WO2012128222A1 - 熱処理変形の小さい機械構造用鋼材 - Google Patents
熱処理変形の小さい機械構造用鋼材 Download PDFInfo
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- WO2012128222A1 WO2012128222A1 PCT/JP2012/056907 JP2012056907W WO2012128222A1 WO 2012128222 A1 WO2012128222 A1 WO 2012128222A1 JP 2012056907 W JP2012056907 W JP 2012056907W WO 2012128222 A1 WO2012128222 A1 WO 2012128222A1
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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
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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
- C22C38/002—Ferrous alloys, e.g. steel alloys containing In, Mg, or other elements not provided for in one single group C22C38/001 - C22C38/60
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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
- C22C38/02—Ferrous alloys, e.g. steel alloys containing silicon
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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
- C22C38/04—Ferrous alloys, e.g. steel alloys containing manganese
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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
- C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
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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
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/20—Ferrous alloys, e.g. steel alloys containing chromium with copper
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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
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/42—Ferrous alloys, e.g. steel alloys containing chromium with nickel with copper
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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
- C22C38/18—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
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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
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/48—Ferrous alloys, e.g. steel alloys containing chromium with nickel with niobium or tantalum
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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
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/50—Ferrous alloys, e.g. steel alloys containing chromium with nickel with titanium or zirconium
Definitions
- the present invention relates to machine structural steel used as power transmission parts such as gears and shafts used in automobiles, industrial machines, and the like, and more particularly to steel for machine structure with small heat treatment deformation.
- heat treatment deformation increases the number of manufacturing processes in order to correct the deformation, or increases the part defect rate if it cannot be corrected.
- heat treatment deformation increases the number of manufacturing processes in order to correct the deformation, or increases the part defect rate if it cannot be corrected.
- this heat treatment deformation is considered to be affected by many factors besides the steel material, such as part shape, influence of pre-heat treatment processes, physical properties of refrigerants such as quenching oil, and non-uniform cooling. By doing so, the deformation of the heat treatment is reduced.
- a material countermeasure a method has been proposed in which a soft ferrite phase is precipitated in the core of a hardened steel material to reduce heat treatment strain (see, for example, Patent Document 1).
- the means for promoting the heat transfer coefficient is due to the convection of the coating material that promotes cooling provided in the portion where cooling is delayed or the coolant formed around the portion where cooling is delayed,
- the means for reducing the heat transfer rate is said to be glass wool or a heat insulating coating material covering a portion where cooling is likely to proceed.
- Patent Document 1 introduces a soft phase having a low strength inside the component, or the technique of Patent Document 2 does not change the heat treatment furnace itself.
- Patent Document 3 is not necessarily a general-purpose means because it requires processing of individual heat-treated parts.
- the present inventors ensure sufficient steel strength without relying on a soft layer such as ferrite, and even when cooling of parts is not uniform under a general technique such as oil quenching, Intensive research was conducted on steel that can keep heat treatment deformation small. As a result, the present inventors can suppress heat treatment deformation to be small by appropriately controlling the chemical composition of steel, the martensite transformation start temperature (Ms point), and the hardenability measured by the Jominy one-side quenching method. I found out.
- an object of the present invention is to provide a steel material with less heat treatment deformation made of mechanical structural steel used as a power transmission component such as a gear or a shaft used in automobiles, industrial machines and the like.
- a steel material for mechanical structure with small heat treatment deformation is in mass%, C: 0.16 to 0.35%, Si: 0.10 to 1.50%, Mn: 0.10 to 1.20%, P: 0 to 0.030%, S: 0 to 0.030%, Cr: 1.30-2.50%, Cu: 0 to 0.30%, Al: 0.008 to 0.800%, O: 0 to 0.0030%, N: 0.0020 to 0.0300% Ni: 0 to 3.00%, Mo: 0 to 0.50% Ti: 0 to 0.200%, Nb: 0 to 0.20% Comprising the balance Fe and inevitable impurities,
- the steel material has a martensitic transformation start temperature (Ms point) of 460 ° C.
- the ratio of the hardness J9 at a distance of 9 mm from the quenching end of the steel to the hardness J1.5 at a distance of 1.5 mm from the quenching end of the steel (J9) /J1.5) is in the range of 0.68 to 0.97, and the distance from the quenching end of the steel to the hardness J1.5 at a distance of 1.5 mm from the quenching end of the steel is 11 mm.
- a steel material for machine structure is provided in which the ratio of the hardness J11 (J11 / J1.5) is in the range of 0.63 to 0.94.
- the steel material does not substantially contain Ni, Mo, Ti and Nb or contains an inevitable impurity level.
- the steel material includes one or two of Ni: 0.20 to 3.00% and Mo: 0.05 to 0.50% in mass%.
- the steel material includes one or two of Ti: 0.020 to 0.200% and Nb: 0.02 to 0.20% in mass%.
- the steel material is one or two of Ni: 0.20 to 3.00% and Mo: 0.05 to 0.50% in terms of mass%, and Ti. : 0.020 to 0.200% and Nb: 0.02 to 0.20%.
- the steel for machine structural use with small heat treatment deformation is, in mass%, C: 0.16-0.35%, Si: 0.10-1.50%, Mn: 0.10-1.20%, P: 0 to 0.030%, S: 0 to 0.030%, Cr: 1.30 to 2.50%, Cu: 0 to 0.30%, Al: 0.008 to 0.800%, O : 0 to 0.0030%, N: 0.0020 to 0.0300%, Ni: 0 to 3.00%, Mo: 0 to 0.50%, Ti: 0 to 0.200%, Nb: 0 to Comprising 0.20%, consisting of the balance Fe and inevitable impurities, preferably consisting essentially of these elements and inevitable impurities, more preferably these elements and inevitable Consisting of only.
- the steel material according to the present invention contains 0.16 to 0.35% of C, preferably 0.20 to 0.30%, more preferably 0.22 to 0.27%.
- C is an element necessary for ensuring the strength after quenching and tempering of steel or the strength of the core after carburizing, quenching and tempering as machine structural parts, and is adjusted to a predetermined range in order to reduce heat treatment deformation. There is a need to. If the C content is less than 0.16%, the strength cannot be secured, and if it exceeds 0.35%, deformation due to heat treatment becomes too large.
- the steel material according to the present invention contains 0.10 to 1.50%, preferably 0.20 to 1.00% of Si.
- Si is an element necessary for deoxidation and is an effective element for imparting necessary strength and hardenability to steel. However, if the Si content is less than 0.10%, the effect cannot be obtained, and if it exceeds 1.50%, the machinability is lowered.
- the steel material according to the present invention contains 0.10 to 1.20% of Mn, preferably 0.20 to 0.80%, more preferably 0.20 to 0.55%.
- Mn is an element necessary for ensuring hardenability. However, if the Mn content is less than 0.10%, sufficient effect on hardenability cannot be obtained, and if it exceeds 1.20%, the machinability is lowered.
- the steel material according to the present invention contains 0 to 0.030% of P, typically more than 0 and 0.030% or less.
- P is an unavoidable element contained from scrap, but if its content exceeds 0.030%, it segregates at the grain boundary and deteriorates properties such as impact strength and bending strength.
- the steel material according to the present invention contains 0 to 0.030% of S, typically more than 0 and 0.030% or less.
- S is an element that improves machinability, but when its content exceeds 0.030%, MnS, which is a non-metallic inclusion, is generated, and the toughness and fatigue strength in the transverse direction are reduced.
- the steel material according to the present invention contains 0 to 3.00% Ni, preferably 0.20 to 3.00% Ni.
- Ni is an optional element that improves hardenability and toughness, and in order to obtain the effect, addition of 0.20% or more is preferable. However, if Ni is contained over 3.00%, the workability is remarkably lowered and the cost is increased.
- the steel material according to the present invention contains 1.30 to 2.50% of Cr, preferably 1.50 to 2.25%.
- Cr is an element necessary for ensuring hardenability. If the Cr content is less than 1.30%, a sufficient effect on hardenability cannot be obtained, and if it exceeds 2.50%, carburization is inhibited, and the machinability also decreases.
- the steel material according to the present invention contains 0 to 0.50% Mo, preferably 0.05 to 0.50%.
- Mo is an optional element that improves hardenability and toughness, and 0.05% or more of addition is necessary to obtain the effect. However, if Mo exceeds 0.50%, workability is reduced.
- the steel material according to the present invention contains 0 to 0.30% of Cu, typically more than 0 and 0.30% or less.
- Cu is an inevitable element contained from scrap, but has aging properties and has an effect of increasing strength. However, when the Cu content exceeds 0.30%, the hot workability is lowered.
- the steel material according to the present invention contains 0.010 to 0.800% Al, preferably 0.014 to 0.600%.
- Al is an element used as a deoxidizing material, and also binds to N and precipitates as AlN as will be described later, thereby bringing about an effect of suppressing grain coarsening. In order to obtain this effect, Al needs to be added in an amount of 0.010% or more. On the other hand, when Al is added in excess of 0.800%, large alumina inclusions are formed, and fatigue characteristics and workability are deteriorated.
- the steel according to the present invention contains 0 to 0.0030%, typically more than 0 and 0.0030% or less, preferably 0.0020% or less.
- O is an element inevitably contained in the steel. However, if O exceeds 0.0030%, workability and fatigue strength are reduced due to an increase in oxide.
- the steel material according to the present invention contains N in an amount of 0.0020 to 0.0300%, preferably 0.0020 to 0.0200%.
- N precipitates finely as AlN or Nb nitride in the steel and brings about an effect of preventing coarsening of crystal grains, and 0.0020% or more needs to be added to obtain the effect.
- nitrides increase, and fatigue strength and workability decrease.
- N is preferably 0.0020 to 0.0100% in order to avoid a decrease in fatigue strength due to excessive TiN formation.
- the steel material according to the present invention contains 0 to 0.200% Ti, preferably 0.020 to 0.200%.
- Ti is an optional element that combines with C in the steel to form carbides finely and has the effect of preventing grain coarsening. To obtain this effect, 0.020% or more of Ti is added. It is preferable. On the other hand, addition exceeding 0.200% impairs machinability.
- the steel material according to the present invention contains 0 to 0.20% Nb, preferably 0.02 to 0.20%, more preferably 0.02 to 0.12%.
- Nb forms carbides or nitrides, and has an effect of preventing crystal grain coarsening.
- nano-order sized NbC or Nb (C, N) finely dispersed in steel suppresses the growth of crystal grains. If Nb is less than 0.02%, the effect cannot be obtained, and if it exceeds 0.20%, the amount of precipitates becomes excessive and the workability deteriorates.
- the martensitic transformation start temperature (Ms point) is restricted to 460 ° C. or less, preferably 450 ° C. or less.
- the reason why heat treatment deformation can be reduced by restricting the Ms point to 460 ° C. or lower is that martensite transformation occurs in a temperature range where the cooling performance of the refrigerant is high even if the parts are not evenly cooled when quenched. This is because it is possible to avoid this, and as a result, it is possible to prevent the time of martensitic transformation from being greatly shifted depending on the parts.
- the heat treatment deformation refers to bending of a shaft-like component or falling or twisting of gear teeth.
- the hardness J1.5 at a distance 1.5 mm from the quenching end of the steel product at a distance 9 mm from the quenching end of the steel product when measured by the Jomini-type one-end quenching method, the hardness J1.5 at a distance 1.5 mm from the quenching end of the steel product at a distance 9 mm from the quenching end of the steel product.
- the ratio of hardness J9 (J9 / J1.5) is in the range of 0.68 to 0.97, and the steel material has a hardness J1.5 at a distance of 1.5 mm from the quenching end of the steel material.
- the ratio of the hardness J11 (J11 / J1.5) at a distance of 11 mm from the quenching end is in the range of 0.63 to 0.94. Within such a range, the heat treatment deformation of the steel material can be kept small.
- the heat treatment deformation referred to here is a change in dimensions (length, diameter, thickness) before and after quenching of the part.
- the mechanism by which heat treatment deformation is suppressed by appropriate control of Jominy hardenability has not yet been elucidated, but even if the hardenability of steel is too low or too high, heat treatment deformation is large. It has been experimentally clarified by the present inventors.
- the comparative example No. 2 shown in Table 2 was used as a structural steel used as a power transmission component such as a gear or a shaft used in automobiles or industrial machines.
- Steel consisting of 1 to 16 component composition, the balance Fe and inevitable impurities was melted in a vacuum induction melting furnace to obtain 100 kg of steel ingot.
- the steel ingots of these inventive examples and comparative examples were heated at 1250 ° C. for 5 hours and then forged into a steel bar having a diameter of 32 mm.
- normalizing was performed by heating and holding at 900 ° C. for 1.5 hours and then air cooling.
- a test piece having a diameter of 20 mm and a length of 200 mm was produced from a steel bar having a diameter of 32 mm, and a groove having a depth of 5 mm, a width of 8 mm, and a length of 200 mm was applied to the side surface of the test piece.
- the cooling rate was varied greatly depending on the portion in the test piece.
- the length of the test piece after groove processing was measured. Then, after heating these test pieces at 930 ° C. for 1 hour, the temperature was lowered to 850 ° C. in the furnace, and further kept for 1 hour, and then quenched into quenching oil at 60 ° C. About the test piece fully cooled after hardening, the bending and length of the test piece were measured.
- a test piece having a diameter of 3 mm and a length of 10 mm was determined from the above-mentioned normalized steel bar having a diameter of 32 mm, and the Ms point, which is the martensitic transformation start temperature of the steel material, was measured using a fully automatic transformation recording measuring device. .
- the Ms point mentioned here is measured under the condition that the cooling process of the part is assumed.
- test piece was prepared from the above-described forged steel bar with a diameter of 32 mm, and “steel hardenability test method (one end) specified in JIS G 0561”. The test was conducted under the conditions according to the quenching method) and evaluated.
- Table 3 shows the measured Ms point of the example of the present invention, J1.5 of hardness at a distance of 1.5 mm, J9 of hardness at a distance of 9 mm, and a distance of 11 mm from the quenching end measured by the Jomini type one-end quenching method.
- the respective values of the hardness J11, and the obtained values (J9 / J1.5) and (J11 / J1.5) are shown.
- the bending (mm) evaluated after quenching the test piece and the absolute value (mm) of the difference in length of the test piece before and after the heat treatment are shown.
- the martensite transformation start temperature that is, the Ms point is in the range of 372 to 442 ° C.
- the following formula (1) of (J9 / J1.5) of this steel material ) Is in the range of 0.70 to 0.95
- the value of the formula (2) shown below in (J11 / J1.5) is in the range of 0.65 to 0.90
- the bend after heat treatment was 0.10 to 0.36 mm
- the absolute value of the difference in length of the test piece before and after the heat treatment was 0.01 to 0.20 mm.
- Table 4 shows the measured Ms point of the steel of the comparative example, J1.5 of the hardness at a distance of 1.5 mm from the quenching end measured by the Jomini type one-end quenching method, and J9 of the hardness at a distance of 9 mm.
- Jominy hardenability which is J11 of hardness at a distance of 11 mm, and the obtained values of (J9 / J1.5) and (J11 / J1.5) are shown.
- the bending (mm) after quenching of the test piece and the absolute value (mm) of the difference in length of the test piece before and after the heat treatment are shown.
- the composition range excluding unavoidable impurities except for Fe, Ni, and Mo in steel materials is shown in Table 1, Ms point is set to 372 to 442 ° C below 460 ° C, and measured by Jomini type one-end quenching method
- the value of (J9 / J1.5) calculated from the equation (1) is in the range of 0.70 to 0.95 and calculated from the equation (2) (J11 /J1.5) in the range of 0.65 to 0.90
- the bending of the specimen after heat treatment is reduced to a small range of 0.10 to 0.36 mm
- the length of the specimen before and after the heat treatment is further increased.
- the absolute value of the difference in thickness could be suppressed to a small range of 0.01 to 0.20 mm.
- the value obtained by the formula (1) and the formula (2) from the hardness measured by the Jomini type one-end quenching method (J9 / J1.5) is in the range of 0.68 to 0.97 15 examples in which the value of (J11 / J1.5) is outside the range of 0.63 to 0.94, the absolute value of the difference in length of the test piece before and after the heat treatment is 0.27 to 0 .45 mm, which is larger than the steel of the invention example. Therefore, among the comparative examples, there was no example in which the absolute value of the difference between the bending of the test piece after the heat treatment and the length of the test piece before and after the heat treatment was equivalent to that of the steel of the present invention.
- heat treatment deformation is evaluated not by carburizing and quenching but by quenching. However, even when carburized and quenched, it is confirmed that the heat treatment deformation of the steel material satisfying the present claim is small.
- the steel material of the present invention is used after tempering after quenching.
- the steel material is processed into a part by the limitation of the steel component, the Ms point which is the martensitic transformation start temperature, and the limitation of the hardenability measured by the Jominy one-side quenching method. Heat treatment deformation when hardening for hardening or carburizing and quenching can be reduced.
- a steel material according to the present invention is a steel material applicable to power transmission parts such as gears and shafts used in automobiles and industrial machines.
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Abstract
Description
C:0.16~0.35%、
Si:0.10~1.50%、
Mn:0.10~1.20%、
P:0~0.030%、
S:0~0.030%、
Cr:1.30~2.50%、
Cu:0~0.30%、
Al:0.008~0.800%、
O:0~0.0030%、
N:0.0020~0.0300%
Ni:0~3.00%、
Mo:0~0.50%
Ti:0~0.200%、
Nb:0~0.20%
を含み、残部Feおよび不可避不純物からなり、
該鋼材が、460℃以下のマルテンサイト変態開始温度(Ms点)を有し、
ジョミニー式一端焼入法により測定した場合に、該鋼材の焼入端からの距離1.5mmにおける硬さJ1.5に対する、該鋼材の焼入端からの距離9mmにおける硬さJ9の比(J9/J1.5)が0.68~0.97の範囲にあり、かつ、該鋼材の焼入端からの距離1.5mmにおける硬さJ1.5に対する、該鋼材の焼入端からの距離11mmにおける硬さJ11の比(J11/J1.5)が0.63~0.94の範囲にある、機械構造用鋼材が提供される。
ただし、
(J9/J1.5)=(ジョミニー式一端焼入法により測定される焼入れ端からの距離9mmの硬さ)÷(ジョミニー式一端焼入法により測定される焼入れ端からの距離1.5mmの硬さ)……(1)
(J11/J1.5)=(ジョミニー式一端焼入法により測定される焼入れ端からの距離11mmの硬さ)÷(ジョミニー式一端焼入法により測定される焼入れ端からの距離1.5mmの硬さ)……(2)
Claims (10)
- 熱処理変形の小さい機械構造用鋼材であって、該鋼材が、質量%で、
C:0.16~0.35%、
Si:0.10~1.50%、
Mn:0.10~1.20%、
P:0~0.030%、
S:0~0.030%、
Cr:1.30~2.50%、
Cu:0~0.30%、
Al:0.008~0.800%、
O:0~0.0030%、
N:0.0020~0.0300%、
Ni:0~3.00%、
Mo:0~0.50%、
Ti:0~0.200%、
Nb:0~0.20%
を含み、残部Feおよび不可避不純物からなり、
該鋼材が、460℃以下のマルテンサイト変態開始温度(Ms点)を有し、
ジョミニー式一端焼入法により測定した場合に、該鋼材の焼入端からの距離1.5mmにおける硬さJ1.5に対する、該鋼材の焼入端からの距離9mmにおける硬さJ9の比(J9/J1.5)が0.68~0.97の範囲にあり、かつ、該鋼材の焼入端からの距離1.5mmにおける硬さJ1.5に対する、該鋼材の焼入端からの距離11mmにおける硬さJ11の比(J11/J1.5)が0.63~0.94の範囲にある、機械構造用鋼材。 - 前記鋼材が、質量%で、C:0.16~0.35%、Si:0.10~1.50%、Mn:0.10~1.20%、P:0~0.030%、S:0~0.030%、Cr:1.30~2.50%、Cu:0~0.30%、Al:0.008~0.800%、O:0~0.0030%、N:0.0020~0.0300%、Ni:0~3.00%、Mo:0~0.50%Ti:0~0.200%、Nb:0~0.20%、残部Feおよび不可避不純物のみからなる、請求項1に記載の機械構造用鋼材。
- 前記鋼材が、Ni、Mo、Ti及びNbを実質的に含まない、請求項1に記載の機械構造用鋼材。
- 前記鋼材が、Ni、Mo、Ti及びNbを実質的に含まない、請求項2に記載の機械構造用鋼材。
- 前記鋼材が、質量%で、Ni:0.20~3.00%及びMo:0.05~0.50%の1種または2種を含む、請求項1に記載の機械構造用鋼材。
- 前記鋼材が、質量%で、Ni:0.20~3.00%及びMo:0.05~0.50%の1種または2種を含む、請求項2に記載の機械構造用鋼材。
- 前記鋼材が、質量%で、Ti:0.020~0.200%及びNb:0.02~0.20%の1種または2種を含む、請求項1に記載の機械構造用鋼材。
- 前記鋼材が、質量%で、Ti:0.020~0.200%及びNb:0.02~0.20%の1種または2種を含む、請求項2に記載の機械構造用鋼材。
- 前記鋼材が、質量%で、Ni:0.20~3.00%及びMo:0.05~0.50%の1種または2種と、Ti:0.020~0.200%及びNb:0.02~0.20%の1種または2種とを含む、請求項1に記載の機械構造用鋼材。
- 前記鋼材が、質量%で、Ni:0.20~3.00%及びMo:0.05~0.50%の1種または2種と、Ti:0.020~0.200%及びNb:0.02~0.20%の1種または2種とを含む、請求項2に記載の機械構造用鋼材。
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| KR1020137024481A KR101850805B1 (ko) | 2011-03-18 | 2012-03-16 | 열처리 변형이 작은 기계 구조용 강재 |
| US14/003,958 US20130343949A1 (en) | 2011-03-18 | 2012-03-16 | Steel Material for Machine Structural Use Reduced in Thermal Deformation |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2011061209A JP5641992B2 (ja) | 2011-03-18 | 2011-03-18 | 熱処理変形の小さい機械構造用鋼材 |
| JP2011-061209 | 2011-03-18 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO2012128222A1 true WO2012128222A1 (ja) | 2012-09-27 |
Family
ID=46879369
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/JP2012/056907 Ceased WO2012128222A1 (ja) | 2011-03-18 | 2012-03-16 | 熱処理変形の小さい機械構造用鋼材 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US20130343949A1 (ja) |
| JP (1) | JP5641992B2 (ja) |
| KR (1) | KR101850805B1 (ja) |
| WO (1) | WO2012128222A1 (ja) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP5668882B1 (ja) * | 2013-07-19 | 2015-02-12 | 愛知製鋼株式会社 | Mo無添加の浸炭用電炉鋼の製造方法 |
| JP7269467B2 (ja) * | 2019-01-11 | 2023-05-09 | 日本製鉄株式会社 | 鋼材 |
| CN115896607B (zh) * | 2021-09-24 | 2024-07-12 | 宝山钢铁股份有限公司 | 一种高淬透性风电螺栓用钢、棒材及其制造方法 |
| CN116790994A (zh) * | 2023-06-30 | 2023-09-22 | 本钢板材股份有限公司 | 一种转炉流程渗碳齿轮轴棒材生产制备方法 |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS56116857A (en) * | 1980-02-20 | 1981-09-12 | Mitsubishi Steel Mfg Co Ltd | Low-heat treated strained steel for gear |
| JPH09137266A (ja) * | 1995-11-08 | 1997-05-27 | Kobe Steel Ltd | 熱処理歪みの少ない肌焼用鋼 |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP3517515B2 (ja) * | 1996-04-23 | 2004-04-12 | エヌケーケー条鋼株式会社 | 高強度、低熱処理変形歯車およびその製造方法 |
| JP2001262203A (ja) * | 2000-03-22 | 2001-09-26 | Daido Steel Co Ltd | 高硬度ガス噴霧ショット |
| US8968495B2 (en) * | 2007-03-23 | 2015-03-03 | Dayton Progress Corporation | Methods of thermo-mechanically processing tool steel and tools made from thermo-mechanically processed tool steels |
| JP4941252B2 (ja) * | 2007-11-26 | 2012-05-30 | 住友金属工業株式会社 | 動力伝達部品用肌焼鋼 |
| JP5381171B2 (ja) * | 2008-03-31 | 2014-01-08 | Jfeスチール株式会社 | 高強度肌焼鋼部品の製造方法 |
| JP5632659B2 (ja) | 2010-06-17 | 2014-11-26 | 株式会社神戸製鋼所 | 熱処理歪みの少ない肌焼鋼 |
| JP5641991B2 (ja) * | 2011-03-18 | 2014-12-17 | 山陽特殊製鋼株式会社 | 熱処理変形の小さい機械構造用鋼材 |
-
2011
- 2011-03-18 JP JP2011061209A patent/JP5641992B2/ja active Active
-
2012
- 2012-03-16 KR KR1020137024481A patent/KR101850805B1/ko active Active
- 2012-03-16 WO PCT/JP2012/056907 patent/WO2012128222A1/ja not_active Ceased
- 2012-03-16 US US14/003,958 patent/US20130343949A1/en not_active Abandoned
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS56116857A (en) * | 1980-02-20 | 1981-09-12 | Mitsubishi Steel Mfg Co Ltd | Low-heat treated strained steel for gear |
| JPH09137266A (ja) * | 1995-11-08 | 1997-05-27 | Kobe Steel Ltd | 熱処理歪みの少ない肌焼用鋼 |
Also Published As
| Publication number | Publication date |
|---|---|
| JP2012197472A (ja) | 2012-10-18 |
| KR101850805B1 (ko) | 2018-04-20 |
| JP5641992B2 (ja) | 2014-12-17 |
| US20130343949A1 (en) | 2013-12-26 |
| KR20140005286A (ko) | 2014-01-14 |
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