Non-tempered steel and nitrided parts

Abstract

To provide non-heat treated steel and a nitrided component which are suppressed in alloy cost and furthermore have excellent machinability, yield strength and fatigue strength.SOLUTION: Non-heat treated steel contains C:0.30 to 0.50%, Si:0.05 to 0.35%, Mn:0.45 to 1.00%, P: 0.080% or less, S:0.035 to 0.100%, Cu: 0.25% or less, Ni: 0.25% or less, Cr:0.03 to 0.25%, Al: 0.020% or less, N:0.0125 to 0.0250%, Ti:0.005 to 0.030%, Ca:0.0003 to 0.0100%, V:0 to 0.02%, and Mo:0 to 0.03%, and the balance composed of Fe and impurities, wherein amount of solid-solution N is 0.008% or more, and in metallographic structure, an area ratio of pro-eutectoid ferrite is 20% or more and balance structure is pearlite, and wherein in oxide-based inclusion in which a sum of the weight concentration of Al and Si is 10% or more, a ratio CT / AS of CT which is a weight concentration of Ca and Ti to AS which is a weight concentration of Al and Si is 0.50 or more.SELECTED DRAWING: None

Description

[Technical field]

[0001] The present invention relates to non-heat treated steels and nitrided parts. [Background technology]

[0002] In order to improve mechanical properties such as hardness, wear resistance, and fatigue strength, medium carbon steel containing about 0.3 to 0.6% carbon may be used as a material for mechanical structural parts (hereinafter simply referred to as parts) used in automobiles, ships, industrial machines, etc. From the viewpoints of mass production and economic efficiency, it is desirable for the steel materials used for these parts and materials to have a minimum level of fatigue strength and to have as low a manufacturing cost as possible.

[0003] In order to reduce the manufacturing cost of parts, it is necessary to use inexpensive steel as the raw material, and also to carry out manufacturing processes such as rolling of steel bars, hot forging, and cutting as inexpensively as possible. For many parts, the cost required for cutting is large among these manufacturing costs. Therefore, improving the machinability of steel is an effective way to reduce manufacturing costs.

[0004] In order to improve the machinability of steel, it is effective to add a large amount of S to the steel, increase the amount of MnS in the steel, and improve chip disposal. In addition, it is also effective to reduce the hardness by reducing the content of alloy elements that improve hardenability. In addition, adding Ca to the steel to generate CaO to suppress tool wear is also effective in improving the machinability of steel.

[0005] In recent years, therefore, in order to improve machinability, various non-tempered steels have been developed that contain large amounts of S and Ca while controlling the alloy components so that the hardness of the hot forged steel is not too high.

[0006] Patent Document 1 shows a technique for improving machinability by using inexpensive carbon steel as a base and compounding S with Ca to change the form of MnS. Steel obtained by this technique has low hardness and high machinability.

[0007] Patent Document 2 discloses a technique for improving machinability by increasing the S content, making the steel structure ferrite + pearlite, and appropriately controlling the C concentration and carbon equivalent of the steel. In order to increase fatigue strength, this steel has a reduced C content of 0.3% or less and contains 0.4% or more Cr and 0.03% or more V. [Prior art documents] [Patent documents]

[0008] [Patent Document 1] JP 2008-57021 A [Patent Document 2] Japanese Patent Application Publication No. 7-179986 Summary of the Invention [Problem to be solved by the invention]

[0009] It is difficult to say that the steel in Patent Document 1 is sufficiently devised to increase fatigue strength. Furthermore, because the hardness of the steel is low, there is a problem in that it is easily deformed or dented due to impacts during handling of the parts or the inclusion of foreign objects.

[0010] In Patent Document 2, Cr and V are contained in amounts greater than those of carbon steel for machine construction specified by JIS. This leads to problems such as increased steel costs. Furthermore, there is a problem that sufficient machinability cannot be obtained depending on the processing conditions because there is insufficient ingenuity for suppressing the variation in hardness of the steel.

[0011] The present invention has been made in consideration of the above circumstances, and an object of the present invention is to provide a non-heat treated steel and a nitrided part that have excellent machinability, yield strength and fatigue strength while suppressing alloy costs. [Means for solving the problem]

[0012] The gist of the present invention is as follows. (1) The non-heat treated steel according to one embodiment of the present invention comprises, in mass%, C: 0.30-0.50%, Si: 0.05 to 0.35%, Mn: 0.45-1.00%, P: 0.080% or less, S: 0.035~0.100%, Cu: 0.25% or less, Ni: 0.25% or less, Cr: 0.03~0.25%, Al: 0.020% or less, N: 0.0125~0.0250%, Ti: 0.005 to 0.030%, Ca: 0.0003~0.0100%, V: 0 to 0.02%, and Mo: 0 to 0.03% with the remainder being Fe and impurities, The amount of solute N Nsol represented by the following formula (1) is 0.008% or more, In the metal structure, the area ratio of pro-eutectoid ferrite is 20% or more, and the remaining structure is pearlite, Among oxide-based inclusions, in those in which the sum of the weight concentrations of Al and Si is 10% or more, the ratio CT, which is the sum of the weight concentrations of Ca and Ti, to AS, which is the sum of the weight concentrations of Al and Si, is 0.50 or more. Nsol=N-Ti / 3.4 (1) However, each element symbol in the above formula (1) represents the content of the corresponding element in mass %.

[0013] (2) A nitrided component according to one aspect of the present invention has a base material made of the non-heat-treated steel described in (1) above, and a nitrided layer made of a compound layer and a diffusion layer formed on a surface layer of the base material. (3) The nitrided part described in (2) above may be a machine structural part. Effect of the Invention

[0014] According to the present invention, it is possible to provide a non-heat treated steel and a nitrided part having excellent machinability, yield strength, and fatigue strength while suppressing alloy costs. Therefore, the non-heat treated steel of the present invention is suitable as a material for machine structural parts of automobiles, industrial machines, etc. [Brief description of the drawings]

[0015] [Figure 1] 1 is a side view of an Ono-type rotating bending fatigue test piece used in the examples, in which the unit of dimensions is mm. [Diagram 2] 1 is a schematic diagram of a tensile test piece used in the examples, in which the unit of dimensions is mm. [Diagram 3] 1 is a side view of an Ono-type rotating bending fatigue test piece used in the examples, in which the unit of dimensions is mm. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

[0016] Hereinafter, a non-heat treated steel (hereinafter also simply referred to as "steel" or "steel material") and a nitrided part according to one embodiment of the present invention will be described.

[0017] The non-heat treated steel according to this embodiment has been discovered based on the following findings (a) to (i) obtained by the present inventors.

[0018] First, the inventors have investigated the conditions for obtaining a steel that can suppress the hardness after hot working and the tool wear during machining, i.e., a steel with excellent machinability. In order to suppress the tool wear during cutting, it is necessary not only to simply reduce the hardness, but also to reduce the amount of oxides in the steel and control the composition of the oxides. The specific findings (a) to (d) are as follows:

[0019] (a) When Ca is added to molten steel, the oxide inclusions (simply called inclusions), which are impurities, change from hard Al2O3 and SiO2 to complex oxides in which CaO is added to them. Since these complex oxides are soft, they can suppress tool wear. (b) When Al and Ca are added to molten steel at the same time, or when Ca is added first and then Al, coarse CaO is produced alone, and the ratio of CaO in the composite oxide does not increase. (c) When the S concentration in the molten steel is high, Ca is consumed to form CaS, making it difficult for CaO to form. In that case, the proportion of CaO in the composite oxide can be increased by extending the holding time after adding Ca. However, if the holding time is too long, the Ca concentration in the molten steel decreases, making it difficult to adjust to the target steel composition. (d) When Ti is added to molten steel, Ti combines with oxygen and nitrogen to form Ti oxides and Ti nitrides. At this time, some of the Ti dissolves in Al2O3 or SiO2 to form a composite oxide containing Ti. This composite oxide containing Ti is soft, so it can suppress tool wear.

[0020] Thus, even in a composition system with a high S content, Ti and Ca can be contained in the molten steel, and the timing of adding Ca to the molten steel and the holding time after the addition can be controlled to make the inclusions advantageous against tool wear. However, in order to sufficiently suppress tool wear, it is necessary not only to control the inclusions as described in (a) to (d) above, but also to increase the pro-eutectoid ferrite fraction in the steel structure and suppress hardness. Therefore, the present inventors have investigated a method of suppressing hardness by adjusting the composition of a steel containing a large amount of S and Ca and controlling the inclusions, and increasing the pro-eutectoid ferrite fraction in the steel structure. As a result, the following findings (e) to (g) have been obtained.

[0021] (e) In order to suppress the increase in hardness of steel, it is sufficient to reduce the contents of Cr, Si, and Mn, which have the effects of increasing hardenability and solid solution strengthening of ferrite. This increases the fraction of pro-eutectoid ferrite and suppresses the strengthening of ferrite, thereby suppressing the hardness of the steel. (f) On the other hand, when alloying elements such as Cr and Mn, which have a solute drag effect, are reduced, depending on the hot working conditions, the austenite grain size tends to become coarse. Such coarse austenite grains increase the hardenability, leading to the formation of bainite. (g) Therefore, in order to prevent bainite from forming in inexpensive steel with a relatively small content of alloying elements even when hot working is performed under various conditions, in addition to controlling the hardenability of the steel to be sufficiently low, pinning by a second phase can be utilized. In order to obtain a stable pinning effect during hot working at temperatures exceeding 1100°C, it is good to utilize TiN. In other words, the pinning effect of TiN can suppress the coarsening of austenite grains, and as a result, it is possible to avoid an increase in hardenability and increase the fraction of pro-eutectoid ferrite.

[0022] As explained above, in order to improve the machinability of steel, it is effective to add a large amount of S and reduce the contents of Si, Mn, and Cr. However, reducing the contents of these alloy elements reduces the yield strength and fatigue strength of the parts. Therefore, we investigated the conditions for obtaining the necessary yield strength and fatigue strength for parts. As a result, we obtained the following findings (h) and (i).

[0023] (h) In order to increase the yield strength and fatigue strength without impairing machinability, the amount of N contained in the steel can be increased. Increasing the amount of N increases the yield strength and fatigue strength without excessively increasing the hardness. Furthermore, since N is a very inexpensive alloying element, increasing the amount of N hardly increases the alloying cost. (i) However, simply increasing the amount of N contained in steel does not increase yield strength. In order to increase yield strength, N must be in a solid solution state. Since Ti fixes N as TiN, in order to increase the amount of dissolved N in steel containing Ti, it is necessary to adjust the N content to an appropriate level according to the amount of Ti contained.

[0024] An embodiment of the present invention, which has been completed based on the above findings, is a non-heat treated steel having the following composition, by mass%, C: 0.30-0.50%, Si: 0.05-0.35%, Mn: 0.45-1.00%, P: 0.080% or less, S: 0.035-0.100%, Cu: 0.25% or less, Ni: 0.25% or less, Cr: 0.03-0.25%, Al: 0.020% or less, N: 0.0125-0.0250%, Ti: 0.005-0.030%, Ca: 0.0003-0.0100%, and V: 0-0. The alloy contains 0.02% Ca and Ti, and 0-0.03% Mo, with the balance being Fe and impurities; the amount of solute N, Nsol, represented by the following formula (1) is 0.008 or more; in the metal structure, the area ratio of pro-eutectoid ferrite is 20% or more, and the balance is pearlite; and in oxide-based inclusions in which the sum of the weight concentrations of Al and Si is 10% or more, the ratio CT / AS of the sum of the weight concentrations of Ca and Ti (CT) to the sum of the weight concentrations of Al and Si (AS) is 0.50 or more. Nsol=N-Ti / 3.4 (1) However, each element symbol in the above formula (1) represents the content of the corresponding element in mass %.

[0025] Hereinafter, a non-heat treated steel and a nitrided part according to an embodiment of the present invention will be described in detail. Note that the "non-heat treated steel" in this embodiment is a steel that is a raw material for a nitrided part, and includes, for example, steel to be subjected to hot forging (e.g., steel bar) and a crude material roughly formed by hot forging. That is, the "non-heat treated steel" in this embodiment is a raw material (steel material) before part processing (machining). Also, the "nitrided part" in this embodiment is, for example, a machine structural part.

[0026] In the following description, "%" for the content of each element means "mass %". The content of each element in the chemical composition may be expressed as "element amount". For example, the C content may be expressed as C amount. Furthermore, a numerical range expressed using "~" means a range that includes the numerical values ​​written before and after "~" as the lower and upper limits. Furthermore, when the numerical values ​​written before and after "~" are followed by "greater than" or "less than", the numerical range means a range that does not include these numerical values ​​as the lower or upper limit.

[0027] [Chemical composition] The chemical composition of the non-heat treated steel according to this embodiment contains the following elements. Note that, since the base material of a nitrided part usually has the same composition as the non-heat treated steel, which is the raw material, the composition of the steel material and the composition of the base material of the part are equivalent, unless otherwise specified.

[0028] C: 0.30-0.50% C has the effect of increasing the hardness and fatigue strength of the steel material. If the C content is too low, the above effect cannot be obtained. On the other hand, if the C content is too high, the amount of pro-eutectoid ferrite is insufficient, causing an excessive increase in hardness, resulting in an increase in cutting resistance and a decrease in machinability. Therefore, the C content is 0.30 to 0.50%. The C content is preferably 0.33% or more, and more preferably 0.35% or more. Moreover, the C content is preferably 0.48% or less, and more preferably 0.45% or less.

[0029] Silicon: 0.05 to 0.35% Silicon has the effect of dissolving in ferrite to strengthen the steel material. If the Si content is too low, the above effect cannot be obtained. On the other hand, if the Si content is too high, the oxide-based inclusions become hard and deteriorate the tool wear. In addition, if the Si content is too high, the ferrite becomes too hard and the machinability may decrease. Therefore, the Si content is 0.05 to 0.35%. The Si content is preferably 0.10% or more, and more preferably 0.15% or more. The Si content is preferably 0.30% or less, more preferably 0.26% or less, and more preferably 0.24% or less.

[0030] Mn: 0.45 to 1.00% Mn forms nitrides and contributes to hardening of the nitrided layer. Mn also has the effect of forming MnS in the steel material to improve the machinability of the steel material. If the Mn content is too low, the above effect cannot be obtained. On the other hand, if the Mn content is too high, the nitrided layer is excessively hardened and the bending straightening property is deteriorated. In addition, if Mn is contained in an excessive amount, the hardenability is increased, the formation of bainite is promoted, and sufficient pro-eutectoid ferrite may not be secured. Therefore, the Mn content is 0.45 to 1.00%. The Mn content is preferably 0.50% or more, more preferably 0.55% or more. The Mn content is preferably 0.90% or less, more preferably 0.80% or less, and more preferably 0.75%.

[0031] P:0.080% or less P is an element contained in steel as an impurity. If the P content is too high, it segregates at grain boundaries and deteriorates hot ductility and toughness. Therefore, the P content is 0.080% or less. The P content is preferably 0.060% or less, and more preferably 0.040% or less. However, P slightly strengthens ferrite and contributes to increasing fatigue strength. In addition, excessive reduction of P leads to increased costs for de-P. For these reasons, the P content may be 0.002% or more. The P content may be preferably 0.005% or more, or 0.008% or more.

[0032] S: 0.035~0.100% S combines with Mn in steel to form MnS, which has the effect of improving the machinability of the steel. In order to inexpensively produce steel containing a C content on the level of medium carbon steel and to ensure desirable machinability, it is necessary to sufficiently increase the S content. On the other hand, if the S content is too high, coarse MnS is formed, and fatigue properties deteriorate. Therefore, the S content is 0.035 to 0.100%. The S content is preferably 0.040% or more, and more preferably 0.045% or more. The upper limit of the S content is preferably 0.090% or less, and more preferably 0.080% or less.

[0033] Cr: 0.03~0.25% Cr has the effect of improving fatigue strength by refining the lamellar spacing of pearlite and strengthening it. If the Cr content is too low, the above effect cannot be obtained. On the other hand, if the Cr content is too high, the hardenability of the steel material improves, and depending on the hot forging conditions, pro-eutectoid ferrite is not sufficiently generated, and the amount of pearlite increases, which may deteriorate the machinability. Therefore, the Cr content is 0.03 to 0.25%. The Cr content is preferably 0.05% or more. The Cr content is preferably 0.20% or less, more preferably 0.15% or less, and even more preferably 0.10% or less.

[0034] Cu: 0.25% or less Cu is contained in iron ore and scrap, and is inevitably contained as an impurity in steel when it is manufactured in a blast furnace or electric furnace. Cu may also be intentionally contained in order to dissolve in ferrite and increase the strength and fatigue strength of the steel. However, if the Cu content is excessively high, it will segregate at the grain boundaries of the steel during hot forging and induce hot cracking. Therefore, the Cu content is 0.25% or less. The Cu content is preferably 0.20% or less, and more preferably 0.15% or less. When Cu is contained to obtain an effect, the Cu content is preferably 0.001% or more, or 0.01% or more.

[0035] Ni: 0.25% or less Ni is contained in iron ore and scrap, and is inevitably contained as an impurity in steel when steel is produced in a blast furnace or electric furnace. Ni may also be intentionally contained in order to dissolve in ferrite and increase the strength and fatigue strength of the steel. Ni also suppresses hot cracking caused by Cu when the steel contains Cu. However, if the Ni content is too high, the effect saturates and the manufacturing cost increases. Therefore, the Ni content is 0.25% or less. The Ni content is preferably 0.20% or less, and more preferably 0.15% or less. When the effect is obtained by containing Ni, the Ni content is preferably 0.001% or more, or 0.01% or more.

[0036] Al: 0.020% or less Al is an element that is mixed into steel as an impurity, but may be contained for deoxidation. If the Al content is too high, hard Al oxides that accelerate tool wear are formed. If elements other than Al can provide sufficient deoxidation, the Al content is preferably low. Therefore, the Al content is 0.020% or less. The Al content is preferably 0.010% or less, and more preferably 0.006% or less. The Al content may be 0%. There is no particular lower limit for the Al content, but when it is contained for deoxidation, it may be 0.001% or more.

[0037] Ti: 0.005 to 0.030% Ti has the effect of softening oxide-based inclusions. Furthermore, Ti combines with N to form TiN, and the pinning effect suppresses the coarsening of austenite grains during hot forging. When the generation of coarse austenite grains is suppressed, the hardenability is reduced, so that pro-eutectoid ferrite can be sufficiently secured, and as a result, the machinability can be improved. If the Ti content is too low, the above effect cannot be obtained. On the other hand, if the Ti content is too high, a large amount of N is consumed for the generation of TiN, and the amount of solid-solubilized N decreases, which may deteriorate the yield strength and fatigue properties. In addition, if Ti is contained excessively, coarse TiO2 and TiN may be generated, which may deteriorate the fatigue properties. Therefore, the Ti content is 0.005 to 0.030%. The Ti content is preferably 0.025% or less, more preferably 0.020% or less. The Ti content is preferably 0.007% or more.

[0038] N: 0.0125~0.0250% N, like C, is a very inexpensive element, and is therefore an important element for increasing the strength of steel materials at low cost. When N is dissolved in steel, it creates a Cotterell atmosphere on dislocations, which contributes to increasing the yield strength. When precipitated as TiN, the pinning effect can suppress the coarsening of austenite, reducing the variation in hardness. If the N content is too low, the above effects cannot be obtained. On the other hand, if the N content is excessive, bubbles due to nitrogen gas may be generated in the steel, deteriorating the fatigue strength. Therefore, the N content is 0.0125 to 0.0250%. The N content is preferably 0.0140% or more, and more preferably 0.0160%. The N content is preferably 0.0230% or less, and more preferably 0.0200% or less.

[0039] Ca:0.0003~0.0100% or less Ca has the effect of suppressing tool wear and extending tool life by changing oxide inclusions into soft composite oxides containing CaO. In order to stably obtain this effect, the Ca content needs to be 0.0003% or more. However, if the Ca content is too high, coarse CaO is generated as a single substance, which aggravates tool wear. Therefore, the Ca content is 0.0003 to 0.0100%. The Ca content is preferably 0.0005% or more, more preferably 0.0010%. The Ca content is preferably 0.0050% or less, more preferably 0.0035% or less.

[0040] V:0.02% or less Mo: 0.03% or less In the non-tempered steel of this embodiment, the contents of V and Mo, which are effective in improving fatigue strength and yield strength, are reduced as much as possible in order to reduce production costs. However, Mo and V may be contained in the steel material as impurities, and in that case, they may be contained since they do not adversely affect production costs. From the viewpoint of production costs, the V content is 0.02% or less, and the Mo content is 0.03% or less. The V content is preferably 0.01% or less, and the Mo content is preferably 0.02% or less. Both the V content and the Mo content may be 0%.

[0041] In the composition of the non-heat treated steel of this embodiment, the balance is Fe and impurities. Here, the impurities refer to substances that are mixed in from raw materials such as ore and scrap, or from the manufacturing environment, during industrial production of steel material, and are permissible within a range that does not adversely affect the steel material for nitriding of the present invention.

[0042] The chemical compositions of the above-mentioned steels and non-tempered steel parts may be measured using ICP-AES (Inductively Coupled Plasma-Atomic Emission Spectrometry). Note that C and S may be measured using the combustion-infrared absorption method, and N may be measured using the inert gas fusion-thermal conductivity method.

[0043] [Metal structure (microstructure)] In the metal structure (microstructure) of the non-heat treated steel of this embodiment, the area ratio of pro-eutectoid ferrite is 20% or more, and the remaining structure is pearlite. That is, the microstructure of this embodiment is a structure mainly composed of pro-eutectoid ferrite and pearlite. If bainite or martensite is mixed into the structure of steel during cutting, the hardness increases and the machinability deteriorates. In addition, the amount of change in hardness due to changes in hot forging conditions also increases. In order to reduce the amount of change in hardness during hot forging, the metal structure needs to be a ferrite and pearlite structure. In addition, when the proportion of pro-eutectoid ferrite in the metal structure is high, the hardness of the steel material is suppressed and the machinability can be improved. In order to obtain such high machinability, the area ratio of pro-eutectoid ferrite in the metal structure needs to be 20% or more. The area ratio of pro-eutectoid ferrite is preferably 30% or more, and more preferably 40% or more.

[0044] The microstructure of this embodiment is a structure mainly composed of pro-eutectoid ferrite and pearlite, and preferably does not contain structures other than pro-eutectoid ferrite and pearlite. In other words, the total area ratio of pro-eutectoid ferrite and pearlite is preferably 100%. However, depending on the manufacturing conditions, a bainite structure may be contained as the remaining structure, but if a bainite structure is generated, machinability decreases. Therefore, it is preferable that the remaining structure is as small as possible, preferably 10% or less, or 5% or less. More preferably, the remaining structure is 0%.

[0045] The area fraction of the metal structure is measured by the following method. The sample for measuring the metal structure is mirror-polished and then etched with nital to reveal the structure. The structure is photographed at 200x magnification using an optical microscope. A square lattice pattern with a mesh spacing of 50 μm is overlaid on the photographed image, and the number of structures at the locations where the lattice points overlap is counted. The number of lattice points on each structure is divided by the number of all measured lattice points to determine the area fraction of the corresponding structure. However, the total number of lattice points used to measure the area fraction of the structure must be 500 or more. There are no restrictions on the size of the image as long as it meets the above conditions, but for example, five images of 0.6 mm x 0.48 mm may be used.

[0046] [Nsol] Simply increasing the N content in steel may not improve fatigue strength or yield strength. In order to improve fatigue strength and yield strength using N, it is necessary to increase the amount of N in solid solution. The amount of solute N in steel that has been allowed to cool after hot working is the N content minus the amount of N that precipitates as TiN. Specifically, the amount of solute N, Nsol, is expressed by equation (1).

[0047] Nsol=N-Ti / 3.4 (1) However, each element symbol in the above formula (1) represents the content of the corresponding element in mass %.

[0048] In order to obtain the above-mentioned effects of solute N, Nsol needs to be 0.008% or more. Nsol may be any large amount as long as the N content is within the above-mentioned range. In other words, from the ranges of the N content and T content in this embodiment described above, the substantial upper limit of Nsol is 0.0235% or less. When high fatigue strength and yield strength are required, Nsol is preferably 0.009% or more, and more preferably 0.010% or more.

[0049] [Average composition of oxide-based composite inclusions (CT / AS: 0.50 or more)] Oxide-based inclusions with a sum of Al and Si weight concentrations of 10% or more are hard and deteriorate tool wear. In order to soften the oxides and suppress tool wear, it is necessary to secure oxide-based composite inclusions by compounding Ti and Ca with the oxide-based inclusions. In order to obtain this effect, when the weight concentrations of Ca, Ti, Al, and Si in the oxide-based composite inclusions are XCa, XTi, XAl, and XSi, respectively, the ratio of the sum of the weight concentrations of Ca and Ti (XCa+XTi) to the sum of the weight concentrations of Al and Si (XAl+XSi) expressed by the following formula (2) needs to be 0.50 or more. It is preferably 0.70 or more. On the other hand, if the CT / AS is too high, TiO or CaO that is not compounded with the oxide-based inclusions may become coarse and have a negative effect on tool wear, so it is preferable to set the CT / AS to 3.0 or less.

[0050] CT / AS=(XCa+XTi) / (XAl+XSi)...(2)

[0051] The weight concentrations XCa, XTi, XAl, and XSi of Ca, Ti, Al, and Si in oxide-based composite inclusions are measured by the following method.

[0052] The sample for measuring the inclusion composition is mirror-polished to obtain the test surface. The inclusions on the test surface of the sample are observed in a scanning electron microscope equipped with an energy dispersive X-ray spectrometer (EDS), and the weight fractions of Ca, Ti, Al, Si, O, and Fe in the inclusions are analyzed by EDS. Although elements other than Ca, Ti, Al, Si, O, and Fe are also detected in the EDS spectrum obtained at this time, the weight fractions are analyzed assuming that the inclusions are composed only of these six elements. In order to eliminate the influence of background Fe from the weight fraction analyzed by EDS, the weight fractions of each element are normalized so that the sum of the weights of the five elements Ca, Ti, Al, Si, and O is 100%. In this case, inclusions with a weight fraction of O of less than 10% are not considered to be oxide-based inclusions, and are excluded from this measurement.

[0053] Next, for inclusions with a weight fraction of O of 10% or more, the weight fraction of each element is normalized again so that the sum of the weights of the four elements Ca, Ti, Al, and Si becomes 100%, and this value is taken as the weight fraction of Ca, Ti, Al, and Si for that inclusion. A similar analysis is performed on all oxide-based inclusions in the observation field (2 mm × 2 mm) whose diameter, when the area on the observation surface is converted into a circle, is 1.0 μm or more. The arithmetic average values ​​of the weight fractions of Ca, Ti, Al, and Si in all the measured oxide inclusions are calculated as XCa, XTi, XAl, and XSi for that sample. These values ​​are substituted into equation (2) to calculate the CT / AS of that sample. In this embodiment, the observation field of view is set to 2 mm × 2 mm, in order to ensure a sufficient number of inclusions to be measured and to suppress the variation in the measurement results. In other words, the field of view size is not limited to the above range as long as the variation in the measurement results can be suppressed. However, when changing the field of view size, it is desirable to set the field of view size so that 100 or more inclusions are present, from the viewpoint of suppressing the variation in the measurement results and obtaining stable measurement data.

[0054] As described above, the non-heat treated steel of this embodiment is a raw material (steel material) before parts processing (machining), such as steel to be subjected to hot processing (e.g., steel bar) or a crude material obtained by hot forging of a steel bar. In other words, the non-heat treated steel of this embodiment, such as a steel bar or a crude material, satisfies all of the above-mentioned regulations regarding the chemical composition, metal structure, and inclusions.

[0055] [Nitriding parts] Next, the nitrided part of this embodiment will be described. The nitrided part of this embodiment is a part obtained by machining and nitriding the non-heat treated steel of this embodiment, and includes a base material and a nitrided layer. The base material has the same chemical composition as the non-heat treated steel described above. The nitrided layer is formed on the surface layer of the base material. The nitrided layer includes a compound layer and a diffusion layer. The compound layer is formed on the outermost layer of the nitrided layer. The diffusion layer is formed under the compound layer.

[0056] Here, the base material is a portion that was not penetrated by nitrogen during nitriding, i.e., a region where there is no change in chemical composition and metal structure or where the change is negligible despite the nitriding treatment, and has the same composition as the non-tempered steel that is the base material of the part. The composition of the base material can also be said to be the composition at a depth of 2.0 mm from the surface of the part, for example. The nitride layer refers to the area where nitrogen has penetrated due to nitriding. In other words, the nitride layer is the area where the chemical composition or metal structure has changed due to the influence of nitriding. For example, it refers to the area from the surface of the part to a depth of about 1.0 mm.

[0057] The nitrided parts manufactured by the well-known nitriding process using the non-heat treated steel of this embodiment have sufficient fatigue strength and high yield strength.

[0058] [Manufacturing method] An example of a method for manufacturing the non-heat treated steel and nitrided parts of this embodiment will be described. The manufacturing method of the nitrided parts of this embodiment includes a steel material preparation step for manufacturing the non-heat treated steel, a molding step, and a machining step. Each step will be described below. However, the manufacturing method of the non-heat treated steel and the nitrided parts of this embodiment is not limited to the following aspects.

[0059] [Steel material preparation process] In the steel material preparation process, non-tempered steel that will be the material for the nitrided parts is manufactured. First, molten steel that satisfies the chemical composition of the steel and the composition of the inclusions of this embodiment is produced. Any method may be used to produce the steel material as long as the chemical components of the steel and the average composition of the oxide-based composite inclusions are within the above ranges. Here, as one example, a method is described in which an ingot is melted in a vacuum and a steel bar is produced as non-tempered steel.

[0060] First, the raw materials for steel, electrolytic iron and graphite, are heated and melted. After that, appropriate amounts of alloying elements other than Ca and Ti are added to the molten steel, taking into account the yield, so that the chemical composition falls within the above range.

[0061] Next, metallic Ti is added to the molten steel, and then a SiCa alloy is added to incorporate Ca. After the SiCa alloy is added and held for 200 seconds or more, the steel is cast into a mold. Since Ca floats to the surface as an inclusion after being added to the molten steel and is then removed, it is necessary to add more Ca to the molten steel than is ultimately required. The holding time after adding the SiCa alloy is an important condition for controlling the CT / AS in oxide-based compound inclusions.

[0062] The ingot may be produced by any method as long as the composition of the oxide-based composite inclusions falls within the specified range. For example, instead of shortening the holding time after the addition of SiCa, a mixed flux with an adjusted composition may be added, or the composition of the slag produced during secondary refining in the converter process may be adjusted and then continuously cast.

[0063] The ingot is then heated, hot worked (rolled, forged, etc.) under typical conditions, and cooled to produce steel bars. The hot working may be hot rolling or hot forging (hot forging and stretching, etc.). The heating temperature may be so-called "hot". The heating temperature is, for example, 1000°C or more and 1300°C or less. The cooling method after the hot working is not particularly limited. Preferably, the cooling rate after the hot working is in the range of a cooling rate that is likely to obtain a structure mainly composed of pro-eutectoid ferrite and pearlite, for example, air cooling or fan cooling. After the hot working, it is not necessary to perform a refining heat treatment such as quenching and tempering. With the steel composition of this embodiment, a ferrite + pearlite structure can be obtained by cooling to room temperature after the hot working. The non-heat treated steel of this embodiment can be manufactured by the above steps.

[0064] Next, the steel bar is machined to form a desired part shape. At this time, the steel bar may be machined directly, or, as in the forming process described below, the steel bar may be roughly formed by hot forging to form a rough shaped material, and then machined.

[0065] [Molding process] When the steel bar is roughly formed before machining, the produced steel bar is hot forged to form a raw material for nitrided parts. After being formed into a raw material for nitrided parts by hot forging, it is preferable to cool it by air cooling or fan cooling in the same manner as above. Note that the metal structure and the above CT / AS do not change in the processes after hot working, so the metal structure and the above CT / AS of the obtained raw material are almost the same.

[0066] [Machining process] The steel bar or the blank for nitrided parts after the forming process is machined to have a desired part shape. Examples of the machining for forming the desired part shape include cutting and grinding.

[0067] [Nitriding] The machined parts are subjected to nitriding. The nitriding can be performed by well-known methods such as gas nitriding, gas soft nitriding, salt bath soft nitriding, and plasma nitriding. The gas used in the nitriding can be only NH3, or a mixed gas containing NH3, N2, H2, CO2, and various hydrocarbons. The cooling after nitriding can be performed by any method such as water cooling, oil cooling, and furnace cooling. Through the above steps, nitrided parts are manufactured.

[0068] The non-heat treated steel produced by the above manufacturing process has a sufficiently low hardness and can suppress tool wear during machining. In addition, the non-heat treated steel of this embodiment has a high yield strength, so it is less likely to suffer from scratches or dents and can obtain the necessary fatigue strength. Therefore, the non-heat treated steel of this embodiment is suitable as a material for machine structural parts for automobiles, industrial machines, etc.

[0069] The nitrided parts produced by the above manufacturing process have low hardness and small hardness variation, making cutting costs low, and have sufficient fatigue strength and high yield strength for parts subjected to moderate loads. EXAMPLES

[0070] The present invention will be described in more detail below with reference to examples, but the present invention is not limited to these examples in any way.

[0071] Using a vacuum melting furnace, 50 kg ingots of steels A to R having the chemical compositions shown in Table 1 were produced. Specifically, electrolytic iron and graphite were first melted by induction heating. After that, appropriate amounts of alloy elements other than Ca and Ti were added to the molten steel in consideration of the yield so that the target chemical composition would be obtained. Next, metal Ti was added, and then an appropriate amount of SiCa alloy wire was added. As shown in the "holding time" in Table 2, steels A to G and I to P were cast into a mold to produce ingots after adding SiCa alloy and holding for 200 seconds. Steels H, Q, and R were cast into ingots after adding SiCa alloy and holding for 600 seconds, 5 seconds, and 30 seconds, respectively. In addition, among the chemical compositions shown in Table 1, "<0.01" and "-" for Cu, Ni, V, and Mo indicate that the corresponding element content is below the detection limit.

[0072] Next, each of the obtained ingots was heated for 4 hours at 1250° C. The heated ingots were forged into square bars with sides of 75 mm, and then allowed to cool to room temperature. To simulate hot forging of parts, the square bars after cooling were heated again to 1250℃, forged into steel bars with a diameter of 60 mm, and cooled to room temperature while blowing air on them with a fan. This forging corresponds to the above-mentioned forming process, and simulates the forming of the raw material before processing into the shape of the parts.

[0073] <Evaluation> From near the midpoint of the line segment connecting the center and the surface of the cross section perpendicular to the longitudinal direction of the obtained steel bar, an Ono-type rotating bending fatigue test piece (parallel part: diameter 8 mm, length 22 mm) as shown in Figure 1, a tensile test piece (parallel part: diameter 6 mm, length 32 mm) as shown in Figure 2, and a cubic test piece with one side of approximately 10 mm were taken for characterization. The numbers in Figures 1 and 2 indicate the dimensions (mm) of each part of the test piece.

[0074] (yield strength) The prepared tensile test pieces were used to measure the yield strength YP (MPa) in a tensile test at room temperature (approximately 25°C) and at a tensile speed of 1.5 mm / min in accordance with JIS Z 2241: 2011. When the ratio of yield strength YP to hardness HV, an index of machinability (YP / HV), was 2.20 or more, the yield strength was determined to be excellent.

[0075] (Fatigue strength) Using the prepared rotating bending fatigue test specimen, an Ono-type rotating bending fatigue test was carried out at room temperature (approximately 25°C) and a rotation speed of 3000 rpm. The number of repeated stress loads was 1.0 x 10 7 The highest stress (maximum stress) of the test piece that did not break after 1000 cycles was defined as the fatigue strength σw (MPa) for that test number. When the ratio of fatigue strength σw to hardness HV, an index of machinability (σw / HV), was 1.55 or more, the fatigue strength was determined to be excellent.

[0076] (Hardness) The test pieces for the validation study were embedded in resin and mirror-polished. The Vickers hardness (HV) was measured near the center of the test surface of the test piece after mirror polishing. The test load was 9.8N, and the measurement was performed five times, and the arithmetic average value was taken as the hardness of the test material.

[0077] (Oxide-based composite inclusions) The specimens for the characterization after the hardness measurement were subjected to measurement by an energy dispersive X-ray spectrometer (EDS) in a scanning electron microscope (SEM). The observation field was set to 2 mm x 2 mm, and all oxide-based inclusions within the field of view that had a diameter of 1.0 μm or more when the cross-sectional area was converted into a circle were subjected to EDS analysis, and the CT / AS value was calculated from the results. This CT / AS value does not change with heat treatment at 1300 ° C or less, and specifically, even if the hot forging treatment or nitriding treatment disclosed in this embodiment is performed, it does not change before and after the treatment.

[0078] (Tool wear (machinability)) Test pieces measuring φ35 x 200 mm were made from the obtained steel bars and subjected to cutting tests using a lathe. The cutting speed was 250 m / min, the feed rate was 0.20 mm / rev, and the cutting depth was 1.5 mm. Without lubrication, a P20 type carbide tool was used under dry conditions to measure the wear amount (μm) of the flank of the tool after machining 2000 m. When the wear amount was 200.0 μm or less, it was determined that the material had excellent machinability.

[0079] The measurement results of each test are shown in Table 2. The holding time in the table is the holding time from adding the SiCa alloy to the molten steel until the start of casting into the mold. In test numbers 1 to 8, tool wear was suppressed to 200 μm or less, the ratio of yield strength to hardness (YP / HV) was high at 2.20 or more, which was excellent in handleability, and the ratio of fatigue strength to hardness (σw / HV) was 1.55 or more, which was excellent in fatigue properties. On the other hand, in test numbers 9 to 18, which are comparative examples, the target properties were not obtained.

[0080] [Table 1]

[0081] [Table 2]

[0082] (nitrided parts) In addition, the steel bars of the invention, which showed good properties in Table 2, were subjected to the following additional evaluation to confirm whether they could be applied to nitriding treatment.

[0083] An Ono-type rotating bending fatigue test specimen was taken from near the midpoint of the line segment connecting the center and the surface of the cross section perpendicular to the longitudinal direction of the above-mentioned φ60 steel bar, as shown in Figure 3. The parallel part had a diameter of 10 mm, a length of 22 mm, and a circular notch (notch base: φ8) with a notch radius R of 3 mm and a depth of 1 mm.

[0084] Next, the fatigue test piece was held at 590°C for 2 hours, and then subjected to a soft nitriding treatment in which it was cooled in oil. The soft nitriding treatment was performed while flowing a mixed gas in which ammonia and RX gas were mixed in a ratio of 1:1. The test piece after the soft nitriding treatment was subjected to an Ono-type rotating bending fatigue test at a rotation speed of 3000 rpm. 1.0×10 7 The maximum stress was regarded as the fatigue strength of the test piece that did not break after the load was applied. In addition, to take stress concentration into account, the evaluation value was calculated by multiplying the nominal stress of the fatigue strength obtained by the load application by a stress concentration factor. The obtained fatigue strength (nominal stress) and evaluation values ​​are shown in Table 3.

[0085] In all test numbers, the evaluation value was approximately 1.5 to 2 times higher than the fatigue strength σw (Table 2) of the unnitrided steel bar. These results confirmed that the invention examples had good properties even after the non-heat treated steel was nitrided to produce nitrided parts.

[0086] [Table 3] [Industrial Applicability]

[0087] The present invention can be used in a wide range of industrial fields as a material for machine structural parts for automobiles, industrial machines, and the like.

Claims

1. In mass percent, C: 0.30-0.50%, Si: 0.05-0.35%, Mn: 0.45-1.00%, P: 0.080% or less, S: 0.035-0.100%, Cu: 0.25% or less, Ni: 0.25% or less, Cr: 0.03-0.25%, Al: 0.020% or less, N: 0.0125-0.0250%, Ti: 0.005-0.030%, Ca: 0.0003-0.0100%, V: 0 to 0.02%, and Mo: 0-0.03% with the remainder being Fe and impurities, The amount of solute N Nsol represented by the following formula (1) is 0.008% or more, In the metal structure, the area ratio of pro-eutectoid ferrite is 20% or more, and the remaining structure is pearlite, A non-tempered steel characterized in that, among oxide-based inclusions, the sum of the weight concentrations of Al and Si is 10% or more, the ratio CT, which is the sum of the weight concentrations of Ca and Ti, to AS, which is the sum of the weight concentrations of Al and Si, is 0.50 or more. Nsol=N-Ti / 3.4... (1) However, each element symbol in the above formula (1) represents the content of the corresponding element in mass %.

2. A base material made of the non-heat treated steel according to claim 1; A nitrided part, comprising a nitrided layer formed on a surface layer of the base material, the nitrided layer being composed of a compound layer and a diffusion layer.

3. 3. The nitrided part according to claim 2, characterized in that said nitrided part is a machine structural part.

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