STEEL FOR HIGH-SPEED COLD WORKING AND METHOD FOR PRODUCTION THEREOF, AND PART FORMED BY HIGH-SPEED COLD WORKING AND METHOD FOR PRODUCTION THEREOF

Information

  • Patent Application
  • 20080156403
  • Publication Number
    20080156403
  • Date Filed
    December 05, 2007
    16 years ago
  • Date Published
    July 03, 2008
    16 years ago
Abstract
Disclosed herein is a steel for high-speed cold working which exhibits good cold workability during working and also exhibits high hardness after working. The steel for high-speed cold working contains C: 0.03 to 0.6% (by mass), Si: 0.005 to 0.6%, Mn: 0.05 to 2%, P: no more than 0.05% (excluding 0%), S: no more than 0.05% (excluding 0%), and N: no more than 0.04% (excluding 0%), with the remainder being iron and inevitable impurities and the amount of dissolved nitrogen in the steel being no less than 0.006%.
Description
BACKGROUND OF THE INVENTION

1. Field of the Invention


The present invention relates to a steel for cold working to be made into machine parts, such as bolts and nuts, particularly automotive parts, said steel being particularly in the form of wire or rod suitable for cold working. The present invention also covers cold-worked parts made out of said steel for cold working.


2. Description of the Related Art


There has been an increasing demand for weight reduction of automotive parts from the view point of fuel economy and environmental protection. Weight reduction needs a high-strength steel, which is obtained usually by increasing the amount of alloying elements in iron.


Various kinds of parts are commonly produced by cold working (in an atmosphere at 200° C. or below) which surpasses hot and warm working in productivity, dimensional accuracy, and yields. High-speed cold working is prevailing for better productivity.


The situation mentioned above requires a steel for cold working which exhibits a low deformation resistance and keeps its deformability at the time of cold working. Any steel with a high deformation resistance leads to a reduced life of molds used for cold working, and any steel with poor deformability is liable to cracking at the time of cold working.


It is known that any steel decreases in deformation resistance and improves in deformability in proportion to the decreasing amounts of its alloying elements such as C, Si, and Mn. The decreased deformation resistance, which is achieved merely by reducing the amount of alloying elements, extends the mold life but adversely affects the strength of worked parts. The conventional way to address this problem, thereby assuring prescribed strength or hardness, was by heat treatment, such as annealing, that follows cold working to make steel into a desired shape.


Unfortunately, heat treatment following cold working brings about a dimensional change in worked parts, and this necessitates additional machining, such as cutting, to restore correct dimensions. It is desirable to ensure prescribed strength for worked parts without heat treatment and ensuing machining from the standpoint of improved productivity and energy saving.


Prior art technologies to address the foregoing problems include the following. Japanese Patent No. 3515923 discloses that a steel keeps a low deformation resistance during working if it has the metallographic structure such that ferrite grains contain fine nitride precipitates which function as nuclei for precipitation of C compounds such as cementite.


Japanese Patent Laid-open No. Sho-60-82618 discloses a steel exempt from age hardening due to dissolved C and dissolved N which contains N and dissolved Al, whose amounts are controlled such that N is fixed in the form of AlN, and which contains C compounds precipitating from C upon aging treatment.


The prior art technologies disclosed in the foregoing documents (Japanese Patent No. 3515923 and Japanese Patent Laid-open No. Sho-60-82618) involve the step of fixing dissolved N and dissolved C in the form of N compounds and C compounds in ferrite grains in order to suppress dynamic strain aging and keep deformation resistance low. The fixing of dissolved N requires incorporation with Al, which is an element to form N compounds. In the presence of 0.039-0.045% Al, as in Example, dissolved N is likely to be nearly absent even though the amount of N is 0.015%. Moreover, N compounds suppress precipitation hardening and prevent crystal grains from becoming coarse, and hence they are likely to increase deformation resistance by other factors than dynamic strain aging.


Japanese Patent Publication No. Sho-57-60416 discloses a method of decreasing deformation resistance at the time of cold working by incorporation with Cr (for solid-solution softening) and Al, thereby fixing dissolved N. This method, however, has the disadvantage that dissolved N is nearly absent (as in the case of technologies disclosed in Japanese Patent No. 3515923 and Japanese Patent Laid-open No. Sho-60-82618 mentioned above) because dissolved N is fixed in the form of N compounds by incorporation with Al. Moreover, N compounds suppress precipitation hardening and prevent crystal grains from becoming coarse, and hence they are likely to increase deformation resistance by other factors than dynamic strain aging, as in the case of the technologies disclosed in Japanese Patent No. 3515923 and Japanese Patent Laid-open No. Sho-60-82618 mentioned above.


Cold-worked parts usually undergo hardening heat treatment, such as quenching and tempering, so that they have prescribed strength. However, such heat treatment should preferably be omitted for improved productivity and energy saving.


For example, Japanese Patent Laid-open No. 2003-266144 discloses that the age hardening treatment (quenching and tempering) after cold working is not necessary if worked parts are cooled at a rate of 50-70° C./h from the temperature raised by cold working to the normal temperature.


OBJECT AND SUMMARY OF THE INVENTION

Workpieces for cold working should meet contradictory requirements—cold workability (deformation resistance and deformability) and strength after cold working. Workpieces with prescribed strength reduce the mold life and undergo cracking during working. By contrast, workpieces with improved cold workability (for better mold life) lacks strength. So far, there is no steel for cold working which meets the foregoing two requirements. It is an object of the present invention to provide a steel for cold working, particularly a steel wire and rod for cold working, which excels in cold workability during working and exhibits good strength after working.


The first aspect of the present invention is directed to a steel for high-speed cold working which contains:


C: 0.03 to 0.6% (by mass),


Si: 0.005 to 0.6%,
Mn: 0.05 to 2%,

P: no more than 0.05% (excluding 0%),


S: no more than 0.05% (excluding 0%), and


N: no more than 0.04% (excluding 0%).


with the remainder being iron and inevitable impurities and the amount of dissolved nitrogen in the steel being no less than 0.006%.


According to the present invention, the steel for cold working may contain C in an amount of 0.03 to 0.15% (in the first embodiment) or 0.15 to 0.6% (in the second embodiment) depending on application and performance required.


According to the basic embodiment and the first and second embodiments of the present invention, the content of N should preferably be no less than 0.007% so that the amount of dissolved N is no less than 0.006%.


According to the basic embodiment and the first and second embodiments of the present invention, the steel may additionally contain, when necessary, Al: no more than 0.1% (excluding 0%).


According to the basic embodiment and the first and second embodiments of the present invention, the steel may additionally contain, when necessary, at least one species selected from the group consisting of:


Zr: no more than 0.2% (excluding 0%),


Ti: no more than 0.1% (excluding 0%),


Nb: no more than 0.1% (excluding 0%),


V: no more than 0.5% (excluding 0%),


Ta: no more than 0.1% (excluding 0%), and


Hf: no more than 0.1% (excluding 0%).


According to the basic embodiment and the first and second embodiments of the present invention, the steel may additionally contain, when necessary, at least one species selected from the group consisting of:


B: no more than 0.0015% (excluding 0%) and/or


Cr: no more than 2% (excluding 0%).


The steel for high-speed cold working mentioned above should preferably satisfy the formula (1) below.





[N]−(14[Al]/27+14[Ti]/47.9+14[Nb]/92.9+14[V]/50.9+14[Zr]/91.2+14[B]/10.8+14[Ta]/180.9+14[Hf]/178.5)≧0.006  Formula (1)


where the square brackets [ ] represent the total amount (in mass %) of each element contained in the steel.


According to the third embodiment of the present invention, the inevitable impurities mentioned above may include:


Al: no more than 0.001% (including 0%),


Ti: no more than 0.002% (including 0%),


Nb: no more than 0.001% (including 0%),


V: no more than 0.001% (including 0%),


Zr: no more than 0.001% (including 0%),


B: no more than 0.0001% (including 0%),


Ta: no more than 0.0001% (including 0%), and


Hf: no more than 0.0001% (including 0%);


and also satisfy the formula (2) below.





14[Al]/27+14[Ti]/47.9+14[Nb]/92.9+14[V]/50.9+14[Zr]/91.2+14[B]/10.8+14[Ta]/180.9+14[Hf]/178.5≦0.002%  Formula (2)


where the square brackets [ ] represent the total amount (in mass %) of each element contained in the steel.


According to the third embodiment of the present invention, the steel may additionally contain:


Cr: no more than 2% (excluding 0%).


According to the present invention, the steel for high-speed cold working may additionally contain, when necessary:


Cu: no more than 5% (excluding 0%).


According to the present invention, the steel for high-speed cold working may additionally contain, when necessary:


Ni: no more than 5% (excluding 0%) and/or


Co: no more than 5% (excluding 0%).


According to the present invention, the steel for high-speed cold working may additionally contain, when necessary:


Mo: no more than 2% (excluding 0%) and/or


W: no more than 2% (excluding 0%).


According to the present invention, the steel for high-speed cold working may additionally contain, when necessary:


at least one species selected from the group consisting of


Ca: no more than 0.05% (excluding 0%),


Rare earth elements (REM): no more than 0.05% (excluding 0%),


Mg: no more than 0.02% (excluding 0%),


Li: no more than 0.02% (excluding 0%),


Pb: no more than 0.1% (excluding 0%), and


Bi: no more than 0.1% (excluding 0.1%).


According to the present invention, the steel for high-speed cold working should desirably be used for high-speed cold working at a working temperature no higher than 200° C. and at a strain rate no lower than 100/s.


Incidentally, the strain rate is defined as a ratio of true strain to unit time.


The present invention is also directed to a method for producing a steel for high-speed cold working, said method comprising subjecting the steel stock having the above-mentioned composition consecutively to heating at a temperature above Ac3 point plus 30° C., hot rolling at a temperature above Ac3 point plus 30° C., and quenching to 500° C. or below at a cooling rate no smaller than 0.5° C./s.


The present invention is also directed to a method for producing a steel for high-speed cold working, said method comprising subjecting the steel stock having the above-mentioned composition to heating at a temperature above Ac3 point plus 30° C. and subsequent quenching to 500° C. or below at a cooling rate no smaller than 0.5° C./s.


The present invention is also directed to a part formed from the above-mentioned steel for high-speed cold working by high-speed cold working at a working temperature no higher than 200° C. and at a strain rate no lower than 100/s, wherein said part has a value of H and a value of DR which satisfy the formula (3) below






H≧(DR+1000)/6  formula (3)


where H denotes the strength of part (in terms of Hv) after high-speed cold working and DR denotes the maximum value of deformation resistance (in terms of MPa) during high-speed cold working.


EFFECT OF THE INVENTION

According to the present invention, the steel for high-speed cold working offers the following advantages.


(a) Containing dissolved N in an amount more than a specific level, it imparts desired strength to cold-worked parts thereof despite the omission of heat treatment (such as quenching and tempering) that follows cold working.


(b) It is intended solely for high-speed cold working (preferably at a strain rate no smaller than 100/s).


(c) It has a specific chemical composition suitable for good cold working.







DESCRIPTION OF THE PREFERRED EMBODIMENTS

According to the present invention, the steel for high-speed cold working is characterized by containing dissolved N in an amount more than a specific level. Therefore, it is suitable for high-speed cold working and it imparts desired strength to cold-worked parts thereof. This fact is contrary to a common brief that a steel containing a large amount of dissolved N has a large deformation resistance, deteriorates the mold life, and causes cracking to cold-worked parts. The steel according to the present invention permits smooth cold working at high speeds. In other words, the steel according to the present invention is intended solely for high-speed cold working. The present invention is based on a new technical idea that the steel containing dissolved N in an amount more than a specific level provides cold-worked parts thereof having improved strength and permits smooth cold working without adverse effect of dissolved N when it undergoes high-speed cold working.


In addition, high-speed cold working contributes to parts productivity and energy saving.


<Chemical Composition of the Steel for High-Speed Cold Working (the Basic Embodiment of the Present Invention)>

According to the basic embodiment of the present invention, the steel for high-speed cold working is characterized by an adequate chemical composition for its good cold-workability. The following is concerned with the chemical composition of the steel and the amount of dissolved N in the steel.


(C: 0.03 to 0.6%)

C is an element essential for the steel to impart adequate strength to parts formed therefrom by high-speed cold working. The content of C is specified as being no less than 0.03%, preferably no less than 0.04%, more preferably no less than 0.05%. By contrast, an excess amount of C adversely affects machinability and cold-workability. Thus, the upper limit of the C content is specified as being 0.6%, preferably 0.5%, more preferably 0.4%.


(Si: 0.005 to 0.6%)

Si is an element which is used as a deoxidizer in the steel-making process. Insufficient Si leads to incomplete deoxidation and causes the steel to give off gas during solidification, and the resulting steel is poor in deformability. The amount necessary for Si to fully exhibit its effect is no less than 0.005%, with a preferable lower limit being 0.008% and a more preferable lower limit being 0.01%. However, excess Si does not produce additional deoxidizing effect but deteriorates cold workability. The upper limit of Si content should be 0.6%, preferably 0.5%.


(Mn: 0.05 to 2%)

Mn is an element which is used for deoxidization and desulfurization in the steel-making process. Insufficient Mn leads to incomplete desulfurization which causes FeS film to separate out in the grain boundary, thereby greatly decreasing grain boundary strength and deteriorating deformability. The amount necessary for Mn to fully exhibit its effect is no less than 0.05%, with a preferable lower limit being 0.1%, and a more preferable lower limit being 1%. However, excess Mn adversely affects cold workability. The upper limit of Mn content should be 2%, preferably 1.5%, more preferably 1%.


(P: no more than 0.05% (excluding 0%))


P is an element in inevitable impurities. When contained in ferrite, P segregates in the ferrite grain boundary, thereby deteriorating cold workability. In addition, P subjects ferrite to solid-solution hardening, thereby increasing deformation resistance. Therefore, the P content should be as low as possible from the standpoint of cold working. However, reducing the P content to an extreme leads to an increased steel making cost. With cold workability and process performance taken into account, the upper limit of P content is specified as being 0.05%, preferably 0.03%. It is industrially difficult to completely eliminate P, however.


(S: no more than 0.05% (excluding 0%))


S is an element in inevitable impurities. S forms MnS as an inclusion, thereby deteriorating deformability. Therefore, the Mn content should be as low as possible from the standpoint of deformability. With deformability taken into account, the upper limit of S content is specified as being 0.05%, preferably 0.03%. On the other hand, S effectively improves machinability and hence it is sometimes added to steel intentionally. With machinability taken into account, the S content should preferably be no less than 0.002%, more preferably no less than 0.006%.


(N: no more than 0.04% (excluding 0%))


The description in this paragraph is concerned with the total amount of N in the steel. N dissolves in steel to form solid solution, thereby improving the strength of cold-worked parts. It plays an important role in the present invention. An excess total amount of N in the steel leads to an excess amount of dissolved N, which would cause cracking at the time of cold working. Moreover, excess dissolved N tends to cause ingot internal defects and slab cracking during continuous casting. The upper limit of the total N content in the steel is specified as being 0.04%, preferably 0.03%, from the standpoint of steel deformability, material stability, and good yields in continuous casting. According to the basic embodiment of the present invention, the lower limit of total N content is specified; however, the total N content should preferably be no less than 0.007%, more preferably no less than 0.008%, and most desirably no less than 0.009%, so that the amount of dissolved N is more than the lower limit mentioned later.


(Dissolved N: No Less than 0.006%)


Dissolved N contributes to the strength of parts produced by high-speed cold working. For its maximum effect, dissolved N should be contained in an amount more than 0.006%, preferably 0.007%, more preferably 0.008%. On the other hand, excess dissolved N deteriorates deformability. Therefore, the amount of dissolved N should preferably be no more than 0.035%, more preferably 0.030%, most desirably 0.025%. Incidentally, the amount of dissolved N does not exceed the total amount of N in the steel as a matter of course. The value of “the amount of dissolved N” in the steel can be calculated by subtracting the total amount of N compounds from the total amount of N in the steel, according to JIS G1228.


(a) The total amount of N in the steel is determined by the inert gas fusion method combined with the heat conduction method. To be concrete, a specimen cut out of steel is placed in a crucible, which is subsequently heated in an inert gas stream so that N is liberated from the molten sample. The liberated N is transferred to a heat conduction cell for measurement of change in heat conduction.


(b) The total amount of N compounds in the steel is determined by indophenol blue absorptiometry that follows ammonia distillation separation. To be concrete, a specimen cut out of steel is electrolyzed with constant current in a 10% AA electrolyte, which is a non-aqueous electrolytic solution incapable of forming passive film on the steel surface (consisting of 10% acetylacetone and 10% tetramethylammonium chloride, with the remainder being methanol). Electrolysis is carried out to such an extent that about 0.5 g of specimen is dissolved. Insoluble residues (N compounds) are filtered out through a polycarbonate filter with a pore size of 0.1 μm. The separated insoluble residues are decomposed in hot sulfuric acid containing potassium sulfate and pure copper chips. The decomposition solution is combined with the filtrate. The resulting solution is rendered alkaline with sodium hydroxide. The alkaline solution undergoes steam distillation and distilled ammonia is absorbed in dilute sulfuric acid. The dilute sulfuric acid which has absorbed ammonia is given phenol, sodium hypochlorite, and sodium pentacyanonitrosylferrate (III) which form a blue complex. The amount of the blue complex is determined by absorptiometry with a photometer.


The amount of total N and the amount of total N compounds, which have been determined as mentioned above, give the amount of dissolved N in the steel from difference between them.


The steel according to the basic embodiment of the present invention has the fundamental chemical composition as mentioned above, with the remainder being essentially iron. It may contain inevitable impurities resulting from raw materials, subsidiary materials, and manufacturing equipment, as a matter of course. Also, it may optionally contain any of the following elements.


(Al: no more than 0.1% (excluding 0%))


Al is an element that essentially functions as a deoxidizer in the steel-making process. It is also effective for steel cracking resistance. The Al content, which varies according to need, should preferably be no less than 0.001%, more preferably no less than 0.005%. According to the basic embodiment of the present invention, the upper limit of the Al content is specified as being 0.1% because Al with a strong affinity with N forms AlN to decrease the amount of dissolved N in the steel. The Al content should preferably be no more than 0.05%, more preferably no more than 0.03%.


(At least one species selected from the group consisting of Zr: no more than 0.2% (excluding 0%), Ti: no more than 0.1% (excluding 0%), Nb: no more than 0.1% (excluding 0%), V: no more than 0.5% (excluding 0%), Ta: no more than 0.1% (excluding 0%), and Hf: no more than 0.1% (excluding 0%))


Any of Zr, Ti, Nb, V, Ta, and Hf combines with N to form N compounds, thereby making crystal grains fine and contributing to toughness of parts obtained by cold working. The steel according to the basic embodiment of the present invention may optionally contain these elements in an amount specified below.


Zr: no less than 0.002%, preferably no less than 0.004%,


Ti: no less than 0.001%, preferably no less than 0.002%,


Nb: no less than 0.001%, preferably no less than 0.002%,


V: no less than 0.001%, preferably no less than 0.002%,


Ta: no less than 0.003%, preferably no less than 0.006%, and


Hf: no less than 0.002%, preferably no less than 0.004%.


These elements also have such a strong affinity that they form N compounds, thereby decreasing the total amount of dissolved N. Consequently, the upper limit of their content is specified as follows according to the basic embodiment of the present invention.


Zr: 0.2%, preferably 0.1%, more preferably 0.05%, most desirably 0.03%;


Ti: 0.1%, preferably 0.05%, more preferably 0.03%;


Nb: 0.1%, preferably 0.06%, more preferably 0.04%;


V: 0.5%, preferably 0.2%, more preferably 0.1%, most desirably 0.05%, particularly 0.03%;


Ta: 0.1%, preferably 0.05%, more preferably 0.03%;


Hf: 0.1%, preferably 0.05%, more preferably 0.03%.


(B: no more than 0.0015% (excluding 0%))


B is an element that enhances the strength of grain boundaries, thereby improving the deformability of steel. Therefore, no less than 0.0001% B, preferably no less than 0.0002% B may optionally be contained in the steel according to the basic embodiment of the present invention. Unfortunately, B has a strong affinity with N and hence forms BN to decrease the amount of dissolved N, and excess B deteriorates cold workability. Therefore, the desirable B content according to the basic embodiment of the present invention is no more than 0.0015%, preferably no more than 0.001%, and more preferably no more than 0.0008%.


(Cr: no more than 2% (excluding 0%))


Cr, like B, improves the deformability of steel. Thus, no less than 0.1% Cr, preferably no less than 0.2% Cr, may optionally be contained in the steel. Unfortunately, excess Cr deteriorates deformability and deteriorates cold workability. Therefore, the Cr content should be no more than 2%, preferably no more than 1.5%, and more preferably no more than 1%.


(Cu: no more than 5% (excluding 0%))


Cu hardens steel through strain aging and hence improves the strength of parts after working. Therefore, no less than 0.1% Cu, preferably no less than 0.5% Cu, may optionally be contained in the steel. However, excess Cu is wasted without any additional effect and adversely affects cold workability and parts' surface state. The Cu content should be limited to 5%, preferably 4%, more preferably 3%, and most desirably 2%.


(Ni: no more than 5% (excluding 0%) and/or Co: no more than 5% (excluding 0%))


Ni effectively improves the deformability of ferrite-pearlite steel. It also effectively eliminates the surface defects of steel containing Cu. The Ni content should be no less than 0.1%, preferably no less than 0.5%. In other words, it should be equal to or more than 70% of the Cu content. Excess Ni (exceeding 5%) is wasted without any additional effect and detrimental to cold workability. The Ni content is limited to 5%, preferably 4%, more preferably 3%, and most desirably 2%.


Co, like Ni, effectively improves the deformability of ferrite-pearlite steel. The Co content should be no less than 0.1%, preferably no less than 0.5%. However, excess Co (exceeding 5%) deteriorates the grain boundary strength in the manufacturing steps, such as casting and rolling, thereby causing cracking. The Co content is limited to 5%, preferably 4%, more preferably 3%, and most desirably 2%.


(Mo: no more than 2% (excluding 0%) and/or W no more than 2% (excluding 0%))


Mo increases hardness after working and enhances deformability. The Mo content should be no less than 0.04%, preferably no less than 0.08%, and more preferably no less than 0.1%. However, Mo in excess of 2% deteriorates cold workability. Thus, the Mo content should be limited to 2%, preferably 1.5%, and more preferably 1%.


W, like Mo, increases hardness after working and enhances deformability. The W content should be no less than 0.04%, preferably no less than 0.08%, and more preferably no less than 0.1%. However, W in excess of 2% deteriorates cold workability. Thus, the W content should be limited to 2%, preferably 1.5%, more preferably 1%, and most desirably 0.5%.


(at least one species selected from the group consisting of Ca: no more than 0.05%, REM: no more than 0.05%, Mg: no more than 0.02%, Li: no more than 0.02%, Pb: no more than 0.1%, and Bi: no more than 0.1%)


Ca, REM, Mg, Li, Pb, and Bi contribute to the machinability of steel. Especially, Li lowers the melting point of Al oxides, thereby making Al oxides harmless, and hence improves machinability. In addition, Ca, REM, Mg, and Li also make sulfide inclusions (such as MnS) spherical, thereby enhancing the toughness and deformability of steel. Each of them should be contained in an amount no less than specified below.


Ca: 0.005%, preferably 0.01%,


REM: 0.005%, preferably 0.01%,


Mg: 0.002%, preferably 0.005%, more preferably 0.008%,


Li: 0.001%, preferably 0.002%, more preferably 0.005%,


Pb: 0.005%, preferably 0.01%, more preferably 0.02%, and


Bi: 0.005%, preferably 0.01%, more preferably 0.02%.


These elements added in excess amounts do not produce additional effects. Excess Pb causes rolling defects. The amount of these elements is limited as specified as above. Their desirable upper limits are as follows.


Ca: 0.04%, preferably 0.03%, more preferably 0.02%,


REM: 0.04%, preferably 0.03%, more preferably 0.02%, most desirably 0.01%,


Mg: 0.018%, preferably 0.015%, more preferably 0.01%,


Li: 0.018%, preferably 0.015%, more preferably 0.01%,


Pb: 0.09%, preferably 0.08%, more preferably 0.06%, and


Bi: 0.09%, preferably 0.08%.


<Method for Producing Steel for High-Speed Cold Working>

The following is concerned with the method for producing the steel for cold working according to the present invention. The steel according to the present invention is characterized in containing no less than 0.006% dissolved N. The desired amount of dissolved N is effectively ensured by (i) increasing the total amount of N in the steel and decreasing the amount of elements having a strong affinity with N in the steel and (ii) heating the steel above a prescribed temperature and then quenching the steel at a cooling rate greater than a prescribed value, thereby increasing the amount of dissolved N.


(i) Method for Increasing the Total Amount of Dissolved N in the Steel and Decreasing the Amount of Elements Having a Strong Affinity with N in the Steel.


Nitrogen in a steel containing Al (which has a strong affinity with N) combines with it to form N compounds, thereby decreasing the amount of dissolved N. However, a steel containing more nitrogen than consumed by Al that forms N compounds will permit dissolved N to remain sufficiently in it. To be concrete, a steel will eventually contain no less than 0.006% dissolved N if it initially contains N in an amount that satisfies the formula (1) below.





[N]−(14[Al]/27+14[Ti]/47.9+14[Nb]/92.9+14[V]/50.9+14[Zr]/91.2+14[B]/10.8+14[Ta]/180.9+14[Hf]/178.5)≧0.006  Formula (1)


where the square brackets [ ] represent the total amount (in mass %) of each element contained in the steel.


(ii) Method for Heating the Steel Above a Prescribed Temperature and then Quenching the Steel at a Cooling Rate Greater than a Prescribed Value, Thereby Increasing the Amount of Dissolved N.


A steel not having the chemical composition that satisfies the formula (1) permits N compounds of Al etc. to be formed in large amounts, and this leads to an insufficient content of dissolved N. This trouble is circumvented by heating and keeping the steel at a temperature at which N compounds resulting from hot rolling dissolves to form solid solution and then quenching the steel. This solid-solution heat treatment to prevent N compounds from precipitation increases the amount of dissolved N. To be concrete, the object is achieved by heating the steel at a temperature above Ac3 point plus 30° C. and then quenching it to 500° C. or below at a cooling rate no smaller than 0.5° C./s.


For the steel to contain a sufficient amount of dissolved N, the heating temperature should be no lower than Ac3 point plus 30° C., preferably Ac3 point plus 40° C., and more preferably Ac3 point plus 50° C. The duration of heating should be no shorter than 10 minutes, preferably no shorter than 30 minutes. The heating temperature determined from the standpoint of production cost is below Ac3 point plus 500° C., preferably Ac3 point plus 450° C., more preferably Ac3 point plus 400° C., and most desirably Ac3 point plus 300° C. The duration of heating should be no longer than 2.5 hours, preferably no longer than 1.5 hours.


The heating step may optionally include hot working such as drawing, rolling, and pressing. Heating should be followed by quenching at a cooling rate no smaller than 0.5° C./s, preferably 1° C./s, more preferably 5° C./s. Quenching down to 500° C. or below, preferably 450° C. or below, for dissolved N to exist stably is desirable. Thus the resulting steel contains sufficient dissolved N without N compounds precipitating.


<Method for Producing Parts by High-Speed Cold Working>

One feature of the present invention resides in a method of high-speed cold working for a steel having the above-mentioned chemical composition and containing dissolved N. For the steel according to the present invention to exhibit good cold workability despite its comparatively high content of dissolved N, it should undergo cold working at a strain rate which is no lower than 100/s, preferably 120/s, more preferably 140/s, particularly 150/s, and most desirably 200/s. However, the strain rate should be within a certain limit so that the steel is protected from cracking due to adiabatic temperature rise. The upper limit of the strain rate is 500/s, preferably 450/s, more preferably 400/s, particularly 300/s, most desirably 280/s, and 260/s most of all.


The working temperature which affects cold workability should be limited to 200° C., preferably 180° C., more preferably 160° C. An excessively high working temperature leads to the dynamic strain aging during deformation which increases deformation resistance and deteriorates the mold life. On the other hand, cold working is usually carried out at room temperature. Cold working at 0° C. or below suffers an increased deformation resistance due to temperature dependency. Therefore, the lower limit of the cold working temperature is 0° C. Incidentally, the working temperature is defined as the ambient temperature at the time of working.


The steel stock (such as wire and rod) produced as mentioned above is made into machine parts (such as bolts and nuts) by high-speed cold working under the foregoing conditions. The cold working includes cold forging, cold pressing, cold rolling, cold drawing, and cold extrusion. The thus produced machine parts may optionally undergo drawing and rolling.


The machine parts produced by high-speed cold working should have adequate strength and adequate deformation resistance which are balanced with each other. High-speed cold working at 200° C. or below at a strain rate of 100/s or above should give machine parts having the hardness (H) which depends on the maximum deformation resistance (DR) experienced during high-speed cold working as defined by the formula (3) below.






H≧(DR+1000)/6  (3)


where, H denotes the strength (Hv) of parts and DR denotes the deformation resistance (MPa).


INDIVIDUAL EMBODIMENTS OF THE PRESENT INVENTION

The basic embodiment of the present invention specifies the steel according to its composition for fundamental components and optional components as mentioned above. It falls under three categories as follows according to applications and desired performance.


First Embodiment of the Present Invention

According to the first embodiment of the present invention, the steel for high-speed cold working contains 0.03-0.15% C, 0.005-0.6% Si, 0.05-2% Mn, no more than 0.05% P (excluding 0%), no more than 0.05% S (excluding 0%), and no more than 0.04% N (excluding 0%), with the remainder being iron and inevitable impurities. It is characterized by containing no less than 0.006% dissolved nitrogen.


(C: 0.03 to 0.15%)

The first embodiment of the present invention specifies that the steel should contain no more than 0.15% C for its good machinability and cold workability. The preferable upper limit of C content is 0.12%, and the lower limit of C content is 0.03%, preferably 0.04%, for good steel strength.


Except for C content, the first embodiment of the present invention is identical with the basic embodiment of the present invention in the content of fundamental components and optional components, the method for steel production, and the balance between parts strength and deformation resistance during high-speed cold working (which has been mentioned with reference to the formula (3) above).


The Second Embodiment of the Present Invention

According to the second embodiment of the present invention, the steel for high-speed cold working contains:


C: more than 0.15% up to 0.6%,


Si: 0.005 to 0.6%,
Mn: 0.05 to 2%,

P: no more than 0.05% (excluding 0%),


S: no more than 0.05% (excluding 0%), and


N: no more than 0.04% (excluding 0%),


with the remainder being iron and inevitable impurities. It is characterized by containing no less than 0.006% dissolved N.


(C: More than 0.15% Up to 0.6%)


The second embodiment of the present invention specifies that the steel should contain more than 0.15% C for its good parts strength. The preferable C content is no less than 0.16%, preferably no less than 0.17%. The upper limit of C content should be 0.6%, preferably 0.5%, and more preferably 0.4%, because excess C deteriorates machinability and cold workability.


Except for C content, the second embodiment of the present invention is identical with the basic embodiment of the present invention in the content of fundamental components and optional components, the method for steel production, and the balance between parts strength and deformation resistance during high-speed cold working (which has been mentioned with reference to the formula (3) above).


The Third Embodiment of the Present Invention

The third embodiment of the present invention specifies the amount of such elements as Al, Ti, Nb, V, Zr, G, Ta, and Hf which reduce the amount of dissolved N in the steel. With the content of these elements kept low, the steel contains sufficient dissolved N, which leads to good cold workability and high parts strength.


According to the third embodiment of the present invention, the steel for high-speed cold working contains:


C: 0.03 to 0.6%,
Si: 0.005 to 0.6%,
Mn: 0.05 to 2%,

P: no more than 0.05% (excluding 0%),


S: no more than 0.05% (excluding 0%), and


N: 0.008 to 0.04%,

with the remainder being iron and inevitable impurities. The inevitable impurities include the following elements.


Al: no more than 0.001% (including 0%),


Ti: no more than 0.002% (including 0%),


Nb: no more than 0.001% (including 0%),


V: no more than 0.001% (including 0%),


Zr: no more than 0.001% (including 0%),


B: no more than 0.0001% (including 0%),


Ta: no more than 0.0001% (including 0%), and


Hf: no more than 0.0001% (including 0%).


The amounts of these elements satisfy the formula (2) below.





14[Al]/27+14[Ti]/47.9+14[Nb]/92.9+14[V]/50.9+14[Zr]/91.2+14[B]/10.8+14[Ta]/180.9+14[Hf]/178.5≦0.002%  Formula (2)


where the square brackets [ ] represent the total amount (in mass %) of each element contained in the steel.


(N: 0.008 to 0.04%)

The third embodiment of the present invention specifies that the lower limit of the total N content should be 0.008%, preferably 0.009%, so that the steel contains a prescribed amount of dissolved N. On the other hand, it also specifies that the upper limit of the total N content should be 0.04%, preferably 0.03%, from the standpoint of steel deformability, steel stability, and yields in continuous casting.


The inevitable impurities mentioned above may include any of Al, T, Nb, V, Zr, B, Ta, and Hf. These elements readily combine with dissolved N to decrease the amount of dissolved N in the steel. Consequently, the third embodiment of the present invention specifies the content of these elements as follows.


Al: no more than 0.001% (including 0%),


Ti: no more than 0.002% (including 0%),


Nb: no more than 0.001% (including 0%),


V: no more than 0.001% (including 0%),


Zr: no more than 0.001% (including 0%),


B: no more than 0.0001% (including 0%),


Ta: no more than 0.0001% (including 0%), and


Hf: no more than 0.0001% (including 0%).


Such elements as Al, Ti, Nb, V, Zr, B, Ta, and Hf readily combine with dissolved N to form nitrides (such as AlN, TiN, NbN, VN, ZrN, BN, TaN, and HfN), thereby decreasing the amount of dissolved N in the steel. These nitrides enhance precipitation strengthening and prevent crystal grains from becoming coarse, thereby increasing deformation resistance. For the steel to contain dissolved N sufficiently and to have adequate deformation resistance, the amounts of these elements should be as small as possible.


Thus, the amounts of these elements are specified as follows in the third embodiment of the present invention.


Al: no more than 0.001%, preferably no more than 0.0005%,


Ti: no more than 0.002%, preferably no more than 0.001%,


Nb: no more than 0.001%, preferably no more than 0.0005%,


V: no more than 0.001%, preferably no more than 0.0005%,


Zr: no more than 0.001%, preferably no more than 0.0005%,


B: no more than 0.0001%, preferably no more than 0.00005%,


Ta: no more than 0.0001%, preferably no more than 0.00005%,


Hf: no more than 0.0001%, preferably no more than 0.00005%.


The most desirable content of these elements is 0%.


The content of Al, Ti, Nb, V, Zr, B, Ta, and Hf should be lower than specified above, but, at the same time, it should satisfy the formula (2) below.





14[Al]/27+14[Ti]/47.9+14[Nb]/92.9+14[V]/50.9+14[Zr]/91.2+14[B]/10.8+14[Ta]/180.9+14[Hf]/178.5≦0.002%  Formula (2)


The term (14[Al]/27) denotes the amount of nitrogen in the form of AlN existing in the steel. The entire left side of the formula (2) represents the total amount of nitrogen combined with any of Al, Ti, Nb, V, Zr, B, Ta, and Hf (or the total amount of N compounds in the steel). For the steel to have an adequate amount of dissolved N, it is desirable that the amount of N compounds should be small. Therefore, the sum of the left side should be smaller than 0.002%, preferably smaller than 0.0018%, more preferably smaller than 0.0016%.


Except for the description of the amount of N, Al, Ti, Nb, V, Zr, B, Ta and Hf, the third embodiment of the present invention is identical with the basic embodiment of the present invention in the content of fundamental components and optional components, the method for steel production, and the balance between parts strength and deformation resistance during high-speed cold working (which has been mentioned with reference to the formula (3) above). Incidentally, although the steel for high-speed cold working in the third embodiment of the present invention may be produced by the above-mentioned manufacturing method, it will contain an adequate amount of dissolved N irrespective of manufacturing method so used long as the formula (2) is satisfied.


EXAMPLES

The invention will be described in more detail with reference the following examples, which are not intended to restrict the scope thereof but may be modified within the scope thereof.


Example 1 and Comparative Example According to the First Embodiment of the Present Invention

Steel samples (in the form of ingot) each having the chemical composition shown in Tables 1 to 3 were prepared by continuous casting from a converter. Each ingot was rolled into a wire, 12 mm in diameter.


The thus obtained wire underwent heat treatment under the conditions shown in Table 4. The heat-treated wire should preferably be kept at the heating temperature for at least 10 minutes, desirably at least 30 minutes. Then, a test specimen measuring 4 mm in diameter and 6 mm long was cut out of the central part of the heat-treated wire. Whether or not the test specimen satisfies the formula (1) is indicated respectively by symbols “◯” and “X”. In Tables 1 to 3, “dissolved N” represents the amount of dissolved N and “N” represents the total amount of N.











TABLE 1









Chemical composition (mass %)



















Material No.
Steel No.
C
Si
Mn
P
S
N
Al
Ti
Nb
V
Zr





I-1
I-1A
0.02
0.07
0.15
0.015
0.015
0.0095
0.001
0
0
0
0.000


I-2
I-1B
0.05
0.17
0.44
0.009
0.012
0.0167
0.012
0
0
0
0.000


I-3
I-1C
0.06
0.15
0.32
0.023
0.028
0.0103
0.001
0
0
0
0.000


I-4
I-1D
0.11
0.12
0.23
0.018
0.021
0.0145
0.008
0
0
0
0.000


I-5
I-1E
0.13
0.06
0.14
0.008
0.008
0.0155
0.001
0
0
0
0.000


I-6
I-1F
0.17
0.06
0.14
0.008
0.008
0.0155
0.001
0
0
0
0.000


I-7
I-1G
0.08
0
0.27
0.013
0.012
0.0189
0.001
0
0
0
0.000


I-8
I-1H
0.1
0.18
0.35
0.006
0.004
0.0169
0.013
0
0
0
0.000


I-9
I-1I
0.08
0.23
0.1
0.005
0.032
0.0123
0.001
0
0
0
0.000


I-10
I-1J
0.12
0.38
0.19
0.007
0.015
0.0175
0.009
0
0
0
0.000


I-11
I-1K
0.09
0.4
0.13
0.015
0.008
0.0093
0.001
0
0
0
0.000


I-12
I-1L
0.11
0.57
0.29
0.009
0.034
0.0217
0.005
0
0
0
0.000


I-13
I-1M
0.05
0.58
0.41
0.018
0.013
0.0193
0.001
0
0
0
0.000


I-14
I-1N
0.08
0.62
0.21
0.009
0.028
0.0098
0.001
0
0
0
0.000


I-15
I-1O
0.06
0.39
0.03
0.045
0.041
0.0241
0.001
0
0
0
0.000


I-16
I-1P
0.09
0.17
0.24
0.019
0.034
0.0151
0.006
0
0
0
0.000


I-17
I-1Q
0.09
0.34
0.22
0.043
0.019
0.0087
0.001
0
0
0
0.000


I-18
I-1R
0.13
0.54
0.45
0.032
0.002
0.0315
0.015
0
0
0
0.000


I-19
I-1S
0.06
0.56
0.48
0.008
0.009
0.0316
0.001
0
0
0
0.000


I-20
I-1T
0.08
0.43
1.03
0.005
0.043
0.0252
0.023
0
0
0
0.000


I-21
I-1U
0.06
0.17
1.15
0.034
0.015
0.0197
0.001
0
0
0
0.000


I-22
I-1V
0.15
0.16
1.89
0.004
0.032
0.0285
0.015
0
0
0
0.000


I-23
I-1W
0.11
0.08
1.95
0.024
0.011
0.0144
0.001
0
0
0
0.000


I-24
I-1X
0.14
0.15
2.08
0.028
0.019
0.0198
0.001
0
0
0
0.000


I-25
I-1Y
0.13
0.35
0.27
0.06
0.004
0.0175
0.001
0
0
0
0.000


I-26
I-1Z
0.12
0.17
0.31
0.09
0.016
0.0307
0.001
0
0
0
0.000


I-27
I-2A
0.08
0.49
0.79
0.033
0.07
0.0108
0.001
0
0
0
0.000


I-28
I-2B
0.09
0.35
0.54
0.009
0.09
0.0108
0.001
0
0
0
0.000


I-29
I-2C
0.12
0.08
0.34
0.012
0.013
0.0061
0.008
0
0
0
0.000


I-30
I-2D
0.14
0.25
0.61
0.013
0.008
0.0075
0.001
0
0
0
0.000


I-31
I-2E
0.08
0.19
0.45
0.005
0.005
0.0195
0.011
0
0
0
0.000


I-32
I-2F
0.05
0.04
0.08
0.021
0.011
0.0199
0.001
0
0
0
0.000


I-33
I-2G
0.09
0.17
0.16
0.017
0.012
0.0256
0.005
0
0
0
0.000


I-34
I-2H
0.14
0.45
0.34
0.025
0.004
0.0218
0.001
0
0
0
0.000


I-35
I-2I
0.08
0.31
0.23
0.021
0.019
0.0335
0.014
0
0
0
0.000



















Formula




Chemical composition


(1)



(mass %)

Dissolved
satisfied
Heat















Material No.
B
Ta
Hf
Others
Ac3 point (° C.)
N (mass %)
or n ot
treatment





I-1
0.0001
0
0

891
0.0081

I-a


I-2
0.0001
0
0

871
0.0096

I-h


I-3
0.0001
0
0

874
0.0089

I-d


I-4
0.0001
0
0

857
0.0095

I-i


I-5
0.0001
0
0

842
0.0141

I-j


I-6
0.0001
0
0

831
0.0141

I-b


I-7
0.0001
0
0

855
0.0175

I-j


I-8
0.0001
0
0

853
0.0093

I-j


I-9
0.0001
0
0

864
0.0109

I-h


I-10
0.0001
0
0

860
0.0120

I-d


I-11
0.0001
0
0

874
0.0079

I-i


I-12
0.0001
0
0

868
0.0183

I-f


I-13
0.0001
0
0

891
0.0179

I-h


I-14
0.0001
0
0

881
0.0084

I-b


I-15
0.0001
0
0

909
0.0227

I-g


I-16
0.0001
0
0

866
0.0111

I-g


I-17
0.0001
0
0

889
0.0073

I-d


I-18
0.0001
0
0

876
0.0229

I-e


I-19
0.0001
0
0

877
0.0302

I-c


I-20
0.0001
0
0

854
0.0124

I-j


I-21
0.0001
0
0

858
0.0183

I-f


I-22
0.0001
0
0

791
0.0199

I-b


I-23
0.0001
0
0

805
0.0130

I-i


I-24
0.0001
0
0

799
0.0184

I-h


I-25
0.0001
0
0

887
0.0161

I-d


I-26
0.0001
0
0

902
0.0293

I-g


I-27
0.0001
0
0

875
0.0094

I-a


I-28
0.0001
0
0

856
0.0094

I-f


I-29
0.0001
0
0

845
0.0011
x
I-j


I-30
0.0001
0
0

837
0.0061

I-e


I-31
0.0001
0
0

856
0.0129

I-g


I-32
0.0001
0
0

880
0.0185

I-h


I-33
0.0001
0
0

866
0.0222

I-c


I-34
0.0001
0
0

862
0.0204

I-d


I-35
0.0001
0
0

880
0.0254

I-f


















TABLE 2







Material
Steel
Chemical composition (mass %)




















No.
No.
C
Si
Mn
P
S
N
Al
Ti
Nb
V
Zr
B





I-36
I-2J
0.04
0.29
0.09
0.01
0.022
0.0376
0.001
0
0
0
0.000
0.0001


I-37
I-2K
0.07
0.25
1.86
0.008
0.025
0.0443
0.001
0
0
0
0.000
0.0001


I-38
I-2L
0.09
0.5
0.94
0.004
0.009
0.0231
0.001
0.04
0
0
0.000
0.0001


I-39
I-2M
0.12
0.11
0.75
0.011
0.032
0.0285
0.006
0
0.03
0
0.000
0.0001


I-40
I-2N
0.13
0.25
0.34
0.016
0.006
0.0229
0.001
0
0.06
0.02
0.000
0.0001


I-41
I-2O
0.09
0.38
0.41
0.023
0.015
0.0223
0.007
0
0
0
0.050
0.0001


I-42
I-2P
0.14
0.05
0.54
0.039
0.027
0.0099
0.001
0
0
0
0.000
0.0006


I-43
I-2Q
0.05
0.17
0.13
0.019
0.005
0.0398
0.023
0.03
0
0.04
0.000
0.0001


I-44
I-2R
0.07
0.35
0.88
0.021
0.002
0.0308
0.018
0
0.04
0
0.005
0.0001


I-45
I-2S
0.09
0.16
1.23
0.025
0.015
0.0185
0.001
0
0
0.03
0.004
0.0001


I-46
I-2T
0.11
0.33
0.14
0.027
0.013
0.0212
0.009
0
0
0
0.000
0.0001


I-47
I-2U
0.1
0.28
0.31
0.038
0.03
0.0301
0.001
0
0
0
0.000
0.0001


I-48
I-2V
0.09
0.16
0.44
0.041
0.019
0.0232
0.018
0
0
0
0.000
0.0013


I-49
I-2W
0.05
0.13
0.3
0.016
0.044
0.0388
0.001
0.05
0
0.05
0.000
0.0001


I-50
I-2X
0.09
0.32
0.22
0.017
0.015
0.0342
0.034
0
0
0
0.020
0.0001


I-51
I-2Y
0.11
0.38
1.53
0.019
0.009
0.0199
0.001
0
0
0
0.000
0.0001


I-52
I-2Z
0.13
0.56
0.09
0.022
0.018
0.0371
0.028
0.01
0.04
0
0.000
0.0001


I-53
I-3A
0.08
0.44
0.32
0.008
0.009
0.0233
0.001
0.01
0
0
0.000
0.0001


I-54
I-3B
0.12
0.22
0.43
0.005
0.045
0.0243
0.008
0.01
0
0
0.000
0.0001


I-55
I-3C
0.09
0.12
0.12
0.012
0.019
0.0198
0.005
0.01
0
0
0.000
0.0001


I-56
I-3D
0.04
0.08
0.65
0.015
0.003
0.0188
0.003
0.03
0
0
0.000
0.0001


I-57
I-3E
0.08
0.09
0.99
0.009
0.023
0.0276
0.012
0.01
0
0
0.000
0.0008


I-58
I-3F
0.04
0.13
0.15
0.003
0.019
0.0324
0.010
0.01
0
0
0.000
0.0001


I-59
I-3G
0.06
0.12
1.22
0.034
0.039
0.0355
0.001
0.01
0
0
0.005
0.0001


I-60
I-3H
0.1
0.08
0.56
0.028
0.011
0.0180
0.001
0.01
0
0
0.000
0.0001


I-61
I-3I
0.11
0.09
0.43
0.018
0.031
0.0233
0.001
0.01
0
0
0.000
0.0001


I-62
I-3J
0.05
0.21
0.39
0.011
0.008
0.0154
0.004
0.01
0
0
0.000
0.0001


I-63
I-3K
0.09
0.39
0.28
0.032
0.015
0.0198
0.001
0.01
0
0
0.000
0.0001


I-64
I-3L
0.14
0.43
0.11
0.008
0.026
0.0221
0.009
0.01
0
0.01
0.000
0.0001


I-65
I-3M
0.11
0.19
0.17
0.01
0.007
0.0308
0.001
0.01
0.02
0
0.000
0.0001


I-66
I-3N
0.08
0.27
0.35
0.008
0.012
0.0203
0.005
0.01
0
0
0.000
0.0001


I-67
I-3O
0.12
0.31
0.28
0.035
0.019
0.0198
0.002
0.01
0
0
0.000
0.0001


I-68
I-3P
0.14
0.37
0.76
0.047
0.013
0.0296
0.006
0.01
0
0
0.008
0.0001


I-69
I-3Q
0.05
0.12
1.89
0.002
0.01
0.0201
0.001
0.01
0
0
0.000
0.0001


I-70
I-3R
0.08
0.18
0.23
0.019
0.002
0.0176
0.011
0.01
0
0.01
0.000
0.0001
















Chemical






Material
composition (mass %)
Ac3 point
Dissolved N
Formula (1) satisfied
Heat














No.
Ta
Hf
Others
(° C.)
(mass %)
or not
treatment





I-36
0
0

887
0.0362

I-b


I-37
0
0

818
0.0429

I-i


I-38
0
0

862
0.0103

I-g


I-39
0
0

833
0.0202

I-i


I-40
0
0

852
0.0074

I-d


I-41
0
0

873
0.0101

I-c


I-42
0
0

848
0.0079

I-e


I-43
0
0

907
0.0078

I-h


I-44
0
0

868
0.0140

I-f


I-45
0
0

841
0.0085

I-j


I-46
0.02
0

876
0.0137

I-a


I-47
0
0.05

876
0.0248

I-c


I-48
0
0.03

879
0.0091

I-g


I-49
0
0

898
0.0096

I-i


I-50
0.01
0

883
0.0116

I-e


I-51
0
0.03

828
0.0162

I-h


I-52
0
0

890
0.0132

I-b


I-53
0
0
Co: 4.5
873
0.0193

I-d


I-54
0
0
Mo: 0.04, Pb: 0.08
847
0.0167

I-c


I-55
0
0
Mo: 1.3
865
0.0137

I-f


I-56
0
0
W: 1.8
877
0.0079

I-a


I-57
0
0
W: 0.05, Ca: 0.016
842
0.0170

I-e


I-58
0
0
Ca: 0.008
881
0.0237

I-j


I-59
0.006
0
Ca: 0.02, REM: 0.009
857
0.0301

I-g


I-60
0
0
REM: 0.042
857
0.0140

I-j


I-61
0
0
Mg: 0.01, Cr: 1.3
851
0.0193

I-c


I-62
0
0
Li: 0.005
876
0.0098

I-b


I-63
0
0
Mg: 0.013, Ca: 0.003
885
0.0155

I-i


I-64
0
0
Co: 2.5, Mo: 0.3
864
0.0115

I-f


I-65
0
0
Cu: 0.4
857
0.0239

I-e


I-66
0
0
Cu: 3.2, Cr: 0.8
866
0.0142

I-e


I-67
0
0
Cu: 1.3, Ni: 3.1
874
0.0153

I-g


I-68
0
0
Ni: 3.5, Bi: 0.08
867
0.0218

I-a


I-69
0.01
0
Ni: 0.9
819
0.0151

I-d


I-70
0
0
Co: 1.9, Pb: 0.06
874
0.0074

I-c


















TABLE 3







Material

Chemical composition (mass %)


















No.
Steel No.
C
Si
Mn
P
S
N
Al
Ti
Nb
V





I-71
I-3S
0.13
0.05
0.25
0.036
0.009
0.0133
0.001
0.01
0
0


I-72
I-3T-1
0.08
0.55
0.11
0.009
0.01
0.0286
0.094
0.03
0
0


I-73
I-3T-2
0.08
0.55
0.11
0.009
0.01
0.0286
0.094
0.03
0
0


I-74
I-3T-3
0.08
0.55
0.11
0.009
0.01
0.0286
0.094
0.03
0
0


I-75
I-3T-4
0.08
0.55
0.11
0.009
0.01
0.0286
0.094
0.03
0
0


I-76
I-3U-1
0.14
0.23
0.94
0.013
0.022
0.0322
0.015
0.07
0
0


I-77
I-3U-2
0.14
0.23
0.94
0.013
0.022
0.0322
0.015
0.07
0
0


I-78
I-3U-3
0.14
0.23
0.94
0.013
0.022
0.0322
0.015
0.07
0
0


I-79
I-3U-4
0.14
0.23
0.94
0.013
0.022
0.0322
0.015
0.07
0
0


I-80
I-3V-1
0.1
0.18
0.43
0.007
0.009
0.0185
0.013
0
0.2
0


I-81
I-3V-2
0.1
0.18
0.43
0.007
0.009
0.0185
0.013
0
0.2
0


I-82
I-3V-3
0.1
0.18
0.43
0.007
0.009
0.0185
0.013
0
0.2
0


I-83
I-3V-4
0.1
0.18
0.43
0.007
0.009
0.0185
0.013
0
0.2
0


I-84
I-3W-1
0.07
0.47
0.23
0.021
0.017
0.0175
0.001
0
0
0.48


I-85
I-3W-2
0.07
0.47
0.23
0.021
0.017
0.0175
0.001
0
0
0.48


I-86
I-3W-3
0.07
0.47
0.23
0.021
0.017
0.0175
0.001
0
0
0.48


I-87
I-3W-4
0.07
0.47
0.23
0.021
0.017
0.0175
0.001
0
0
0.48


I-88
I-3X-1
0.12
0.05
0.12
0.018
0.012
0.0199
0.001
0
0
0


I-89
I-3X-2
0.12
0.05
0.12
0.018
0.012
0.0199
0.001
0
0
0


I-90
I-3X-3
0.12
0.05
0.12
0.018
0.012
0.0199
0.001
0
0
0


I-91
I-3X-4
0.12
0.05
0.12
0.018
0.012
0.0199
0.001
0
0
0


I-92
I-3Y-1
0.07
0.19
0.08
0.007
0.047
0.0099
0.012
0
0
0


I-93
I-3Y-2
0.07
0.19
0.08
0.007
0.047
0.0099
0.012
0
0
0


I-94
I-3Y-3
0.07
0.19
0.08
0.007
0.047
0.0099
0.012
0
0
0


I-95
I-3Y-4
0.07
0.19
0.08
0.007
0.047
0.0099
0.012
0
0
0


I-96
I-3Z-1
0.09
0.09
0.19
0.032
0.022
0.0221
0.035
0
0
0


I-97
I-3Z-2
0.09
0.09
0.19
0.032
0.022
0.0221
0.035
0
0
0


I-98
I-3Z-3
0.09
0.09
0.19
0.032
0.022
0.0221
0.035
0
0
0


I-99
I-3Z-4
0.09
0.09
0.19
0.032
0.022
0.0221
0.035
0
0
0


I-100
I-4A-1
0.05
0.33
0.28
0.005
0.003
0.0214
0.001
0
0
0


I-101
I-4A-2
0.05
0.33
0.28
0.005
0.003
0.0214
0.001
0
0
0


I-102
I-4A-3
0.05
0.33
0.28
0.005
0.003
0.0214
0.001
0
0
0


I-103
I-4A-4
0.05
0.33
0.28
0.005
0.003
0.0214
0.001
0
0
0



















Formula





Ac3

(1)


Material
Chemical composition (mass %)
point
Dissolved N
satisfied
Heat
















No.
Zr
B
Ta
Hf
Others
(° C.)
(mass %)
or not
treatment





I-71
0.000
0.0001
0
0
Mo: 1.1
861
0.0093

I-b


I-72
0.000
0.0001
0
0

930
0.0051
x
I-a


I-73
0.000
0.0001
0
0

930
0.0123
x
I-c


I-74
0.000
0.0001
0
0

930
0.0128
x
I-e


I-75
0.000
0.0001
0
0

930
0.0126
x
I-h


I-76
0.000
0.0001
0
0

859
0.0046
x
I-a


I-77
0.000
0.0001
0
0

859
0.0037
x
I-b


I-78
0.000
0.0001
0
0

859
0.0071
x
I-i


I-79
0.000
0.0001
0
0

859
0.0079
x
I-j


I-80
0.000
0.0001
0
0

851
0.0056
x
I-b


I-81
0.000
0.0001
0
0

851
0.0066
x
I-g


I-82
0.000
0.0001
0
0

851
0.0076
x
I-h


I-83
0.000
0.0001
0
0

851
0.0134
x
I-i


I-84
0.000
0.0001
0
0

936
0.0001
x
I-a


I-85
0.000
0.0001
0
0

936
0.0005
x
I-d


I-86
0.000
0.0001
0
0

936
0.0072
x
I-f


I-87
0.000
0.0001
0
0

936
0.0121
x
I-i


I-88
0.180
0.0001
0
0

852
0.0005
x
I-a


I-89
0.180
0.0001
0
0

852
0.0007
x
I-b


I-90
0.180
0.0001
0
0

852
0.0062
x
I-i


I-91
0.180
0.0001
0
0

852
0.0066
x
I-j


I-92
0.000
0.0014
0
0

872
0.0045
x
I-b


I-93
0.000
0.0014
0
0

872
0.0089
x
I-e


I-94
0.000
0.0014
0
0

872
0.0089
x
I-g


I-95
0.000
0.0014
0
0

872
0.0091
x
I-i


I-96
0.000
0.0001
0.038
0

884
0.0005
x
I-a


I-97
0.000
0.0001
0.038
0

884
0.0022
x
I-g


I-98
0.000
0.0001
0.038
0

884
0.0151
x
I-h


I-99
0.000
0.0001
0.038
0

884
0.0208
x
I-i


I-100
0.000
0.0001
0
0.04

875
0.0007
x
I-b


I-101
0.000
0.0001
0
0.04

875
0.0198
x
I-e


I-102
0.000
0.0001
0
0.04

875
0.0206
x
I-h


I-103
0.000
0.0001
0
0.04

875
0.0208
x
I-j




















TABLE 4





Heat



Cooling stop


treatment
Heating

Cooling rate
temperature


pattern
temperature (° C.)
Hot working
(° C./s)
(° C.)



















I-a
800
Yes
1
500


I-b
800
No
1
450


I-c
900
Yes
0.5
500


I-d
900
No
1
500


I-e
1000
Yes
0.5
480


I-f
1000
Yes
5
500


I-g
1000
No
1
500


I-h
1000
Yes
1
500


I-i
1100
Yes
1
430


I-j
1200
Yes
3
500









Each test specimen shown in Tables 1 to 3 was forged into parts by using a servo hydraulic type testing machine (with a capacity of 200 kN) under the following conditions.


Strain rate: 0.001 to 240/s


Working temperature: 20 to 400° C.


Compression ratio: 20 to 80%


The strain rate is an average of values measured during working (elastic deformation). The resulting parts were examined for their surface under a stereomicroscope with a magnification of ×20 to see if there is cracking. Tables 5 to 7 show the test results including working conditions, cracking, and deformation resistance.


Each part was also tested for Vickers hardness (Hv) by using a Vickers hardness tester under the following conditions.


Load: 1000 g

Position of measurement: D/4 off the center of the cross section of the part (D=diameter of part)


Number of repetitions of measurement: 5


The results of measurement are shown in Tables 5 to 7.


















TABLE 5










Compression
Deformation
Hardness after
Formula (3)



Part
Material
Steel
Strain
Working
ratio
resistance
working
satisfied


No.
No.
No.
rate (/s)
temperature (° C.)
(%)
(MPa)
(Hv)
or not
Cracking
























I-1
I-1
I-1A
100
60
20
362
233

Yes


I-2
I-2
I-1B
140
80
80
427
249

No


I-3
I-3
I-1C
180
20
60
432
248

No


I-4
I-4
I-1D
220
60
80
516
263

No


I-5
I-5
I-1E
120
20
40
544
282

No


I-6
I-6
I-1F
100
40
80
608
292

Yes


I-7
I-7
I-1G
160
60
80
459
278

Yes


I-8
I-8
I-1H
140
20
60
525
264

No


I-9
I-9
I-1I
100
80
60
467
259

No


I-10
I-10
I-1J
180
20
80
556
277

No


I-11
I-11
I-1K
140
100
80
501
256

No


I-12
I-12
I-1L
220
20
20
563
297

No


I-13
I-13
I-1M
160
60
80
459
279

No


I-14
I-14
I-1N
100
40
40
515
260

Yes


I-15
I-15
I-1O
120
20
60
427
288

Yes


I-16
I-16
I-1P
240
60
80
484
263

No


I-17
I-17
I-1Q
200
80
20
500
254

No


I-18
I-18
I-1R
140
20
80
621
321

No


I-19
I-19
I-1S
180
20
20
488
321

No


I-20
I-20
I-1T
140
20
80
586
284

No


I-21
I-21
I-1U
100
20
20
537
293

No


I-22
I-22
I-1V
160
40
60
725
329

No


I-23
I-23
I-1W
220
20
40
703
305

No


I-24
I-24
I-1X
120
60
80
787
335

Yes


I-25
I-25
I-1Y
100
20
80
588
295

Yes


I-26
I-26
I-1Z
140
80
80
555
329

Yes


I-27
I-27
I-2A
200
20
20
557
270

Yes


I-28
I-28
I-2B
100
40
80
548
268

Yes


I-29
I-29
I-2C
160
20
20
547
243
x
No


I-30
I-30
I-2D
180
20
60
622
271

No


I-31
I-31
I-2E
0.001
20
80
681
301

Yes


I-32
I-31
I-2E
0.1
60
80
610
289

Yes


I-33
I-31
I-2E
1
20
40
575
283

Yes


I-34
I-31
I-2E
10
80
80
539
277

Yes


I-35
I-31
I-2E
100
100
20
504
271

No


I-36
I-31
I-2E
200
200
60
493
270

No


I-37
I-32
I-2F
220
300
80
551
296

Yes


I-38
I-33
I-2G
140
400
20
668
326

Yes


I-39
I-34
I-2H
100
20
80
622
314

No


I-40
I-35
I-2I
160
20
80
483
305

No

























TABLE 6










Compression
Deformation
Hardness after




Part
Material
Steel
Strain
Working
ratio
resistance
working
Formula (3)


No.
No.
No.
rate (/s)
temperature (° C.)
(%)
(MPa)
(Hv)
satisfied or not
Cracking
























I-41
I-36
I-2J
120
60
40
466
335

No


I-42
I-37
I-2K
180
80
60
637
384

Yes


I-43
I-38
I-2L
100
80
20
612
282

No


I-44
I-39
I-2M
140
20
80
602
309

No


I-45
I-40
I-2N
220
20
80
582
268

No


I-46
I-41
I-2O
120
60
20
539
269

No


I-47
I-42
I-2P
200
40
80
594
271

No


I-48
I-43
I-2Q
160
100
40
435
245

No


I-49
I-44
I-2R
100
20
20
551
282

No


I-50
I-45
I-2S
180
40
80
602
304

No


I-51
I-46
I-2T
100
20
60
541
280

No


I-52
I-47
I-2U
140
60
80
535
312

No


I-53
I-48
I-2V
200
20
40
513
261

No


I-54
I-49
I-2W
160
80
20
417
247

No


I-55
I-50
I-2X
220
20
40
502
267

No


I-56
I-51
I-2Y
180
150
80
691
312

No


I-57
I-52
I-2Z
100
20
40
594
287

No


I-58
I-53
I-3A
120
40
60
564
300

No


I-59
I-54
I-3B
100
60
80
634
304

No


I-60
I-55
I-3C
160
20
80
527
278

No


I-61
I-56
I-3D
140
80
60
471
251

No


I-62
I-57
I-3E
200
20
80
598
299

No


I-63
I-58
I-3F
220
20
80
412
289

No


I-64
I-59
I-3G
100
150
20
597
339

No


I-65
I-60
I-3H
100
40
60
600
291

No


I-66
I-61
I-3I
180
60
40
593
305

No


I-67
I-62
I-3J
200
80
80
474
257

No


I-68
I-63
I-3K
100
20
40
578
291

No


I-69
I-64
I-3L
120
20
60
646
291

No


I-70
I-65
I-3M
180
20
80
576
316

No


I-71
I-66
I-3N
240
60
20
540
281

No


I-72
I-67
I-3O
140
20
60
618
298

No


I-73
I-68
I-3P
160
40
80
708
332

No


I-74
I-69
I-3Q
220
40
40
632
299

No


I-75
I-70
I-3R
100
60
60
533
260

No


I-76
I-71
I-3S
160
20
80
605
277

No


I-77
I-72
I-3T-1
120
20
20
502
248
x
No


I-78
I-73
I-3T-2
180
80
80
496
268

No


I-79
I-74
I-3T-3
100
40
40
505
271

No


I-80
I-75
I-3T-4
140
20
80
500
270

No

























TABLE 7









Working

Deformation
Hardness after




Part
Material
Steel
Strain
temperature
Compression
resistance
working
Formula (3)


No.
No.
No.
rate (/s)
(° C.)
ratio (%)
(MPa)
(Hv)
satisfied or not
Cracking
























I-81
I-76
I-3U-1
200
20
40
663
273
x
No


I-82
I-77
I-3U-2
100
60
80
678
273
x
No


I-83
I-78
I-3U-3
160
40
20
668
281

No


I-84
I-79
I-3U-4
240
20
40
660
282

No


I-85
I-80
I-3V-1
120
40
60
560
259
x
No


I-86
I-81
I-3V-2
180
20
40
553
261

No


I-87
I-82
I-3V-3
100
60
80
563
265

No


I-88
I-83
I-3V-4
140
20
20
557
282

No


I-89
I-84
I-3W-1
240
80
80
524
236
x
No


I-90
I-85
I-3W-2
160
40
60
531
239
x
No


I-91
I-86
I-3W-3
100
20
60
539
260

No


I-92
I-87
I-3W-4
120
40
80
536
274

No


I-93
I-88
I-3X-1
180
60
40
538
240
x
No


I-94
I-89
I-3X-2
160
20
20
540
241
x
No


I-95
I-90
I-3X-3
200
100
80
537
257

No


I-96
I-91
I-3X-4
140
20
20
543
259

No


I-97
I-92
I-3Y-1
100
80
40
440
236
x
No


I-98
I-93
I-3Y-2
220
40
60
430
247

No


I-99
I-94
I-3Y-3
120
60
80
438
248

No


I-100
I-95
I-3Y-4
160
20
80
434
248

No


I-101
I-96
I-3Z-1
180
100
20
481
230
x
No


I-102
I-97
I-3Z-2
240
20
80
477
235
x
No


I-103
I-98
I-3Z-3
140
20
40
486
275

No


I-104
I-99
I-3Z-4
100
40
80
491
293

No


I-105
I-100
I-4A-1
220
20
20
421
221
x
No


I-106
I-101
I-4A-2
120
20
60
430
280

No


I-107
I-102
I-4A-3
200
40
80
423
281

No


I-108
I-103
I-4A-4
160
60
40
426
282

No









Steels in this example are rated as good in cold workability if they give crack-free parts and exhibit low deformation resistance relative to parts hardness (or satisfy the formula (3)).


Those parts having a Vickers hardness (Hv) larger than 240 are rated as good in strength. Incidentally, Tables 5 to 7 show whether or not each specimen satisfies the formula (3) by symbols “◯” and “X” respectively.


It is noted from Tables 5 to 7 that the steel containing chemical components and dissolved nitrogen as specified in the first embodiment of the present invention excels in cold workability and gives parts having high strength when it is worked under desirable conditions (such as strain rate and working temperature). By contrast, the steel failing to meet the requirements specified in the first embodiment of the present invention lacks good cold workability or gives parts poor in strength as mentioned below.


Part No. I-1 (Steel No. I-1A) is low in strength because of insufficient carbon content (which is responsible for its hardness (Hv) lower than 240).


Part No. I-6 (Steel No. I-1F) suffers cracking due to excess carbon content.


Part No. I-7 (Steel No. I-1G) suffers cracking due to low Si content.


Part No. I-14 (Steel No. I-1N) suffers cracking due to excess Si content.


Part No. I-15 (Steel No. I-1O) suffers cracking due to low Mn content.


Part No. I-24 (Steel No. I-1X) suffers cracking due to excess Mn content.


Part Nos. I-25 and I-26 (Steel Nos. I-1Y and I-1Z) suffer cracking due to excess P content.


Example 2 and Comparative Example According to the Second Embodiment of the Present Invention

Steel samples, numbered II-1A to II-4A, (in the form of ingot) each having the chemical composition shown in Tables 8 to 10 were prepared by continuous casting from a converter. Each ingot was rolled into a wire, 12 mm in diameter. The thus obtained wire underwent heat treatment under the conditions shown in Table 11. The heat-treated wire should preferably be kept at the heating temperature for at least 10 minutes, desirably at least 30 minutes.


Then, a test specimen measuring 4 mm in diameter and 6 mm long was cut out of the central part of the heat-treated wire. Whether or not the test specimen satisfies the formula (1) is indicated respectively by symbols “◯” and “X”. In Tables 8 to 10, “dissolved N” represents the amount of dissolved N and “N” represents the total amount of N.











TABLE 8







Material
Steel
Chemical composition (mass %)


















No.
No.
C
Si
Mn
P
S
N
Al
Ti
Nb
V





II-1
II-1A
0.13
0.07
0.15
0.015
0.015
0.0095
0.001
0.001
0.001
0.001


II-2
II-1B
0.25
0.17
0.44
0.009
0.012
0.0167
0.012
0.001
0.001
0.001


II-3
II-1C
0.34
0.15
0.32
0.023
0.028
0.0103
0.001
0.001
0.001
0.001


II-4
II-1D
0.43
0.12
0.23
0.018
0.021
0.0145
0.008
0.001
0.001
0.001


II-5
II-1E
0.56
0.06
0.14
0.008
0.008
0.0155
0.001
0.001
0.001
0.001


II-6
II-1F
0.64
0.06
0.14
0.008
0.008
0.0155
0.001
0.001
0.001
0.001


II-7
II-1G
0.46
0.002
0.27
0.013
0.012
0.0189
0.001
0.001
0.001
0.001


II-8
II-1H
0.21
0.18
0.35
0.006
0.004
0.0169
0.013
0.001
0.001
0.001


II-9
II-1I
0.19
0.23
0.10
0.005
0.032
0.0123
0.001
0.001
0.001
0.001


II-10
II-1J
0.42
0.38
0.19
0.007
0.015
0.0175
0.009
0.001
0.001
0.001


II-11
II-1K
0.26
0.40
0.13
0.015
0.008
0.0093
0.001
0.001
0.001
0.001


II-12
II-1L
0.18
0.57
0.29
0.009
0.034
0.0217
0.005
0.001
0.001
0.001


II-13
II-1M
0.54
0.58
0.41
0.018
0.013
0.0193
0.001
0.001
0.001
0.001


II-14
II-1N
0.58
0.62
0.21
0.009
0.028
0.0098
0.001
0.001
0.001
0.001


II-15
II-1O
0.16
0.39
0.03
0.045
0.041
0.0241
0.001
0.001
0.001
0.001


II-16
II-1P
0.38
0.17
0.24
0.019
0.034
0.0151
0.006
0.001
0.001
0.001


II-17
II-1Q
0.41
0.34
0.22
0.043
0.019
0.0087
0.001
0.001
0.001
0.001


II-18
II-1R
0.27
0.54
0.45
0.032
0.002
0.0315
0.015
0.001
0.001
0.001


II-19
II-1S
0.38
0.56
0.48
0.008
0.009
0.0316
0.001
0.001
0.001
0.001


II-20
II-1T
0.27
0.43
1.03
0.005
0.043
0.0252
0.023
0.001
0.001
0.001


II-21
II-1U
0.31
0.17
1.15
0.034
0.015
0.0197
0.001
0.001
0.001
0.001


II-22
II-1V
0.34
0.16
1.89
0.004
0.032
0.0285
0.015
0.001
0.001
0.001


II-23
II-1W
0.19
0.08
1.95
0.024
0.011
0.0144
0.001
0.001
0.001
0.001


II-24
II-1X
0.55
0.15
2.08
0.028
0.019
0.0198
0.001
0.001
0.001
0.001


II-25
II-1Y
0.22
0.35
0.27
0.060
0.004
0.0175
0.001
0.001
0.001
0.001


II-26
II-1Z
0.35
0.17
0.31
0.090
0.016
0.0307
0.001
0.001
0.001
0.001


II-27
II-2A
0.40
0.49
0.79
0.033
0.070
0.0108
0.001
0.001
0.001
0.001


II-28
II-2B
0.52
0.35
0.54
0.009
0.090
0.0108
0.001
0.001
0.001
0.001


II-29
II-2C
0.33
0.08
0.34
0.012
0.013
0.0061
0.008
0.001
0.001
0.001


II-30
II-2D
0.17
0.25
0.61
0.013
0.008
0.0075
0.001
0.001
0.001
0.001


II-31
II-2E
0.37
0.19
0.45
0.005
0.005
0.0195
0.011
0.001
0.001
0.001


II-32
II-2F
0.45
0.04
0.08
0.021
0.011
0.0199
0.001
0.001
0.001
0.001


II-33
II-2G
0.28
0.17
0.16
0.017
0.012
0.0256
0.005
0.001
0.001
0.001


II-34
II-2H
0.32
0.45
0.34
0.025
0.004
0.0218
0.001
0.001
0.001
0.001


II-35
II-2I
0.46
0.31
0.23
0.021
0.019
0.0335
0.014
0.001
0.001
0.001



















Formula





Ac3

(1)


Material
Chemical composition (mass %)
point
Dissolved N
satisfied
Heat
















No.
Zr
B
Ta
Hf
Others
(° C.)
(mass %)
or not
treatment





II-1
0.0001
0.0001
0
0

847
0.0081

II-a


II-2
0.0001
0.0001
0
0

814
0.0096

II-h


II-3
0.0001
0.0001
0
0

805
0.0089

II-d


II-4
0.0001
0.0001
0
0

791
0.0095

II-i


II-5
0.0001
0.0001
0
0

763
0.0141

II-j


II-6
0.0001
0.0001
0
0

753
0.0141

II-b


II-7
0.0001
0.0001
0
0

774
0.0175

II-j


II-8
0.0001
0.0001
0
0

824
0.0093

II-j


II-9
0.0001
0.0001
0
0

833
0.0109

II-h


II-10
0.0001
0.0001
0
0

799
0.0120

II-d


II-11
0.0001
0.0001
0
0

832
0.0079

II-i


II-12
0.0001
0.0001
0
0

849
0.0183

II-f


II-13
0.0001
0.0001
0
0

788
0.0179

II-h


II-14
0.0001
0.0001
0
0

784
0.0084

II-b


II-15
0.0001
0.0001
0
0

878
0.0227

II-g


II-16
0.0001
0.0001
0
0

801
0.0111

II-g


II-17
0.0001
0.0001
0
0

819
0.0073

II-d


II-18
0.0001
0.0001
0
0

844
0.0229

II-e


II-19
0.0001
0.0001
0
0

802
0.0302

II-c


II-20
0.0001
0.0001
0
0

806
0.0124

II-j


II-21
0.0001
0.0001
0
0

795
0.0183

II-f


II-22
0.0001
0.0001
0
0

751
0.0199

II-b


II-23
0.0001
0.0001
0
0

784
0.0130

II-i


II-24
0.0001
0.0001
0
0

724
0.0184

II-h


II-25
0.0001
0.0001
0
0

865
0.0161

II-d


II-26
0.0001
0.0001
0
0

852
0.0293

II-g


II-27
0.0001
0.0001
0
0

804
0.0094

II-a


II-28
0.0001
0.0001
0
0

770
0.0094

II-f


II-29
0.0001
0.0001
0
0

799
0.0011
x
II-j


II-30
0.0001
0.0001
0
0

829
0.0061

II-e


II-31
0.0001
0.0001
0
0

790
0.0129

II-g


II-32
0.0001
0.0001
0
0

789
0.0185

II-h


II-33
0.0001
0.0001
0
0

820
0.0222

II-c


II-34
0.0001
0.0001
0
0

823
0.0204

II-d


II-35
0.0001
0.0001
0
0

800
0.0254

II-f


















TABLE 9







Material

Chemical composition (mass %)



















No.
Steel No.
C
Si
Mn
P
S
N
Al
Ti
Nb
V
Zr





II-36
II-2J
0.23
0.29
0.09
0.010
0.022
0.0376
0.001
0.001
0.001
0.001
0.0001


II-37
II-2K
0.42
0.25
1.86
0.008
0.025
0.0443
0.001
0.001
0.001
0.001
0.0001


II-38
II-2L
0.16
0.50
0.94
0.004
0.009
0.0231
0.001
0.040
0.001
0.001
0.0001


II-39
II-2M
0.57
0.11
0.75
0.011
0.032
0.0285
0.006
0.001
0.030
0.001
0.0001


II-40
II-2N
0.56
0.25
0.34
0.016
0.006
0.0229
0.001
0.001
0.060
0.020
0.0001


II-41
II-2O
0.32
0.38
0.41
0.023
0.015
0.0223
0.007
0.001
0.001
0.001
0.05


II-42
II-2P
0.24
0.05
0.54
0.039
0.027
0.0099
0.001
0.001
0.001
0.001
0.0001


II-43
II-2Q
0.19
0.17
0.13
0.019
0.005
0.0398
0.023
0.030
0.001
0.040
0.0001


II-44
II-2R
0.47
0.35
0.88
0.021
0.002
0.0308
0.018
0.001
0.040
0.001
0.005


II-45
II-2S
0.50
0.16
1.23
0.025
0.015
0.0155
0.001
0.001
0.001
0.030
0.004


II-46
II-2T
0.32
0.33
0.14
0.027
0.013
0.0212
0.009
0.001
0.001
0.001
0.0001


II-47
II-2U
0.49
0.28
0.31
0.038
0.030
0.0301
0.001
0.001
0.001
0.001
0.0001


II-48
II-2V
0.18
0.16
0.44
0.041
0.019
0.0232
0.018
0.001
0.001
0.001
0.0001


II-49
II-2W
0.39
0.13
0.30
0.016
0.044
0.0388
0.001
0.050
0.001
0.050
0.0001


II-50
II-2X
0.27
0.32
0.22
0.017
0.015
0.0342
0.034
0.001
0.001
0.001
0.02


II-51
II-2Y
0.24
0.38
1.53
0.019
0.009
0.0199
0.001
0.001
0.001
0.001
0.0001


II-52
II-2Z
0.47
0.56
0.09
0.022
0.018
0.0371
0.028
0.010
0.040
0.001
0.0001


II-53
II-3A
0.38
0.44
0.32
0.008
0.009
0.0233
0.001
0.010
0.001
0.001
0.0001


II-54
II-3B
0.32
0.22
0.43
0.005
0.045
0.0243
0.008
0.010
0.001
0.001
0.0001


II-55
II-3C
0.27
0.12
0.12
0.012
0.019
0.0198
0.005
0.010
0.001
0.001
0.0001


II-56
II-3D
0.19
0.08
0.65
0.015
0.003
0.0188
0.003
0.030
0.001
0.001
0.0001


II-57
II-3E
0.47
0.09
0.99
0.009
0.023
0.0276
0.012
0.010
0.001
0.001
0.0001


II-58
II-3F
0.54
0.13
0.15
0.003
0.019
0.0324
0.010
0.010
0.001
0.001
0.0001


II-59
II-3G
0.28
0.12
1.22
0.034
0.039
0.0355
0.001
0.010
0.001
0.001
0.005


II-60
II-3H
0.23
0.08
0.56
0.028
0.011
0.0180
0.001
0.010
0.001
0.001
0.0001


II-61
II-3I
0.41
0.09
0.43
0.018
0.031
0.0233
0.001
0.010
0.001
0.001
0.0001


II-62
II-3J
0.53
0.21
0.39
0.011
0.008
0.0154
0.004
0.010
0.001
0.001
0.0001


II-63
II-3K
0.26
0.39
0.28
0.032
0.015
0.0198
0.001
0.010
0.001
0.001
0.0001


II-64
II-3L
0.51
0.43
0.11
0.008
0.026
0.0221
0.009
0.010
0.001
0.010
0.0001


II-65
II-3M
0.32
0.19
0.17
0.010
0.007
0.0308
0.001
0.010
0.020
0.001
0.0001


II-66
II-3N
0.50
0.27
0.35
0.008
0.012
0.0203
0.005
0.010
0.001
0.001
0.0001


II-67
II-3O
0.27
0.31
0.28
0.035
0.019
0.0198
0.002
0.010
0.001
0.001
0.0001


II-68
II-3P
0.32
0.37
0.76
0.047
0.013
0.0296
0.006
0.010
0.001
0.001
0.008


II-69
II-3Q
0.38
0.12
1.89
0.002
0.010
0.0201
0.001
0.010
0.001
0.001
0.0001


II-70
II-3R
0.35
0.18
0.23
0.019
0.002
0.0176
0.011
0.005
0.001
0.010
0.0001



















Formula







(1)


Material
Chemical composition (mass %)
Ac3 point
Dissolved N
satisfied
Heat















No.
B
Ta
Hf
Others
(° C.)
(mass %)
or not
treatment





II-36
0.0001
0
0

831
0.0362

II-1b


II-37
0.0001
0
0

740
0.0429

II-1i


II-38
0.0001
0
0

842
0.0103

II-1g


II-39
0.0001
0
0

750
0.0202

II-1i


II-40
0.0001
0
0

773
0.0074

II-1d


II-41
0.0001
0
0

819
0.0101

II-1c


II-42
0.0006
0
0

825
0.0079

II-1e


II-43
0.0001
0
0

864
0.0078

II-1h


II-44
0.0001
0
0

782
0.0140

II-1f


II-45
0.0001
0
0

758
0.0055
x
II-1j


II-46
0.0001
0.02
0

829
0.0137

II-1a


II-47
0.0001
0
0.05

798
0.0248

II-1c


II-48
0.0013
0
0.03

854
0.0091

II-1g


II-49
0.0001
0
0

817
0.0096

II-1i


II-50
0.0001
0.01
0

838
0.0116

II-1e


II-51
0.0001
0
0.03

796
0.0162

II-1h


II-52
0.0001
0
0

824
0.0132

II-1b


II-53
0.0001
0
0
Co: 4.5
805
0.0193

II-1d


II-54
0.0001
0
0
Mo: 0.04, Pb: 0.08
803
0.0167

II-1c


II-55
0.0001
0
0
Mo: 1.3
821
0.0137

II-1f


II-56
0.0001
0
0
W: 1.8
829
0.0079

II-1a


II-57
0.0008
0
0
W: 0.05, Ca: 0.016
760
0.0170

II-1e


II-58
0.0001
0
0
Ca: 0.008
772
0.0237

II-1j


II-59
0.0001
0.006
0
Ca: 0.02, REM: 0.009
800
0.0301

II-1g


II-60
0.0001
0
0
REM: 0.042
823
0.0140

II-1j


II-61
0.0001
0
0
Mg: 0.01, Cr: 1.3
788
0.0193

II-1c


II-62
0.0001
0
0
Li: 0.005
773
0.0098

II-1b


II-63
0.0001
0
0
Mg: 0.013, Ca: 0.003
842
0.0155

II-1i


II-64
0.0001
0
0
Co: 2.5, Mo: 0.3
795
0.0115

II-1f


II-65
0.0001
0
0
Cu: 0.4
810
0.0239

II-1e


II-66
0.0001
0
0
Cu: 3.2, Cr: 0.8
780
0.0142

II-1e


II-67
0.0001
0
0
Cu: 1.3, Ni: 3.1
839
0.0153

II-1g


II-68
0.0001
0
0
Ni: 3.5, Bi: 0.08
828
0.0218

II-1a


II-69
0.0001
0.01
0
Ni: 0.9
739
0.0151

II-1d


II-70
0.0001
0
0
Co: 1.9, Pb: 0.06
812
0.0074

II-1c


















TABLE 10







Material
Steel
Chemical composition (mass %)


















No.
No.
C
Si
Mn
P
S
N
Al
Ti
Nb
V





II-71
II-3S
0.25
0.05
0.25
0.036
0.009
0.0133
0.001
0.01
0.001
0.001


II-72
II-3T
0.45
0.55
0.11
0.009
0.01
0.0286
0.094
0.03
0.001
0.001


II-73
II-3T
0.45
0.55
0.11
0.009
0.01
0.0286
0.094
0.03
0.001
0.001


II-74
II-3T
0.45
0.55
0.11
0.009
0.01
0.0286
0.094
0.03
0.001
0.001


II-75
II-3T
0.45
0.55
0.11
0.009
0.01
0.0286
0.094
0.03
0.001
0.001


II-76
II-3U
0.19
0.23
0.94
0.013
0.022
0.0322
0.015
0.07
0.001
0.001


II-77
II-3U
0.19
0.23
0.94
0.013
0.022
0.0322
0.015
0.07
0.001
0.001


II-78
II-3U
0.19
0.23
0.94
0.013
0.022
0.0322
0.015
0.07
0.001
0.001


II-79
II-3U
0.19
0.23
0.94
0.013
0.022
0.0322
0.015
0.07
0.001
0.001


II-80
II-3V
0.31
0.18
0.43
0.007
0.009
0.0185
0.013
0.001
0.2
0.001


II-81
II-3V
0.31
0.18
0.43
0.007
0.009
0.0185
0.013
0.001
0.2
0.001


II-82
II-3V
0.31
0.18
0.43
0.007
0.009
0.0185
0.013
0.001
0.2
0.001


II-83
II-3V
0.31
0.18
0.43
0.007
0.009
0.0185
0.013
0.001
0.2
0.001


II-84
II-3W
0.27
0.47
0.23
0.021
0.017
0.0175
0.001
0.001
0.001
0.48


II-85
II-3W
0.27
0.47
0.23
0.021
0.017
0.0175
0.001
0.001
0.001
0.48


II-86
II-3W
0.27
0.47
0.23
0.021
0.017
0.0175
0.001
0.001
0.001
0.48


II-87
II-3W
0.27
0.47
0.23
0.021
0.017
0.0175
0.001
0.001
0.001
0.48


II-88
II-3X
0.20
0.05
0.12
0.018
0.012
0.0199
0.001
0.001
0.001
0.001


II-89
II-3X
0.20
0.05
0.12
0.018
0.012
0.0199
0.001
0.001
0.001
0.001


II-90
II-3X
0.20
0.05
0.12
0.018
0.012
0.0199
0.001
0.001
0.001
0.001


II-91
II-3X
0.20
0.05
0.12
0.018
0.012
0.0199
0.001
0.001
0.001
0.001


II-92
II-3Y
0.38
0.19
0.08
0.007
0.047
0.0099
0.012
0.001
0.001
0.001


II-93
II-3Y
0.38
0.19
0.08
0.007
0.047
0.0099
0.012
0.001
0.001
0.001


II-94
II-3Y
0.38
0.19
0.08
0.007
0.047
0.0099
0.012
0.001
0.001
0.001


II-95
II-3Y
0.38
0.19
0.08
0.007
0.047
0.0099
0.012
0.001
0.001
0.001


II-96
II-3Z
0.51
0.09
0.19
0.032
0.022
0.0221
0.035
0.001
0.001
0.001


II-97
II-3Z
0.51
0.09
0.19
0.032
0.022
0.0221
0.035
0.001
0.001
0.001


II-98
II-3Z
0.51
0.09
0.19
0.032
0.022
0.0221
0.035
0.001
0.001
0.001


II-99
II-3Z
0.51
0.09
0.19
0.032
0.022
0.0221
0.035
0.001
0.001
0.001


II-100
II-4A
0.35
0.33
0.28
0.005
0.003
0.0214
0.032
0.001
0.001
0.001


II-101
II-4A
0.35
0.33
0.28
0.005
0.003
0.0214
0.032
0.001
0.001
0.001


II-102
II-4A
0.35
0.33
0.28
0.005
0.003
0.0214
0.032
0.001
0.001
0.001


II-103
II-4A
0.35
0.33
0.28
0.005
0.003
0.0214
0.032
0.001
0.001
0.001



















Formula





Ac3
Dissolved
(1)


Material
Chemical composition (mass %)
point
N
satisfied
Heat
















No.
Zr
B
Ta
Hf
Others
(° C.)
(mass %)
or not
treatment





II-71
0.0001
0.0001
0
0
Mo: 1.1
833
0.0093

II-b


II-72
0.0001
0.0001
0
0

851
0.0051
x
II-a


II-73
0.0001
0.0001
0
0


0.0123
x
II-c


II-74
0.0001
0.0001
0
0


0.0128
x
II-e


II-75
0.0001
0.0001
0
0


0.0126
x
II-h


II-76
0.0001
0.0001
0
0

847
0.0046
x
II-a


II-77
0.0001
0.0001
0
0


0.0037
x
II-b


II-78
0.0001
0.0001
0
0


0.0071
x
II-i


II-79
0.0001
0.0001
0
0


0.0079
x
II-j


II-80
0.0001
0.0001
0
0

803
0.0056
x
II-b


II-81
0.0001
0.0001
0
0


0.0066
x
II-g


II-82
0.0001
0.0001
0
0


0.0076
x
II-h


II-83
0.0001
0.0001
0
0


0.0134
x
II-i


II-84
0.0001
0.0001
0
0

884
0.0001
x
II-a


II-85
0.0001
0.0001
0
0


0.0005
x
II-d


II-86
0.0001
0.0001
0
0


0.0072
x
II-f


II-87
0.0001
0.0001
0
0


0.0121
x
II-i


II-88
0.18
0.0001
0
0

831
0.0005
x
II-a


II-89
0.18
0.0001
0
0


0.0007
x
II-b


II-90
0.18
0.0001
0
0


0.0062
x
II-i


II-91
0.18
0.0001
0
0


0.0066
x
II-j


II-92
0.0001
0.0014
0
0

801
0.0045
x
II-b


II-93
0.0001
0.0014
0
0


0.0089
x
II-e


II-94
0.0001
0.0014
0
0


0.0089
x
II-g


II-95
0.0001
0.0014
0
0


0.0091
x
II-i


II-96
0.0001
0.0001
0.038
0

800
0.0005
x
II-a


II-97
0.0001
0.0001
0.038
0


0.0022
x
II-b


II-98
0.0001
0.0001
0.038
0


0.0151
x
II-h


II-99
0.0001
0.0001
0.038
0


0.0208
x
II-i


II-100
0.0001
0.0001
0
0.038

800
0.0007
x
II-b


II-101
0.0001
0.0001
0
0.038


0.0198
x
II-e


II-102
0.0001
0.0001
0
0.038


0.0206
x
II-h


II-103
0.0001
0.0001
0
0.038


0.0208
x
II-j




















TABLE 11





Heat



Cooling stop


treatment
Heating

Cooling rate
temperature


pattern
temperature (° C.)
Hot working
(° C./s)
(° C.)



















II-a
800
Yes
5
500


II-b
800
No
5
450


II-c
900
Yes
5
500


II-d
900
No
5
500


II-e
1000
Yes
0.5
480


II-f
1000
Yes
1
500


II-g
1000
No
5
500


II-h
1000
Yes
5
500


II-i
1100
Yes
1
430


II-j
1200
Yes
3
500









Each test specimen shown in Tables 8 to 10 was forged into parts by using a servo hydraulic type testing machine (with a capacity of 200 kN) under the following conditions.


Strain rate: 0.001 to 240/s


Working temperature: 20 to 400° C.


Compression ratio: 20 to 80%


The strain rate is an average of values measured during working (elastic deformation).


The resulting parts were examined for their surface under a stereomicroscope with a magnification of ×20 to see if there is cracking. Tables 12 to 14 show the test results including working conditions, cracking, and deformation resistance.


Each part was also tested for Vickers hardness (Hv) by using a Vickers hardness tester under the following conditions.


Load: 1000 g

Position of measurement: D/4 off the center of the cross section of the part (D=diameter of part)


Number of repetitions of measurement: 5


The results of measurement are shown in Tables 12 to 14.


















TABLE 12










Compression
Deformation
Hardness after




Part
Material
Steel
Strain
Working
ratio
resistance
working

Formula (3)


No.
No.
No.
rate (/s)
temperature (° C.)
(%)
(MPa)
(Hv)
Cracking
satisfied or not
























II-1
II-1
II-1A
100
60
20
390
234
No



II-2
II-2
II-1B
140
80
80
671
282
No



II-3
II-3
II-1C
180
20
60
643
277
No



II-4
II-4
II-1D
220
60
80
697
286
No



II-5
II-5
II-1E
120
20
40
905
326
No



II-6
II-6
II-1F
100
40
80
1019
345
Yes



II-7
II-7
II-1G
160
60
80
807
313
Yes



II-8
II-8
II-1H
140
20
60
548
261
No



II-9
II-9
II-1I
100
80
60
614
274
No



II-10
II-10
II-IJ
180
20
80
727
294
No



II-11
II-11
II-1K
140
100
80
687
283
No



II-12
II-12
II-1L
220
20
20
416
248
No



II-13
II-13
II-1M
160
60
80
952
337
No



II-14
II-14
II-1N
100
40
40
1035
342
Yes



II-15
II-15
II-1O
120
20
60
486
264
Yes



II-16
II-16
II-1P
240
60
80
622
275
No



II-17
II-17
II-1Q
200
80
20
746
292
No



II-18
II-18
II-1R
140
20
80
674
296
No



II-19
II-19
II-1S
180
20
20
740
314
No



II-20
II-20
II-1T
140
20
80
734
295
No



II-21
II-21
II-1U
100
20
20
828
317
No



II-22
II-22
II-1V
160
40
60
881
327
No



II-23
II-23
II-1W
220
20
40
585
271
No



II-24
II-24
II-1X
120
60
80
1182
376
Yes



II-25
II-25
II-1Y
100
20
80
628
282
Yes



II-26
II-26
II-1Z
140
80
80
770
318
Yes



II-27
II-27
II-2A
200
20
20
760
297
Yes



II-28
II-28
II-2B
100
40
80
998
336
Yes



II-29
II-29
II-2C
160
20
20
652
271
No
x


II-30
II-30
II-2D
180
20
60
468
245
No



II-31
II-31
II-2E
0.001
20
80
960
334
Yes



II-32
II-31
II-2E
0.1
60
80
1000
340
Yes



II-33
II-31
II-2E
1
20
40
958
333
Yes



II-34
II-31
II-2E
10
80
80
1005
341
Yes



II-35
II-31
II-2E
100
100
20
890
322
No



II-36
II-31
II-2E
200
200
60
840
314
No



II-37
II-32
II-2F
220
300
80
928
334
Yes



II-38
II-33
II-2G
140
400
20
993
348
Yes



II-39
II-34
II-2H
100
20
80
768
309
No



II-40
II-35
II-2I
160
20
80
793
318
No


























TABLE 13










Compression
Deformation
Hardness after




Part
Material
Steel
Strain
Working
ratio
resistance
working

Formula (3)


No.
No.
No.
rate (/s)
temperature (° C.)
(%)
(MPa)
(Hv)
Cracking
satisfied or not
























II-41
II-36
II-2J
120
60
40
624
301
No



II-42
II-37
II-2K
180
80
60
978
367
Yes



II-43
II-38
II-2L
100
80
20
703
288
No



II-44
II-39
II-2M
140
20
80
966
342
No



II-45
II-40
II-2N
220
20
80
807
303
No



II-46
II-41
II-2O
120
60
20
786
302
No



II-47
II-42
II-2P
200
40
80
528
256
No



II-48
II-43
II-2Q
160
100
40
551
260
No



II-49
II-44
II-2R
100
20
20
981
338
No



II-50
II-45
II-2S
180
40
80
929
321
No
x


II-51
II-46
II-2T
100
20
60
735
297
No



II-52
II-47
II-2U
140
60
80
903
336
No



II-53
II-48
II-2V
200
20
40
429
241
No



II-54
II-49
II-2W
160
80
20
788
302
No



II-55
II-50
II-2X
220
20
40
508
257
No



II-56
II-51
II-2Y
180
150
80
825
314
No



II-57
II-52
II-2Z
100
20
40
906
325
No



II-58
II-53
II-3A
120
40
60
878
326
No



II-59
II-54
II-3B
100
60
80
856
320
No



II-60
II-55
II-3C
160
20
80
620
278
No



II-61
II-56
II-3D
140
80
60
668
280
No



II-62
II-57
II-3E
200
20
80
872
323
No



II-63
II-58
II-3F
220
20
80
806
319
No



II-64
II-59
II-3G
100
150
20
988
355
No



II-65
II-60
II-3H
100
40
60
729
296
No



II-66
II-61
II-3I
180
60
40
817
316
No



II-67
II-62
II-3J
200
80
80
923
324
No



II-68
II-63
II-3K
100
20
40
744
300
No



II-69
II-64
II-3L
120
20
60
955
331
No



II-70
II-65
II-3M
180
20
80
663
295
No



II-71
II-66
II-3N
240
60
20
818
311
No



II-72
II-67
II-3O
140
20
60
688
291
No



II-73
II-68
II-3P
160
40
80
802
316
No



II-74
II-69
II-3Q
220
40
40
889
324
No



II-75
II-70
II-3R
100
60
60
860
311
No



II-76
II-71
II-3S
160
20
80
604
271
No



II-77
II-72
II-3T
120
20
20
860
305
No
x


II-78
II-73
II-3T
180
80
80
830
311
No



II-79
II-74
II-3T
100
40
40
910
325
No



II-80
II-75
II-3T
140
20
80
830
312
No


























TABLE 14









Working

Deformation
Hardness after




Part
Material
Steel
Strain
temperature
Compression
resistance
working

Formula (3)


No.
No.
No.
rate (/s)
(° C.)
ratio (%)
(MPa)
(Hv)
Cracking
satisfied or not
























II-81
II-76
II-3U
200
20
40
515
247
No
x


II-82
II-77
II-3U
100
60
80
705
278
No
x


II-83
II-78
II-3U
160
40
20
596
267
No



II-84
II-79
II-3U
240
20
40
456
245
No



II-85
II-80
II-3V
120
40
60
757
288
No
x


II-86
II-81
II-3V
180
20
40
647
275
No



II-87
II-82
II-3V
100
60
80
807
303
No



II-88
II-83
II-3V
140
20
20
707
292
No



II-89
II-84
II-3W
240
80
80
609
258
No
x


II-90
II-85
II-3W
160
40
60
689
272
No
x


II-91
II-86
II-3W
100
20
60
759
294
No



II-92
II-87
II-3W
120
40
80
750
298
No



II-93
II-88
II-3X
180
60
40
495
240
No
x


II-94
II-89
II-3X
160
20
20
485
238
No
x


II-95
II-90
II-3X
200
100
80
505
251
No



II-96
II-91
II-3X
140
20
20
515
253
No



II-97
II-92
II-3Y
100
80
40
835
300
No
x


II-98
II-93
II-3Y
220
40
60
615
272
No



II-99
II-94
II-3Y
120
60
80
785
300
No



II-100
II-95
II-3Y
160
20
80
685
284
No



II-101
II-96
II-3Z
180
100
20
866
302
No
x


II-102
II-97
II-3Z
240
20
80
696
275
No
x


II-103
II-98
II-3Z
140
20
40
847
317
No



II-104
II-99
II-3Z
100
40
80
927
336
No



II-105
II-100
II-4A
220
20
20
605
258
No
x


II-106
II-101
II-4A
120
20
60
756
307
No



II-107
II-102
II-4A
200
40
80
656
291
No



II-108
II-103
II-4A
160
60
40
736
304
No










Steels in this example are rated as good in cold workability if they give crack-free parts and exhibit low deformation resistance relative to parts hardness (or satisfy the formula (3)). Those parts having a Vickers hardness (Hv) larger than 240 are rated as good in strength.


Incidentally, Tables 12 to 14 show whether or not each specimen satisfies the formula (3) by symbols “◯” and “X” respectively.


It is noted from Tables 12 to 14 that the steel containing chemical components and dissolved nitrogen as specified in the second embodiment of the present invention excels in cold workability and gives parts having high strength when it is worked under desirable conditions (such as strain rate and working temperature).


By contrast, the steel failing to meet the requirements specified in the second embodiment of the present invention is vulnerable to cracking or poor in balance between cold workability and parts hardness, with the formula (3) not satisfied, as mentioned below.


Part No. II-1 (formed from steel No. II-1A with a C content lower than specified in the second embodiment of the present invention) has a lower hardness than specified.


Part No. II-6 (formed from steel No. II-1F with a C content higher than specified in the second embodiment of the present invention) suffers cracking.


Part No. II-7 (formed from steel No. II-1G with a Si content lower than specified in the second embodiment of the present invention) suffers cracking.


Part No. II-14 (formed from steel No. II-1N with a Si content higher than specified in the second embodiment of the present invention) suffers cracking.


Part No. II-15 (formed from steel No. II-1O with a Mn content lower than specified in the second embodiment of the present invention) suffers cracking.


Part No. II-24 (formed from steel No. II-1X with a Mn content higher than specified in the second embodiment of the present invention) suffers cracking.


Parts No. II-25 and II-26 (formed from steels No. II-1Y and II-1Z respectively with a P content higher than specified in the second embodiment of the present invention) suffer cracking.


Parts No. II-27 and II-28 (formed from steels No. II-2A and II-2B respectively with a S content higher than specified in the second embodiment of the present invention) suffer cracking.


Part No. II-29 (formed from steel No. II-2C with a lower content of dissolved N than specified (no less than 0.007%) in the second embodiment of the present invention) does not satisfy the formula (2) and hence is poor in balance between cold workability and hardness.


Part No. II-42 (formed from steel No. II-2K with a higher content of dissolved N than specified in the second embodiment of the present invention) suffers cracking.


Parts No. II-31 to II-34 (formed from steel No. II-2E having the chemical composition as specified in the second embodiment of the present invention) suffer cracking due to dynamic strain ageing which results from a low strain rate at the time of high-speed cold working.


Parts No. II-37 and II-38 (formed from steels No. II-2F and II-2G respectively having the chemical composition as specified in the second embodiment of the present invention) suffer cracking due to dynamic strain ageing which results from a high temperature at the time of high-speed cold working.


Part No. II-50 (formed from steel II-2S containing a less amount of dissolved N than specified, with the formula (1) not satisfied, as shown in Table 9) is poor in balance between cold workability and hardness, with the formula (3) not satisfied. Those steels which do not satisfy the formula (1) may contain an adequate amount of dissolved N as specified in the second embodiment of the present invention if they undergo heat treatment adequately. This is true with material Nos. II-73, 74, 75, 78, 79, 81, 82, 83, 86, 87, 90, 91, 93, 94, 95, 98, 99, 101, 102, and 103, shown in Table 10.


Parts Nos. II-77, 81, 82, 85, 89, 90, 93, 94, 97, 101, 102, and 105 (formed from steels Nos. II-2S and II-3T to II-4A with the chemical composition specified in the second embodiment of the present invention) do not contain the prescribed amount of dissolved N because they are not produced according to the heat treatment patterns II-a to II-j shown in Table 11 and hence they do not satisfy the formula (3). In other words, they are poor in balance between cold workability and parts hardness.


Example 3 and Comparative Example According to the Third Embodiment of the Present Invention

Steel samples, numbered III-LA to III-3S, (in the form of ingot) each having the chemical composition shown in Tables 15 and 16, were prepared by continuous casting from a converter. (Steel numbers are accompanied by parts numbers for the sake of convenience.) Each ingot was rolled into a wire, 12 mm in diameter. The thus obtained wire underwent heat treatment consisting of steps of heating, (hot working), and quenching. This heat treatment conforms to the patterns III-a to III-j shown in Table 17. The heat-treated wire should preferably be kept at the heating temperature for at least 10 minutes, desirably at least 30 minutes.


Then, a test specimen measuring 4 mm in diameter and 6 mm long was cut out of the central part of the heat-treated wire.


In Tables 15 to 16, “N” represents the total amount of N (in mass %), “dissolved N” represents the amount of dissolved N (in mass %), and “N compounds” represents the amount of N compounds (in mass %). The amount of dissolved N is a difference between the total amount of N and the amount of N compounds in the steel calculated according to JIS G1228.










TABLE 15







Steel No./III-part
Chemical composition (mass %)

















No.
C
Si
Mn
P
S
N
Al
Ti
Nb
V





III-1A/III-1
0.01
0.10
0.17
0.018
0.020
0.0107
0.0008
0.0017
0.0007
0.0007


III-1B/III-2
0.07
0.16
0.49
0.008
0.015
0.0133
0.0009
0.0007
0.0007
0.0008


III-1C/III-3
0.12
0.13
0.34
0.025
0.030
0.0092
0.0009
0.0016
0.0007
0.0007


III-1D/III-4
0.25
0.09
0.24
0.023
0.022
0.0119
0.0008
0.0017
0.0007
0.0007


III-1E/III-5
0.51
0.02
0.12
0.005
0.010
0.0130
0.0007
0.0009
0.0007
0.0006


III-1F/III-6
0.64
0.08
0.16
0.012
0.013
0.0124
0.0006
0.0017
0.0008
0.0007


III-1G/III-7
0.12
0.003
0.24
0.012
0.014
0.0138
0.0006
0.0017
0.0007
0.0006


III-1H/III-8
0.08
0.19
0.39
0.010
0.005
0.0138
0.0006
0.0018
0.0007
0.0005


III-1I/III-9
0.14
0.25
0.13
0.006
0.030
0.0097
0.0006
0.0011
0.0006
0.0005


III-1J/III-10
0.21
0.43
0.17
0.012
0.017
0.0124
0.0007
0.0017
0.0006
0.0006


III-1K/III-11
0.19
0.39
0.12
0.016
0.005
0.0123
0.0007
0.0012
0.0006
0.0006


III-1L/III-12
0.28
0.51
0.26
0.014
0.038
0.0156
0.0007
0.0017
0.0007
0.0006


III-1M/III-13
0.07
0.58
0.44
0.021
0.016
0.0144
0.0007
0.0017
0.0007
0.0007


III-1N/III-14
0.31
0.65
0.20
0.019
0.026
0.0096
0.0007
0.0013
0.0007
0.0007


III-1O/III-15
0.08
0.37
0.01
0.043
0.040
0.0168
0.0007
0.0017
0.0008
0.0007


III-1P/III-16
0.21
0.21
0.21
0.018
0.031
0.0106
0.0008
0.0017
0.0008
0.0008


III-1Q/III-17
0.23
0.37
0.18
0.040
0.022
0.0098
0.0008
0.0017
0.0008
0.0008


III-1R/III-18
0.32
0.53
0.47
0.028
0.002
0.0236
0.0008
0.0006
0.0008
0.0008


III-1S/III-19
0.12
0.58
0.52
0.006
0.012
0.0234
0.0008
0.0019
0.0008
0.0009


III-1T/III-20
0.17
0.48
1.04
0.007
0.042
0.0176
0.0006
0.0019
0.0007
0.0009


III-1U/III-21
0.15
0.14
1.17
0.031
0.017
0.0144
0.0007
0.0019
0.0007
0.0009


III-1V/III-22
0.45
0.20
1.54
0.003
0.037
0.0214
0.0007
0.0019
0.0007
0.0009


III-1W/III-23
0.33
0.07
1.94
0.027
0.008
0.0116
0.0007
0.0018
0.0007
0.0009


III-1X/III-24
0.56
0.19
2.07
0.030
0.023
0.0144
0.0007
0.0008
0.0007
0.0008


III-1Y/III-25
0.34
0.36
0.29
0.063
0.003
0.0142
0.0008
0.0018
0.0007
0.0008


III-1Z/III-26
0.25
0.19
0.34
0.091
0.020
0.0221
0.0008
0.0018
0.0007
0.0008


III-2A/III-27
0.26
0.54
0.77
0.026
0.071
0.0107
0.0007
0.0019
0.0007
0.0007


III-2B/III-28
0.22
0.37
0.58
0.014
0.095
0.0088
0.0008
0.0018
0.0008
0.0007


III-2C/III-29
0.19
0.09
0.37
0.015
0.014
0.0057
0.0007
0.0018
0.0007
0.0006


III-2D/III-30
0.27
0.23
0.60
0.015
0.013
0.0082
0.0008
0.0018
0.0008
0.0006


III-2E/III-31-36
0.13
0.21
0.47
0.006
0.008
0.0139
0.0007
0.0018
0.0008
0.0006


III-2F/III-37
0.22
0.01
0.13
0.023
0.021
0.0154
0.0007
0.0017
0.0007
0.0006


III-2G/III-38
0.33
0.21
0.13
0.022
0.010
0.0185
0.0007
0.0017
0.0007
0.0005


III-2H/III-39
0.32
0.48
0.38
0.027
0.003
0.0169
0.0007
0.0017
0.0007
0.0007


III-2I/III-40
0.24
0.29
0.22
0.022
0.016
0.0249
0.0007
0.0018
0.0008
0.0007


III-2J/III-41
0.09
0.28
0.13
0.008
0.018
0.0271
0.0007
0.0017
0.0009
0.0006


III-2K/III-42
0.32
0.22
1.87
0.010
0.023
0.0413
0.0007
0.0016
0.0009
0.0006


III-2L/III-43
0.30
0.55
0.99
0.001
0.011
0.0163
0.0007
0.0016
0.0009
0.0007


III-2M/III-44
0.31
0.12
0.76
0.015
0.029
0.0220
0.0007
0.0016
0.0009
0.0007


III-2N/III-45
0.28
0.30
0.39
0.019
0.005
0.0162
0.0008
0.0010
0.0008
0.0007
















Dissolved
N



Steel No./III-part
Chemical composition (mass %)
N
compounds
Heat















No.
Zr
B
Ta
Hf
Others
(mass %)
(mass %)
treatment





III-1A/III-1
0.0009
0.00008
0.00006
0.00005

0.0093
0.0014
III-a


III-1B/III-2
0.0009
0.00008
0.00006
0.00005

0.0121
0.0012
III-h


III-1C/III-3
0.0009
0.00008
0.00008
0.00005

0.0077
0.0015
III-c


III-1D/III-4
0.0008
0.00009
0.00008
0.00005

0.0105
0.0014
III-g


III-1E/III-5
0.0008
0.00009
0.00008
0.00005

0.0119
0.0011
III-j


III-1F/III-6
0.0009
0.00009
0.00007
0.00006

0.0110
0.0014
III-f


III-1G/III-7
0.0008
0.00009
0.00006
0.00006

0.0124
0.0013
III-a


III-1H/III-8
0.0008
0.00009
0.00006
0.00005

0.0124
0.0013
III-j


III-1I/III-9
0.0009
0.00009
0.00006
0.00005

0.0085
0.0011
III-b


III-1J/III-10
0.0009
0.00008
0.00006
0.00004

0.0110
0.0014
III-i


III-1K/III-11
0.0009
0.00008
0.00007
0.00004

0.0111
0.0012
III-i


III-1L/III-12
0.0009
0.00009
0.00007
0.00003

0.0142
0.0014
III-g


III-1M/III-13
0.0008
0.00008
0.00008
0.00006

0.0130
0.0014
III-h


III-1N/III-14
0.0007
0.00008
0.00008
0.00006

0.0083
0.0013
III-f


III-1O/III-15
0.0007
0.00009
0.00007
0.00005

0.0154
0.0014
III-g


III-1P/III-16
0.0007
0.00009
0.00007
0.00006

0.0091
0.0015
III-g


III-1Q/III-17
0.0007
0.00009
0.00008
0.00006

0.0083
0.0015
III-d


III-1R/III-18
0.0007
0.00009
0.00007
0.00006

0.0225
0.0012
III-e


III-1S/III-19
0.0008
0.00008
0.00007
0.00006

0.0218
0.0016
III-j


III-1T/III-20
0.0008
0.00007
0.00007
0.00007

0.0162
0.0014
III-j


III-1U/III-21
0.0008
0.00007
0.00007
0.00008

0.0129
0.0015
III-h


III-1V/III-22
0.0008
0.00007
0.00006
0.00008

0.0199
0.0015
III-g


III-1W/III-23
0.0008
0.00007
0.00006
0.00007

0.0101
0.0015
III-d


III-1X/III-24
0.0008
0.00007
0.00005
0.00007

0.0133
0.0011
III-h


III-1Y/III-25
0.0008
0.00008
0.00005
0.00007

0.0127
0.0015
III-e


III-1Z/III-26
0.0007
0.00008
0.00006
0.00006

0.0206
0.0015
III-f


III-2A/III-27
0.0008
0.00008
0.00006
0.00006

0.0093
0.0014
III-j


III-2B/III-28
0.0008
0.00008
0.00006
0.00007

0.0073
0.0015
III-b


III-2C/III-29
0.0008
0.00008
0.00007
0.00007

0.0043
0.0014
III-i


III-2D/III-30
0.0008
0.00008
0.00007
0.00007

0.0067
0.0015
III-d


III-2E/III-31-36
0.0008
0.00008
0.00007
0.00007

0.0125
0.0014
III-g


III-2F/III-37
0.0009
0.00007
0.00007
0.00007

0.0141
0.0014
III-g


III-2G/III-38
0.0009
0.00008
0.00007
0.00007

0.0172
0.0013
III-f


III-2H/III-39
0.0008
0.00008
0.00006
0.00007

0.0155
0.0014
III-c


III-2I/III-40
0.0008
0.00008
0.00006
0.00007

0.0234
0.0014
III-f


III-2J/III-41
0.0008
0.00008
0.00006
0.00006

0.0257
0.0014
III-b


III-2K/III-42
0.0007
0.00008
0.00006
0.00006

0.0400
0.0013
III-i


III-2L/III-43
0.0007
0.00009
0.00006
0.00006

0.0150
0.0014
III-d


III-2M/III-44
0.0008
0.00009
0.00006
0.00006

0.0206
0.0014
III-j


III-2N/III-45
0.0008
0.00008
0.00006
0.00007

0.0149
0.0012
III-g

















TABLE 16







Steel No./III-
Chemical composition (mass %)


















part No.
C
Si
Mn
P
S
N
Al
Ti
Nb
V
Zr





III-2O/III-46
0.25
0.41
0.44
0.021
0.018
0.0166
0.0008
0.0016
0.0008
0.0008
0.0008


III-2P/III-47
0.33
0.15
0.64
0.038
0.029
0.0142
0.0009
0.0016
0.0008
0.0008
0.0009


III-2Q/III-48
0.06
0.15
0.11
0.016
0.008
0.0299
0.0009
0.0017
0.0008
0.0009
0.0008


III-2R/III-49
0.34
0.34
0.87
0.024
0.004
0.0219
0.0009
0.0017
0.0008
0.0008
0.0008


III-2S/III-50
0.21
0.34
1.08
0.012
0.006
0.0089
0.0045
0.0015
0.0008
0.0008
0.0007


III-2T/III-51
0.31
0.29
0.10
0.025
0.011
0.0167
0.0009
0.0017
0.0008
0.0008
0.0008


III-2U/III-52
0.35
0.04
0.84
0.023
0.034
0.0102
0.0017
0.0017
0.0009
0.0008
0.0008


III-2V/III-53
0.08
0.54
0.43
0.008
0.012
0.0123
0.0008
0.0230
0.0008
0.0007
0.0008


III-2W/III-54
0.11
0.40
0.08
0.032
0.019
0.0067
0.0008
0.0017
0.0008
0.0034
0.0008


III-2X/III-55
0.15
0.31
0.21
0.021
0.019
0.0248
0.0008
0.0016
0.0008
0.0007
0.0008


III-2Y/III-56
0.38
0.41
1.56
0.020
0.010
0.0148
0.0008
0.0016
0.0008
0.0006
0.0007


III-2Z/III-57
0.51
0.11
1.54
0.041
0.005
0.0091
0.0021
0.0025
0.0007
0.0033
0.0006


III-3A/III-58
0.28
0.47
0.35
0.013
0.014
0.0162
0.0007
0.0017
0.0007
0.0007
0.0007


III-3B/III-59
0.34
0.23
0.44
0.004
0.044
0.0188
0.0007
0.0016
0.0008
0.0007
0.0007


III-3C/III-60
0.25
0.05
0.12
0.011
0.018
0.0154
0.0008
0.0016
0.0008
0.0008
0.0008


III-3D/III-61
0.13
0.13
0.70
0.017
0.005
0.0137
0.0008
0.0016
0.0008
0.0009
0.0008


III-3E/III-62
0.26
0.12
1.02
0.012
0.026
0.0201
0.0008
0.0017
0.0009
0.0009
0.0009


III-3F/III-63
0.05
0.15
0.17
0.001
0.017
0.0252
0.0008
0.0015
0.0009
0.0009
0.0008


III-3G/III-64
0.31
0.13
1.23
0.038
0.043
0.0258
0.0007
0.0016
0.0008
0.0009
0.0008


III-3H/III-65
0.40
0.12
0.60
0.032
0.015
0.0125
0.0007
0.0016
0.0008
0.0009
0.0008


III-3I/III-66
0.38
0.12
0.46
0.021
0.034
0.0168
0.0006
0.0015
0.0008
0.0008
0.0008


III-3J/III-67
0.15
0.22
0.40
0.012
0.009
0.0114
0.0006
0.0015
0.0008
0.0008
0.0008


III-3K/III-68
0.31
0.42
0.31
0.035
0.018
0.0141
0.0006
0.0015
0.0008
0.0008
0.0006


III-3L/III-69
0.37
0.44
0.12
0.009
0.027
0.0165
0.0007
0.0014
0.0008
0.0008
0.0006


III-3M/III-70
0.27
0.17
0.15
0.008
0.005
0.0240
0.0007
0.0014
0.0008
0.0008
0.0006


III-3N/III-71
0.25
0.26
0.34
0.007
0.011
0.0157
0.0008
0.0014
0.0008
0.0008
0.0006


III-3O/III-72
0.34
0.32
0.29
0.036
0.020
0.0147
0.0006
0.0014
0.0007
0.0008
0.0006


III-3P/III-73
0.42
0.34
0.73
0.044
0.010
0.0234
0.0007
0.0006
0.0007
0.0008
0.0008


III-3Q/III-74
0.33
0.13
1.90
0.003
0.011
0.0150
0.0006
0.0015
0.0008
0.0009
0.0008


III-3R/III-75
0.25
0.20
0.25
0.021
0.005
0.0128
0.0006
0.0015
0.0007
0.0009
0.0008


III-3S/III-76
0.27
0.08
0.28
0.039
0.012
0.0092
0.0006
0.0015
0.0008
0.0009
0.0007

















N



Steel No./III-
Chemical composition (mass %)
Dissolved N
compounds
Heat














part No.
B
Ta
Hf
Others
(mass %)
(mass %)
treatment





III-2O/III-46
0.00008
0.00006
0.00006

0.0152
0.0014
III-f


III-2P/III-47
0.00008
0.00006
0.00006

0.0127
0.0015
III-i


III-2Q/III-48
0.00007
0.00007
0.00005

0.0284
0.0016
III-h


III-2R/III-49
0.00007
0.00007
0.00006

0.0204
0.0015
III-f


III-2S/III-50
0.00008
0.00007
0.00005

0.0056
0.0033
III-j


III-2T/III-51
0.00008
0.00006
0.00006

0.0152
0.0015
III-g


III-2U/III-52
0.00200
0.00006
0.00006

0.0057
0.0045
III-c


III-2V/III-53
0.00009
0.00006
0.00006

0.0046
0.0077
III-e


III-2W/III-54
0.00008
0.00007
0.00007

0.0045
0.0022
III-h


III-2X/III-55
0.00008
0.00006
0.00007

0.0234
0.0014
III-f


III-2Y/III-56
0.00007
0.00006
0.00007

0.0135
0.0014
III-g


III-2Z/III-57
0.00018
0.00006
0.00007

0.0059
0.0032
III-b


III-3A/III-58
0.00008
0.00006
0.00006
Co: 4.2
0.0148
0.0014
III-d


III-3B/III-59
0.00008
0.00006
0.00005
Mo: 0.08, Pb: 0.02
0.0174
0.0014
III-c


III-3C/III-60
0.00008
0.00006
0.00005
Mo: 1.5
0.0139
0.0014
III-e


III-3D/III-61
0.00008
0.00007
0.00005
W: 1.2
0.0122
0.0015
III-b


III-3E/III-62
0.00007
0.00007
0.00005
W: 0.08, Ca: 0.024
0.0185
0.0015
III-e


III-3F/III-63
0.00006
0.00007
0.00006
Ca: 0.011
0.0238
0.0014
III-h


III-3G/III-64
0.00007
0.00007
0.00006
Ca: 0.04, REM: 0.01
0.0244
0.0014
III-f


III-3H/III-65
0.00007
0.00007
0.00007
REM: 0.03
0.0111
0.0014
III-d


III-3I/III-66
0.00008
0.00006
0.00007
Mg: 0.015, Cr: 1.7
0.0155
0.0013
III-j


III-3J/III-67
0.00008
0.00006
0.00008
Li: 0.012
0.0101
0.0013
III-b


III-3K/III-68
0.00009
0.00006
0.00008
Mg: 0.011, Ca: 0.02
0.0128
0.0013
III-i


III-3L/III-69
0.00008
0.00006
0.00008
Co: 3.4, Mo: 0.8
0.0152
0.0013
III-f


III-3M/III-70
0.00008
0.00007
0.00007
Cu: 0.5
0.0227
0.0013
III-e


III-3N/III-71
0.00008
0.00006
0.00007
Cu: 2.1, Cr: 1.2
0.0144
0.0014
III-e


III-3O/III-72
0.00008
0.00006
0.00006
Cu: 0.9, Ni: 2.1
0.0135
0.0012
III-g


III-3P/III-73
0.00008
0.00006
0.00006
Ni: 2.4, Bi: 0.05
0.0223
0.0011
III-e


III-3Q/III-74
0.00006
0.00006
0.00006
Ni: 1.2
0.0137
0.0013
III-b


III-3R/III-75
0.00006
0.00005
0.00006
Co: 0.8, Pb: 0.03
0.0115
0.0013
III-c


III-3S/III-76
0.00006
0.00005
0.00007
Mo: 1.5
0.0079
0.0013
III-a




















TABLE 17





Heat



Cooling stop


treatment
Heating

Cooling rate
temperature


pattern No.
temperature (° C.)
Working
(° C./s)
(° C.)



















III-a
800
Yes
1
300


III-b
800
No
1
400


III-c
900
Yes
1
500


III-d
900
No
1
300


III-e
1000
Yes
0.5
300


III-f
1000
Yes
1
500


III-g
1000
No
5
400


III-h
1000
Yes
10
500


III-i
1100
Yes
1
300


III-j
1200
Yes
1
500









Each test specimen shown in Tables 15 and 16 was forged into parts by using a servo hydraulic type testing machine (with a capacity of 200 kN) under the following conditions.


Strain rate: 0.001 to 240/s


Working temperature: 20 to 400° C.


Compression ratio: 20 to 80%


The strain rate is an average of values measured during working (elastic deformation).


The resulting parts were examined for their surface under a stereomicroscope with a magnification of ×20 to see if there is cracking. Tables 18 and 19 show the test results including working conditions, cracking, and deformation resistance.


Each part was also tested for Vickers hardness (Hv) by using a micro-Vickers hardness tester under the following conditions.


Load: 1000 g

Position of measurement: D/4 off the center of the cross section of the part (D=diameter of part)


Number of repetitions of measurement: 5


The results of measurement are shown in Tables 18 and 19.

















TABLE 18








Working
Compression
Deformation
Hardness




Part
Steel
Strain
temperature
ratio
resistance
after
Formula (3)


No.
No.
rate (/s)
(° C.)
(%)
(MPa)
working (Hv)
satisfied or not
Cracking























III-1
III-1A
100
60
20
365
237

Yes


III-2
III-1B
140
80
80
417
254

No


III-3
III-1C
180
20
60
428
243

No


III-4
III-1D
220
60
80
486
261

No


III-5
III-1E
120
20
40
706
302

No


III-6
III-1F
100
40
80
785
313

Yes


III-7
III-1G
160
60
80
448
261

Yes


III-8
III-1H
140
20
60
515
272

No


III-9
III-1I
100
80
60
461
251

No


III-10
III-1J
180
20
80
548
273

No


III-11
III-1K
140
100
80
528
270

No


III-12
III-1L
220
20
20
559
284

No


III-13
III-1M
160
60
80
454
263

No


III-14
III-1N
100
40
40
513
259

Yes


III-15
III-1O
120
20
60
426
266

Yes


III-16
III-1P
240
60
80
474
255

No


III-17
III-1Q
200
80
20
509
258

No


III-18
III-1R
140
20
80
611
318

No


III-19
III-1S
180
20
20
483
295

No


III-20
III-1T
140
20
80
579
294

No


III-21
III-1U
100
20
20
531
276

No


III-22
III-1V
160
40
60
725
329

No


III-23
III-1W
220
20
40
693
295

No


III-24
III-1X
120
60
80
769
317

Yes


III-25
III-1Y
100
20
80
586
284

Yes


III-26
III-1Z
140
80
80
543
301

Yes


III-27
III-2A
200
20
20
555
269

Yes


III-28
III-2B
100
40
80
538
260

Yes


III-29
III-2C
160
20
20
537
251
x
No


III-30
III-2D
180
20
60
619
272

No


III-31
III-2E
0.001
20
80
671
298

Yes


III-32
III-2E
0.1
60
80
601
291

Yes


III-33
III-2E
1
20
40
566
295

Yes


III-34
III-2E
10
80
80
531
284

Yes


III-35
III-2E
100
100
20
496
302

No


III-36
III-2E
200
200
60
486
307

No


III-37
III-2F
220
300
80
548
360

Yes


III-38
III-2G
140
400
20
662
304

Yes


III-39
III-2H
100
20
80
602
311

No


III-40
III-2I
160
20
80
479
273

No
























TABLE 19








Working

Deformation
Hardness




Part
Steel
Strain
temperature
Compression
resistance
after
Formula (2)


No.
No.
rate (/s)
(° C.)
ratio (%)
(MPa)
working (Hv)
satisfied or not
Cracking























III-41
III-2J
120
60
40
463
271

No


III-42
III-2K
180
80
60
629
292

Yes


III-43
III-2L
100
80
20
607
335

No


III-44
III-2M
140
20
80
593
309

No


III-45
III-2N
220
20
80
568
279

No


III-46
III-2O
120
60
20
548
286

No


III-47
III-2P
200
40
80
567
310

No


III-48
III-2Q
160
100
40
433
273

No


III-49
III-2R
100
20
20
548
322

No


III-50
III-2S
180
40
80
691
261
x
No


III-51
III-2T
100
20
60
537
279

No


III-52
III-2U
140
60
80
771
274
x
No


III-53
III-2V
200
20
40
470
234
x
No


III-54
III-2W
160
80
20
466
223
x
No


III-55
III-2X
220
20
40
498
273

No


III-56
III-2Y
180
150
80
687
300

No


III-57
III-2Z
100
20
40
985
317
x
No


III-58
III-3A
120
40
60
560
313

No


III-59
III-3B
100
60
80
626
326

No


III-60
III-3C
160
20
80
524
269

No


III-61
III-3D
140
80
60
470
273

No


III-62
III-3E
200
20
80
590
277

No


III-63
III-3F
220
20
80
410
255

No


III-64
III-3G
100
150
20
585
292

No


III-65
III-3H
100
40
60
579
313

No


III-66
III-3I
180
60
40
575
288

No


III-67
III-3J
200
80
80
469
267

No


III-68
III-3K
100
20
40
568
310

No


III-69
III-3L
120
20
60
636
296

No


III-70
III-3M
180
20
80
571
278

No


III-71
III-3N
240
60
20
534
261

No


III-72
III-3O
140
20
60
605
295

No


III-73
III-3P
160
40
80
680
327

No


III-74
III-3Q
220
40
40
617
297

No


III-75
III-3R
100
60
60
528
259

No


III-76
III-3S
160
20
80
589
275

No









Steels in this example are rated as good in cold workability if they give crack-free parts and exhibit low deformation resistance relative to parts hardness (or satisfy the formula (3)). Those parts which are rated as good in strength have a Vickers hardness (Hv) larger than 240.


Incidentally, Tables 18 and 19 show whether or not each specimen satisfies the formula (3) by symbols “◯” and “X” respectively.


The results shown in Tables 18 and 19 suggest the following.


All the parts (wires and rods) numbered as follows, which are formed by high-speed cold working as recommended in the present invention from the steels meeting the requirements of the third embodiment of the present invention, exhibit good balance between cold workability and strength (hardness) as wells as good cracking resistance.
















Part Nos.
Steel Nos.









III-2 to III-5
III-1B to III-1E



III-8 to III-13
III-1H to III-1M



III-16 to III-23
III-1P to III-1W



III-30
III-2D



III-35 and III-36
III-2E



III-39 to III-41
III-2H to III-2J



III-43 to III-49
III-2L to III-2R



III-51
III-2T



III-55 and III-56
III-2X and III-2Y



III-58 to III-76
III-3A to III-3S










By contrast, those parts failing to meet the requirements specified in the third embodiment of the present invention are vulnerable to cracking during high-speed cold working or poor in balance between cold workability and strength (hardness), with the formula (3) not satisfied, as mentioned below.


Part No. III-1 (formed from steel No. III-1A with a low C content) suffers cracking after working.


Part No. III-6 (formed from steel No. III-1F with a high C content) suffers cracking.


Part No. III-7 (formed from steel No. III-1G with a low Si content) suffers cracking.


Part No. III-14 (formed from steel No. III-1N with a high Si content) suffers cracking.


Part No. III-15 (formed from steel No. III-1O with a low Mn content) suffers cracking.


Part No. III-24 (formed from steel No. III-1X with a high Mn content) suffers cracking.


Parts Nos. III-25 and III-26 (formed from steels Nos. III-1Y and III-1Z respectively with a high P content) suffer cracking.


Parts Nos. III-27 and III-28 (formed from steels Nos. III-2A and III-2B respectively with a high S content) suffer cracking.


Part No. III-29 (formed from steel No. III-2C with a low N content and hence with a low content of dissolved N) is poor in balance between cold workability and hardness.


Part No. III-42 (formed from steel No. III-2K with a high N content) suffers cracking.


Parts No. III-31 to III-34 (formed from steel No. III-2E having the chemical composition as specified in the third embodiment of the present invention) suffer cracking due to dynamic strain ageing which results from a low strain rate at the time of high-speed cold working.


Parts No. III-37 and III-38 (formed from steels No. III-2F and III-2G respectively having the chemical composition as specified in the third embodiment of the present invention) suffer cracking due to dynamic strain ageing which results from a high temperature at the time of high-speed cold working.


Part No. III-50 (formed from steel No. III-2S with a high Al content, with the formula (2) not satisfied, is poor in balance between cold workability and hardness.


Part No. III-52 (formed from steel No. III-2U with a high B content, with the formula (2) not satisfied, is poor in balance between cold workability and hardness.


Part No. III-53 (formed from steel No. III-2V with a high Ti content, with the formula (2) not satisfied, is poor in balance between cold workability and hardness.


Part No. III-54 (formed from steel No. III-2W with a high V content, with the formula (2) not satisfied, is poor in balance between cold workability and hardness.


Part No. III-57 (formed from steel No. III-2Z with a high content of Ti, V, and B, with the formula (2) not satisfied, is poor in balance between cold workability and hardness.

Claims
  • 1. A steel for high-speed cold working, comprising: C: 0.03 to 0.6% (by mass),Si: 0.005 to 0.6%,Mn: 0.05 to 2%,P: no more than 0.05% (excluding 0%),S: no more than 0.05% (excluding 0%), andN: no more than 0.04% (excluding 0%).
  • 2. The steel for high-speed cold working as defined in claim 1, wherein the C content is 0.03 to 0.15%.
  • 3. The steel for high-speed cold working as defined in claim 1, wherein the C content is more than 0.15% up to 0.6%.
  • 4. The steel for high-speed cold working as defined in claim 1, wherein the N content is no less than 0.007%.
  • 5. The steel for high-speed cold working as defined in claim 1, wherein the Al content is no more than 0.1% (excluding 0%).
  • 6. The steel for high-speed cold working as defined in claim 1, further comprising at least one species selected from the group consisting of: Zr: no more than 0.2% (excluding 0%),Ti: no more than 0.1% (excluding 0%),Nb: no more than 0.1% (excluding 0%),V: no more than 0.5% (excluding 0%),Ta: no more than 0.1% (excluding 0%), andHf: no more than 0.1% (excluding 0%).
  • 7. The steel for high-speed cold working as defined in claim 1, further comprising: B: no more than 0.0015% (excluding 0%) and/orCr: no more than 2% (excluding 0%).
  • 8. The steel for high-speed cold working as defined in claim 1, which satisfies the formula (1) below. [N]−(14[Al]/27+14[Ti]/47.9+14[Nb]/92.9+14[V]/50.9+14[Zr]/91.2+14[B]/10.8+14[Ta]/180.9+14[Hf]/178.5)≧0.006  Formula (1)
  • 9. The steel for high-speed cold working as defined in claim 1, which contains inevitable impurities as follows: Al: no more than 0.001% (including 0%),Ti: no more than 0.002% (including 0%),Nb: no more than 0.001% (including 0%),V: no more than 0.001% (including 0%),Zr: no more than 0.001% (including 0%),B: no more than 0.0001% (including 0%),Ta: no more than 0.0001% (including 0%), andHf: no more than 0.0001% (including 0%);
  • 10. The steel for high-speed cold working as defined in claim 9, further comprising: Cr: no more than 2% (excluding 0%).
  • 11. The steel for high-speed cold working as defined in claim 1, further comprising: Cu: no more than 5% (excluding 0%).
  • 12. The steel for high-speed cold working as defined in claim 1, further comprising: Ni: no more than 5% (excluding 0%) and/orCo: no more than 5% (excluding 0%).
  • 13. The steel for high-speed cold working as defined in claim 1, further comprising: Mo: no more than 2% (excluding 0%) and/orW: no more than 2% (excluding 0%).
  • 14. The steel for high-speed cold working as defined in claim 1, further comprising at least one species selected from the group consisting of: Ca: no more than 0.05% (excluding 0%),Rare earth elements: no more than 0.05% (excluding 0%),Mg: no more than 0.02% (excluding 0%),Li: no more than 0.02% (excluding 0%),Pb: no more than 0.1% (excluding 0%), andBi: no more than 0.1% (excluding 0%).
  • 15. A method for producing parts by high-speed cold working, said method comprising performing high-speed cold working at a working temperature no higher than 200° C. on the steel for high-speed cold working as defined in claim 1.
  • 16. A method for producing parts by high-speed cold working, said method comprising performing high-speed cold working at a strain rate no lower than 100/s on the steel for high-speed cold working as defined in claim 1.
  • 17. A method for producing a steel for high-speed cold working, said method comprising subjecting the steel stock having the composition defined in claim 1 consecutively to heating at a temperature above Ac3 point plus 30° C., hot rolling at a temperature above Ac3 point plus 30° C., and quenching to 500° C. or below at a cooling rate no smaller than 0.5° C./s.
  • 18. A method for producing a steel for high-speed cold working, said method comprising subjecting the steel stock having the composition defined in claim 1 to heating at a temperature above Ac3 point plus 30° C. and subsequent quenching to 500° C. or below at a cooling rate no smaller than 0.5° C./s.
  • 19. A machine part formed from the steel for high-speed cold working as defined in claim 1 by high-speed cold working at a working temperature no higher than 200° C. and a strain rate no lower than 100/s, said machine part being characterized in having a value of H and a value of DR which satisfy the formula (3) below H≧(DR+1000)/6  formula (3)
Priority Claims (3)
Number Date Country Kind
2006-355497 Dec 2006 JP national
2007-097457 Apr 2007 JP national
2007-103027 Apr 2007 JP national