Machine Structural Steel Excellent in Machinability and Strength Properties

Information

  • Patent Application
  • 20090274573
  • Publication Number
    20090274573
  • Date Filed
    December 25, 2007
    16 years ago
  • Date Published
    November 05, 2009
    14 years ago
Abstract
The invention provides a machine structural steel excellent in machinability and strength properties that has good machinability over a broad range of machining speeds and also has high impact properties and high yield ratio, which machine structural steel comprises, in mass %, C: 0.1 to 0.85%, Si: 0.01 to 1.5%, Mn: 0.05 to 2.0%, P: 0.005 to 0.2%, S: 0.001 to 0.15%, total Al: greater than 0.05% and not greater than 0.3%, Sb: less than 0.0150% (including 0%), and total N: 0.0035 to 0.020%, solute N being limited to 0.0020% or less, and a balance of Fe and unavoidable impurities.
Description
FIELD OF THE INVENTION

This invention relates to a machine structural steel that is to be machined and particularly to a machine structural steel excellent in machinability and strength properties that is amenable to machining over a broad spectrum of machining speeds ranging from relatively low-speed machining with a high-speed steel drill to relatively high speed machining such as longitudinal turning with a super-steel coated tool.


DESCRIPTION OF THE RELATED ART

Although recent years have seen the development of steels of higher strength, there has concurrently emerged a problem of declining machinability. An increasing need is therefore felt for the development of steels that maintain excellent strength without experiencing a decline in machining performance. Addition of machinability-enhancing elements such as S, Pb and Bi is known to be effective for improving steel machinability. However, while Pb and Bi are known to improve machinability and to have relatively little effect on forgeability, they are also known to degrade strength properties.


Moreover, Pb is being used in smaller quantities these days owing to the tendency to avoid use because of concern about the load Pb puts on the natural environment. S improves machinability by forming inclusions, such as MnS, that soften in a machining environment, but MnS grains are larger than the those of Pb and the like, so that it readily becomes a stress concentration raiser. Of particular note is that at the time of elongation by forging or rolling, MnS produces anisotropy, which makes the steel extremely weak in a particular direction. It also becomes necessary to take such anisotropy into account during steel design. When S is added, therefore, it becomes necessary to utilize a technique for reducing the anisotropy.


As pointed out in the foregoing, it has been difficult to achieve good strength properties and good machinability simultaneously because addition of machinability-enhancing elements degrades the strength properties. Further technological innovation is therefore needed to enable simultaneous realization of satisfactory steel machinability and strength properties.


This situation has led to efforts to provide a machine structural steel enabling prolongation of machine tool life by, for example, incorporating a total of 0.005 mass % or greater of at least one member selected from among solute V, solute Nb and solute Al, and further incorporating 0.001% or greater of solute N, thereby enabling nitrides formed by machining heat during machining to adhere to the tool to function as a tool protective coating (see Japanese Patent Publication (A) No. 2004-107787). In addition, there has been proposed a machine structural steel that achieve improved shavings disposal and mechanical properties by defining C, Si, Mn, S and Mg contents, defining the ratio of Mg content to S content, and optimizing the aspect ratio and number of sulfide inclusions in the steel (see Japanese Patent No. 3706560). The machine structural steel taught by Patent No. 3706560 defines the content of Mg as 0.02% or less (not including 0%) and the content of Al, when included, as 0.1% or less.


SUMMARY OF THE INVENTION

However, the foregoing existing technologies have the following drawbacks. The steel taught by Japanese Patent Publication (A) No. 2004-107787 is liable not to give rise to the aforesaid phenomenon unless the amount of heat produced by the machining exceeds a certain level. The machining speed must therefore be somewhat high to realize the desired effect, so the invention has a problem in the point that the effect cannot be anticipated in the low speed range. Japanese Patent No. 3706560 is totally silent regarding the strength properties of the steel it teaches. Moreover, the steel of this patent is incapable of achieving adequate strength properties because it gives no consideration to machine tool life or yield ratio.


The present invention was achieved in light of the foregoing problems and has as its object to provide a machine structural steel that has good machinability over a broad range of machining speeds and also has high impact properties and high yield ratio.


The machine structural steel excellent in machinability and strength properties according to the present invention comprises, in mass %, C, 0.1 to 0.85%, Si: 0.01 to 1.5%, Mn: 0.05 to 2.0%, P: 0.005 to 0.2%, S: 0.001 to 0.15%, total Al: greater than 0.05% and not greater than 0.3%, Sb: less than 0.0150% (including 0%), and total N, 0.0035 to 0.020%, solute N being limited to 0.0020% or less, and a balance of Fe and unavoidable impurities.


The machine structural steel can further comprise, in mass %, Ca: 0.0003 to 0.0015%.


The machine structural steel can further comprise, in mass %, one or more elements selected from the group consisting of Ti: 0.001 to 0.1%, Nb: 0.005 to 0.2%, W: 0.01 to 1.0%, and V: 0.01 to 1.0%.


The machine structural steel can further comprise, in mass %, one or more elements selected from the group consisting of Mg: 0.0001 to 0.0040%, Zr: 0.0003 to 0.01%, and REMs: 0.0001 to 0.015%.


The machine structural steel can further comprise, in mass %, one or more elements selected from the group consisting of Sn: 0.005 to 2.0%, Zn: 0.0005 to 0.5%, B: 0.0005 to 0.015%, Te: 0.0003 to 0.2%, Bi: 0.005 to 0.5%, and Pb: 0.005 to 0.5%.


The machine structural steel can further comprise, in mass %, one or two elements selected from the group consisting of Cr: 0.01 to 2.0% and Mo: 0.01 to 1.0%.


The machine structural steel can further comprise, in mass %, one or two elements selected from the group consisting of Ni: 0.05 to 2.0% and Cu: 0.01 to 2.0%.





BRIEF DESCRIPTION OF THE DRAWINGS


FIG. 1 is a diagram showing a region from which a Charpy impact test piece was cut.





DETAILED DESCRIPTION OF THE INVENTION

Preferred embodiments of the present invention are explained in detail in the following. The machine structural steel excellent in machinability and strength properties according to the present invention achieves the foregoing object by providing a machine structural steel wherein solute N acting to degrade machinability and impact properties is minimized by adjusting the amounts of added N and nitride-forming elements such as Al, wherein effective cutting performance is established with respect to a broad cutting speed range extending from low to high speed by ensuring presence of suitable amounts of solute Al serving to improve high-temperature embrittlement property and machinability, and Sb serving to produce a matrix embrittlement effect, and forming a crystal structure exhibiting high-temperature embrittlement effect and cleavage, thereby ensuring an appropriate amount of AlN serving to improve machinability, and wherein high impact properties are also realized by increasing Al addition so that at the slab stage segregation is made smaller and MnS of highly uniform dispersibility (type III MnS by SIMS analysis) is made more abundant than in conventional Al-killed steel. Moreover, the steel further achieves a high yield ratio owing to fine precipitation of AlN and presence of solute Al.


Specifically, the machine structural steel according to the present invention comprises, in mass %, C, 0.1 to 0.85%, Si: 0.01 to 1.5%, Mn: 0.05 to 2.0%, P: 0.005 to 0.2%, S: 0.001 to 0.15%, total Al: greater than 0.05% and not greater than 0.3%, Sb: less than 0.0150% (including 0%), and total N, 0.0035 to 0.020%, solute N being limited to 0.0020% or less, and a balance of Fe and unavoidable impurities.


The individual elements constituting the machine structural steel of the present invention and the contents thereof of will first be explained. In the ensuing explanation, percentage composition by mass of the steel components is denoted simply by the symbol %. C, 0.1 to 0.85%


C has a major effect on the fundamental strength of the steel. When the C content is less than 0.1%, adequate strength cannot be achieved, so that large amounts of other alloying elements must be incorporated. When C content exceeds 0.85%, machinability declines markedly because carbon concentration becomes nearly hypereutectoid to produce heavy precipitation of hard carbides. In order to achieve sufficient strength, the present invention therefore defines C content as 0.1 to 0.85%. The preferred lower limit of C content is 0.2%. Si: 0.01 to 1.5%


Si is generally added as a deoxidizing element but also contributes to ferrite strengthening and temper-softening resistance. When Si content is less than 0.01%, the deoxidizing effect is insufficient. On the other hand, an Si content in excess of 1.5% degrades the steel's embrittlement and other properties and also impairs machinability. Si content is therefore defined as 0.01 to 1.5%. The preferred upper limit of Si content is 1.0%.


Mn: 0.05 to 2.0%

Mn is required for its ability to fix and disperse sulfur (S) in the steel in the form of MnS and also, by dissolving into the matrix, to improve hardenability and ensure good strength after quenching. When Mn content is less than 0.05%, the steel is embrittled because S therein combines with Fe to form FeS. When Mn content is high, specifically when it exceeds 2.0%, base metal hardness increases to degrade cold workability, while its strength and hardenability improving effects saturates. Mn content is therefore defined as 0.05 to 2.0%.


P: 0.005 to 0.2%

P has a favorable effect on machinability but the effect is not obtained at a P content of less than 0.005%. When P content is high, specifically when it exceeds 0.2%, base metal hardness increases to degrade not only cold workability but also hot workability and casting properties. P content is therefore defined as 0.005 to 0.2%,


S: 0.001 to 0.15%

S combines with Mn to produce MnS that is present in the steel in the form of inclusions. MnS improves machinability but S must be added to a content of 0.001% or greater for achieving this effect to a substantial degree. When S content exceeds 0.15%, the impact value of the steel declines markedly. In the case of adding S to improve machinability, therefore, the S content is made 0.001 to 0.15%.


Total Al: Greater than 0.05% and not Greater than 0.3%


Al not only forms oxides but also promotes precipitation of AlN, which contributes to grain size control and machinability, and further improves machinability by passing into solid solution. Al must be added to a content of greater than 0.05% in order to form solute Al in an amount sufficient to enhance machinability. Al also affects the form of MnS grains/precipitation. Moreover, when Al is added in an amount exceeding 0.05%, segregation at the slab stage can be made smaller and MnS of highly uniform dispersibility (type III MnS by SIMS analysis) be made more abundant than in a conventional Al-killed steel. This makes it possible to obtain a machine structural steel also having high impact properties and further to achieve a high yield ratio owing to fine precipitation of AlN and the presence of solute Al. However, machinability starts to decline when total Al content exceeds 0.3%. Total Al content is therefore defined as greater than 0.05% and not greater than 0.3%. The lower limit of total Al content is preferably 0.08% and more preferably 0.1%.


Sb: Less than 0.0150% (Including 0%)


Sb improves machinability by suitably embrittling ferrite. This effect of Sb is pronounced particularly when solute Al content is high but is not observed when Sb content is less than 0.0005%. When Sb content is high, specifically when it reaches 0.0150% or greater, Sb macro-segregation becomes excessive, so that the impact value of the steel declines markedly. Sb content is therefore defined as 0.0005% or greater and less than 0.0150%. When high machinability is not required or total Al is greater than 0.1%, addition of Sb can be omitted (Sb content of 0%).


Total N, 0.0035 to 0.020%

N, which is present not only as solute N but also in nitrides of Ti, Al V and the like, suppresses austenite grain growth. However, no substantial effect is obtained at a total N content of less than 0.0035%. When total N content exceeds 0.020%, it leads to the occurrence of roll marks during rolling. Total N content is therefore defined as 0.0035 to 0.020%.


Solute N, 0.0020% or Less

Solute N hardens the steel. Of particular concern is that it shortens cutting tool life by causing steel near the cutting edge to harden under dynamic strain aging. It also causes occurrence of roll marks during rolling. High solute N content, specifically a content in excess of 0.0020%, aggravates tool wear during cutting because cutting resistance rises due to increased local hardness. Solute N content is therefore held to 0.0020% or less. This helps to reduce tool wear. Moreover, high solute N content also degrades impact properties by causing matrix embrittlement, but such matrix embrittlement can also be mitigated by holding solute N content to 0.0020% or less. Solute N content as termed here means the value obtained by subtracting the N content of AlN, NbN, TiN, VN and other such nitrides from total N content. It can be calculated, for example, in accordance with Equation (1) shown below, using the total N content determined by the inert gas fusion thermal conductivity method and the N content of nitrides determined by SPEED (Selective Potentiostatic Etching by Electrolytic Dissolution) analysis and indophenol absorbency analysis of residue electrolytically extracted using a 0.1 μm filter.





(Solute N content)=(Total N content)−(Nitride N content)  (1)


Solute N content can be lowered by the methods explained below:


1) Hold total N content to a low level within the range defined by the present invention. Although total N is defined as 0.020% or less, it is preferably held to 0.01% or less and more preferably to 0.006% or less.


2) When total N content is high, it is helpful to increase the amount of N compounds by adding suitable amounts of Al, a nitride-forming element, as well as other nitride-forming elements.


3) Solute N reduction by fine precipitation of nitrides is preferable in a machine structural steel from the viewpoint of inhibiting grain coarsening. Taking into account that reduction of solute N content by fine precipitation of nitrides requires holding at a high temperature enabling more complete solution treatment into N and nitride-forming element content, solution heat treatment is conducted at a temperature of 1100° C. or greater, preferably 1200° C. or greater, and more preferably 1250° C. or greater, whereafter precipitation is performed by conducting a heat treatment such as normalizing or carburization. Of particular note is that in the case of AlN, solute N can be reduced by utilizing prolonged retention near 850° C. to increase precipitation. By “prolonged” here is meant 0.8 hr or greater, preferably 1 hr or greater and more preferably 1.2 hr or greater.


The machine structural steel of the present invention can contain Ca in addition to the foregoing components.


Ca: 0.0003 to 0.0015%

Ca is a deoxidizing element that forms oxides in the steel. In the machine structural steel of the present invention, which has a total Al content of greater than 0.05% and not greater than 0.3%, Ca forms calcium aluminate (CaOAl2O3). As CaOAl2O3 is an oxide having a lower melting point than Al2O3, it improves machinability by constituting a tool protective film during high-speed cutting However, this machinability-improving effect is not observed when the Ca content is less than 0.0003%. When Ca content exceeds 0.0015%, CaS forms in the steel, so that machinability is instead degraded. Therefore, when Ca is added, its content is defined as 0.0003 to 0.0015%.


When the machine structural steel of the present invention needs to be given high strength by forming carbides, it can include in addition to the foregoing components one or more elements selected from the group consisting of Ti: 0.001 to 0.1%, Nb: 0.005 to 0.2%, W: 0.01 to 1.0%, and V: 0.01 to 1.0%. Ti: 0.001 to 0.1%


Ti forms carbonitrides that inhibit austenite grain growth and contribute to strengthening. It is used as a grain size control element for preventing grain coarsening in steels requiring high strength and steels requiring low distortion. Ti is also a deoxidizing element that improves machinability by forming soft oxides. However, these effects of Ti are not observed at a content of less than 0.001%, and when the content exceeds 0.1%, Ti has the contrary effect of degrading mechanical properties by causing precipitation of insoluble coarse carbonitrides that cause hot cracking. Therefore, when Ti is added, its content is defined as 0.001 to 0.1%.


Nb: 0.005 to 0.2%

Nb also forms carbonitrides. As such, it is an element that contributes to steel strength through secondary precipitation hardening and to austenite grain growth inhibition and strengthening. Ti is therefore used as a grain size control element for preventing grain coarsening in steels requiring high strength and steels requiring low distortion. However, no high strength imparting effect is observed at an Nb content of less than 0.005%, and when Nb is added to a content exceeding 0.2%, it has the contrary effect of degrading mechanical properties by causing precipitation of insoluble coarse carbonitrides that cause hot cracking. Therefore, when Nb is added, its content is defined as 0.005 to 0.2%.


W: 0.01 to 1.0%

W is also an element that forms carbonitrides and can strengthen the steel through secondary precipitation hardening. However, no high strength imparting effect is observed when W content is less than 0.01%, Addition of W in excess of 1.0% has the contrary effect of degrading mechanical properties by causing precipitation of insoluble coarse carbonitrides that cause hot cracking. Therefore, when W is added, its content is defined as 0.01 to 1.0%.


V: 0.01 to 1.0%.

V is also an element that forms carbonitrides and can strengthen the steel through secondary precipitation hardening. It is suitably added to steels requiring high strength. However, no high strength imparting effect is observed when V content is less than 0.01%, Addition of V in excess of 1.0% has the contrary effect of degrading mechanical properties by causing precipitation of insoluble coarse carbonitrides that cause hot cracking. Therefore, when V is added, its content is defined as 0.01 to 1.0%.


When the machine structural steel of the present invention is subjected to deoxidization control for controlling sulfide morphology, it can comprise in addition to the foregoing components one or more elements selected from the group consisting of Mg: 0.0001 to 0.0040%, Zr: 0.0003 to 0.01%, and REMs: 0.0001 to 0.015%.


Mg: 0.0001 to 0.0040%

Mg is a deoxidizing element that forms oxides in the steel. When Al deoxidization is adopted, Mg reforms Al2O3, which impairs machinability, into relatively soft and finely dispersed MgO and Al2O3—Mg. Moreover, its oxide readily acts as a precipitation nucleus of MnS and thus works to finely disperse MnS. However, these effects are not observed at an Mg content of less than 0.0001%. Moreover, while Mg acts to make MnS spherical by forming a metal-sulfide complex therewith, excessive Mg addition, specifically addition to a content of greater than 0.0040%, degrades machinability by promoting simple MgS formation. Therefore, when Mg is added, its content is defined as to 0.0001 to 0.0040%.


Zr: 0.0003 to 0.01%.

Zr is a deoxidizing element that forms an oxide in the steel. The oxide is thought to be ZrO2, which acts as a precipitation nucleus for MnS. Since addition of Zr therefore increases the number of MnS precipitation sites, it has the effect of uniformly dispersing MnS. Moreover, Zr dissolves into MnS to form a metal-sulfide complex therewith, thus decreasing MnS deformation, and therefore also works to inhibit MnS grain elongation during rolling and hot forging. In this manner, Zr effectively reduces anisotropy. But no substantial effect in these respects is observed at a Zr content of less than 0.0003%. On the other hand, addition of Zr in excess of 0.01% radically degrades yield. Moreover, by causing formation of large quantities of ZrO2, ZrS and other hard compounds, it has the contrary effect of degrading mechanical properties such as machinability, impact value, fatigue properties and the like. Therefore, when Zr is added, its content is defined as to 0.0003 to 0.01%.


REMs: 0.0001 to 0.015%

REMs (rare earth metals) are deoxidizing elements that form low-melting-point oxides that help to prevent nozzle clogging during casting and also dissolve into or combine with MnS to decrease MnS deformation, thereby acting to inhibit MnS shape elongation during rolling and hot forging. REMs thus serve to reduce anisotropy. However, this effect does not appear at an REM content of less than 0.0001%. When the content exceeds 0.015%, machinability is degraded owing to the formation of large amounts of REM sulfides. Therefore, when REMs are added, their content is defined as 0.0001 to 0.015%.


When the machine structural steel of the present invention is to be improved in machinability, it can include in addition to the foregoing components one or more elements selected from the group consisting of Sn: 0.005 to 2.0%, Zn: 0.0005 to 0.5%, B: 0.0005 to 0.015%, Te: 0.0003 to 0.2%, Bi: 0.005 to 0.5%, and Pb: 0.005 to 0.5%.


Sn: 0.005 to 2.0%

Sn extends tool life by embrittling ferrite and also improves surface roughness. These effects are not observed when the Sn content is less than 0.005%, and the effects saturate when Sn is added in excess of 2.0%. Therefore, when Sn is added, its content is defined as 0.005 to 2.0%.


Zn: 0.0005 to 0.5%

Zn extends tool life by embrittling ferrite and also improves surface roughness. These effects are not observed when the Zn content is less than 0.0005%, and the effects saturate when Zn is added in excess of 0.5%. Therefore, when Zn is added, its content is defined as 0.0005 to 0.5%.


B: 0.0005 to 0.015%

B, when in solid solution, has a favorable effect on grain boundary strength and hardenability. When it precipitates, it precipitates as BN and therefore helps to improve machinability. These effects are not notable at a B content of less than 0.0005%. When B is added to a content of greater than 0.015%, the effects saturate and mechanical properties are to the contrary degraded owing to excessive precipitation of BN. Therefore, when B is added, its content is defined as 0.0005 to 0.015%.


Te: 0.0003 to 0.2%

Te improves machinability. It also forms MnTe and, when co-present with MnS, decreases MnS deformation, thereby acting to inhibit MnS shape elongation. Te is thus an element effective for reducing anisotropy. These effects are not observed when Te content is less than 0.0003%, and when the content thereof exceeds 0.2%, the effects saturate and hot rolling ductility declines, increasing the likelihood of flaws. Therefore, when Te is added, its content is defined as: 0.0003 to 0.2%.


Bi: 0.005 to 0.5%

Bi improves machinability. This effect is not observed when Bi content is less than 0.005%. When it exceeds 0.5%, machinability improvement saturates and hot rolling ductility declines, increasing the likelihood of flaws. Therefore, when Bi is added, its content is defined as 0.005 to 0.5%.


Pb: 0.005 to 0.5%

Pb improves machinability. This effect is not observed when Pb content is less than 0.005%. When it exceeds 0.5%, machinability improvement saturates and hot rolling ductility declines, increasing the likelihood of flaws. Therefore, when Pb is added, its content is defined as 0.005 to 0.5%.


When the machine structural steel of the present invention is to be imparted with strength by improving its hardenability and/or temper-softening resistance, it can include in addition to the foregoing components one or two elements selected from the group consisting of Cr: 0.01 to 2.0% and Mo: 0.01 to 1.0%.


Cr: 0.01 to 2.0%

Cr improves hardenability and also imparts temper-softening resistance. It is therefore added to a steel requiring high strength. These effects are not obtained at a Cr content of less than 0.01%. When Cr content is high, specifically when it exceeds 2.0%, the steel is embrittled owing to formation of Cr carbides. Therefore, when Cr is added, its content is defined as 0.01 to 2.0%.


Mo: 0.01 to 1.0%

Mo imparts temper-softening resistance and also improves hardenability. It is therefore added to a steel requiring high strength. These effects are not obtained at an Mo content of less than 0.01%. When Mo is added in excess of 1.0%, its effects saturate. Therefore, when Mo is added, its content is defined as 0.01 to 1.0%.


When the machine structural steel of the present invention is to be subjected to ferrite strengthening, it can include in addition to the foregoing components one or two elements selected from the group consisting of Ni: 0.05 to 2.0% and Cu: 0.01 to 2.0%.


Ni: 0.05 to 2.0%

Ni strengthens ferrite, thereby improving ductility, and is also effective for hardenability improvement and anticorrosion improvement. These effects are not observed an Ni content of less than 0.05%. When Ni is added in excess of 2.0%, mechanical property improving effect saturates and machinability is degraded. Therefore, when Ni is added, its content is defined as 0.05 to 2.0%.


Cu: 0.01 to 2.0%

Cu strengthens ferrite and is also effective for hardenability improvement and anticorrosion improvement. These effects are not observed a Cui content of less than 0.01%. When Cu is added in excess of 2.0%, mechanical property improving effect saturates. Therefore, when Cu is added, its content is defined as 0.01 to 2.0%. A particular concern regarding Cu is that its effect of lowering hot rollability may lead to occurrence of flaws during rolling. Cu is therefore preferably added simultaneously with Ni.


As explained in the foregoing, the machine structural steel of the present invention is minimized in solute N content and therefore achieves better machinability and impact properties than conventional machine structural steels. Moreover, total Al content and Sb content are controlled to suitable levels to ensure presence of proper amounts of solute Al, Sb and AlN serving to improve machinability, thereby establishing effective cutting performance with respect to a broad cutting speed range extending from low to high speed. The steel also achieves a high yield ratio owing to fine precipitation of the AlN and presence of solute Al. In addition, excellent impact properties are realized by appropriately regulating the contents of elements affecting MnS precipitation so as to obtain an abundance of MnS of highly uniform dispersibility.


The machine structural steel excellent in machinability and strength properties according to the present invention can be produced by hot-forging a billet having the aforesaid steel composition into a bar at a temperature of 1200° C. or greater, subjecting the bar to solution heat treatment at a temperature of 1100° C. or greater, and then to a heat treatment such as normalizing or carburization. Of particular note is that in the case of a steel containing the carbide AlN, a machine structural steel markedly reduced in solute N can be obtained by prolonged retention following the solution heat treatment at 1100° C. or greater for 0.8 hr or greater, preferably 1 hr or greater, and more preferably 1.2 hr or greater.


EXAMPLES
First Set of Examples

The effects of the present invention will now be specifically explained giving Examples and Comparative Examples. In this set of Examples, steels of the compositions shown in Table 1 and Table 2, 150 kg each, were produced in a vacuum furnace, hot-forged under a temperature condition of 1250° C., and elongation-forged into 65-mm diameter bars. The properties of the Example and Comparative Example steels were evaluated by subjecting them to machinability testing, Charpy impact testing and tensile testing by the methods set out below. In Table 2, underlining indicates a value outside the invention range.











TABLE 1









Composition (mass %)






















No.
C
Si
Mn
P
S
Cr
V
Sb
Ca
Ttl Al
Ttl N
Sol N
Other

























In-
1
0.42
0.19
0.80
0.014
0.022


0.0100
0.0012
0.110
0.0052
0.0012



vention
2
0.40
0.25
0.76
0.012
0.034


0.0089
0.0008
0.051
0.0060
0.0013


Exam-
3
0.41
0.24
0.76
0.013
0.038

0.1
0.0086

0.051
0.0060
0.0013


ples
4
0.40
0.23
0.78
0.015
0.038


0.0067

0.052
0.0045
0.0014



5
0.43
0.23
0.75
0.011
0.022


0.0087

0.060
0.0049
0.0012
Mg: 0.0020



6
0.43
0.20
0.77
0.013
0.039


0.0074

0.051
0.0065
0.0013
Ti: 0.04



7
0.44
0.20
0.78
0.012
0.040


0.0068

0.052
0.0075
0.0016
Nb: 0.02



8
0.41
0.21
0.77
0.011
0.047


0.0083

0.090
0.0058
0.0014
W: 0.2



9
0.45
0.22
0.79
0.012
0.045


0.0058

0.080
0.0055
0.0013
Ni: 0.2



10
0.43
0.23
0.71
0.011
0.051


0.0071

0.110
0.0045
0.0017
Cu: 0.5



11
0.44
0.22
0.72
0.014
0.041


0.0087

0.053
0.0052
0.0010
Sn: 0.05



12
0.45
0.20
0.74
0.010
0.033


0.0069

0.070
0.0051
0.0014
Zn: 0.007



13
0.43
0.24
0.76
0.015
0.041


0.0077

0.090
0.0053
0.0019
B: 0.002



14
0.45
0.22
0.71
0.011
0.043


0.0073

0.080
0.0046
0.0015
Te: 0.002



15
0.43
0.19
0.74
0.011
0.051
1.0

0.0051

0.090
0.0047
0.0016



16
0.44
0.21
0.72
0.013
0.023
0.1

0.0085

0.070
0.0048
0.0013



17
0.42
0.21
0.73
0.012
0.048


0.0088

0.110
0.0071
0.0010
Ti: 0.03, Mg: 0.0025



18
0.41
0.20
0.72
0.012
0.035


0.0059

0.090
0.0075
0.0011
Ti: 0.04, Zn: 0.004



19
0.42
0.24
0.74
0.013
0.040
1.0

0.0083

0.060
0.0071
0.0012
Ti: 0.03



20
0.44
0.23
0.75
0.010
0.034


0.0089

0.110
0.0077
0.0015
Ti: 0.03, Cu: 0.3



21
0.40
0.20
0.71
0.010
0.037


0.0074

0.110
0.0054
0.0010
Ti: 0.02, Mg: 0.0025, Sn: 0.04



22
0.42
0.21
0.73
0.012
0.053
1.1

0.0098

0.110
0.0074
0.0019
Ti: 0.03, Mg: 0.0025



23
0.43
0.21
0.77
0.014
0.052


0.0071

0.070
0.0062
0.0019
Ti: 0.03, Mg: 0.0025, Cu: 0.4



24
0.41
0.19
0.74
0.013
0.054
1.0

0.0076

0.100
0.0061
0.0015
Ti: 0.02, Mg: 0.0025, Sn: 0.04



25
0.43
0.23
0.71
0.014
0.021


0.0058

0.060
0.0060
0.0012
Ti: 0.03, Mg: 0.0025, Sn: 0.04, Cu: 0.3



26
0.43
0.25
0.76
0.013
0.024
1.0

0.0085

0.070
0.0074
0.0010
Ti: 0.03, Mg: 0.0025, Cu: 0.4



27
0.45
0.23
0.72
0.015
0.034
1.0

0.0086

0.100
0.0055
0.0012
Ti: 0.03, Sn: 0.04



28
0.41
0.19
0.78
0.011
0.025


0.0087

0.080
0.0061
0.0016
Ti: 0.03, Sn: 0.04. Cu: 0.3



29
0.41
0.21
0.70
0.015
0.025
0.9

0.0057

0.051
0.0062
0.0017
Ti: 0.04, Sn: 0.04. Cu: 0.3



30
0.44
0.23
0.71
0.012
0.036
1.0

0.0052

0.060
6.0056
0.0012
Ti: 0.03, Cu: 0.3


















TABLE 2









Composition (mass %)






















No.
C
Si
Mn
P
S
Cr
V
Sb
Ca
Ttl Al
Ttl N
Sol N
Other

























Examples
31
0.44
0.20
0.77
0.014
0.055


0.0081

0.110
0.0047
0.0010
Mg: 0.0025, Zn: 0.003



32
0.45
0.21
0.79
0.011
0.029
1.0

0.0099

0.060
0.0049
0.0013
Mg: 0.0019, Zn: 0.003



33
0.43
0.21
0.74
0.010
0.038


0.0078

0.110
0.0048
0.0014
Mg: 0.0022, Ca: 0.3



34
0.42
0.25
0.77
0.011
0.036
1.0

0.0087

0.090
0.0046
0.0014
Mg: 0.0020, Sn: 0.04



35
0.44
0.25
0.78
0.015
0.055


0.0079

0.100
0.0050
0.0018
Mg: 0.0025, Sn: 0.04, Cu: 0.1



36
0.42
0.19
0.74
0.013
0.022
1.0

0.0062

0.052
0.0047
0.0019
Mg: 0.0021, Sn: 0.02, Cu: 0.1



37
0.41
0.19
0.77
0.010
0.025
1.1

0.0050

0.110
0.0049
0.0019
Mg: 0.0029, Cu: 0.1



38
0.43
0.20
0.79
0.011
0.020
1.0

0.0060

0.060
0.0049
0.0010
Sn: 0.04



39
0.42
0.23
0.80
0.015
0.048


0.0086

0.070
0.0046
0.0016
Sn: 0.03, Cu: 0.1



40
0.41
0.19
0.78
0.010
0.042
1.0

0.0069

0.100
0.0046
0.0009
Sn: 0.04, Cu: 0.1



41
0.43
0.21
0.79
0.010
0.035
0.9

0.0080

0.080
0.0046
0.0014
Cu: 0.2



42
0.44
0.19
0.77
0.013
0.042


0.0087

0.060
0.0055
0.0014
Nb: 0.01, Mg: 0.0026, Sn: 0.04, Ca: 0.3


Comparative
43
0.45
0.24
0.78
0.010
0.025


0.0069


0.025

0.0052
0.0018


Examples
44
0.43
0.25
0.76
0.010
0.041


0.0092


0.035

0.0051
0.0019



45
0.41
0.24
0.73
0.011
0.035


0.0098


0.040

0.0053
0.0017



46
0.44
0.25
0.78
0.014
0.022


0.0059


0.030

0.0034
0.0019



47
0.41
0.24
0.72
0.011
0.051


0.0087


0.003

0.0049

0.0034




48
0.44
0.25
0.77
0.015
0.052


0.0062


0.358

0.0062
0.0011



49
0.41
0.21
0.72
0.013
0.021


0.0055

0.103
0.0058

0.0025




50
0.42
0.20
0.73
0.013
0.037


0.0077

0.153
0.0057

0.0026




51
0.44
0.24
0.79
0.013
0.038



0.0157


0.067
0.0054
0.0016



52
0.45
0.23
0.76
0.010
0.036



0.0175


0.103
0.0049
0.0010



53
0.44
0.19
0.73
0.014
0.044



0.0211


0.243
0.0046
0.0016



54
0.45
0.19
0.71
0.010
0.025



0.0223


0.060
0.0046
0.0009









Machinability Test

Machinability testing was conducted with respect to Example and Comparative Example steels that had been elongation-forged under heating at 1250° C. by first subjecting them to heat treatment consisting of normalization under temperature condition of 850° C. for 1 hr, 0.5 hr in the case of Comparative Examples No. 49 and No. 50, followed by air-cooling. A machinability evaluation test piece was then cut from each heat-treated steel and the machinabilities of the Example and Comparative Example steels were evaluated by conducting drill boring testing under the cutting conditions shown in Table 3 and to longitudinal turning testing under the conditions shown in Table 4. The maximum cutting speed VL1000 enabling cutting up to a cumulative hole depth of 1000 mm was used as the evaluation index in the drill boring test, and the maximum width VB_max of wear of the relief flank after 10 min was used as the evaluation index in the longitudinal turning test.












TABLE 3









Cutting
Speed: 10-120 m/min



conditions
Feed: 0.25 mm/rev




Cutting fluid: Water-soluble




cutting oil



Drill
Drill diameter: 3 mm




NACHI ordinary drill




Overhang: 45 mm



Other
Hole depth: 9 mm




Tool life: Until breakage




















TABLE 4









Cutting
Cutting speed: 250 m/min



conditions
Feed: 0.3 mm/rev




Depth of cut: 1.5 mm




Dry cutting



Tool
Holder: PTGNR2525M16




Tool shape: TNMG160408N-




UZ




Material: AC2000










Charpy Impact Test


FIG. 1 is a diagram showing a region from which a Charpy impact test piece was cut. In the Charpy impact test, first, as shown in FIG. 1, a cylinder 2 measuring 25 mm in diameter was cut from a steel 1 heat-treated by the same method and under the same conditions as the aforesaid machinability test piece so that its axis was perpendicular to the elongation-forging direction of the steel 1. Next, the cylinder 2 was held under temperature condition of 850° C. for 1 hr, 0.5 hr in the case of Comparative Examples No. 49 and No. 50, then oil-quenched by cooling to 60° C., and further subjected to tempering with water cooling in which it was held under temperature condition of 550° C. for 30 min. Next, the cylinder 2 was machined to fabricate a Charpy test piece 3 in conformance with JIS Z 2202, which was subjected to a Charpy impact test at room temperature in accordance with the method prescribed by JIS Z 2242. Absorbed energy per unit area (J/cm2) was adopted as the evaluation index.


Tensile Test

A cylinder 2 sampled parallel to the elongation-forging direction was oil-quenched and tempered by the same methods and under the same conditions as in the aforesaid Charpy impact test, whereafter it was processed into a tensile test piece measuring 8 mm in parallel section diameter and 30 mm in parallel section length, and then tensile tested at room temperature in accordance with the method prescribed by JIS Z 2241. Yield ratio (=(0.2% proof stress YP)/(tensile strength TS) was adopted as the evaluation index.


The results of the foregoing tests are shown in Tables 5 and 6.















TABLE 5










Impact





VL1000
VB_max
value



No.
(m/min)
(μm)
(J/cm2)
YP/TS





















Examples
1
87
118
27
0.85



2
89
119
22
0.83



3
85
124
20
0.89



4
88
126
25
0.82



5
85
125
20
0.84



6
89
123
21
0.86



7
89
128
22
0.83



8
92
129
22
0.86



9
89
126
20
0.86



10
92
122
21
0.82



11
91
121
21
0.83



12
87
130
22
0.84



13
90
127
22
0.82



14
90
125
21
0.84



15
90
125
24
0.86



16
85
121
26
0.87



17
93
128
24
0.86



18
86
124
22
0.85



19
90
128
25
0.86



20
89
126
20
0.82



21
89
121
24
0.84



22
96
125
21
0.82



23
93
129
22
0.83



24
94
126
23
0.82



25
82
126
26
0.82



26
86
120
25
0.84



27
89
130
26
0.85



28
86
127
20
0.86



29
83
129
20
0.84



30
86
122
24
0.86



31
95
129
26
0.86



32
89
130
22
0.83



33
89
123
21
0.87



34
90
126
24
0.85



35
94
121
22
0.82



36
83
127
20
0.85



37
83
121
20
0.85



38
82
127
30
0.83



39
93
127
21
0.83



40
90
124
27
0.86



41
89
127
23
0.84



42
91
126
21
0.87






















TABLE 6










Impact





VL1000
VB_max
value



No.
(m/min)
(μm)
(J/cm2)
YP/TS





















Comparative
43

54


149

21

0.68



Examples
44

62


141

24

0.66




45

60


142

25

0.67




46

53


158

22

0.68




47

64


178

9

0.65




48

48


178

22
0.82



49

62


149


16

0.83



50

69


150


15

0.85



51
99
122

14

0.85



52
98
124

11

0.87



53
104 
128

12

0.84



54
100 
128

13

0.85









The Steels No. 1 to No. 42 shown in Tables 1, 2 and 5 are Examples of the present invention, and the steels No. 43 to No. 51 shown in Tables 2 and 6 are Comparative Example steels. As shown in Tables 5 and 6, the steels of Examples No 1 to No. 42 exhibited good values for all of the evaluation indexes, namely VL1000, VB_max, impact value (absorbed energy), and YP/TS (yield ratio), but the steels of the Comparative Examples were each inferior to the Example steels in at least one of the properties. Specifically, the steels of Comparative Examples No. 43 to No. 46 had total Al contents below the range of the present invention and were therefore inferior to the Example steels in machinability evaluation index VL1000 and yield ratio (YP/TS). Moreover, the steel of Comparative Example No. 47 had a total Al content far below the range of the present invention, so that its solute N content was above the range of the present invention, and the steel was therefore inferior to the steels of the Examples in machinability (VL1000, VB_max), impact value, and yield ratio (YP/TS).


The steel of Comparative Example No. 48 had a total Al content above the range of the present invention, so that its hardness increased, and the steel was therefore inferior in machinability (VL1000, VB_max). The steels of Comparative Examples No. 49 and No. 50 were maintained at 850° C., the temperature at which AlN readily precipitates, for a shorter holding time than the steels of the Examples, so that their solute N contents were above the range of the present invention, and the steels were therefore inferior to the steels of the Examples in machinability (VL1000, VB_max) and impact value. The steels of Comparative Examples No. 51 to No. 54 had Sb contents above the range of the present invention and were therefore inferior to the steels of the Examples in impact value.


Second Set of Examples

In this set of Examples, steels of the compositions shown in Table 7 and Table 8, 150 kg each, were produced in a vacuum furnace, hot-forged under a temperature condition of 1250° C., and elongation-forged into 65 mm diameter bars. The properties of the Example and Comparative Example steels were evaluated by subjecting them to machinability testing, Charpy impact testing and tensile testing by the methods set out below. In Tables 7 and 8, underlining indicates a value outside the invention range.











TABLE 7









Composition (mass %)




















No
C
Si
Mn
P
S
Cr
Ca
Ttl Al
Ttl N
Sol N
Other























Examples
1
0.44
0.25
0.76
0.015
0.017

0.0000
0.121
0.0052
0.0012




2
0.44
0.26
0.76
0.015
0.012

0.0006
0.101
0.0052
0.0012



3
0.44
0.25
0.75
0.016
0.010

0.0008
0.250
0.0060
0.0013



4
0.44
0.25
0.76
0.015
0.008

0.0010
0.075
0.0045
0.0011



5
0.46
0.26
0.76
0.015
0.013

0.0006
0.099
0.0049
0.0012
Mg: 0.0020



6
0.44
0.24
0.74
0.015
0.011

0.0008
0.193
0.0065
0.0013
Ti: 0.04



7
0.45
0.25
0.74
0.015
0.013

0.0008
0.178
0.0075
0.0016
Nb: 0.02



8
0.44
0.24
0.74
0.015
0.011

0.0006
0.169
0.0058
0.0014
W: 0.2



9
0.45
0.24
0.74
0.016
0.010

0.0012
0.175
0.0055
0.0013
Ni: 0.2



10
0.46
0.26
0.76
0.015
0.014

0.0005
0.142
0.0045
0.0017
Cu: 0.5



11
0.44
0.26
0.75
0.015
0.015

0.0007
0.127
0.0052
0.0010
Sn: 0.05



12
0.44
0.25
0.76
0.015
0.011

0.0004
0.147
0.0051
0.0014
Zn: 0.007



13
0.45
0.24
0.76
0.014
0.011

0.0012
0.144
0.0053
0.0019
B: 0.002



14
0.45
0.26
0.75
0.015
0.011

0.0012
0.187
0.0046
0.0015
Te: 0.002



15
0.41
0.24
0.78
0.015
0.014
1.0
0.0010
0.108
0.0047
0.0016



16
0.44
0.25
0.76
0.015
0.013
0.1
0.0012
0.112
0.0048
0.0013



17
0.44
0.24
0.74
0.015
0.010

0.0006
0.131
0.0071
0.0010
Ti: 0.03, Mg: 0.0025



18
0.45
0.26
0.75
0.016
0.010

0.0009
0.109
0.0075
0.0010
Ti: 0.04, Zn: 0.004



19
0.41
0.24
0.75
0.016
0.010
1.0
0.0008
0.168
0.0071
0.0012
Ti: 0.03



20
0.44
0.26
0.74
0.016
0.010

0.0011
0.113
0.0077
0.0015
Ti: 0.03, Cu: 0.3



21
0.44
0.24
0.75
0.016
0.014

0.0008
0.104
0.0054
0.0010
Ti: 0.02, Mg: 0.0025, Sn: 0.04



22
0.41
0.25
0.75
0.015
0.010
1.1
0.0005
0.192
0.0074
0.0019
Ti: 0.03, Mg: 0.0025



23
0.45
0.24
0.75
0.015
0.013

0.0009
0.119
0.0062
0.0019
Ti: 0.03, Mg: 0.0025, Cu: 0.4



24
0.40
0..26
0.75
0.015
0.012
1.0
0.0005
0.198
0.0061
0.0015
Ti: 0.02, Mg: 0.0025, Sn: 0.04



25
0.44
0.26
0.75
0.014
0.015

0.0008
0.169
0.0060
0.0012
Ti: 0.03, Mg: 0.0025, Sn: 0.04,














Cu: 0.3



26
0.42
0.24
0.75
0.014
0.013
1.0
0.0011
0.116
0.0074
0.0010
Ti: 0.03, Mg: 0.0025, Cu: 0.4



27
0.41
0.24
0.74
0.015
0.014
1.0
0.0004
0.198
0.0055
0.0012
Ti: 0.03, Sn: 0.04



28
0.46
0.25
0.75
0.015
0.010

0.0010
0.179
0.0061
0.0016
Ti: 0.03, Sn: 0.04, Cu: 0.3



29
0.41
0.25
0.75
0.016
0.011
0.9
0.0008
0.156
0.0062
0.0017
Ti: 0.04, Sn: 0.04, Cu: 0.3



30
0.41
0.26
0.75
0.014
0.012
1.0
0.0009
0.137
0.0056
0.0012
Ti: 0.03, Cu: 0.3



31
0.45
0.24
0.75
0.015
0.013

0.0013
0.109
0.0047
0.0010
Mg: 0.0025, Zn: 0.003



32
0.41
0.25
0.76
0.016
0.015
1.0
0.0011
0.104
0.0049
0.0013
Mg: 0.0019, Zn: 0.003



33
0.45
0.24
0.75
0.015
0.011

0.0013
0.109
0.0048
0.0014
Mg: 0.0022, Cu:: 0.3



34
0.40
0.25
0.75
0.016
0.015
1.0
0.0008
0.105
0.0046
0.0014
Mg: 0.0020, Sn: 0.04



35
0.45
0.24
0.74
0.015
0.014

0.0009
0.110
0.0050
0.0018
Mg: 0.0025, Sn: 0.04, Cu: 0.1



36
0.42
0.25
0.75
0.014
0.012
1.0
0.0012
0.107
0.0047
0.0019
Mg: 0.0021, Sn: 0.02, Cu: 0.1



37
0.41
0.24
0.75
0.015
0.014
1.1
0.0005
0.104
0.0049
0.0019
Mg: 0.0029, Cu:: 0.1



38
0.42
0.25
0.76
0.015
0.011
1.0
0.0009
0.102
0.0049
0.0010
Sn: 0.04



39
0.44
0.24
0.76
0.015
0.012

0.0010
0.110
0.0046
0.0016
Sn: 0.03, Cu: 0.1



40
0.41
0.25
0.75
0.015
0.011
1.0
0.0009
0.108
0.0046
0.0009
Sn: 0.04, Cu: 0.1



41
0.41
0.25
0.75
0.015
0.011
0.9
0.0003
0.102
0.0046
0.0014
Cu: 0.2



42
0.46
0.25
0.76
0.015
0.011

0.0003
0.102
0.0055
0.0014
Nb: 0.01, Mg: 0.0026, Sn: 0.04,














Cu: 0.3


Comparative
43
0.44
0.24
0.76
0.014
0.011

0.0006
0.025
0.0052
0.0018


Examples
44
0.45
0.25
0.76
0.015
0.014

0.0006
0.035
0.0051
0.0019



45
0.45
0.24
0.75
0.015
0.014

0.0008
0.040
0.0053
0.0017



46
0.45
0.25
0.76
0.014
0.011

0.0010
0.030
0.0034
0.0019



47
0.46
0.25
0.74
0.016
0.011

0.0008
0.003
0.0043
0.0034



48
0.44
0.24
0.75
0.014
0.009

0.0007
0.103
0.0058
0.0025


















TABLE 8









Composition (mass %)




















No
C
Si
Mn
P
S
Cr
Ca
Ttl Al
Ttl N
Sol N
Other























Examples
52
0.45
0.26
0.75
0.016
0.025

0.0002
0.101
0.0052
0.0012




53
0.44
0.25
0.76
0.015
0.030

0.0000
0.250
0.0060
0.0013



54
0.45
0.25
0.74
0.015
0.042

0.0001
0.123
0.0048
0.0012



55
0.45
0.24
0.75
0.015
0.090

0.0002
0.106
0.0049
0.0013



56
0.45
0.24
0.75
0.014
0.042

0.0001
0.102
0.0052
0.0011
Mg: 0.0020



57
0.45
0.24
0.74
0.015
0.042

0.0001
0.190
0.0065
0.0016
Ti: 0.04



58
0.46
0.25
0.76
0.016
0.047

0.0001
0.154
0.0075
0.0012
Nb: 0.02



59
0.45
0.25
0.74
0.015
0.044

0.0001
0.129
0.0058
0.0017
W: 0.2



60
0.44
0.25
0.76
0.015
0.044

0.0001
0.109
0.0055
0.0015
Ni: 0.2



61
0.45
0.26
0.74
0.016
0.041

0.0001
0.148
0.0045
0.0015
Cu: 0.5



62
0.46
0.25
0.75
0.016
0.047

0.0000
0.111
0.0052
0.0013
Sn: 0.03



63
0.46
0.25
0.75
0.015
0.051

0.0001
0.188
0.0051
0.0012
Zn: 0.007



64
0.45
0.24
0.76
0.015
0.073

0.0002
0.197
0.0053
0.0011
B: 0.002



65
0.44
0.25
0.75
0.015
0.092

0.0002
0.109
0.0046
0.0010
Te: 0.002



66
0.45
0.25
0.74
0.015
0.062

0.0000
0.200
0.0046
0.0011
Cr: 0.1



67
0.45
0.26
0.76
0.014
0.049

0.0001
0.109
0.0070
0.0012



68
0.45
0.26
0.76
0.016
0.040

0.0000
0.172
0.0072
0.0010
Ti: 0.03, Mg: 0.0025



69
0.45
0.25
0.75
0.014
0.040

0.0001
0.110
0.0068
0.0010
Ti: 0.04, Zn: 0.004



70
0.41
0.25
0.75
0.015
0.043
0.9
0.0000
0.125
0.0075
0.0009
Ti: 0.03



71
0.45
0.25
0.76
0.015
0.043

0.0002
0.110
0.0069
0.0009
Ti: 0.03, Cu: 0.3



72
0.45
0.24
0.76
0.015
0.047

0.0000
0.125
0.0062
0.0018
Ti: 0.03, Mg: 0.0015, Sn: 0.04



73
0.40
0.26
0.75
0.014
0.049
1.0
0.0001
0.142
0.0065
0.0017
Ti: 0.03, Mg: 0.0025



74
0.45
0.24
0.75
0.015
0.044

0.0001
0.149
0.0062
0.0017
Ti: 0.03, Mg: 0.0025, Cu: 0.4



75
0.41
0.26
0.76
0.016
0.041
1.0
0.0001
0.129
0.0059
0.0019
Ti: 0.05, Mg: 0.0025, Sn: 0.04



76
0.44
0.24
0.76
0.015
0.043

0.0001
0.188
0.0061
0.0014
Ti: 0.03, Mg: 0.0025,














Sn: 0.04, Cu: 0.3



77
0.40
0.26
0.75
0.016
0.046
0.9
0.0001
0.172
0.0064
0.0013
Ti: 0.03, Mg: 0.0025, Cu: 0.4



78
0.41
0.25
0.75
0.016
0.042
1.0
0.0000
0.111
0.0063
0.0013
Ti: 0.03, Sn: 0.04



79
0.46
0.25
0.76
0.015
0.047

0.0001
0.151
0.0067
0.0012
Ti: 0.03, Sn: 0.04, Cu: 0.3



80
0.40
0.26
0.76
0.016
0.043
0.9
0.0001
0.120
0.0072
0.0017
Ti: 0.02, Sn: 0.04, Cu: 0.3



81
0.41
0.26
0.74
0.015
0.046
1.1
0.0001
0.144
0.0069
0.0010
Ti: 0.03, Cu: 0.3



82
0.46
0.24
0.76
0.014
0.040

0.0001
0.105
0.0051
0.0010
Mg: 0.0028, Zn: 0.003



83
0.41
0.24
0.76
0.014
0.047
0.9
0.0000
0.102
0.0052
0.0013
Mg: 0.0019, Zn: 0.003



84
0.45
0.24
0.76
0.015
0.041

0.0001
0.102
0.0069
0.0011
Mg: 0.0022, Cu:: 0.3



85
0.41
0.26
0.75
0.016
0.041
1.0
0.0000
0.109
0.0055
0.0012
Mg: 0.0020, Sn: 0.04



86
0.44
0.25
0.76
0.016
0.047

0.0001
0.103
0.0062
0.0010
Mg: 0.0025, Sn: 0.04, Cu: 0.1



87
0.42
0.26
0.75
0.015
0.042
1.0
0.0001
0.101
0.0057
0.0011
Mg: 0.0017, Sn: 0.04, Cu: 0.1



88
0.41
0.25
0.75
0.015
0.046
1.1
0.0001
0.106
0.0067
0.0013
Mg: 0.0025, Cu:: 0.1



89
0.41
0.25
0.74
0.014
0.046
1.0
0.0000
0.109
0.0059
0.0016
Sn: 0.02



90
0.45
0.26
0.75
0.015
0.042

0.0001
0.100
0.0066
0.0013
Sn: 0.04, Cu: 0.1



91
0.41
0.24
0.74
0.015
0.046
1.1
0.0001
0.105
0.0065
0.0012
Sn: 0.04, Cu: 0.1



92
0.41
0.26
0.75
0.015
0.040
1.1
0.0000
0.109
0.0058
0.0014
Cu: 0.1



93
0.44
0.24
0.75
0.015
0.057

0.0001
0.101
0.0051
0.0017
Nb: 0.01, Mg: 0.0025,














Sn: 0.04, Cu: 0.3


Comparative
94
0.45
0.25
0.74
0.014
0.026

0.0001
0.025
0.0051
0.0017


Examples
95
0.45
0.24
0.75
0.014
0.043

0.0001
0.024
0.0052
0.0018



96
0.46
0.24
0.75
0.016
0.046

0.0002
0.032
0.0051
0.0019



97
0.46
0.24
0.76
0.015
0.046

0.0002
0.104
0.0078
0.0034



98
0.45
0.25
0.74
0.016
0.043

0.0001
0.103
0.0058
0.0025



99
0.44
0.26
0.76
0.016
0.051

0.0000
0.243
0.0057
0.0026



100
0.45
0.24
0.75
0.014
0.073

0.0001
0.111
0.0067
0.0031



101
0.46
0.25
0.75
0.014
0.099

0.0001
0.142
0.0077
0.0035









Machinability Test

Machinability testing was conducted with respect to Example and Comparative Example steels that had been elongation-forged under heating at 1250° C. by first subjecting them to heat treatment consisting of normalization under temperature condition of 850° C. for 1 hr, 0.5 hr in the case of Comparative Examples No. 48, No. 49 and No. 97 to No. 101, followed by air-cooling. A machinability evaluation test piece was then cut from each heat-treated steel and the machinabilities of the Example and Comparative Example steels were evaluated by conducting drill boring testing under the cutting conditions shown in Table 9 and to longitudinal turning testing under the conditions shown in Table 10. The maximum cutting speed VL1000 enabling cutting up to a cumulative hole depth of 1000 mm was used as the evaluation index in the drill boring test, and the maximum width VB_max of wear of the relief flank after 10 min was used as the evaluation index in the longitudinal turning test.













TABLE 9









Cutting
Speed
10-120 m/min



conditions
Feed
0.25 mm/rev




Cutting
Water-soluble




fluid
cutting oil



Drill
Drill
3 mm




diameter (φ)




NACHI
Ordinary drill




Overhang
45 mm



Other
Hole depth
9 mm




Tool life
Until breakage





















TABLE 10









Cutting
Cutting
250 m/min



conditions
speed




Feed
0.3 mm/rev




Mode
Dry cutting



Tool
Holder
PTGNR2525M16




Shape
TNMG160408N-UZ




Material
AC2000










Charpy Impact Test


FIG. 1 is a diagram showing a region from which a Charpy impact test piece was cut. In the Charpy impact test, first, as shown in FIG. 1, a cylinder 2 measuring 25 mm in diameter was cut from a steel 1 heat-treated by the same method and under the same conditions as the aforesaid machinability test piece so that its axis was normal to the elongation-forging direction of the steel 1. Next, the cylinder 2 was held under temperature condition of 850° C. for 1 hr, 0.5 hr in the case of Comparative Examples No. 48, No. 49 and No. 97 to No. 101, then oil-quenched by cooling to 60° C., and further subjected to tempering with water cooling in which it was held under temperature condition of 550° C. for 30 min. Next, the cylinder 2 was machined to fabricate a Charpy test piece 3 in conformance with JIS Z 2202, which was subjected to a Charpy impact test at room temperature in accordance with the method prescribed by JIS Z 2242. Absorbed energy per unit area (J/cm2) was adopted as the evaluation index.


Tensile Test

A cylinder 2 oil-quenched and tempered by the same methods and under the same conditions as in the aforesaid Charpy impact test was processed into a tensile test piece measuring 8 mm in parallel section diameter and 30 mm in parallel section length, and then tensile tested at room temperature in accordance with the method prescribed by JIS Z 2241. Yield ratio (=(0.2% proof stress YP)/(tensile strength TS) was adopted as the evaluation index.


The results of the foregoing tests are shown in Tables 11 and 12.















TABLE 11










Impact





VL1000
VB_max
value



No.
(m/min)
(μm)
(J/cm2)
YP/TS





















Examples
1
70
121
39
0.87



2
65
121
40
0.82



3
65
123
41
0.84



4
65
125
42
0.80



5
70
115
39
0.83



6
65
121
42
0.83



7
65
123
41
0.86



8
65
120
40
0.85



9
65
116
42
0.85



10
65
122
43
0.86



11
70
123
44
0.85



12
70
120
38
0.83



13
70
119
39
0.84



14
70
120
40
0.85



15
55
132
37
0.89



16
65
124
40
0.86



17
65
125
40
0.82



18
70
124
39
0.85



19
55
131
39
0.84



20
65
126
38
0.82



21
70
118
39
0.83



22
55
133
39
0.84



23
70
128
38
0.83



24
60
130
39
0.85



25
70
119
39
0.83



26
55
131
40
0.83



27
65
132
40
0.83



28
70
121
40
0.84



29
60
131
39
0.86



30
55
131
38
0.85



31
70
120
41
0.83



32
55
133
37
0.86



33
70
125
40
0.87



34
60
134
39
0.86



35
70
120
39
0.87



36
60
133
41
0.87



37
55
131
41
0.84



38
60
130
38
0.86



39
70
119
39
0.86



40
60
131
38
0.84



41
55
132
37
0.84



42
65
124
41
0.83


Comparative
43
45
122
41
0.66


Examples
44
45
116
40
0.67



45
45
117
41
0.67



46
50
110
42
0.67



47
35
156
22
0.68



48
50
149
30
0.87



49
50
140
29
0.85






















TABLE 12










Impact





VL1000
VB_max
value



No.
(m/min)
(μm)
(J/cm2)
YP/TS





















Examples
52
85
121
25
0.85



53
85
123
24
0.85



54
95
121
23
0.82



55
105
112
21
0.85



56
95
120
22
0.85



57
95
123
22
0.85



58
90
123
22
0.85



59
95
121
22
0.83



60
90
124
22
0.83



61
95
120
22
0.87



62
95
115
22
0.83



63
95
125
22
0.85



64
100
117
21
0.84



65
105
113
21
0.84



66
95
121
20
0.86



67
80
131
20
0.83



68
95
122
25
0.87



69
100
120
24
0.84



70
80
131
20
0.84



71
95
122
23
0.85



72
100
118
26
0.83



73
80
130
21
0.84



74
95
122
25
0.85



75
85
128
20
0.85



76
100
119
25
0.86



77
80
132
22
0.83



78
85
128
20
0.82



79
100
120
24
0.82



80
85
126
21
0.84



81
80
133
21
0.83



82
105
120
23
0.84



83
80
130
21
0.83



84
95
124
24
0.86



85
85
129
22
0.87



86
95
117
23
0.87



87
85
128
21
0.84



88
80
129
21
0.86



89
85
126
20
0.83



90
95
119
21
0.86



91
85
125
20
0.87



92
80
133
20
0.83



93
100
112
22
0.86


Comparative
94
60
180
22
0.68


Examples
95
65
179
20
0.69



96
65
174
19
0.68



97
70
157
18
0.84



98
75
149
18
0.82



99
70
143
18
0.86



100
75
152
15
0.79



101
75
163
12
0.86









The steels No. 1 in Tables 7 and 11 are embodiments of claim 1 and the steels No. 2 to No. 42 in the same tables are embodiments of claim 2. The steels No. 52 to No. 93 in Table 8 and Table 12 are embodiments of claim 1. The comparative steels No. 43 to No. 49 satisfy the S content and Ca content requirements of claim 2, and the comparative steels No. 94 to No. 101 satisfy the S content and Ca content requirements of claim 1.


As shown in Tables 11 and 12, the steels of Examples No 1 to No. 42 and No. 52 to No. 93 exhibited good values for all of the evaluation indexes, namely VL1000, VB_max, impact value (absorbed energy), and YP/TS (yield ratio), but the steels of the Comparative Examples were each inferior to the Example steels in at least one of the properties. Specifically, the steels of Comparative Examples No. 43 to No. 46 had total Al contents below the range of the present invention and were therefore inferior to the Example steels in machinability (VL1000) and yield ratio (YP/TS). Moreover, the steel of Comparative Example No. 47 had a total Al content below the range of the present invention, so that its solute N content was above the range of the present invention, and the steel was therefore inferior to the steels of the Examples in machinability (VL1000, VB_max), impact value, and yield ratio (YP/TS).


The steels of Comparative Examples No. 48 and No. 49 were maintained at 850° C., the temperature at which AlN readily precipitates, for a shorter holding time than the steels of the Examples, so that their solute N contents were above the range of the present invention, and the steels were therefore inferior to the steels of the Examples in machinability (VL1000, VB_max) and impact value. Moreover, the steels of Comparative Examples No. 94 to No. 96 had a total Al content below the range of the present invention and were therefore inferior to the steels of the Examples in machinability (VL1000, VB_max) and yield ratio (YP/TS). Further, the steels of Comparative Examples No. 97 to No. 101 were maintained at 850° C., the temperature at which AlN readily precipitates, for a shorter holding time than the steels of the Examples, so that their solute N contents were above the range of the present invention, and the steels were therefore inferior to the steels of the Examples in machinability (VL1000, VB_max) and impact value.


INDUSTRIAL APPLICABILITY

The present invention provides a machine structural steel that has good machinability over a broad range of machining speeds and also has high impact properties and high yield ratio.

Claims
  • 1. A machine structural steel excellent in machinability and strength properties comprising, in mass %: C, 0.1 to 0.85%,Si: 0.01 to 1.5%,Mn: 0.05 to 2.0%,P: 0.005 to 0.2%,S: 0.001 to 0.15%,total Al: greater than 0.05% and not greater than 0.3%,Sb: less than 0.0150% (including 0%), and total N, 0.0035 to 0.020%,solute N being limited to 0.0020% or less, and a balance of Fe and unavoidable impurities.
  • 2. A machine structural steel excellent in machinability and strength properties according to claim 1, further comprising, in mass %, one or more of Ca: 0.0003 to 0.0015%, Ti: 0.001 to 0.1%, Nb: 0.005 to 0.2%, W: 0.01 to 1.0%, V: 0.01 to 1.0%, Mg: 0.0001 to 0.0040%, Zr: 0.0003 to 0.01%, REMs: 0.0001 to 0.015%, Sn: 0.005 to 2.0%, Zn: 0.0005 to 0.5%, B: 0.0005 to 0.015%, Te: 0.0003 to 0.2%, Bi: 0.005 to 0.5%, Pb: 0.005 to 0.5%, Cr: 0.01 to 2.0%, Mo: 0.01 to 1.0%, Ni: 0.05 to 2.0% and Cu: 0.01 to 2.0%.
Priority Claims (1)
Number Date Country Kind
2006-347928 Dec 2006 JP national
PCT Information
Filing Document Filing Date Country Kind 371c Date
PCT/JP2007/075350 12/25/2007 WO 00 9/30/2008