JP5206911B1 - Non-tempered steel for hot forging, non-tempered hot forged product, and method for producing the same - Google Patents
Non-tempered steel for hot forging, non-tempered hot forged product, and method for producing the same Download PDFInfo
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- 229910000831 Steel Inorganic materials 0.000 title claims abstract description 64
- 239000010959 steel Substances 0.000 title claims abstract description 64
- 238000005242 forging Methods 0.000 title claims abstract description 35
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 12
- 238000001816 cooling Methods 0.000 claims abstract description 31
- 230000006698 induction Effects 0.000 claims abstract description 30
- 229910001563 bainite Inorganic materials 0.000 claims abstract description 27
- 239000000203 mixture Substances 0.000 claims abstract description 8
- 239000012535 impurity Substances 0.000 claims abstract description 5
- 239000000463 material Substances 0.000 claims description 11
- 229910052720 vanadium Inorganic materials 0.000 abstract description 8
- 229910052750 molybdenum Inorganic materials 0.000 abstract description 6
- 229910052799 carbon Inorganic materials 0.000 abstract description 5
- 229910052757 nitrogen Inorganic materials 0.000 abstract description 5
- 229910052710 silicon Inorganic materials 0.000 abstract description 5
- 229910052804 chromium Inorganic materials 0.000 abstract description 3
- 229910052748 manganese Inorganic materials 0.000 abstract description 3
- 229910052717 sulfur Inorganic materials 0.000 abstract description 3
- 229910052782 aluminium Inorganic materials 0.000 abstract description 2
- 230000006866 deterioration Effects 0.000 abstract description 2
- 229910052698 phosphorus Inorganic materials 0.000 abstract description 2
- 230000000694 effects Effects 0.000 description 19
- 229910001566 austenite Inorganic materials 0.000 description 16
- 238000000034 method Methods 0.000 description 14
- 238000010438 heat treatment Methods 0.000 description 11
- 238000001556 precipitation Methods 0.000 description 11
- 239000000047 product Substances 0.000 description 11
- 230000007423 decrease Effects 0.000 description 8
- 230000002829 reductive effect Effects 0.000 description 8
- 229910000859 α-Fe Inorganic materials 0.000 description 8
- 230000009466 transformation Effects 0.000 description 7
- 238000005728 strengthening Methods 0.000 description 6
- 229910045601 alloy Inorganic materials 0.000 description 5
- 239000000956 alloy Substances 0.000 description 5
- 238000005520 cutting process Methods 0.000 description 5
- 150000004767 nitrides Chemical class 0.000 description 5
- 239000002244 precipitate Substances 0.000 description 5
- 238000005496 tempering Methods 0.000 description 5
- 229910052726 zirconium Inorganic materials 0.000 description 5
- UCKMPCXJQFINFW-UHFFFAOYSA-N Sulphide Chemical compound [S-2] UCKMPCXJQFINFW-UHFFFAOYSA-N 0.000 description 4
- 229910000734 martensite Inorganic materials 0.000 description 4
- 230000000717 retained effect Effects 0.000 description 4
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- 150000003568 thioethers Chemical class 0.000 description 4
- 238000005452 bending Methods 0.000 description 3
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- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
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- 238000005498 polishing Methods 0.000 description 2
- 238000003303 reheating Methods 0.000 description 2
- 238000005096 rolling process Methods 0.000 description 2
- 229920006395 saturated elastomer Polymers 0.000 description 2
- 239000002344 surface layer Substances 0.000 description 2
- 229910000975 Carbon steel Inorganic materials 0.000 description 1
- 229910000677 High-carbon steel Inorganic materials 0.000 description 1
- 238000003917 TEM image Methods 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
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- 229910052797 bismuth Inorganic materials 0.000 description 1
- 229910052791 calcium Inorganic materials 0.000 description 1
- 239000010962 carbon steel Substances 0.000 description 1
- 230000008094 contradictory effect Effects 0.000 description 1
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J1/00—Preparing metal stock or similar ancillary operations prior, during or post forging, e.g. heating or cooling
- B21J1/003—Selecting material
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J1/00—Preparing metal stock or similar ancillary operations prior, during or post forging, e.g. heating or cooling
- B21J1/06—Heating or cooling methods or arrangements specially adapted for performing forging or pressing operations
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- 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
- C21D1/10—Surface hardening by direct application of electrical or wave energy; by particle radiation by electric induction
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- 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
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/06—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of rods or wires
- C21D8/065—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of rods or wires of ferrous alloys
-
- 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
- C21D9/30—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for crankshafts; for camshafts
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- 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
- C22C38/02—Ferrous alloys, e.g. steel alloys containing silicon
-
- 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
- C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
-
- 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
- C22C38/38—Ferrous alloys, e.g. steel alloys containing chromium with more than 1.5% by weight of manganese
-
- 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
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/44—Ferrous alloys, e.g. steel alloys containing chromium with nickel with molybdenum or tungsten
-
- 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
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/46—Ferrous alloys, e.g. steel alloys containing chromium with nickel with vanadium
-
- 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
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- 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
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/002—Bainite
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- 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
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/004—Dispersions; Precipitations
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- 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
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/06—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of rods or wires
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P10/00—Technologies related to metal processing
- Y02P10/25—Process efficiency
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Manufacturing & Machinery (AREA)
- Heat Treatment Of Steel (AREA)
Abstract
本発明は、高周波焼入れを可能とする熱間鍛造用非調質鋼と、熱間鍛造後の冷却で部品内の組織を制御することによって高強度に伴う被削性の低下を抑制し、疲労強度を向上させた熱間鍛造非調質品および、その製造方法を提供することを目的とする。
本発明鋼は、質量%で、C:0.45〜0.60%、Si:0.02〜0.15%、Mn:1.50〜3.00%、P:0.0002〜0.150%、S:0.001〜0.200%、Cr:0.02〜1.00%、Al:0.001〜0.300%、V:0.01〜0.30%、Mo:0.03〜1.00%、N:0.0020〜0.0070%、を含有し、残部がFeおよび不可避不純物よりなることを特徴とする。同鋼組成からなり、鋼組織が、面積率で95%以上がベイナイト組織であり、鋼中にMo炭窒化物が分散した高周波焼入れが可能な熱間鍛造非調質品および、その製造方法。The present invention suppresses the deterioration of machinability associated with high strength by controlling the structure in the part by non-heat treated steel for hot forging that enables induction hardening and cooling after hot forging, and fatigue. An object of the present invention is to provide a hot forged non-heat treated product with improved strength and a method for producing the same.
The steel of the present invention is in mass%, C: 0.45 to 0.60%, Si: 0.02 to 0.15%, Mn: 1.50 to 3.00%, P: 0.0002 to 0.00. 150%, S: 0.001 to 0.200%, Cr: 0.02 to 1.00%, Al: 0.001 to 0.300%, V: 0.01 to 0.30%, Mo: 0 0.03 to 1.00%, N: 0.0020 to 0.0070%, and the balance is made of Fe and inevitable impurities. A hot-forged non-tempered product having the same steel composition, having a steel structure having a bainite structure with an area ratio of 95% or more and capable of induction hardening in which Mo carbonitride is dispersed in the steel, and a method for producing the same.
Description
本発明は、熱間で鍛造された後、調質処理を施すことなく、自動車、産業用機械などの機械部品に加工される熱間鍛造用非調質鋼素材と、それを用いた熱間鍛造非調質品、ならびにその製造方法に関するものであって、特に熱間鍛造のままで、調質処理しないでも高強度、高耐久比を有し、かつ高周波焼入れが可能なものである。 The present invention relates to a non-heat treated steel material for hot forging that is processed into machine parts such as automobiles and industrial machines without being subjected to a tempering treatment after hot forging, and a hot work using the same. The present invention relates to a forged non-tempered product and a method for producing the same, and is particularly hot forged, has a high strength and a high durability ratio without being tempered, and can be induction hardened.
旧来、自動車や産業機械等の機械構造部品の多くは、素材棒鋼から部品形状に熱間鍛造した後、再加熱し、焼入れ焼戻しの調質処理を施すことによって、高強度および高靱性を付与してきた。近年では、製造コストの低減の観点から、焼入れ焼戻しの調質処理工程の省略が進められており、例えば、特許文献1などに見られるように、熱間鍛造のままで、調質処理しないでも高強度および高靱性を付与できる非調質鋼が提案されてきた。その中でも、クランクシャフト等のシャフト類部品では、熱間加工後、冷却して所定の強度を付与し、更に機械加工等により所定の形状に加工した後、必要な部位に高周波焼入れを施して表面硬化層を形成することによって、耐摩耗性及び疲労強度を向上させている。 Traditionally, many machine structural parts such as automobiles and industrial machines have been given high strength and high toughness by hot forging from raw steel bar to part shape and then reheating and quenching and tempering treatment. It was. In recent years, the tempering process for quenching and tempering has been omitted from the viewpoint of reducing the manufacturing cost. For example, as seen in Patent Document 1, the hot forging remains as it is without tempering. Non-tempered steel that can impart high strength and high toughness has been proposed. Among them, for shaft parts such as crankshafts, after hot working, they are cooled to give a predetermined strength, further processed into a predetermined shape by machining, etc., and then subjected to induction quenching on the necessary parts. By forming the hardened layer, wear resistance and fatigue strength are improved.
特許文献1には、Siを1.0%超添加し、S、V、Nを多量に添加した鋼材を用いて、熱間鍛造のままで従来の調質材以上の強度と低温靱性を有する熱間鍛造非調質鋼が得られたことが記載されている。しかし、この非調質鋼の疲労強度、耐久比に関しては、何ら記載は無い。 Patent Document 1 has a strength and low temperature toughness that are higher than those of conventional tempered materials while still being hot forged, using a steel material to which Si is added in excess of 1.0% and a large amount of S, V, and N are added. It is described that hot forged non-tempered steel was obtained. However, there is no description regarding the fatigue strength and durability ratio of this non-heat treated steel.
これまでにも高周波焼入れ用非調質鋼について、いくつか報告がなされている。例えば、特許文献2記載の発明は、高周波焼入れ前の組織をベイナイト率75%以上にすることで、高周波焼入れ後の残留フェライトの生成による表層硬さ、表面硬化層の深さの低下を防止する発明である。しかし、特許文献2記載の高周波焼入れ用非調質鋼は、疲労強度、耐久比に関しては、何ら記載は無く、これらの特性は全く考慮されていない。 There have been some reports on non-heat treated steel for induction hardening. For example, the invention described in Patent Document 2 prevents a decrease in surface layer hardness and surface hardened layer depth due to generation of residual ferrite after induction hardening by setting the structure before induction hardening to a bainite ratio of 75% or more. It is an invention. However, the non-heat treated steel for induction hardening described in Patent Document 2 has no description regarding fatigue strength and durability ratio, and these characteristics are not considered at all.
また、例えば、特許文献3記載の発明は、高周波焼入れ後の残留オーステナイト量を低減する発明である。しかし、特許文献3記載の高周波焼入れ用非調質鋼では、疲労強度、耐久比に関して、何ら記載は無く、これらの特性は全く考慮されていない。また、被削性向上のために、S、Pb、Bi、Te、Se、およびCaを適量添加してもよいことが記載されているが、引張強さ1100MPa以上では、それら被削性向上の効果は小さいことが分かっている。 For example, the invention described in Patent Document 3 is an invention that reduces the amount of retained austenite after induction hardening. However, in the non-heat treated steel for induction hardening described in Patent Document 3, there is no description regarding fatigue strength and durability ratio, and these characteristics are not considered at all. Further, it is described that an appropriate amount of S, Pb, Bi, Te, Se, and Ca may be added to improve machinability. However, when the tensile strength is 1100 MPa or more, the machinability is improved. The effect is known to be small.
これら高強度の非調質鋼の機械構造用鋼部品への適用において、実際に障害となるものは高疲労強度化と被削性との相反する性質を両立させることである。一般に疲労強度は引張強さに依存するとされ、引張強さを高くすれば疲労強度は高くなる。その一方で引張強さの上昇は被削性を低下する。機械構造用鋼部品の多くは、熱間鍛造後、切削加工を必要とし、その切削コストの大幅な増加につながる。一般に機械構造用鋼部品の疲労強度を高めるために引張強さを高くした場合、引張強さが1300MPaを超えると被削性が著しく低下することがわかっている。切削製造コストが大幅に増加するため、引張強さ1300MPaの強度を超える高強度化は実用上困難である。従って、これら機械構造用部品において、被削性の低下による切削コストの増加は高疲労強度化のネックであり、高疲労強度化と被削性の両立技術が求められている。 In the application of these high-strength non-heat-treated steels to steel parts for machine structural use, what actually becomes an obstacle is to achieve both the high fatigue strength and the contradictory properties of machinability. In general, the fatigue strength depends on the tensile strength, and the fatigue strength increases as the tensile strength is increased. On the other hand, an increase in tensile strength decreases machinability. Many steel parts for machine structures require cutting after hot forging, leading to a significant increase in cutting costs. In general, when the tensile strength is increased in order to increase the fatigue strength of steel parts for machine structural use, it has been found that if the tensile strength exceeds 1300 MPa, the machinability is significantly reduced. Since the cutting manufacturing cost is greatly increased, it is practically difficult to increase the strength exceeding the tensile strength of 1300 MPa. Therefore, in these machine structural parts, an increase in cutting cost due to a decrease in machinability is a bottleneck in achieving high fatigue strength, and a technique for achieving both high fatigue strength and machinability is required.
例えば、特許文献4には、被削性確保のため熱間鍛造後の強度向上を抑制し、高周波焼入れによる表面硬化層の深さを深くすることで部品全体の疲労強度を向上させる発明が記載されている。 For example, Patent Document 4 describes an invention in which the improvement in strength after hot forging is suppressed to ensure machinability, and the fatigue strength of the entire component is improved by increasing the depth of the surface hardened layer by induction hardening. Has been.
また、高疲労強度化と被削性を両立させる手段として、疲労強度と引張強さの比、すなわち耐久比(=疲労強度/引張強さ)を向上させることが有効である。例えば、特許文献5では、ベイナイト主体の金属組織とし組織中の高炭素島状マルテンサイトおよび残留オーステナイトを低減することが有効であると提案している。しかしながら、耐久比は高々0.56以下であり、被削性を低下させることなく、強度を高めるには限界があり、これら疲労強度はいずれも低い。 In order to achieve both high fatigue strength and machinability, it is effective to improve the ratio between fatigue strength and tensile strength, that is, the durability ratio (= fatigue strength / tensile strength). For example, Patent Document 5 proposes that it is effective to reduce the high-carbon island-like martensite and retained austenite in the bainite-based metal structure. However, the durability ratio is at most 0.56 or less, and there is a limit to increasing the strength without reducing the machinability, and these fatigue strengths are both low.
特許文献6には、高い耐摩耗性、疲労強度を得ることができるとともに、高い機械加工性を両立させたクランクシャフトおよびその製造方法が記載されている。この方法では、軟窒化処理前の熱間鍛造品のミクロ金属組織をベイナイト主体(70%以上)の組織とし、更にこの熱間鍛造品を550〜650℃の温度条件下で軟窒化することにより、クランクシャフトの疲労強度等の機械的性質を向上させている。軟窒化後の内部硬度を適度に増加させ、高疲労強度を得るために、鋼材のC、Si、Mn、Cr、Mo及びVの量を特定の関係式で表したパラメータHgを用いて鋼材成分を規定している。しかし、軟窒化処理は、通常、窒素を含んだ雰囲気中に暴露し、オーステナイト化温度以下の温度域で加熱することにより行う必要があり、高周波焼入れによる表面硬化処理と比較して、設備とコストがかかる。また、一定時間をかけて軟窒化処理することを目的とする鋼素材はSi量が多いため表面のみの瞬間的な誘導加熱による高周波焼入れでは、内部組織に残留オーステナイトが残存し、高い疲労強度は得られない。 Patent Document 6 describes a crankshaft that can achieve high wear resistance and fatigue strength, and that is compatible with high machinability, and a method for manufacturing the crankshaft. In this method, the microstructure of the hot forged product before soft nitriding is made to be a bainite-based (70% or more) microstructure, and the hot forged product is soft nitrided under a temperature condition of 550 to 650 ° C. The mechanical properties such as fatigue strength of the crankshaft are improved. In order to increase the internal hardness after nitrocarburizing moderately and to obtain high fatigue strength, the steel material components are obtained using the parameters Hg representing the amounts of C, Si, Mn, Cr, Mo and V of the steel material with specific relational expressions. Is stipulated. However, the soft nitriding treatment usually requires exposure to an atmosphere containing nitrogen and heating in a temperature range below the austenitizing temperature, and the equipment and cost are compared with the surface hardening treatment by induction hardening. It takes. In addition, because the steel material intended for soft nitriding over a certain time has a large amount of Si, in the induction hardening by instantaneous induction heating only on the surface, residual austenite remains in the internal structure, and high fatigue strength is I can't get it.
そこで、本発明は、以上のような課題を有利に解決し、高周波焼入れを可能とする熱間鍛造用非調質鋼と、熱間鍛造後の冷却で部品内の組織を制御することによって高強度に伴う被削性の低下を抑制し、疲労強度を向上させた熱間鍛造非調質品および、その製造方法を提供することを目的とする。 Therefore, the present invention advantageously solves the above-described problems and controls the microstructure in the part by non-heat treated steel for hot forging that enables induction hardening and cooling after hot forging. An object of the present invention is to provide a hot forged non-heat treated product that suppresses a decrease in machinability associated with strength and improves fatigue strength, and a manufacturing method thereof.
本発明は、高周波焼入れを施して高い表面硬度を得られる高炭素鋼に多量のMoを添加した鋼を用いて、熱間鍛造後の冷却過程で、多量のMo炭窒化物を析出させ、マトリックスの転位等の欠陥密度を少なくすることにより高耐久比を有し、高強度に伴う被削性の低下を抑制し、疲労強度を向上させた熱間鍛造非調質品を得ることを見出し、本発明を完成した。ここで、本明細書で用いる「炭窒化物」とは、炭窒化物及び炭化物の意味である。 The present invention uses a steel in which a large amount of Mo is added to a high carbon steel that can be induction hardened to obtain a high surface hardness, and in the cooling process after hot forging, a large amount of Mo carbonitride is precipitated, It has been found that it has a high durability ratio by reducing the defect density such as dislocation, and suppresses the deterioration of machinability associated with high strength, and obtains a hot forged non-heat treated product with improved fatigue strength, The present invention has been completed. Here, “carbonitride” used in the present specification means carbonitride and carbide.
本発明の要旨は、以下の通りである。 The gist of the present invention is as follows.
(1)質量%で、C:0.45〜0.60%、Si:0.02〜0.15%、Mn:1.50〜3.00%、P:0.0002〜0.150%、S:0.001〜0.200%、Cr:0.02〜1.00%、Al:0.001〜0.300%、V:0.01〜0.30%、Mo:0.03〜1.00%、N:0.0020〜0.0070%、を含有し、残部がFe及び不可避不純物からなる高周波焼入れ処理が可能な熱間鍛造用非調質鋼。 (1) By mass%, C: 0.45 to 0.60%, Si: 0.02 to 0.15%, Mn: 1.50 to 3.00%, P: 0.0002 to 0.150% , S: 0.001 to 0.200%, Cr: 0.02 to 1.00%, Al: 0.001 to 0.300%, V: 0.01 to 0.30%, Mo: 0.03 Non-tempered steel for hot forging containing ˜1.00%, N: 0.0020 to 0.0070%, the balance being Fe and unavoidable impurities.
(2)さらに、質量%で、Ca:0.0002〜0.0100%、Te:0.0002〜0.1000%、Zr:0.0002〜0.2000%のうちの1種または2種以上を含有することを特徴とする上記(1)に記載の高周波焼入れ処理可能な熱間鍛造用非調質鋼。 (2) Further, by mass%, one or more of Ca: 0.0002 to 0.0100%, Te: 0.0002 to 0.1000%, Zr: 0.0002 to 0.2000% The non-tempered steel for hot forging capable of induction hardening as described in (1) above.
(3)上記(1)または(2)に記載の鋼成分を有し、鋼組織が、面積率で95%以上がベイナイト組織であり、鋼中に分散したMo炭窒化物の平均サイズが4nm以上、11nm以下であることを特徴とする高周波焼入れが可能な熱間鍛造非調質品。 (3) The steel component according to the above (1) or (2) is included, the steel structure is an area ratio of 95% or more is a bainite structure, and the average size of Mo carbonitride dispersed in the steel is 4 nm. As described above, a hot-forged non-tempered product capable of induction hardening characterized by being 11 nm or less.
(4)上記(1)または(2)に記載の成分組成からなる鋼材を、1000℃以上、1250℃以下に加熱して熱間鍛造し、該熱間鍛造後、200℃までにおける平均冷却速度を0.05℃/秒以上、0.80℃/秒以下で冷却し、強度が必要な部位に高周波焼入れ処理を施すことを特徴とする熱間鍛造非調質品の製造方法。 (4) The steel material comprising the component composition described in (1) or (2) above is heated to 1000 ° C. or more and 1250 ° C. or less for hot forging, and after the hot forging, the average cooling rate up to 200 ° C. Is heated at 0.05 ° C./second or more and 0.80 ° C./second or less, and induction hardening is performed on a portion where strength is required.
本発明の鋼は、切削コストの増加を抑えつつ、高疲労強度を備えた高周波焼入れ可能な熱間鍛造非調質鋼部品用の素材として最適である。また本発明の製造方法により、高耐久比、および高疲労強度を有する高周波焼入れ可能な熱間鍛造非調質品を製造することができる。さらに、本発明の熱間鍛造非調質品は、自動車用あるいは産業機械用の部品として使用するとき、高周波焼入れ可能であるため、部品の一層の高強度化が可能で、車両の軽量化、燃費低減、および低コスト化に貢献できる。 The steel of the present invention is optimal as a raw material for hot forged non-heat treated steel parts capable of induction hardening with high fatigue strength while suppressing an increase in cutting cost. In addition, by the production method of the present invention, it is possible to produce a hot forged non-tempered product having a high durability ratio and high fatigue strength and capable of induction hardening. Furthermore, the hot forged non-heat treated product of the present invention can be induction hardened when used as a part for automobiles or industrial machines, so that the parts can be further strengthened, and the weight of the vehicle can be reduced. Contributes to reducing fuel consumption and cost.
本発明者らは、上述した目的に対し、鋼成分範囲、組織形態、および熱処理条件について鋭意検討し、以下の知見を見出した。すなわち、
(a)面積率で95%以上のベイナイト組織中に、微細なMo炭窒化物を分散させることによって、従来の非調質鋼より高い耐久比(=疲労強度/引張強さ)を有する。熱間鍛造後の冷却速度の影響が大きく、冷却速度が小さいほど耐久比は向上する。これは、冷却速度が小さいほどMo炭窒化物が析出する温度域にとどまる時間が長くなり析出量が増えることによって、引張強さおよび疲労強度は上昇するが、冷却速度が小さければ小さいほど、その炭窒化物は粗大化し引張強さは顕著に低下する一方、疲労強度は低下することなく上昇または維持するためである。一般的に析出強化に用いられるMo等の炭窒化物の析出は、疲労強度だけでなく引張強度も上昇し、被削性を著しく低下するため高疲労強度化と良被削性は両立しない。析出物を粗大化し、Mo炭窒化物のサイズを4nm以上、11nm以下に制御することによって、被削性に影響を及ぼす引張強さは上げずに疲労強度を高めることができることがわかった。ただし、主体組織をベイナイト組織とし、それ以外の初析フェライトや残留オーステナイト組織を面積率5%未満にする必要がある。
(b)VはMoと同様に、炭窒化物を形成し耐久比向上に寄与するものの、高Nではより高温で安定なV窒化物を形成し、熱間鍛造後の冷却過程で初析フェライトの核となり、強度および耐久比の低下につながる。V炭窒化物による耐久比向上の効果を十分に利用するには低Nが必要条件である。The present inventors diligently studied the steel component range, the structure morphology, and the heat treatment conditions for the above-mentioned objects, and found the following findings. That is,
(A) It has a higher durability ratio (= fatigue strength / tensile strength) than conventional non-tempered steel by dispersing fine Mo carbonitrides in a bainite structure of 95% or more in area ratio. The influence of the cooling rate after hot forging is large, and the durability ratio is improved as the cooling rate is decreased. This is because the tensile strength and fatigue strength increase as the cooling rate decreases and the amount of precipitation increases as the time in which the Mo carbonitride precipitates increases, but the smaller the cooling rate, the more This is because the carbonitride is coarsened and the tensile strength is remarkably reduced, while the fatigue strength is increased or maintained without decreasing. In general, precipitation of carbonitride such as Mo used for precipitation strengthening increases not only fatigue strength but also tensile strength and remarkably reduces machinability, so that high fatigue strength and good machinability are not compatible. It was found that fatigue strength can be increased without increasing the tensile strength affecting machinability by coarsening the precipitate and controlling the size of the Mo carbonitride to 4 nm or more and 11 nm or less. However, it is necessary that the main structure is a bainite structure and the other pro-eutectoid ferrite and retained austenite structure is less than 5%.
(B) V, like Mo, forms carbonitrides and contributes to improving the durability ratio. However, high N forms V nitrides that are stable at higher temperatures, and proeutectoid ferrite in the cooling process after hot forging. It leads to a decrease in strength and durability ratio. Low N is a necessary condition for fully utilizing the effect of improving the durability ratio by V carbonitride.
本発明は、これら知見に基づいて、さらに検討を重ねて初めてなされたものである。 The present invention has been made for the first time after further studies based on these findings.
以下、本発明について詳細に説明する。まず、上述した鋼成分範囲の限定理由について説明する。 Hereinafter, the present invention will be described in detail. First, the reason for limiting the steel component range described above will be described.
C:0.45〜0.60%
Cは鋼の強度を決める重要な元素である。他の合金元素に比べて合金コストは安く、Cを多量に添加することができれば鋼材の合金コストは低減できる。また高周波焼入れ処理した後の表面硬さは鋼中のC量で決まり必要強度を得るためには、下限を0.45%とする。しかしながら、多量のCを添加すると、ベイナイト変態時にラスの境界にCが濃縮した残留オーステナイトや島状マルテンサイトが生成し、耐久比が低下するため、上限は0.60%とする。なお、本発明の高周波焼入れ処理が可能な鋼とは、高周波焼入れ処理した後の表面硬さが要求される強度以上になりうる鋼のことである。したがって、本発明において、0.45%以上のC量を有する鋼のことである。より高い強度を得るには、0.5%を超えるC量が好ましい。 C: 0.45-0.60%
C is an important element that determines the strength of steel. Compared to other alloy elements, the alloy cost is low. If a large amount of C can be added, the alloy cost of the steel material can be reduced. Further, the surface hardness after induction hardening is determined by the amount of C in the steel, and in order to obtain the required strength, the lower limit is made 0.45%. However, when a large amount of C is added, residual austenite or island martensite in which C is concentrated at the boundary of the lath during bainite transformation is formed and the durability ratio is lowered, so the upper limit is made 0.60%. In addition, the steel which can be induction-hardened of the present invention is steel that can have a surface hardness after the induction-hardening treatment that is higher than the required strength. Therefore, in the present invention, it is steel having a C content of 0.45% or more. In order to obtain higher strength, an amount of C exceeding 0.5% is preferable.
Si:0.02〜0.15%
Siは、熱間鍛造後の冷却過程におけるベイナイト変態で、鋼中に残留オーステナイト量を増加させる元素である。表層のみ加熱する高周波焼入れ処理を施す場合、非加熱部では残留オーステナイトが残存し、Si量が0.15%を超えると疲労強度、耐久比は顕著に低下する。したがって、その量を0.15%以下に制限する。しかし、0.02%未満に抑制すると製造コストが多大なものとなるため、下限を0.02%とする。 Si: 0.02-0.15%
Si is an element that increases the amount of retained austenite in steel by bainite transformation in the cooling process after hot forging. When an induction hardening process for heating only the surface layer is performed, residual austenite remains in the non-heated part, and when the Si content exceeds 0.15%, the fatigue strength and the durability ratio are significantly reduced. Therefore, the amount is limited to 0.15% or less. However, if the content is suppressed to less than 0.02%, the manufacturing cost becomes great, so the lower limit is made 0.02%.
Mn:1.50〜3.00%
Mnはベイナイト変態を促進する元素であり、熱間鍛造後の冷却過程で組織をベイナイトとするために重要な元素である。さらにSと結合して硫化物を形成し、被削性を向上させる効果がある。これら効果を発揮するためには、下限は1.50%とする。一方、3.00超のMn量を添加すると素地の硬さが大きくなり脆くなるため、かえって被削性が顕著に低下する。上限は3.00とする。特に、2.0%を超えるMn量は、遅い冷却速度においても面積率で95%のベイナイト組織となるので、好ましい。 Mn: 1.50 to 3.00%
Mn is an element that promotes bainite transformation, and is an important element for making the structure bainite in the cooling process after hot forging. Furthermore, it combines with S to form sulfides and has the effect of improving machinability. In order to exert these effects, the lower limit is made 1.50%. On the other hand, if an amount of Mn exceeding 3.00 is added, the hardness of the substrate increases and becomes brittle, so that the machinability is significantly lowered. The upper limit is 3.00. In particular, an amount of Mn exceeding 2.0% is preferable because a bainite structure with an area ratio of 95% is obtained even at a low cooling rate.
P:0.0002〜0.150%
Pは鋼中に不可避的不純物として通常、0.0002%以上は含有しているため、下限を0.0002%以上とする。多量に添加すると、Pは旧オーステナイトの粒界等に偏析し、高周波焼入れ後の割れを助長する元素であるため、上限は0.150%とする。好ましくは0.100%以下であり、より好ましくは0.050%以下である。 P: 0.0002 to 0.150%
Since P usually contains 0.0002% or more as an inevitable impurity in steel, the lower limit is made 0.0002% or more. When P is added in a large amount, P segregates at the grain boundaries of prior austenite and promotes cracking after induction hardening, so the upper limit is made 0.150%. Preferably it is 0.100% or less, More preferably, it is 0.050% or less.
S:0.001〜0.200%
SはMnと硫化物を形成し、被削性を向上させる効果があり、その効果を発揮するためには、下限を0.001%とする。SはMnと硫化物を形成し、被削性を向上させる効果があり、またオーステナイト粒の成長を抑制し高靱性を維持する効果もある。これら効果を発揮するためには、下限は0.001%とする。しかし、Mn量にも依存するが、多量に添加すると機械的性質に異方性が大きくなることから、上限は0.200%とする。 S: 0.001 to 0.200%
S forms sulfides with Mn and has an effect of improving machinability, and in order to exert the effect, the lower limit is made 0.001%. S forms sulfides with Mn and has an effect of improving machinability, and also has an effect of suppressing the growth of austenite grains and maintaining high toughness. In order to exert these effects, the lower limit is made 0.001%. However, although depending on the amount of Mn, since anisotropy increases in mechanical properties when added in a large amount, the upper limit is made 0.200%.
Cr:0.02〜1.00%
CrはMnと同様にベイナイト変態を促進するのに有効な元素であり、その効果を発揮するためには、下限を0.02%とする。しかしながら、Crを多量に添加すると、Fe系炭化物を安定化させ、高周波焼入れした場合の表面硬さが低下することから、上限は1.00%とする。 Cr: 0.02 to 1.00%
Cr, like Mn, is an element effective for promoting the bainite transformation, and in order to exert its effect, the lower limit is made 0.02%. However, if a large amount of Cr is added, the Fe-based carbide is stabilized and the surface hardness when induction hardening is reduced, so the upper limit is made 1.00%.
Al:0.001〜0.300%
Alは窒化物として鋼中に析出分散することにより、鍛造再加熱時のオーステナイト組織の粗大化を防止し、その後のベイナイト組織の粗大化も防止する効果がある。さらにAlは機械加工時に酸素と結合して工具面に付着し、工具摩耗の防止に効果がある。これら効果を発揮するためには、下限は0.001%とする。好ましくは、0.050%以上とし、より好ましくは0.100%とする。一方、0.300%超では多量の硬質介在物を形成し耐久比および被削性のいずれも低下する。したがって、上限は0.300%とする。 Al: 0.001 to 0.300%
Al precipitates and disperses in the steel as a nitride, thereby preventing the austenite structure from coarsening during forging reheating and preventing the subsequent bainite structure from becoming coarse. Furthermore, Al combines with oxygen during machining, adheres to the tool surface, and is effective in preventing tool wear. In order to exert these effects, the lower limit is made 0.001%. Preferably, it is 0.050% or more, more preferably 0.100%. On the other hand, if it exceeds 0.300%, a large amount of hard inclusions are formed, and both the durability ratio and the machinability are lowered. Therefore, the upper limit is set to 0.300%.
V:0.01〜0.30%
Vはベイナイト変態を促進するのに有効な元素であり、また炭窒化物を形成し、ベイナイト組織を析出強化し強度、および耐久比を高めるのに有効な元素である。この効果を発揮するには0.01%以上の含有量が必要である。一方、0.30%を超えると、その効果は飽和するため、上限は0.30%とする。 V: 0.01-0.30%
V is an element effective for promoting the bainite transformation, and is an element effective for forming a carbonitride, strengthening the precipitation of the bainite structure, and increasing the strength and durability ratio. In order to exhibit this effect, a content of 0.01% or more is necessary. On the other hand, if it exceeds 0.30%, the effect is saturated, so the upper limit is made 0.30%.
Mo:0.03〜1.00%
Moはベイナイト変態を促進するのに有効な元素だけでなく、合金炭化物による析出強化が得られるV、TiやNb等の合金元素に比べて、オーステナイト中の固溶度が最も大きく、冷却過程においてMo炭窒化物の大きな析出量が得られる。一般的に析出強化に用いられるMo等の炭窒化物の析出は疲労強度だけでなく、引張強さも上昇し被削性を著しく低下させるため好ましくない。しかし、Mo炭窒化物のサイズが4nm以上、11nm以下に制御すると、被削性に影響を及ぼす引張強さは上げずに疲労強度のみ上げることができ、つまり、疲労強度、および耐久比を高めることがわかった。この効果を発揮するには0.03%以上の含有量が必要である。一方、1.00%を超えると、その効果は飽和するため、上限を1.00%とする。 Mo: 0.03-1.00%
Mo is not only an element effective for promoting bainite transformation, but also has the highest solid solubility in austenite compared to alloy elements such as V, Ti, Nb, etc., which can provide precipitation strengthening due to alloy carbide, and in the cooling process A large amount of Mo carbonitride is obtained. Generally, precipitation of carbonitride such as Mo used for precipitation strengthening is not preferable because not only fatigue strength but also tensile strength is increased and machinability is remarkably lowered. However, when the size of Mo carbonitride is controlled to 4 nm or more and 11 nm or less, only the fatigue strength can be increased without increasing the tensile strength affecting the machinability, that is, the fatigue strength and the durability ratio are increased. I understood it. In order to exhibit this effect, a content of 0.03% or more is necessary. On the other hand, if it exceeds 1.00%, the effect is saturated, so the upper limit is made 1.00%.
N:0.0020〜0.0070%
Nは、一般的にはVと窒化物を形成して熱間鍛造時のオーステナイト組織の粗大化を防止することに利用されるが、V窒化物は初析フェライトの核となり、かえって初析フェライトの変態を促進し強度、および耐久比を低下させる。V窒化物の生成を抑制するには、N量の上限を0.0070%とする。また鋼中の不可避的不純物として通常、0.0020%以上は含有しているため、下限を0.0020%とする。 N: 0.0020 to 0.0070%
N is generally used to form a nitride with V to prevent coarsening of the austenite structure during hot forging, but V nitride serves as the nucleus of pro-eutectoid ferrite. The transformation is promoted to reduce the strength and durability ratio. In order to suppress the formation of V nitride, the upper limit of the N amount is set to 0.0070%. Moreover, since 0.0020% or more is usually contained as an inevitable impurity in steel, the lower limit is made 0.0020%.
Ca:0.0002〜0.0100%、Te:0.0002〜0.1000%、Zr:0.0002〜0.2000%のうちの1種または2種以上を含有する
Ca、Te、Zrはいずれも酸化物を形成し、Mn硫化物の晶出核となりMn硫化物を均一微細分散する効果がある。また、いずれの元素もMn硫化物中に固溶し、その変形能を低下させ、圧延や熱間鍛造後のMn硫化物形状の伸延を抑制し、機械的性質の異方性を小さくする効果がある。これら効果を発揮するには、Ca、Te、Zrの下限はそれぞれ0.0002%とする。一方、Caは0.0100%、Teは0.1000%、Zrは0.2000%を超えると、かえってこれら酸化物や硫化物等の硬質介在物を多量に生成し、耐久比および被削性は低下する。したがって、Caの上限は0.0100%とし、Teの上限は0.1000%とし、Zrの上限は0.2000%とする。Ca: 0.0002 to 0.0100%, Te: 0.0002 to 0.1000%, Zr: containing one or more of 0.0002 to 0.2000% Ca, Te, Zr are All of them have an effect of forming oxides, becoming crystallization nuclei of Mn sulfide, and uniformly and finely dispersing Mn sulfide. In addition, any element dissolves in Mn sulfide, reduces its deformability, suppresses elongation of Mn sulfide shape after rolling or hot forging, and reduces the anisotropy of mechanical properties There is. In order to exert these effects, the lower limits of Ca, Te, and Zr are each 0.0002%. On the other hand, when Ca exceeds 0.0100%, Te exceeds 0.1000%, and Zr exceeds 0.2000%, a large amount of hard inclusions such as oxides and sulfides are generated, and the durability ratio and machinability are increased. Will decline. Therefore, the upper limit of Ca is 0.0100%, the upper limit of Te is 0.1000%, and the upper limit of Zr is 0.2000%.
次に上述した熱間鍛造非調質品の鋼組織の限定理由について説明する。 Next, the reason for limiting the steel structure of the above-mentioned hot forged non-heat treated product will be described.
(面積率で95%以上のベイナイト組織)
組織を面積率で95%以上のベイナイト組織に規定したのは、主体組織がベイナイト組織であれば高耐久比を有するものの、その残部組織であるフェライト、残留オーステナイトまたは島状マルテンサイトが面積率で5%以上からなる場合、耐久比は著しく低下するためである。これら残部組織が少なければ少ないほど、耐久比は高く、好ましくは面積率で97%以上である。(Bainitic structure with an area ratio of 95% or more)
The structure is defined as a bainite structure with an area ratio of 95% or more. If the main structure is a bainite structure, it has a high durability ratio, but the remaining structure is ferrite, residual austenite, or island martensite. This is because the durability ratio is significantly reduced when the content is 5% or more. The fewer these remaining structures are, the higher the durability ratio is, and the area ratio is preferably 97% or more.
(鋼中に分散したMo炭窒化物の平均サイズが4nm以上、11nm以下である)
ベイナイト組織中のMo炭窒化物の平均サイズを4nm以上に規定したのは、その平均サイズが4nm未満では、高い疲労強度を有するが同時に引張強さも高く、耐久比の値としては小さいため、高疲労強度化と被削性の両立は実現できないからである。より好ましくはその平均サイズ8nm以上である。またMo炭窒化物の平均サイズの上限値を11nmに規定したのは、その平均サイズが11nm超では、引張強さだけでなく疲労強度も著しく低下するため高疲労強度化を達成できないからである。なお、Mo炭窒化物の形状は針状であり、本明細書で用いるMo炭窒化物のサイズは長手方向の長さである。(The average size of Mo carbonitride dispersed in steel is 4 nm or more and 11 nm or less)
The reason why the average size of Mo carbonitrides in the bainite structure is specified to be 4 nm or more is that when the average size is less than 4 nm, the fatigue strength is high but the tensile strength is also high and the durability ratio is small. This is because it is impossible to achieve both fatigue strength and machinability. More preferably, the average size is 8 nm or more. Further, the upper limit value of the average size of Mo carbonitride is defined as 11 nm because when the average size exceeds 11 nm, not only the tensile strength but also the fatigue strength is remarkably lowered, so that high fatigue strength cannot be achieved. . In addition, the shape of Mo carbonitride is acicular and the size of Mo carbonitride used in this specification is the length in the longitudinal direction.
次に上述した熱間鍛造非調質品の製造方法の限定理由について説明する。 Next, the reason for limitation of the manufacturing method of the hot forged non-heat treated product described above will be described.
(鋼材を1000℃以下、1250℃以上に加熱)
上述した成分組成からなる鋼材を1000℃以下、1250℃以上に加熱することを規定したのは、冷却過程でMo、Vの炭窒化物を十分に析出させることが目的で、熱間鍛造前の加熱によってMo、Vを鋼中に十分に溶体化させるためである。加熱温度1000℃未満では、Mo、Vを鋼中に十分に溶体化させることができず、その後の冷却過程での析出強化量が小さく、疲労強度、耐久比は小さくなる。一方、必要以上に加熱温度を上げることは、オーステナイト粒の成長を促し、その後の冷却過程で変態した組織が粗大となりかえって耐久比が低下する。したがって、加熱温度の上限を1250℃とする。(Steel is heated to 1000 ° C or lower and 1250 ° C or higher)
The reason why the steel material having the above-described component composition is heated to 1000 ° C. or lower and 1250 ° C. or higher is to sufficiently precipitate carbonitrides of Mo and V in the cooling process, before hot forging. This is because Mo and V are sufficiently dissolved in the steel by heating. If the heating temperature is less than 1000 ° C., Mo and V cannot be sufficiently dissolved in the steel, the precipitation strengthening amount in the subsequent cooling process is small, and the fatigue strength and durability ratio are small. On the other hand, raising the heating temperature more than necessary promotes the growth of austenite grains, and the structure transformed in the subsequent cooling process becomes coarse, and the durability ratio decreases. Therefore, the upper limit of the heating temperature is 1250 ° C.
(熱間鍛造後、200℃以下まで平均冷却速度は0.05℃/秒以上、0.80℃/秒以下に冷却)
熱間鍛造した後、200℃以下まで平均冷却速度は0.05℃/秒以上、0.80℃/秒以下に規定したのは、Mo炭窒化物が析出する温度域にとどまる時間を長くして、冷却過程で析出量を増加させ、その炭窒化物サイズを制御するためである。平均冷却速度が0.80℃/秒以上では、Mo炭化膣物の析出量が十分得られず、強度、および耐久比向上効果が小さい。特にMo炭窒化物を粗大化し高耐久比を有するには、好ましくは平均冷却速度0.50℃/秒以下が望ましい。より好ましくは0.30℃/秒以下である。一方、平均冷却速度が0.05℃/秒未満では、ベイナイトラス境界に面積率で5%以上の初析フェライトが生成し、疲労強度、および耐久比を顕著に低下する。(After hot forging, the average cooling rate is 0.05 ° C / second or more and 0.80 ° C / second or less to 200 ° C or less)
After hot forging, the average cooling rate up to 200 ° C or less is specified to be 0.05 ° C / second or more and 0.80 ° C / second or less because the time staying in the temperature range where Mo carbonitride precipitates is lengthened. This is because the precipitation amount is increased in the cooling process and the carbonitride size is controlled. When the average cooling rate is 0.80 ° C./second or more, the precipitation amount of Mo carbonized vagina is not sufficiently obtained, and the effect of improving the strength and the durability ratio is small. In particular, in order to coarsen Mo carbonitride and have a high durability ratio, an average cooling rate of 0.50 ° C./second or less is desirable. More preferably, it is 0.30 ° C./second or less. On the other hand, when the average cooling rate is less than 0.05 ° C./second, proeutectoid ferrite having an area ratio of 5% or more is generated at the bainite lath boundary, and the fatigue strength and the durability ratio are significantly reduced.
なお、本発明によって高疲労強度を有する高周波焼入れが可能な熱間鍛造非調質品が得られるが、被削性を十分に確保するためには、引張強さは1300MPa以下にすることが望ましい。 Although the present invention provides a hot forged non-tempered product capable of induction hardening with high fatigue strength, it is desirable that the tensile strength be 1300 MPa or less in order to ensure sufficient machinability. .
本発明を実施例によって以下に詳述する。なお、これら実施例は本発明の技術的意義、効果を説明するためのものであり、本発明の範囲を限定するものではない。 The invention is described in detail below by means of examples. These examples are for explaining the technical significance and effects of the present invention, and do not limit the scope of the present invention.
表1に示す化学組成の鋼を150kg真空溶解炉にて溶製した。これを直径100mmの棒鋼に圧延後、鍛造用試験片を切り出し、表2に示す条件で鍛造、熱処理を行った。熱間鍛造した後、200℃までの冷却方法は空冷または炉冷を行い、冷却速度は試験片の直径を変えることで制御した。平均冷却速度は、熱間鍛造した後の試験片の温度から200℃を差し引いた値を、熱間鍛造した後200℃まで冷却するのに要した時間で割って求めた。その他に比較のため、従来鋼S55Cを溶製し、本発明と同程度の引張強さになるように熱処理した。試験片を1100℃に加熱後、室温まで水冷し、再度450℃で1時間熱処理した。なお、表1および表2の下線部は本発明の範囲外条件である。 Steels having chemical compositions shown in Table 1 were melted in a 150 kg vacuum melting furnace. After rolling this into a steel bar having a diameter of 100 mm, a forging specimen was cut out and subjected to forging and heat treatment under the conditions shown in Table 2. After hot forging, the cooling method to 200 ° C. was performed by air cooling or furnace cooling, and the cooling rate was controlled by changing the diameter of the test piece. The average cooling rate was obtained by dividing the value obtained by subtracting 200 ° C. from the temperature of the test piece after hot forging by the time required for cooling to 200 ° C. after hot forging. For comparison, the conventional steel S55C was melted and heat-treated so as to have the same tensile strength as that of the present invention. The test piece was heated to 1100 ° C., cooled to room temperature, and heat-treated again at 450 ° C. for 1 hour. The underlined portions in Tables 1 and 2 are conditions outside the scope of the present invention.
これら鍛造材の中央部よりJIS Z 2201の14号引張試験片、およびJIS Z 2274の1号回転曲げ疲労試験片を採取し、引張強さ、疲労強度を求めた。ここで、疲労強度は回転曲げ疲労試験にて107回転で破断せず耐久した応力振幅と定義した。また求められた疲労強度と引張強さの比を耐久比(疲労強度/引張強さ)として求めた。A JIS Z 2201 No. 14 tensile test piece and a JIS Z 2274 No. 1 bending bending fatigue test piece were sampled from the center of these forgings, and the tensile strength and fatigue strength were determined. Here, the fatigue strength was defined as the stress amplitude that did not break in 10 7 rotations in the rotating bending fatigue test. Further, the ratio of the obtained fatigue strength and tensile strength was obtained as the durability ratio (fatigue strength / tensile strength).
鍛造材のL方向の1/4厚み部から組織観察用試験片を採取した。ベイナイトの面積率は、試験片を鏡面になるまで研磨後、レペラーエッチングを行い、ベイナイト以外の残部である初析フェライト、残留オーステナイト、島状マルテンサイト等の組織を確認し、500倍の光学顕微鏡写真を各10視野撮影した後、画像解析により算出した。 A specimen for observing the structure was taken from a 1/4 thickness part in the L direction of the forged material. The area ratio of bainite is determined by polishing the specimen until it becomes a mirror surface, then performing repeller etching, and confirming the microstructure of proeutectoid ferrite, residual austenite, island martensite, and the like other than bainite. The microphotographs were taken by 10 fields of view and then calculated by image analysis.
Mo炭窒化物の平均サイズは、試験片を電解研磨法により薄膜に仕上げた後、透過型電子顕微鏡にて、15000倍の透過型電子顕微鏡写真を各10視野撮影し、その中で観察されたMo炭窒化物の長手方向の長さを画像解析で求め、その平均値を求めた。 The average size of the Mo carbonitride was observed in 10 views of 15,000-fold transmission electron micrographs taken with a transmission electron microscope after finishing the test piece into a thin film by electrolytic polishing. The length in the longitudinal direction of the Mo carbonitride was determined by image analysis, and the average value was determined.
No.1〜18の本発明鋼は、いずれも面積率で95%以上のベイナイト組織で、Mo炭窒化物の平均サイズは4.6nm以上、10.8nm以下であり、耐久比は0.58以上の高耐久比を有する。被削性の確保のために引張強さは1300MPa以下ではあるが、同程度の引張強さと比較すると明らかのように、従来例No.28の炭素鋼の調質鋼より高疲労強度を実現している。 No. The present invention steels 1 to 18 all have a bainite structure of 95% or more in area ratio, the average size of Mo carbonitride is 4.6 nm or more and 10.8 nm or less, and the durability ratio is 0.58 or more. Has a high durability ratio. In order to ensure machinability, the tensile strength is 1300 MPa or less, but as is apparent when compared with the comparable tensile strength, the conventional example No. Higher fatigue strength is achieved than tempered steel of 28 carbon steel.
これに対して、比較例No.23、24、27はC、SiまたはNのいずれかの含有量が多く、またNo.21は規定した鋼組成範囲内ではあるが、平均冷却速度が規定外で、ベイナイトラス境界にフェライトや残留オーステンサイト等の残部の量が多く、Mo炭窒化物の平均サイズが規定外ため、強度および耐久比が低い。No.19、22は鋼組成、または熱処理条件が規定外で、十分な析出強化が得られず耐久比が低い。No.20は必要以上に加熱温度を高くしたために、ベイナイト組織が粗大化し、かえって耐久比が低い。No.25は必要以上にMnを添加され、引張強さが高く、切削が非常に困難である。一方、No.26は必要以上にAlが添加され、かえって疲労強度および耐久比が低くなる。 In contrast, Comparative Example No. Nos. 23, 24 and 27 have a high content of either C, Si or N. 21 is within the specified steel composition range, but the average cooling rate is not specified, the amount of the remainder such as ferrite and residual austenite is large at the bainite lath boundary, and the average size of Mo carbonitride is not specified, Low strength and durability ratio. No. Nos. 19 and 22 have steel compositions or heat treatment conditions that are not specified, and sufficient precipitation strengthening cannot be obtained, resulting in a low durability ratio. No. Since the heating temperature of No. 20 was increased more than necessary, the bainite structure was coarsened, and the durability ratio was rather low. No. No. 25 has Mn added more than necessary, has high tensile strength, and is very difficult to cut. On the other hand, no. In No. 26, Al is added more than necessary, and the fatigue strength and durability ratio are lowered.
これから明らかなように、本発明で規定する条件をすべて満たすものは比較例、従来例より靱性および疲労特性が優れている。 As is clear from this, those satisfying all of the conditions defined in the present invention are superior in toughness and fatigue characteristics than the comparative example and the conventional example.
Claims (4)
C:0.45〜0.60%、
Si:0.02〜0.15%、
Mn:1.50〜3.00%、
P:0.0002〜0.150%、
S:0.001〜0.200%、
Cr:0.02〜1.00%、
Al:0.001〜0.300%、
V:0.01〜0.30%、
Mo:0.03〜1.00%、
N:0.0020〜0.0070%、
を含有し、残部がFe及び不可避不純物からなる高周波焼入れ処理が可能な熱間鍛造用非調質鋼。% By mass
C: 0.45-0.60%,
Si: 0.02 to 0.15%,
Mn: 1.50 to 3.00%,
P: 0.0002 to 0.150%,
S: 0.001 to 0.200%,
Cr: 0.02 to 1.00%,
Al: 0.001 to 0.300%,
V: 0.01-0.30%,
Mo: 0.03-1.00%,
N: 0.0020 to 0.0070%,
Non-tempered steel for hot forging, which can be induction-hardened with the balance being Fe and inevitable impurities.
Ca:0.0002〜0.0100%、
Te:0.0002〜0.1000%、
Zr:0.0002〜0.2000%
のうちの1種または2種以上を含有することを特徴とする請求項1に記載の高周波焼入れ処理可能な熱間鍛造用非調質鋼。Furthermore, in mass%,
Ca: 0.0002 to 0.0100%,
Te: 0.0002 to 0.1000%,
Zr: 0.0002 to 0.2000%
The non-tempered steel for hot forging capable of induction hardening according to claim 1, comprising one or more of them.
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JP4251229B1 (en) * | 2007-09-19 | 2009-04-08 | 住友金属工業株式会社 | Low alloy steel for high pressure hydrogen gas environment and container for high pressure hydrogen |
-
2012
- 2012-08-03 WO PCT/JP2012/069861 patent/WO2013018893A1/en active Application Filing
- 2012-08-03 JP JP2012552207A patent/JP5206911B1/en active Active
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Patent Citations (5)
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JPS61166919A (en) * | 1985-01-18 | 1986-07-28 | Nippon Steel Corp | Manufacture of unrefined warm-forged article having high toughness |
JPH06235043A (en) * | 1993-02-05 | 1994-08-23 | Aichi Steel Works Ltd | High strength non-heattreated rolled bar steel |
JPH07316720A (en) * | 1994-05-26 | 1995-12-05 | Sumitomo Metal Ind Ltd | Non-heat treated steel having high durability ratio and high strength, and its production |
JPH10298703A (en) * | 1997-04-21 | 1998-11-10 | Mitsubishi Seiko Muroran Tokushuko Kk | Bainite type high strength and high toughness non-refined steel for hot forging, excellent in yield ratio and endurance ratio |
JP2006161150A (en) * | 2004-11-09 | 2006-06-22 | Jfe Steel Kk | Carbon steel for induction hardening and component for machine structure |
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WO2013018893A1 (en) | 2013-02-07 |
KR20140012209A (en) | 2014-01-29 |
JPWO2013018893A1 (en) | 2015-03-05 |
KR101458348B1 (en) | 2014-11-04 |
CN103228809B (en) | 2016-07-27 |
CN103228809A (en) | 2013-07-31 |
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