longer be performed at normal production efficiency. Therefore, the realization of a non-heat treated steel that improves the fatigue strength without deteriorating the machinability has been desired.
- the durability ratio is at most about 0.55, and the machinability is extremely low, at most about twice that of conventional non-heat treated payinite steel. Not improved.
- the present inventors first paid attention to a pearlite-containing structure having good machinability, and firstly, deposited TiN and VN on MnS in a complex manner, thereby reducing austenite crystal grains during forging heating.
- the composite precipitate is used as a nucleation site to finely precipitate ferrite.
- V carbide or V coal is further deposited on the ferrite matrix in the precipitated pearlite.
- Fatigue strength and machinability are obtained by combining the technique of utilizing two-stage precipitation to obtain a metal structure with a fine structure and pearlite that is precipitation-strengthened.
- the present invention provides a non-heat treated steel for hot forging having high fatigue strength, tensile strength and machinability, which has been difficult to achieve with conventional non-heat treated steel. Disclosure of the invention
- the easiest way to achieve high fatigue strength is to increase the tensile strength (hardness).
- a low-temperature transformed structure such as martensite or bainite may be introduced.
- such a method significantly deteriorates machinability.
- the present inventors have studied the fatigue characteristics and machinability of several types of hot forged materials having a metal structure in which an appropriate amount of a payinite structure is mixed with a light structure.
- a composite precipitate of MnS + TiN + VN is used as a precipitation nucleus of ferrite for the purpose of refining the structure.
- a bainite structure whose hardness is controlled by reducing C and N.
- We have invented a non-heat treated steel for hot forging of the fly-painite type which can secure the possible level.
- C 0.10 to 0.35%
- Si 0.15 to 2.00%
- Mn 0.40 to 2.00%
- the remainder has a composition consisting of Fe and impurity elements.
- the structure ratio f of the bainite structure is 1. with respect to the carbon content C (%).
- composition of the first invention steel was further increased to Cr: 0.02 to 1.50%, Mo: 0.02 to 1.00%, Nb: 0.001 to 0.20%, Pb: 0.05 to 30%, Ca: 0.0005 to 0.010%, and one or more of them.
- Si an element that adjusts the deoxidation and bainite microstructure ratio. If it is less than 0.15%, its effect is small, and if it exceeds 2.00%, both the durability ratio and machinability decrease, so it is 0. 15% to 2.00%.
- Mn An element that becomes the basis of composite precipitates that are ferrite precipitation sites by adjusting the bainite structure ratio and becoming Mn S. If the content is less than 0.40%, the effect is small, and 2.00% Exceeding that, a large amount of bainite is generated and both the durability ratio and machinability are reduced, so the content is set to 0.40 to 2.00%.
- a 1 Element with deoxidizing and grain refining effects. Less than 0.0005%, the effect is small, and if more than 0.050%, hard inclusions are formed and the durability ratio and machinability are poor. Since the deviation also decreases, it should be 0.0005 to 0.050%.
- T i An element that forms a complex precipitate that precipitates as nitride on MnS and becomes a precipitate site of the fiber. Its effect is small when it is less than 0.003%, and it is coarse when it exceeds 0.005%. Since the formation of hard inclusions is promoted and the durability ratio and machinability are both reduced, the content is set to 0.003 to 0.050%.
- ⁇ An element that forms a nitride or carbonitride with Ti and V.
- the content is less than 0.0020%, the effect is small, and when it exceeds 0.0070%, both the durability ratio and machinability are reduced. 0020 to 0.0070%.
- V An element that forms complex precipitates with MnS and TiN and strengthens matrix flux in bainite. Its effect is small when it is less than 0.30%, and it is durable when it exceeds 0.70%. Both the ratio and the machinability decrease, so it should be 0.30 to 0.70%.
- the components of the first invention steel further include Cr, Mo, Nb, Pb, and Ca in order to refine the crystal grains, adjust the proportion of the payneite structure, and further improve the machinability.
- One or more types are contained. The reasons for limiting these chemical components are described below.
- Mo An element that has almost the same effect as Mn and Cr.If it is less than 0.02%, its effect is small, and if it exceeds 1.00%, a large amount of bainite is generated and durability ratio and machinability are poor. Since the deviation also decreases, it is set to 0.02 to 1.00%.
- Nb An element that has almost the same effect as Ti and V. If it is less than 0.001%, the effect is small, and if it exceeds 0.20%, both the durability ratio and machinability are reduced. 00 1 to 0.20%.
- Pb An element that improves machinability. If its content is less than 0.05%, its effect is small, and if it exceeds 0.30%, its effect is saturated and its fatigue strength and durability ratio decrease.
- % And n C a An element having almost the same effect as Pb. If it is less than 0.005%, the effect is small. If it exceeds 0.010%, the effect is saturated and the fatigue strength and durability ratio decrease. Therefore, it is set to 0.000% to 0.010%.
- the two phase structure of fly tobainite and the presence of an adequate amount of bainite ensure high tensile strength, high fatigue strength and machinability.
- the payinite microstructure can be controlled by the C content of the steel, the hardenability, and the cooling rate from the austenitic zone.
- its organization ratio ⁇ In order to effectively use a paynight organization, its organization ratio ⁇ must be 4 C or more with respect to the carbon content C (%), whereas if it exceeds 1.4 C + 0.4, the machinability Is extremely deteriorated, so the payinite organization ratio f is set to 1.4 C or more and 1.4 C + 0.4 or less with respect to the carbon content C (%).
- the cooling method after hot forging is not particularly specified. Natural cooling is naturally desirable from the viewpoint of power equipment and manufacturing costs.
- the payinite tissue ratio f is determined by observing the corroded test specimen with an optical microscope, determining the tissue hardness with a micro-Vickers hardness tester, and finally measuring the area ratio.
- a cutting test piece was taken from the same material, and a 30 mm deep blind hole was drilled using an SKH9 lOmm0 straight shank drill, and the total drilling distance until the drill broke its life was measured.
- the total drilling distance of the conventional steel No. steel was set to 1.00, and the machinability was evaluated based on the relative ratio to that.
- the cutting speed was 5 Om / min
- the feed rate was 0.35 mm / rev
- the cutting oil was 7 L / min.
- Table 2 shows the bainite microstructure ratio and performance evaluation results of each test material.
- the durability ratio of tempered steel No. 42 was 0.47 'machinability of 1.00, while the durability ratio of No. 120 of the present invention was 0.57 or more, and the machinability was also higher. Is almost twice or three times better than No. 42.
- No. 21 of the comparative example has low fatigue strength because of low C content and low tensile strength and low durability ratio.
- Comparative Example No. 22 since the amount of C was too high, martensite was generated, and the conditions of the payite structure ratio of the present invention could not be satisfied. Is bad.
- Comparative Example No. 23 since the amount of Si was low, the degree of deoxidation was low and the durability ratio was lower than that of the present invention. In Comparative Example No. 24, since the amount of 5i was high, martensite was generated, and the condition of the bainite structure ratio of the present invention could not be satisfied.
- Comparative Example No. 25 since the amount of Mn was low, the precipitation of composite precipitates was small, and the durability ratio was low. It is lower than the present invention. In Comparative Example No. 26, since the amount of Mn was high, martensite was generated, and the condition of the payinite structure ratio of the present invention could not be satisfied.
- Comparative Example No. 27 since the amount of S was low, the precipitation of composite inclusions was small, the durability ratio was lower than that of the present invention, and the machinability improvement effect of MnS was not obtained, so the machinability was poor.
- No. 28 of the comparative example the amount of S was high, so that the precipitation of MnS was excessive, and the durability ratio was lower than that of the example of the present invention.
- N 0.29 of the comparative example has a low A1 content, so the degree of deoxidation and the effect of refining crystal grains are small, and the durability ratio is lower than that of the present invention.
- No. 30 of the comparative example hard inclusions were formed due to the high A1 content, and the durability ratio was lower than that of the inventive example, and the machinability was poor.
- No. 31 of the comparative example has a low Ti content, so that the precipitation of composite precipitates is small, and the durability ratio is lower than that of the inventive example.
- No. 32 of the comparative example had a high Ti content, so that a hard inclusion was formed, and the durability ratio was lower than that of the inventive example, and the machinability was poor.
- No. 33 of the comparative example has a low N content, so that the precipitation of composite precipitates is small, and the durability ratio is lower than that of the inventive example.
- the matrix was hardened due to the high N content, and the durability ratio was lower than that of the inventive example, and the machinability was poor.
- Comparative Example No. 35 since the amount of V was low, the precipitation of composite precipitates was small and the effect of strengthening the precipitation of matrix ferrite was small, so that the durability ratio was lower than that of the present invention. Since No. 36 of the comparative example has a high V content, the durability ratio is lower than that of the example of the present invention, and the machinability is also poor.
- No. 41 of the comparative example had a high Ca content, so the machinability was good but the durability ratio was poor.
- Scope of the present invention Actual tensile strength Fatigue strength Durability ratio First invention example 0.65 123.7 73.1 0.5S 2.02
- Second Invention 0.70 109.5 B4.0 0.58 2.28 o o l—
- No. 45 46 47 and No. 48 show that the organization rate f, which is the condition of the bainite organization rate of the present invention, is 1.4 C + 0.4 or more and 1.4 C or less with respect to the carbon content C (%).
- the cooling rate was reduced, and the structure was mostly ferrite or ferrite + spherical cementite, and the proportion of the payinite structure was low.
- the durability ratio is as low as 0.54 or less, and the machinability is poor as compared with the inventive examples.
- No. 49 has a structure mainly composed of martensite by increasing the cooling rate. Although the tensile strength is increased, the durability ratio is extremely low, and the machinability is poor and the tool life is short. Table 3
- Comparative steel Current preparation R material After tempering, water cooling
- the steel of the present invention obtains high tensile strength and secures machinability by forming a ferrite-to-bainite two-phase structure, and is formed of MnS, Ti nitride and V nitride.
- V carbides or carbonitrides
- the durability ratio that is, the fatigue characteristics, is maintained without impairing the machinability. It has become possible to present a non-heat-treated steel for hot forging that satisfies the long-sought long-lasting high tensile strength, high fatigue strength and machinability. Great effect.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Heat Treatment Of Steel (AREA)
- Forging (AREA)
Description
Claims
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR1019950702391A KR0180938B1 (ko) | 1993-10-12 | 1994-10-11 | 인장강도, 피로강도 및 피삭성이 우수한 열간 단조 비조질 강 |
DE69419720T DE69419720T2 (de) | 1993-10-12 | 1994-10-11 | Wärmeunbehandelter warmgeschmiedeter stahl mit hervorragender zugfestigkeit, ermüdungsfestigkeit und bearbeitbarkeit |
EP94929026A EP0674014B1 (en) | 1993-10-12 | 1994-10-11 | Non-heat-treated hot-forging steel excellent in tensile strength, fatigue strength and machinability |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP5/254335 | 1993-10-12 | ||
JP25433593A JP3241897B2 (ja) | 1993-10-12 | 1993-10-12 | 引張強度、疲労強度および被削性に優れる熱間鍛造用非調質鋼 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO1995010637A1 true WO1995010637A1 (fr) | 1995-04-20 |
Family
ID=17263582
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/JP1994/001693 WO1995010637A1 (fr) | 1993-10-12 | 1994-10-11 | Acier de forgeage a chaud sans traitement thermique, presentant d'excellentes caracteristiques de resistance a la traction et a la fatigue et une tres bonne aptitude a l'usinage |
Country Status (6)
Country | Link |
---|---|
EP (1) | EP0674014B1 (ja) |
JP (1) | JP3241897B2 (ja) |
KR (1) | KR0180938B1 (ja) |
CN (1) | CN1039035C (ja) |
DE (1) | DE69419720T2 (ja) |
WO (1) | WO1995010637A1 (ja) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2774098A1 (fr) * | 1998-01-28 | 1999-07-30 | Ascometal Sa | Acier et procede pour la fabrication de pieces de mecanique secables |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20010048426A (ko) * | 1999-11-26 | 2001-06-15 | 이계안 | 앞차축 빔용 저 탄소계 고인성 비조질강 단조품 |
KR100435461B1 (ko) * | 1999-12-20 | 2004-06-10 | 주식회사 포스코 | 재질편차가 적은 냉간압조용 강재의 제조방법 |
JP3888865B2 (ja) * | 2000-10-25 | 2007-03-07 | 株式会社ゴーシュー | 鍛造方法 |
KR100401571B1 (ko) * | 2001-02-20 | 2003-10-17 | 한국기계연구원 | 고강도 베이나이트계 열간단조용 비조질강재 및 그제조방법 |
WO2004083475A1 (ja) * | 2003-03-18 | 2004-09-30 | Sumitomo Metal Industries Ltd. | 非調質コネクティングロッド及びその製造方法 |
CA2531615A1 (en) * | 2004-12-28 | 2006-06-28 | Kabushiki Kaisha Kobe Seiko Sho (Kobe Steel, Ltd.) | High strength thin steel sheet having high hydrogen embrittlement resisting property |
CN100500918C (zh) * | 2007-03-29 | 2009-06-17 | 攀钢集团成都钢铁有限责任公司 | 大口径非调质石油套管用钢 |
CN102851471A (zh) * | 2012-09-27 | 2013-01-02 | 攀枝花学院 | 低碳合金钢快速获得细小铁素体晶粒的热处理方法 |
ES2733805T3 (es) * | 2015-11-16 | 2019-12-03 | Deutsche Edelstahlwerke Specialty Steel Gmbh & Co Kg | Acero fino estructural con estructura bainitica, pieza forjada fabricada a partir del mismo y procedimiento para fabricar una pieza forjada |
CN105734414A (zh) * | 2016-02-19 | 2016-07-06 | 唐山钢铁集团有限责任公司 | 一种中碳非调质钢及其生产方法 |
US11261511B2 (en) * | 2017-10-31 | 2022-03-01 | Nippon Steel Corporation | Hot forged steel material |
CN111154945B (zh) * | 2020-01-17 | 2021-05-28 | 中天钢铁集团有限公司 | 一种Ti、V微合金化铝脱氧含硫非调质钢中液析氮化物的控制方法 |
CN115896614A (zh) * | 2022-10-31 | 2023-04-04 | 中国第一汽车股份有限公司 | 一种含铌贝氏体非调质钢材料、转向节以及制备方法 |
Citations (3)
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JPS61104049A (ja) * | 1984-10-26 | 1986-05-22 | Daido Steel Co Ltd | 機械構造用鋼 |
JPS61261464A (ja) * | 1985-05-13 | 1986-11-19 | Daido Steel Co Ltd | 機械構造用鋼 |
JPH04210449A (ja) * | 1990-12-12 | 1992-07-31 | Toa Steel Co Ltd | 高靱性熱間鍛造用非調質鋼 |
Family Cites Families (5)
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JPS589813B2 (ja) * | 1978-03-14 | 1983-02-23 | 住友金属工業株式会社 | 非調質鍛鋼品の製造方法 |
JPS62167855A (ja) * | 1986-01-21 | 1987-07-24 | Nippon Kokan Kk <Nkk> | 耐疲労特性の優れた熱間鍛造用非調質鋼 |
JPH01176055A (ja) * | 1987-12-28 | 1989-07-12 | Kawasaki Steel Corp | 被削性に優れた熱間鍛造用非調質鋼 |
JP2929835B2 (ja) * | 1992-03-30 | 1999-08-03 | 住友金属工業株式会社 | 高温延性の優れた高強度非調質鋼 |
JPH0673490A (ja) * | 1992-08-26 | 1994-03-15 | Aichi Steel Works Ltd | 高靭性非調質圧延棒鋼 |
-
1993
- 1993-10-12 JP JP25433593A patent/JP3241897B2/ja not_active Expired - Fee Related
-
1994
- 1994-10-11 DE DE69419720T patent/DE69419720T2/de not_active Expired - Fee Related
- 1994-10-11 WO PCT/JP1994/001693 patent/WO1995010637A1/ja active IP Right Grant
- 1994-10-11 EP EP94929026A patent/EP0674014B1/en not_active Expired - Lifetime
- 1994-10-11 KR KR1019950702391A patent/KR0180938B1/ko not_active IP Right Cessation
- 1994-10-11 CN CN94190781A patent/CN1039035C/zh not_active Expired - Fee Related
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS61104049A (ja) * | 1984-10-26 | 1986-05-22 | Daido Steel Co Ltd | 機械構造用鋼 |
JPS61261464A (ja) * | 1985-05-13 | 1986-11-19 | Daido Steel Co Ltd | 機械構造用鋼 |
JPH04210449A (ja) * | 1990-12-12 | 1992-07-31 | Toa Steel Co Ltd | 高靱性熱間鍛造用非調質鋼 |
Non-Patent Citations (1)
Title |
---|
See also references of EP0674014A4 * |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2774098A1 (fr) * | 1998-01-28 | 1999-07-30 | Ascometal Sa | Acier et procede pour la fabrication de pieces de mecanique secables |
WO1999039018A1 (fr) * | 1998-01-28 | 1999-08-05 | Ascometal | Acier et procede pour la fabrication de pieces de mecanique secables |
Also Published As
Publication number | Publication date |
---|---|
EP0674014B1 (en) | 1999-07-28 |
CN1039035C (zh) | 1998-07-08 |
EP0674014A1 (en) | 1995-09-27 |
KR950704530A (ko) | 1995-11-20 |
DE69419720D1 (de) | 1999-09-02 |
KR0180938B1 (ko) | 1999-02-18 |
JPH07109545A (ja) | 1995-04-25 |
JP3241897B2 (ja) | 2001-12-25 |
DE69419720T2 (de) | 1999-12-16 |
CN1115582A (zh) | 1996-01-24 |
EP0674014A4 (en) | 1996-02-07 |
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