High-nitrogen ferritic heat-resisting steel with high vanadium content and method of production thereof

BACKGROUND OF THE INVENTION
1. Field of the Invention
This invention relates to a ferritic heat-resisting steel, more particularly to a high-nitrogen ferritic heat-resisting steel containing chromium, and being appropriate for use in a high-temperature, high-pressure environment, and to a method of producing the same.
2. Description of the Prior Art
Recent years have seen a marked increase in the temperatures and pressures under which thermal power plant boilers are required to operate. Some plans already call for operation at 566.degree. C. and 314 bar and it is expected that operation under conditions of 650.degree. C. and 355 bar will be implemented in the future. These are extremely severe conditions from the viewpoint of the boiler materials used.
At operating temperatures exceeding 550.degree. C., it has, from the viewpoints of oxidation resistance and high-temperature strength, been necessary to switch from ferritic 2.multidot.1/4 Cr-1 Mo steel to high-grade austenitic steels such as 18-8 stainless steel. In other words, it has been necessary to adopt expensive materials with properties exceeding what is required.
Decades have been spent in search of steels for filling in the gap between 2.multidot.1/4 Cr-1 Mo steel and austenitic stainless steel. Medium Cr (e.g. 9 Cr and 12 Cr) steel boiler pipes are made of heat-resisting steels that were developed against this backdrop. They achieve high-temperature strength and creep rupture strength on a par with austenitic steels by use of a base metal composition which includes various alloying elements for precipitation hardening and solution hardening.
The creep rupture strength of a heat-resisting steel is governed by solution hardening in the case of short-term aging and by precipitation hardening in the case of prolonged aging. This is because the solution-hardening elements initially present in solid solution in the steel for the most part precipitate as stable carbides such as M.sub.23 C.sub.6 during aging, and then when the aging is prolonged these precipitates coagulate and enlarge, with a resulting decrease in creep rupture strength.
Thus, with the aim of maintaining the creep rupture strength of heat-resisting steels at a high level, a considerable amount of research has been done for discovering ways for avoiding the precipitation of the solution hardening elements and maintaining them in solid solution for as long as possible.
For example, Japanese Patent Public Disclosures No. Sho 63-89644, Sho 61-231139 and Sho 62-297435 teach ferritic steels that achieve dramatically higher creep rupture strength than conventional Mo-containing ferritic heat-resisting steels by the use of W as a solution hardening element.
While the solution hardening by W in these steels may be more effective than by Mo, the precipitates are still fundamentally carbides of the M.sub.23 C.sub.6 type, so that it is not possible to avoid reduction of the creep rupture strength with prolonged aging.
Moreover, the use of ferritic heat-resisting steels at up to 650.degree. C. has been considered difficult because of their inferior high-temperature oxidation resistance as compared with austenitic heat-resisting steels. A particular problem with these steels is the pronounced degradation of high-temperature oxidation resistance that results from the precipitation of Cr in the form of coarse M.sub.23 C.sub.6 type precipitates at the grain boundaries.
The highest temperature limit for use of ferritic heat-resisting steel has therefore been considered to be 600.degree. C.
The need for heat-resisting steels capable of standing up under extremely severe conditions has grown more acute not only because of the increasingly severe operating conditions mentioned earlier but also because of plans to reduce operating costs by extending the period of continuous power plant operation from the current 100 thousand hours up to around 150 thousand hours.
Although ferritic heat-resisting steels are somewhat inferior to austenitic steels in high-temperature strength and anticorrosion property, they have a cost advantage. Furthermore, for reasons related to the difference in thermal expansion coefficient, among the various steam oxidation resistance properties they are particularly superior in scale defoliation resistance. For these reasons, they are attracting attention as a boiler material.
For the reasons set out above, however, it is clearly not possible with the currently available technology to develop ferritic heat-resisting steels that are capable of standing up for 150 thousand hours under operating conditions of 650.degree. C. and 355 bar, that are low in price and that exhibit good steam oxidation resistance.
Based on the foregoing knowledge and as described in Japanese Patent Application No. Hei 2-37895, the inventors earlier disclosed that a high-nitrogen ferritic heat-resisting steel estimated by linear extrapolation to exhibit a creep rupture strength of not less than 147 MPa under operating conditions of 650.degree. C. and 355 bar for 150 thousand hours can be obtained by using a pressurized atmosphere to add nitrogen exceeding the solution limit and thus inducing precipitation of the excess nitrogen in the form of fine nitrides and carbo-nitrides. The gist of their disclosure was a ferritic heat-resisting steel characterized in comprising, in weight per cent, 0.01-0.30% C, 0.02-0.80% Si, 0.20-1.00% Mn, 8.00-13.00% Cr, 0.50-3.00% W, 0.005-1.00% Mo, 0.05-0.50% V, 0.02-0.12% Nb and 0.10-0.50% N and being controlled to include not more than 0.050% P, not more than 0.010% S and not more than 0.020% O, and optionally comprising (A) one or both of 0.01-1.00% Ta and 0.01-1.00% Hf and/or (B) one or both of 0.0005-0.10% Zr and 0.01-0.10% Ti, the balance being Fe and unavoidable impurities, and a method of producing the steel wherein the steel components are melted and equilibrated in an atmosphere of a mixed gas of a prescribed nitrogen partial pressure or nitrogen gas, and the resulting melt is thereafter cast or solidified in an atmosphere controlled to have a nitrogen partial pressure of not less than 1.0 bar and a total pressure of not less than 4.0 bar, with the relationship between the partial pressure p and the total pressure P being
10.sup.p <P.sup.0.37 +log.sub.10.spsb.6
thereby obtaining good quality ingot free of blowholes.
Based on the results of tests for determining the creep rupture strength of the steel taught by Japanese Patent Application No. Hei 2-37895 up to 50 thousand hours, the inventors discovered that the creep rupture strength of the steel at 150 thousand hours, as estimated by linear extrapolation, is no more than 176 MPa and, in particular, that the steel experiences a marked decrease in creep rupture strength between 30 and 50 thousand hours. Further studies showed that the reason for the decrease in creep rupture strength was that during the creep test large Fe.sub.2 W grains measuring 1 .mu.m or more in diameter precipitated in large amounts, principally at the grain boundaries, leading to large-scale loss of W as a solid solution element from the steel.
Based on this finding, they discovered that by limiting the W content to not more than 1.5% so as to prevent precipitation of W as Fe.sub.2 W and, moreover, by adding V in the range of 0.30-2.00% so that fine, stable VN becomes the principal precipitation hardening factor, it is possible to obtain a ferritic heat-resisting steel exhibiting a creep rupture strength at 650.degree. C., 355 bar and 150 thousand hours of not less than 200 MPa, as estimated by linear extrapolation.
While Nb nitrides are formed in the steel according to the invention, the NbN precipitates, although stable, are relatively large so that VN makes a greater contribution to precipitation hardening. Moreover it precipitates finely and thus has less adverse effect on toughness.
The inventors thus further discovered that a heat-resisting steel having excellent toughness after prolonged aging and also exhibiting high creep rupture strength can be obtained by adding V at 0.30-2.00% while keeping Nb addition to less than 0.020%, and also that owing to the increase in the N solution limit resulting from the addition of V the pressurized atmosphere conditions required for casting of sound ingot become a total pressure of not less than 2.77 bar and a nitrogen partial pressure of not less than 1.0 bar, with the relationship between the total pressure P and the nitrogen partial pressure p being
P>2.77p.
There have been few papers published on research into high-nitrogen ferritic heat-resisting steels and the only known published report in this field is Ergebnisse der Werkstoff-Forschung, Band I, Varlag Schweizerische Akademie der Werkstoffwissenschaften "Thubal-Kain", Zurich, 1987, 161-180.
However, the research described in this report is limited to that in connection with ordinary heat-resisting steel and there is no mention of materials which can be used under such severe conditions as 650.degree. C., 355 bar and 150 thousand hours continuous operation.
SUMMARY OF THE INVENTION
An object of this invention is to provide a high-nitrogen ferritic heat-resisting steel which overcomes the shortcomings of the conventional heat-resisting steels, and particularly to provide such a steel exhibiting outstanding creep rupture strength and capable of being used under severe operating conditions, wherein the decrease in creep rupture strength following prolonged aging and the degradation of high-temperature oxidation resistance caused by precipitation of carbides are mitigated by adding nitrogen to supersaturation so as to precipitate fine nitrides and/or carbo-nitrides which suppress the formation of carbides such as the M.sub.23 C.sub.6 precipitates seen in conventional steels.
This invention was accomplished in the light of the aforesaid knowledge and, in one aspect, pertains substantially to a high-nitrogen ferritic heat-resisting steel with high vanadium content comprising, in weight percent, 0.01-0.30% C, 0.02-0.80% Si, 0.20-1.00% Mn, 8.00-13.00% Cr, 0.005-1.00% Mo, 0.20-1.50% W, 0.30-2.00% V and 0.10-0.50% N and being controlled to include less than 0.020% Nb, not more than 0.050% P, not more than 0.010% S and not more than 0.020% O, and optionally comprising (A) one or both of 0.01-1.00% Ta and 0.01-1.00% Hf and/or (B) one or both of 0.0005-0.10% Zr and 0.01-0.10% Ti, the balance being Fe and unavoidable impurities.
Another aspect of the invention pertains to a method of producing such a high-nitrogen ferritic heat-resisting steel with high vanadium content, wherein the steel components are melted and equilibrated in an atmosphere of a mixed gas of a prescribed nitrogen partial pressure or nitrogen gas, and the resulting melt is thereafter cast or solidified in an atmosphere controlled to have a total pressure of not less than 2.77 bar and a nitrogen partial pressure of not less than 1.0 bar, with the relationship between the nitrogen partial pressure p and the total pressure P being
P>2.77p
thereby obtaining sound ingot free of flowholes.
The above and other features of the present invention will become apparent from the following description made with reference to the drawings.

BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a perspective view of an ingot and the manner in which it is to be cut.
FIG. 2 is a graph showing the relationship between the steel nitrogen content and the weight percentage of the total of M.sub.23 C.sub.6 +M.sub.6 C+Cr.sub.2 N+VC+VN among the precipitates in the steel accounted for by M.sub.23 C.sub.6 +M.sub.6 C+VC and the relationship between the steel nitrogen content and the weight percentage of the total of M.sub.23 C.sub.6 +M.sub.6 C+Cr.sub.2 N+VC+VN among the precipitates in the steel accounted for by Cr.sub.2 N+VN.
FIG. 3 is a graph showing conditions under which blowholes occur in the ingot in terms of the relationship between the total pressure and nitrogen partial pressure of the atmosphere during casting.
FIG. 4 is a schematic view showing the manner in which creep test pieces are taken from a pipe specimen and a rolled plate specimen.
FIG. 5 is a graph showing the relationship between steel nitrogen content and estimated creep rupture strength at 650.degree. C., 150 thousand hours.
FIG. 6 is a graph showing the relationship between steel V content and estimated creep rupture strength at 650.degree. C., 150 thousand hours.
FIG. 7 is a graph comparing the Charpy impact absorption energies at 0.degree. C. of steels of varying Nb content after they were aged at 700.degree. C. for 3000 hours.
FIG. 8 is a graph showing the relationship between steel W content and estimated creep rupture strength at 650.degree. C., 150 thousand hours.
FIG. 9 is a graph showing examples of creep test results in terms of stress vs rupture time for steels of varying nitrogen content.
FIG. 10 is a graph showing the relationship between steel nitrogen content and Charpy impact absorption energy at 0.degree. C. following aging at 700.degree. C. for 3000 hours.
FIG. 11 is a graph showing the relationship between steel nitrogen content and the thickness of the oxidation scale formed on the surface of a test piece after oxidation at 650.degree. C. for 10 thousand hours.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT
The reasons for the limits placed on the components of the high-nitrogen ferritic heat-resisting steel with high V content according to this invention will now be explained.
C is required for achieving strength. Adequate strength cannot be achieved at a C content of less than 0.01%, while at a C content exceeding 0.30% the steel is strongly affected by welding heat and undergoes hardening which becomes a cause for low-temperature cracking. The C content range is therefore set at 0.01-0.30%.
Si is important for achieving oxidation resistance and is also required as a deoxidizing agent. It is insufficient for these purposes at a content of less than 0.02%, whereas a content exceeding 0.80% reduces the creep rupture strength. The Si content range is therefore set at 0.02-0.80%.
Mn is required for deoxidation and also for achieving strength. It has to be added in an amount of at least 0.20% for adequately exhibiting its effect. When it exceeds 1.00% it may in some cases reduce creep rupture strength. The Mn content range is therefore set at 0.20-1.00%.
Cr is indispensable to oxidation resistance. It also contributes to increasing creep resistance by combining with N and finely precipitating in the base metal matrix in the form of Cr.sub.2 N, Cr.sub.2 (C,N) and the like. Its lower limit is set at 8.00% from the viewpoint of oxidation resistance. Its upper limit is set at 13.00% for maintaining the Cr equivalent value at a low level so as to realize a martensite phase texture.
W produces a marked increase in creep rupture strength by solution hardening. Its effect toward increasing creep rupture strength over long periods at high temperatures of 550.degree. C. and higher is particularly pronounced. Its upper limit is set at 1.50% because at contents higher than this level it precipitates in large quantities in the form of carbide and intermetallic compounds which sharply reduce the toughness of the base metal. The lower limit is set at 0.20% because it does not exhibit adequate solution hardening effect at lower levels.
Mo increases high-temperature strength through solution hardening. It does not exhibit adequate effect at a content of less than 0.005% and at a content higher than 1.00% it may, when added together with W, cause heavy precipitation of Mo.sub.2 C type oxides which markedly reduce base metal toughness. The Mo content range is therefore set at 0.005-1.00%.
V produces a marked increase in the high-temperature creep rupture strength of the steel regardless of whether it forms precipitates or, like W, enters solid solution in the matrix. When it precipitates, the resulting VN serves as precipitation nuclei for Cr.sub.2 N and NbN, which has a pronounced effect toward promoting fine dispersion of the precipitates. At a content below 0.30% the VN does not disperse as the primary precipitate and when present at higher than 2.00% the NV forms clusters which lower toughness. The V content range is therefore set at 0.30-2.00%.
Nb increases high-temperature strength by precipitating as NbN, (Nb, V)N, Nb(C, N) and (Nb, V)(C, N). Also, similarly to V, it promotes fine precipitate dispersion by forming precipitation nuclei for Cr.sub.2 N, Cr.sub.2 (C, N) and the like. However, when V is added to the steel, Nb causes precipitate enlargement and may in some cases cause reduced toughness by markedly increasing the strength of the steel at normal temperature. The maximum Nb content is therefore set at less than 0.020%.
N dissolves in the matrix and also forms nitride and carbo-nitride precipitates. As the form of the precipitates is mainly VN, Cr.sub.2 N and Cr.sub.2 (C, N), there is less precipitate-induced consumption of Cr and W than in the case of the M.sub.23 C.sub.6, M.sub.6 C and other such precipitates observed in conventional steels. N thus increases oxidation resistance and creep rupture strength. At least 0.10% is required for precipitation of nitrides and carbo-nitrides and suppressing precipitation of M.sub.23 C.sub.6 and M.sub.6 C. The upper limit is set at 0.50% for preventing coagulation and enlargement of nitride and carbo-nitride precipitates by the presence of excessive nitrogen.
P, S and O are present in the steel according to this invention as impurities. P and S hinder the achievement of the purpose of the invention by lowering strength, while O has the adverse effect of forming oxides which reduce toughness. The upper limits on these elements is therefore set at 0.050%, 0.010% and 0.020%, respectively.
The basic components of the steel according to this invention (aside from Fe) are as set out above. Depending on the purpose to which the steel is to be put, however, it may additionally contain (A) one or both of 0.01-1.00% Ta and 0.01-1.00% Hf and/or (B) one or both of 0.0005-0.10% Zr and 0.01-0.10% Ti.
At low concentrations Ta and Hf act as deoxidizing agents. At high concentrations they form fine high melting point nitrides and carbo-nitrides and, as such, increase toughness by decreasing the austenite grain size. In addition, they also reduce the degree to which Cr and W dissolve in precipitates and by this effect enhance the effect of supersaturation with nitrogen. Neither element exhibits any effect at less than 0.01%. When either is present at greater than 1.00%, it reduces toughness by causing enlargement of nitride and carbo-nitride precipitates. The content range of each of these elements is therefore set at 0.01-1.00%.
Acting to govern the deoxidation equilibrium in the steel, Zr suppresses the formation of oxides by markedly reducing the amount of oxygen activity. In addition, its strong affinity for N promotes precipitation of fine nitrides and carbo-nitrides which increase creep rupture strength and high-temperature oxidation resistance. When present at less than 0.0005% it does not provide an adequate effect of governing the deoxidation equilibrium and when present at greater than 0.10% it results in heavy precipitation of coarse ZrN and ZrC which markedly reduce the toughness of the base metal. The Zr content range is therefore set at 0.0005-0.10%.
Ti raises the effect of excess nitrogen by precipitating in the form of nitrides and carbo-nitrides. At a content of less than 0.01% it has no effect while a Ti content of over 0.10% results in precipitation of coarse nitrides and carbo-nitrides which reduce toughness. The Ti content range is therefore set at 0.01-0.10%.
The aforesaid alloying components can be added individually or in combinations.
The object of this invention is to provide a tough ferritic heat-resisting steel that is superior in creep rupture strength and high-temperature oxidation resistance. Depending on the purpose of use it can be produced by various methods and be subjected to various types of heat treatment. These methods and treatments in no way diminish the effect of the invention.
However, in view of the need to supersaturate the steel with nitrogen, it is necessary during casting to raise the total pressure of the atmosphere to not less than 2.77 bar and to control the relationship between the total pressure P and the nitrogen partial pressure p to satisfy the inequation P>2.77p. As an auxiliary gas to be mixed with the nitrogen gas it is appropriate to use an inert gas such as Ar, Ne, Xe or Kr. These casting conditions were determined by the following experiment.
Steel of a chemical composition, aside from nitrogen, as indicated in the present invention was melted in an induction heating furnace installed in a chamber that could be pressurized up to 150 bar. A mixed gas of argon and nitrogen having a prescribed nitrogen partial pressure was introduced into the furnace and maintained at a pressure which was varied from test to test. After the nitrogen and molten metal had reached chemical equilibrium, the molten metal was cast into a mold that had been installed in the chamber beforehand, whereby there was obtained a 5-ton ingot.
The ingot was cut vertically as shown in FIG. 1 and the ingot 1 was visually examined for the presence of blowholes.
Following this examination, a part of the ingot was placed in a furnace and maintained at 1180.degree. C. for 1 hour and then forged into a plate measuring 50 mm in thickness, 750 mm in width and 4,000 mm in length.
This plate was subjected to solution treatment at 1200.degree. C. for 1 hour and to tempering at 800.degree. C. for 3 hours. The steel was then chemically analyzed and the dispersion state and morphology of the nitrides and carbo-nitrides were investigated by observation with an optical microscope, an electron microscope, X-ray diffraction and electron beam diffraction, whereby the chemical structure was determined.
Among the precipitates present within the as-heat-treated steel, FIG. 2 shows how the proportion of the precipitates in the steel accounted for by M.sub.23 C.sub.6 type carbides and M.sub.6 C or VC type carbides and the proportion thereof accounted for by Cr.sub.2 N type nitrides and VN type nitrides vary with nitrogen concentration. At a nitrogen concentration of 0.10%, nitrides account for the majority of the precipitates in the steel of the invention, while at a nitrogen concentration of 0.15%, substantially 100% of the precipitates are nitrides with virtually no carbides present whatsoever. Thus for the effect of this invention to be adequately manifested it is necessary for the nitrogen concentration of the steel to be not less than 0.10%.
The graph of FIG. 3 shows how the state of blowhole occurrence varies depending on the relationship between the total and nitrogen partial pressures of the atmosphere. For achieving a nitrogen concentration of 0.10% or higher it is necessary to use a total pressure of not less than 2.77 bar. Equilibrium calculation based on Sievert's law shows that in this case the nitrogen partial pressure in the steel of this invention is not less than 1.0 bar.
Moreover, where for controlling the amount of nitride and carbo-nitride precipitation the nitrogen partial pressure is maintained at 1.0-6.0 bar (nitrogen concentration within the steel of approximately 0.5 mass %), it becomes necessary to vary the total pressure between 2.77 and about 16.62 bar, the actual value selected depending on the nitrogen partial pressure. Namely, it is necessary to use a total pressure falling above the broken line representing the boundary pressure in FIG. 3.
When the boundary line of FIG. 3 is determined experimentally it is found to lie at
P=2.77p
meaning that the steel according to this invention can be obtained by selecting an atmosphere of a pressure and composition meeting the condition of the inequality
P>2.77p.
It is therefore necessary to use furnace equipment enabling pressure and atmosphere control. Without such equipment, it is difficult to produce the steel of the present invention.
There are no limitations whatever on the melting method. Based on the chemical composition of the steel and cost considerations, it suffices to select from among processes using a converter, an induction heating furnace, an arc melting furnace or an electric furnace.
The situation regarding refining is similar. Insofar as the atmosphere is controlled to a total pressure of not less than 2.77 bar and a nitrogen partial pressure of not less than 1.0 bar, it is both possible and effective to use a ladle furnace, an electro-slag remelting furnace or a zone melting furnace.
After casting under a pressurized atmosphere of a total pressure of not less than 2.77 bar and a nitrogen partial pressure of not less than 1.0 bar, it is possible to process the steel into billet, bloom or plate by forging or hot rolling. Since the steel of this invention includes finely dispersed nitrides and carbo-nitrides, it is superior to conventional ferritic heat-resisting steels in hot-workability. This is also one reason for employing nitrides and carbo-nitrides obtained by adding nitrogen to beyond the solution limit.
For processing the steel into products, it is possible to first process it into round or rectangular billet and then form it into seamless pipe or tube by hot extrusion or any of various seamless rolling methods. Otherwise it can be formed into sheet by hot and cold rolling and then made into welded tube by electric resistance welding. Alternatively, it can be processed into welded pipe or tube by use of TIG, MIG, SAW, LASER and EB welding, individually or in combination. Moreover, it is possible to expand the size range of products to which the present invention can be applied by following any of the aforesaid processes by hot or warm stretch reduction or sizing.
The steel according to the invention can also be provided in the form of plate or sheet. The plate or sheet can, in its hot-rolled state or after whatever heat treatment is found necessary, be provided as a heat-resisting material in various shapes, without any influence on the effects provided by the invention.
The pipe, tube, plate, sheet and variously shaped heat-resisting materials referred to above can, in accordance with their purpose and application, be subjected to various heat treatments, and it is important for them to be so treated for realizing the full effect of the invention.
While the production process ordinarily involves normalizing (solution heat treatment)+tempering, it is also possible and useful additionally to carry out one or a combination of two or more of quenching, tempering and normalizing. It is also possible, without influencing the effects of the present invention in any way, to repeatedly carry out one or more of the aforesaid processes to whatever degree is necessary for adequately bringing out the steel properties.
The aforesaid processes can be appropriately selected and applied to the manufacture of the steel according to the invention.
WORKING EXAMPLES
The steels indicated in Tables 1-14, each having a composition according to the present invention; were separately melted in amounts of 5 tons each in an induction heating furnace provided with pressurizing equipment. The resulting melt was cleaned by ladle furnace processing (under bubbling with a gas of the same composition as the atmosphere) for reducing its impurity content, whereafter the atmosphere was regulated using a mixed gas of nitrogen and argon so as to satisfy the conditions of the inequality P>2.77p. The melt was then cast into a mold and processed into a round billet, part of which was hot extruded to obtain a tube 60 mm in outside diameter and 10 mm in wall thickness and the remainder of which was subjected to seamless rolling to obtain a pipe 380 mm in outside diameter and 50 mm in wall thickness. The tube and pipe were subjected to a single normalization at 1200.degree. C. for 1 hour and were then tempered at 800.degree. C. for 3 hours.
In addition, a 5 ton ingot was cast and forged into a slab which was hot rolled into 25 mm and 50 mm thick plates.
As shown in FIG. 4, creep test pieces 6 measuring 6 mm in diameter were taken along the axial direction 4 of the pipe or tube 3 and along the rolling direction 5 of the plates and subjected to creep test measurement at 650.degree. C. Based on the data obtained, a linear extrapolation was made for estimating the creep rupture strength at 150 thousand hours. A creep rupture strength of 150 MPa was used as the creep rupture strength evaluation reference value. The creep rupture strength at 650.degree. C., 150 thousand hours is hereinafter defined as the linearly extrapolated value at 150 thousand hours on the creep rupture strength vs rupture time graph.
Toughness was evaluated through an accelerated evaluation test in which aging was carried out at 700.degree. C. for 3000 hours. JIS No. 4 tension test pieces were cut from the aged steel and evaluated for impact absorption energy. Assuming an assembled plant evaluation test at 0.degree. C., the toughness evaluation reference value was set at 70 J.
High-temperature oxidation resistance was evaluated by suspending a 25 mm.times.25 mm.times.5 mm test piece cut from the steel in 650.degree. C. atmospheric air in a furnace for 10 thousand hours and then cutting the test piece parallel to the direction of growth of the scale and measuring the oxidation scale thickness.
The 650.degree. C., 150 thousand hour creep rupture strength, the Charpy impact absorption energy at 0.degree. C. after aging at 700.degree. C. for 3000 hours and the oxidation scale thickness after oxidation at 650.degree. C. for 10 thousand hours are shown in Tables 2, 4, 6, 8, 10, 12, and 14.
For comparison, steels of compositions not falling within the present invention were melted, processed and tested in the same way as described above. Their chemical compositions and the evaluation results are shown in Tables 15 and 16.
FIG. 5 shows the relationship between the nitrogen content of the steels and the estimated creep rupture strength at 650.degree. C., 150 thousand hours. It will be noted that the creep rupture strength attains high values exceeding 150 MPa at a steel nitrogen content of 0.1% or higher but falls below 150 MPa and fails to satisfy the evaluation reference value that was set at a steel nitrogen content of less than 0.1%.
FIG. 6 shows the relationship between the V content of the steels and the estimated creep rupture strength at 650.degree. C., 150 thousand hours. It will be noted that the creep rupture strength attains values exceeding 150 MPa at a steel V content of 0.30% or higher but at a V content exceeding 2.0% the creep rupture strength is instead lowered owing to the precipitation of coarse VN Laves phase at the melting stage.
FIG. 7 shows the relationship between the Nb content and the Charpy impact absorption energy at 0.degree. C. after aging at 700.degree. C. for 3000 hours of steels added with V in the range of 0.30-2.00%. It will be noted that when the Nb content is 0.020% or higher the Charpy impact absorption energy does not exceed 70 J but when the Nb content is less than 0.020% the Charpy impact absorption energy is above 70 J.
FIG. 8 shows the relationship between the W content of the steel and the estimated creep rupture strength at 650.degree. C., 150 thousand hours. The creep rupture strength is below 150 MPa at a W content of less than 0.2% and is 150 MPa or higher in a content range of 0.2-1.5%. When the W is present in excess of 1.5%, the creep rupture strength falls below 150 MPa owing to coarse Fe.sub.2 W precipitating at the grain boundaries.
FIG. 9 shows the results of the creep test in terms of stress vs rupture time. A good linear relationship can be noted between stress and rupture time at a steel nitrogen content of not less than 0.1%. Moreover, the creep rupture strength is high. On the other hand, when the steel nitrogen content falls below 0.1%, the relationship between stress and rupture time exhibits a pronounced decline in creep rupture strength with increasing time lapse. Either the linearity is not maintained, or the slope of the creep rupture curve is steep, with the short-term side creep rupture strength being high but the long-term creep rupture strength being low, or the creep rupture strength is low throughout. This is because W and the other solution hardening elements precipitate as carbides whose coagulation and enlargement degrades the creep rupture strength property of the base metal. In contrast, at a nitrogen content of 0.1% or higher, fine nitrides are preferentially precipitated so that the formation of carbides is greatly delayed. Therefore, since the dissolution of the solution hardening elements into carbides was suppressed and also because the finely precipitated nitride remained present in a stable state without coagulating and enlarging during the long-term high-temperature creep test, a high creep rupture strength was maintained in the long-term creep test.
FIG. 10 shows the relationship between Charpy impact absorption energy at 0.degree. C. following aging at 700.degree. C. for 3000 hours and steel nitrogen content. When the steel nitrogen content falls within the range of 0.1-0.5%, the impact absorption energy exceeds 70 J. In contrast, when it falls below 0.1%, there is little or no suppression of grain growth by residual high melting point nitrides during solution treatment and, as a result, the impact absorption energy decreases, and when it exceeds 0.5%, the impact absorption energy is reduced by heavy nitride precipitation.
FIG. 11 shows the relationship between the thickness of the oxidation scale formed on the surface of a test piece after oxidation at 650.degree. C. for 10 thousand hours and the steel nitrogen content. Although the oxidation scale thickness is between 400 and 800 .mu.m when the steel nitrogen content falls below 0.1%, it decreases to 50 .mu.m or less when the steel nitrogen content is 0.1% or higher.
Reference is now made to the comparison steels shown in Table 5. Nos. 161 and 162 are examples in which insufficient steel nitrogen content resulted in a low estimated creep rupture strength at 650.degree. C., 150 thousand hours and also to poor high-temperature oxidation resistance. Nos. 163 and 164 are examples in which excessive steel nitrogen content caused heavy precipitation of coarse nitrides and carbo-nitrides, resulting in a Charpy impact absorption energy at 0.degree. C. after aging at 700.degree. C. for 3000 hours of not more than 70 J. No. 165 is an example in which a low W concentration resulted in a low creep rupture strength at 650.degree. C., 150 thousand hours owing to insufficient solution hardening notwithstanding that the steel nitrogen content fell within the range of the invention. No. 166 is an example in which a high W concentration led to low rupture strength and toughness owing to precipitation of coarse Fe.sub.2 W type Laves phase at the grain boundaries during creep. No. 167 is an example in which a low V content resulted in a low estimated creep rupture strength at 650.degree. C., 150 thousand hours. No. 168 is an example in which a high V content caused profuse precipitation of coarse Fe.sub.2 Nb type Laves phase during creep, which in turn lowered both the estimated creep rupture strength at 650.degree. C., 150 thousand hours and the Charpy impact absorption energy at 0.degree. C. after aging at 700.degree. C. for 3000 hours. No. 169 is an example in which the Charpy impact absorption energy at 0.degree. C. after aging at 700.degree. C. for 3000 hours was low because the Nb content was 0.020% or more. No. 170 is an example in which heavy precipitation of coarse ZrN caused by a Zr concentration in excess of 0.1% resulted in a Charpy impact absorption energy at 0.degree. C. after aging at 700.degree. C. for 3000 hours of less than 70 J. Nos. 171, 172 and 173 are examples similar to the case of No. 170 except that the elements present in excess were Ta, Hf and Ti, respectively. As a result, heavy precipitation of coarse TaN, HfN and TiN resulted in a Charpy impact absorption energy at 0.degree. C. after aging at 700.degree. C. for 3000 hours of less than 70 J. No. 174 is an example in which, notwithstanding that the steel composition satisfied the conditions of the present invention, since the nitrogen partial pressure was 2.2 bar and the total pressure was 2.77 bar, values not satisfying the inequality, P>2.77p, many large blowholes formed in the ingot, making it impossible to obtain either a sound ingot or a plate and leading to a reduction in both the estimated creep rupture strength at 650.degree. C., 150 thousand hours and the Charpy impact absorption energy at 0.degree. C. after aging at 700.degree. C. for 3000 hours.
TABLE 1______________________________________(mass %) Invention steelsNo. C Si Mn P S Nb V Cr Mo______________________________________ 1 0.059 0.618 0.765 0.048 0.006 0.011 1.54 11.50 0.625 2 0.053 0.073 0.629 0.011 0.006 0.011 1.92 10.19 0.164 3 0.134 0.683 0.663 0.016 0.004 0.015 0.471 11.15 0.387 4 0.218 0.257 0.618 0.029 0.007 0.012 0.884 10.28 0.480 5 0.062 0.110 0.653 0.020 0.007 0.012 1.81 8.55 0.635 6 0.018 0.390 0.510 0.035 0.009 0.010 1.02 9.42 0.050 7 0.284 0.463 0.340 0.022 0.003 0.017 1.35 8.78 0.386 8 0.176 0.458 0.283 0.047 0.008 0.013 1.43 10.00 0.835 9 0.202 0.158 0.508 0.020 0.007 0.009 0.756 9.18 0.11610 0.262 0.474 0.753 0.027 0.007 0.013 1.31 9.65 0.38111 0.123 0.395 0.779 0.036 0.005 0.008 1.72 9.90 0.33512 0.124 0.432 0.309 0.013 0.008 0.010 1.46 10.76 0.15513 0.182 0.753 0.724 0.048 0.003 0.015 0.879 10.80 0.04114 0.200 0.325 0.556 0.027 0.010 0.018 1.08 10.85 0.16215 0.093 0.087 0.769 0.018 0.003 0.015 1.60 9.50 0.23616 0.058 0.557 0.296 0.047 0.008 0.010 0.999 10.01 0.41317 0.147 0.332 0.898 0.024 0.003 0.017 0.482 8.39 0.90518 0.128 0.729 0.726 0.035 0.003 0.012 0.371 8.14 0.90519 0.053 0.722 0.726 0.048 0.010 0.019 0.959 12.61 0.58220 0.124 0.454 0.643 0.030 0.003 0.012 0.865 10.26 0.62621 0.242 0.071 0.636 0.048 0.007 0.008 0.440 9.54 0.73722 0.183 0.111 0.848 0.011 0.004 0.016 0.826 11.36 0.58923 0.285 0.732 0.242 0.046 0.002 0.018 0.663 9.25 0.88424 0.027 0.119 0.558 0.040 0.002 0.017 1.10 11.56 0.80325 0.181 0.749 0.738 0.041 0.001 0.015 0.753 9.20 0.023______________________________________
TABLE 2__________________________________________________________________________(Continued from Table 1) (mass %) Invention steelsNo. W Zr Ta Hf Ti N O CS MPa VE J TO .mu.m__________________________________________________________________________ 1 0.408 -- -- -- -- 0.225 0.013 150 73.5 21 2 0.795 -- -- -- -- 0.313 0.003 184 104.1 24 3 1.382 -- -- -- -- 0.394 0.016 219 90.3 47 4 0.451 -- -- -- -- 0.142 0.019 178 74.4 18 5 0.222 -- -- -- -- 0.434 0.005 228 127.0 43 6 0.279 -- -- -- -- 0.148 0.016 187 79.3 12 7 0.845 -- -- -- -- 0.153 0.017 173 121.6 49 8 0.878 -- -- -- -- 0.123 0.004 155 86.0 24 9 1.289 -- -- -- -- 0.335 0.006 152 103.7 2410 0.994 -- -- -- -- 0.266 0.010 184 95.8 3711 0.249 0.027 -- -- -- 0.387 0.008 168 73.4 4912 0.592 0.065 -- -- -- 0.176 0.005 174 78.6 2913 0.987 0.047 -- -- -- 0.307 0.014 220 91.5 4314 0.341 0.091 -- -- -- 0.257 0.011 175 123.7 3915 0.240 0.016 -- -- -- 0.295 0.007 207 126.6 4616 0.892 0.041 -- -- -- 0.498 0.015 237 111.5 3017 1.261 0.034 -- -- -- 0.152 0.013 231 90.0 1818 0.295 0.065 -- -- -- 0.122 0.011 161 103.6 4019 0.818 0.052 -- -- -- 0.486 0.005 193 102.5 4120 0.469 0.012 -- -- -- 0.118 0.007 247 128.7 3021 1.482 -- 0.496 -- -- 0.290 0.010 191 72.7 3322 0.810 -- 0.212 -- -- 0.478 0.011 243 126.1 1923 0.677 -- 0.111 -- -- 0.158 0.002 224 120.3 3524 0.662 -- 0.041 -- -- 0.410 0.015 201 126.8 2825 0.349 -- 0.324 -- -- 0.302 0.007 243 126.2 25__________________________________________________________________________ CS: Creep rupture strength at 650.degree. C., 150 thousand hours; VE: Charpy impact absorption energy at 0.degree. C. after aging at 700.degree C. for 3000 hours; TO: Oxidation scale thickness after 650.degree. C., 10 thousand hour hightemperature oxidation
TABLE 3______________________________________(mass %) Invention steelsNo. C Si Mn P S Nb V Cr Mo______________________________________26 0.227 0.445 0.546 0.016 0.010 0.016 1.65 8.19 0.24327 0.217 0.517 0.527 0.032 0.003 0.006 1.57 11.93 0.15028 0.208 0.720 0.428 0.019 0.010 0.011 0.812 11.33 0.42229 0.105 0.415 0.401 0.041 0.009 0.012 0.551 9.86 0.25630 0.114 0.549 0.209 0.049 0.005 0.018 1.12 11.04 0.34731 0.138 0.075 0.380 0.047 0.008 0.011 1.98 10.65 0.36932 0.088 0.708 0.674 0.025 0.003 0.008 0.887 9.68 0.50533 0.021 0.643 0.840 0.010 0.007 0.019 1.56 11.63 0.95734 0.278 0.030 0.632 0.010 0.006 0.017 0.956 12.39 0.90735 0.189 0.570 0.990 0.030 0.004 0.005 1.88 10.36 0.03936 0.096 0.453 0.868 0.020 0.005 0.008 1.29 11.50 0.03537 0.059 0.226 0.815 0.047 0.009 0.006 0.337 9.25 0.58338 0.275 0.427 0.595 0.017 0.001 0.018 1.06 12.11 0.38939 0.218 0.418 0.743 0.020 0.003 0.016 0.388 8.46 0.13540 0.234 0.739 0.617 0.042 0.007 0.018 0.309 9.27 0.99241 0.085 0.750 0.361 0.011 0.001 0.019 0.305 10.43 0.16842 0.115 0.600 0.527 0.014 0.005 0.015 0.701 12.90 0.33943 0.095 0.054 0.475 0.019 0.002 0.015 0.972 10.18 0.70244 0.071 0.414 0.340 0.033 0.004 0.016 0.554 10.62 0.42845 0.102 0.668 0.683 0.024 0.002 0.012 1.51 12.71 0.22946 0.097 0.173 0.446 0.020 0.009 0.008 1.57 12.35 0.76647 0.107 0.639 0.981 0.027 0.006 0.018 1.06 10.49 0.73548 0.189 0.258 0.836 0.013 0.005 0.010 0.323 10.55 0.33349 0.252 0.747 0.570 0.046 0.004 0.010 1.35 8.52 0.23850 0.206 0.687 0.319 0.013 0.003 0.018 1.91 10.25 0.133______________________________________
TABLE 4__________________________________________________________________________(Continued from Table 3) (mass %) Invention steelsNo. W Zr Ta Hf Ti N O CS MPa VE J TO .mu.m__________________________________________________________________________26 0.646 -- 0.311 -- -- 0.109 0.019 170 70.4 3627 1.143 -- 0.014 -- -- 0.113 0.017 249 119.9 2628 1.428 -- 0.414 -- -- 0.377 0.004 198 105.7 2329 0.448 -- 0.259 -- -- 0.385 0.012 190 101.4 3530 0.415 -- 0.425 -- -- 0.416 0.016 241 116.1 1131 0.245 0.077 0.208 -- -- 0.140 0.003 170 71.8 3532 0.844 0.098 0.138 -- -- 0.233 0.001 196 129.8 1833 1.154 0.087 0.203 -- -- 0.169 0.016 186 120.8 4534 1.430 0.063 0.035 -- -- 0.420 0.014 159 115.3 2435 0.589 0.044 0.010 -- -- 0.258 0.007 236 126.3 2336 1.487 0.050 0.047 -- -- 0.367 0.007 234 104.1 5037 1.116 0.049 0.310 -- -- 0.221 0.001 223 89.8 1138 0.385 0.060 0.162 -- -- 0.486 0.010 220 125.1 3539 1.485 0.002 0.032 -- -- 0.447 0.018 196 71.4 4840 0.746 0.046 0.415 -- -- 0.378 0.012 217 119.2 3941 1.020 -- -- 0.512 -- 0.141 0.003 152 129.4 3442 0.603 -- -- 0.884 -- 0.226 0.013 174 115.6 2243 1.047 -- -- 0.847 -- 0.109 0.001 198 117.4 3044 1.267 -- -- 0.099 -- 0.258 0.015 245 116.7 2645 0.895 -- -- 0.802 -- 0.148 0.004 231 123.7 1746 0.793 -- -- 0.171 -- 0.260 0.017 227 90.5 3047 0.560 -- -- 0.362 -- 0.464 0.002 199 117.4 1248 0.450 -- -- 0.596 -- 0.431 0.018 220 127.4 3249 1.352 -- -- 0.053 -- 0.446 0.014 155 100.4 3850 0.249 -- -- 0.888 -- 0.378 0.010 174 106.8 35__________________________________________________________________________ CS: Creep rupture strength at 650.degree. C., 150 thousand hours; VE: Charpy impact absorption energy at 0.degree. C. after aging at 700.degree C. for 3000 hours; TO: Oxidation scale thickness after 650.degree. C., 10 thousand hour hightemperature oxidation
TABLE 5______________________________________(mass %) Invention steelsNo. C Si Mn P S Nb V Cr Mo______________________________________51 0.103 0.595 0.642 0.022 0.004 0.016 0.648 9.26 0.21952 0.145 0.254 0.487 0.040 0.006 0.008 1.26 8.95 0.67553 0.096 0.193 0.807 0.015 0.009 0.009 1.53 12.78 0.19554 0.155 0.554 0.948 0.035 0.005 0.016 0.907 11.65 0.95255 0.229 0.705 0.660 0.045 0.007 0.010 1.42 11.52 0.64856 0.230 0.406 0.898 0.016 0.006 0.015 0.841 10.83 0.96457 0.214 0.186 0.603 0.033 0.009 0.011 1.17 10.50 0.58958 0.230 0.193 0.733 0.023 0.008 0.010 1.92 9.02 0.71559 0.195 0.194 0.243 0.037 0.009 0.007 1.68 12.31 0.03560 0.014 0.318 0.865 0.019 0.001 0.010 1.61 8.73 0.21061 0.174 0.729 0.369 0.018 0.008 0.017 1.18 9.31 0.94562 0.290 0.748 0.858 0.020 0.004 0.007 1.52 9.74 0.89763 0.281 0.198 0.551 0.034 0.001 0.006 1.37 8.89 0.82264 0.059 0.754 0.367 0.029 0.009 0.016 1.81 12.45 0.86465 0.255 0.229 0.462 0.010 0.007 0.018 1.49 11.43 0.72566 0.048 0.317 0.972 0.045 0.006 0.014 0.692 11.68 0.57567 0.221 0.394 0.856 0.042 0.002 0.009 0.612 11.68 0.11168 0.249 0.600 0.265 0.048 0.008 0.010 1.57 9.89 0.51469 0.041 0.300 0.940 0.031 0.006 0.007 1.31 9.69 0.97370 0.082 0.424 0.238 0.018 0.007 0.010 1.03 9.55 0.18971 0.144 0.739 0.718 0.017 0.008 0.014 1.90 12.97 0.34272 0.280 0.599 0.520 0.016 0.006 0.014 1.67 10.82 0.11973 0.249 0.150 0.992 0.041 0.004 0.007 0.665 9.03 0.20174 0.252 0.704 0.680 0.020 0.007 0.016 1.74 11.02 0.76975 0.201 0.079 0.547 0.021 0.003 0.015 1.84 12.79 0.035______________________________________
TABLE 6__________________________________________________________________________(Continued from Table 5) (mass %) Invention steelsNo. W Zr Ta Hf Ti N O CS MPa VE J TO .mu.m__________________________________________________________________________51 1.305 0.061 -- 0.823 -- 0.294 0.011 245 99.7 3252 0.854 0.013 -- 0.541 -- 0.287 0.002 239 89.5 1653 1.091 0.006 -- 0.219 -- 0.217 0.013 171 116.9 3554 0.946 0.015 -- 0.535 -- 0.358 0.002 163 103.8 1755 1.337 0.001 -- 0.218 -- 0.400 0.010 234 122.3 4856 0.535 0.091 -- 0.918 -- 0.410 0.002 202 123.2 3857 0.750 0.047 -- 0.352 -- 0.265 0.011 185 87.0 1258 0.925 0.091 -- 0.671 -- 0.238 0.012 152 85.4 3859 0.655 0.041 -- 0.098 -- 0.198 0.017 171 129.2 2460 0.812 0.016 -- 0.775 -- 0.429 0.003 212 109.9 1861 0.356 -- 0.412 0.436 -- 0.200 0.009 243 128.7 2662 1.440 -- 0.207 0.253 -- 0.189 0.003 184 77.8 3763 1.154 -- 0.048 0.391 -- 0.470 0.005 150 86.3 3764 0.975 -- 0.446 0.568 -- 0.118 0.002 216 78.1 1665 1.169 -- 0.263 0.967 -- 0.210 0.006 247 93.3 3966 1.298 -- 0.152 0.760 -- 0.225 0.011 209 111.5 1467 0.990 -- 0.051 0.148 -- 0.218 0.010 226 86.4 2968 0.476 -- 0.253 0.816 -- 0.491 0.019 166 118.7 3269 1.288 -- 0.198 0.944 -- 0.301 0.010 244 98.4 2970 1.086 -- 0.422 0.728 -- 0.334 0.009 231 97.9 4971 1.418 0.071 0.285 0.359 -- 0.254 0.015 197 128.5 3872 0.568 0.054 0.046 0.021 -- 0.343 0.007 159 80.7 4673 1.370 0.056 0.080 0.380 -- 0.476 0.006 187 86.4 1874 0.826 0.045 0.255 0.659 -- 0.326 0.005 199 96.8 4275 1.138 0.090 0.037 0.522 -- 0.368 0.010 164 92.5 46__________________________________________________________________________ CS: Creep rupture strength at 650.degree. C., 150 thousand hours; VE: Charpy impact absorption energy at 0.degree. C. after aging at 700.degree C. for 3000 hours; TO: Oxidation scale thickness after 650.degree. C., 10 thousand hour hightemperature oxidation
TABLE 7______________________________________(mass %) Invention steelsNo. C Si Mn P S Nb V Cr Mo______________________________________76 0.295 0.366 0.337 0.012 0.009 0.007 0.422 12.76 0.66777 0.296 0.535 0.592 0.038 0.006 0.017 0.337 9.31 0.35578 0.263 0.360 0.283 0.010 0.007 0.010 1.09 11.00 0.80279 0.099 0.356 0.334 0.033 0.008 0.019 1.26 8.59 0.66780 0.152 0.676 0.911 0.035 0.002 0.017 0.344 10.66 0.16481 0.186 0.302 0.960 0.024 0.008 0.008 0.358 8.12 0.96782 0.255 0.158 0.232 0.047 0.002 0.007 0.752 9.38 0.76883 0.268 0.385 0.873 0.032 0.007 0.011 1.86 10.37 0.74984 0.282 0.754 0.246 0.047 0.008 0.009 1.47 9.61 0.61485 0.061 0.617 0.888 0.038 0.005 0.009 1.57 12.95 0.53586 0.235 0.122 0.550 0.013 0.001 0.015 1.62 11.33 0.69387 0.284 0.193 0.982 0.020 0.001 0.007 1.95 10.68 0.78288 0.247 0.187 0.720 0.025 0.004 0.010 1.18 11.90 0.48889 0.060 0.284 0.750 0.038 0.006 0.005 0.516 8.60 0.51690 0.046 0.602 0.399 0.025 0.009 0.010 1.93 9.09 0.53891 0.273 0.137 0.630 0.015 0.004 0.012 1.52 9.39 0.75192 0.205 0.185 0.774 0.013 0.005 0.014 0.436 10.32 0.33693 0.048 0.514 0.594 0.028 0.006 0.005 0.700 10.40 0.97494 0.287 0.490 0.239 0.047 0.007 0.009 1.78 10.55 0.86795 0.255 0.256 0.257 0.018 0.007 0.013 0.614 11.71 0.69596 0.294 0.343 0.392 0.048 0.005 0.014 1.73 12.27 0.13997 0.170 0.132 0.408 0.026 0.002 0.008 0.388 8.24 0.39698 0.226 0.147 0.844 0.017 0.009 0.010 1.98 8.02 0.14999 0.226 0.526 0.640 0.010 0.009 0.017 0.879 12.50 0.081100 0.079 0.268 0.371 0.032 0.009 0.010 0.821 10.22 0.889______________________________________
TABLE 8__________________________________________________________________________(Continued from Table 7) (mass %) Invention steelsNo. W Zr Ta Hf Ti N O CS MPa VE J TO .mu.m__________________________________________________________________________76 1.236 0.0007 0.224 0.659 -- 0.278 0.013 199 85.4 1877 0.722 0.022 0.636 0.279 -- 0.133 0.018 176 86.9 4478 1.148 0.096 0.430 0.044 -- 0.401 0.002 212 77.6 3379 1.433 0.052 0.234 0.621 -- 0.164 0.003 223 127.9 3180 1.191 0.006 0.163 0.754 -- 0.288 0.017 234 71.8 4881 0.666 -- -- -- 0.066 0.462 0.002 159 128.5 4982 1.386 -- -- -- 0.034 0.355 0.006 169 70.4 2383 0.360 -- -- -- 0.030 0.443 0.014 182 87.9 1684 0.437 -- -- -- 0.072 0.193 0.003 165 101.6 1785 1.197 -- -- -- 0.043 0.487 0.013 189 93.8 1286 0.275 -- -- -- 0.093 0.395 0.019 223 105.8 3087 0.519 -- -- -- 0.015 0.399 0.006 184 88.0 1888 0.880 -- -- -- 0.095 0.368 0.016 241 112.8 2389 0.318 -- -- -- 0.036 0.381 0.013 214 70.5 3390 0.356 -- -- -- 0.034 0.113 0.012 170 92.5 1591 1.254 0.003 -- -- 0.017 0.237 0.007 181 101.0 3892 0.639 0.074 -- -- 0.090 0.428 0.009 212 75.8 4793 0.711 0.081 -- -- 0.092 0.161 0.013 233 119.1 3294 0.419 0.005 -- -- 0.084 0.313 0.005 214 91.8 3995 0.651 0.053 -- -- 0.037 0.355 0.015 173 95.6 3696 0.990 0.054 -- -- 0.059 0.162 0.019 177 110.6 5097 0.401 0.023 -- -- 0.031 0.417 0.012 248 89.7 4998 1.058 0.079 -- -- 0.017 0.391 0.015 153 103.4 4199 1.269 0.091 -- -- 0.076 0.355 0.004 160 72.7 12100 0.628 0.078 -- -- 0.092 0.188 0.010 189 98.5 11__________________________________________________________________________ CS: Creep rupture strength at 650.degree. C., 150 thousand hours; VE: Charpy impact absorption energy at 0.degree. C. after aging at 700.degree C. for 3000 hours; TO: Oxidation scale thickness after 650.degree. C., 10 thousand hour hightemperature oxidation
TABLE 9______________________________________(mass %) Invention steelsNo. C Si Mn P S Nb V Cr Mo______________________________________101 0.132 0.288 0.974 0.011 0.001 0.006 1.24 12.05 0.757102 0.292 0.334 0.991 0.035 0.001 0.015 1.65 11.42 0.369103 0.179 0.565 0.986 0.029 0.006 0.017 0.643 9.31 0.915104 0.284 0.344 0.304 0.044 0.009 0.016 1.93 11.62 0.584105 0.221 0.589 0.689 0.024 0.001 0.014 0.746 9.30 0.062106 0.052 0.290 0.302 0.020 0.008 0.015 0.803 10.82 0.533107 0.117 0.759 0.887 0.037 0.008 0.012 1.57 12.06 0.196108 0.180 0.571 0.993 0.043 0.007 0.010 1.68 11.52 0.727109 0.153 0.279 0.376 0.046 0.009 0.018 0.597 10.12 0.326110 0.235 0.412 0.783 0.033 0.004 0.010 0.321 8.76 0.166111 0.189 0.332 0.356 0.033 0.009 0.010 0.332 10.91 0.439112 0.067 0.579 0.857 0.011 0.006 0.015 0.956 12.51 0.838113 0.218 0.510 0.419 0.036 0.002 0.018 1.62 11.91 0.533114 0.258 0.295 0.819 0.015 0.009 0.009 1.87 12.71 0.742115 0.100 0.063 0.588 0.036 0.009 0.019 1.97 10.74 0.133116 0.083 0.733 0.671 0.026 0.008 0.015 0.543 11.92 0.386117 0.266 0.127 0.832 0.033 0.009 0.014 1.32 12.26 0.703118 0.269 0.728 0.819 0.025 0.009 0.011 1.22 12.67 0.275119 0.287 0.337 0.775 0.048 0.009 0.009 0.554 9.07 0.275120 0.090 0.272 0.854 0.031 0.001 0.011 0.491 9.90 0.893121 0.014 0.291 0.806 0.020 0.007 0.012 1.34 8.61 0.821122 0.264 0.145 0.777 0.023 0.004 0.008 1.75 8.62 0.252123 0.170 0.771 0.526 0.028 0.003 0.016 1.17 10.91 0.866124 0.075 0.353 0.592 0.022 0.003 0.009 1.61 8.85 0.349125 0.178 0.605 0.731 0.013 0.004 0.013 0.860 10.92 0.389______________________________________
TABLE 10__________________________________________________________________________(Continued from Table 9) (mass %) Invention steelsNo. W Zr Ta Hf Ti N O CS MPa VE J TO .mu.m__________________________________________________________________________101 1.313 -- 0.045 -- 0.035 0.359 0.019 209 103.5 25102 0.984 -- 0.026 -- 0.014 0.156 0.006 188 127.6 41103 0.529 -- 0.091 -- 0.089 0.441 0.011 244 92.6 27104 0.836 -- 0.517 -- 0.099 0.494 0.010 198 99.6 30105 0.206 -- 0.053 -- 0.013 0.190 0.017 217 100.1 39106 0.481 -- 0.074 -- 0.031 0.406 0.015 219 104.7 40107 1.010 -- 0.055 -- 0.077 0.411 0.017 224 95.0 20108 0.977 -- 0.120 -- 0.034 0.485 0.010 152 83.0 48109 0.345 -- 0.104 -- 0.054 0.103 0.013 168 78.1 11110 0.634 -- 0.342 -- 0.019 0.334 0.004 244 93.2 16111 0.798 0.026 0.132 -- 0.036 0.259 0.013 249 79.3 11112 0.429 0.072 0.015 -- 0.077 0.154 0.017 150 77.6 24113 1.062 0.085 0.135 -- 0.023 0.290 0.009 216 128.4 41114 0.370 0.086 0.207 -- 0.071 0.341 0.002 216 124.2 11115 0.517 0.094 0.231 -- 0.013 0.388 0.009 218 105.4 40116 1.103 0.075 0.276 -- 0.047 0.300 0.005 242 83.5 17117 1.080 0.052 0.045 -- 0.054 0.153 0.003 157 100.3 49118 0.691 0.090 0.187 -- 0.051 0.428 0.008 181 106.7 23119 1.473 0.058 0.090 -- 0.099 0.396 0.012 233 83.5 27120 1.073 0.026 0.527 -- 0.080 0.127 0.010 229 71.4 28121 0.378 -- -- 0.455 0.011 0.498 0.006 241 82.9 14122 0.945 -- -- 0.090 0.046 0.385 0.012 238 129.3 12123 0.410 -- -- 0.801 0.020 0.270 0.005 189 71.6 31124 0.319 -- -- 0.806 0.085 0.223 0.005 211 101.5 17125 0.909 -- -- 0.269 0.033 0.319 0.017 173 108.7 17__________________________________________________________________________ CS: Creep rupture strength at 650.degree. C., 150 thousand hours; VE: Charpy impact abosrption energy at 0.degree. C. after aging at 700.degree. C. for 3000 hours; TO: Oxidation scale thickness after 650.degree. C., 10 thousand hour hightemperature oxidation
TABLE 11______________________________________(mass %) Invention steelsNo. C Si Mn P S Nb V Cr Mo______________________________________126 0.102 0.508 0.305 0.029 0.008 0.008 0.946 8.13 0.193127 0.185 0.579 0.635 0.036 0.002 0.011 1.27 11.24 0.405128 0.194 0.203 0.295 0.022 0.009 0.018 1.38 8.80 0.747129 0.039 0.294 0.220 0.015 0.004 0.010 1.56 11.75 0.903130 0.065 0.617 0.569 0.022 0.001 0.018 0.428 10.98 0.551131 0.180 0.532 0.693 0.031 0.001 0.017 0.854 9.99 0.382132 0.148 0.582 0.339 0.049 0.009 0.015 0.623 9.68 0.094133 0.172 0.523 0.861 0.044 0.010 0.010 0.892 11.02 0.362134 0.160 0.109 0.803 0.044 0.004 0.010 1.12 9.91 0.375135 0.164 0.654 0.724 0.015 0.003 0.011 1.65 12.33 0.827136 0.095 0.360 0.767 0.045 0.005 0.016 1.09 9.19 0.904137 0.152 0.139 0.273 0.042 0.005 0.005 0.581 8.86 0.779138 0.099 0.546 0.611 0.014 0.007 0.019 1.33 9.91 0.165139 0.284 0.555 0.325 0.047 0.001 0.008 1.95 8.23 0.237140 0.030 0.678 0.749 0.010 0.005 0.011 1.03 9.66 0.663141 0.262 0.310 0.454 0.028 0.010 0.011 0.625 12.77 0.658142 0.169 0.358 0.773 0.032 0.009 0.009 1.87 10.89 0.891143 0.093 0.202 0.671 0.047 0.003 0.015 1.71 10.04 0.076144 0.087 0.367 0.685 0.041 0.004 0.017 1.30 8.59 0.862145 0.206 0.611 0.966 0.022 0.004 0.019 1.80 12.49 0.457146 0.216 0.311 0.478 0.037 0.005 0.016 1.86 12.73 0.056147 0.029 0.383 0.563 0.014 0.004 0.010 1.78 10.26 0.842148 0.275 0.596 0.977 0.040 0.003 0.019 1.06 8.50 0.011149 0.141 0.307 0.663 0.023 0.008 0.009 0.829 10.86 0.732150 0.113 0.049 0.565 0.011 0.001 0.012 1.40 8.25 0.199______________________________________
TABLE 12__________________________________________________________________________(Continued from Table 11) (mass %) Invention steelsNo. W Zr Ta Hf Ti N O CS MPa VE J TO .mu.m__________________________________________________________________________126 0.494 -- -- 0.387 0.016 0.230 0.016 194 75.8 21127 1.235 -- -- 0.351 0.096 0.436 0.006 193 103.9 34128 1.447 -- -- 0.835 0.065 0.411 0.018 239 113.6 24129 0.726 -- -- 0.046 0.074 0.425 0.018 250 87.0 19130 1.251 -- -- 0.156 0.096 0.160 0.010 195 124.7 27131 1.325 0.067 -- 0.356 0.012 0.287 0.007 193 88.1 15132 0.551 0.045 -- 0.819 0.062 0.477 0.002 211 108.0 29133 1.110 0.015 -- 0.761 0.042 0.413 0.009 221 106.9 39134 0.653 0.098 -- 0.364 0.012 0.166 0.012 241 95.4 32135 1.377 0.062 -- 0.791 0.034 0.412 0.007 187 84.1 14136 0.917 0.025 -- 0.755 0.034 0.425 0.013 180 85.0 13137 0.799 0.002 -- 0.937 0.074 0.283 0.009 239 109.7 18138 0.663 0.076 -- 0.032 0.083 0.458 0.005 232 108.4 34139 0.725 0.002 -- 0.204 0.030 0.225 0.006 228 123.0 31140 0.560 0.051 -- 0.160 0.069 0.259 0.014 245 104.5 15141 0.441 -- 0.010 0.074 0.080 0.235 0.007 152 124.2 14142 1.244 -- 0.023 0.638 0.081 0.227 0.014 168 103.2 35143 0.630 -- 0.030 0.063 0.045 0.114 0.004 163 113.6 46144 0.768 -- 0.247 0.997 0.077 0.171 0.014 154 75.8 35145 1.270 -- 0.435 0.160 0.059 0.467 0.004 160 121.3 29146 0.435 -- 0.013 0.697 0.051 0.481 0.014 198 79.4 33147 0.450 -- 0.876 0.338 0.074 0.274 0.018 241 114.9 19148 0.274 -- 0.310 0.266 0.054 0.151 0.013 205 117.1 31149 0.774 -- 0.059 0.651 0.097 0.164 0.019 210 97.9 39150 0.254 -- 0.159 0.700 0.085 0.201 0.003 174 127.9 50__________________________________________________________________________ CS: Creep rupture strength at 650.degree. C., 150 thousand hours; VE: Charpy impact absorption energy at 0.degree. C. after aging at 700.degree C. for 3000 hours; TO: Oxidation scale thickness after 650.degree. C., 10 thousand hour hightemperature oxidation
TABLE 13______________________________________(mass %) Invention steelsNo. C Si Mn P S Nb V Cr Mo______________________________________151 0.102 0.359 0.441 0.030 0.005 0.016 0.561 9.14 0.097152 0.020 0.608 0.445 0.028 0.001 0.016 1.17 9.49 0.118153 0.059 0.154 0.312 0.033 0.006 0.016 1.01 10.17 0.943154 0.137 0.713 0.604 0.013 0.007 0.010 1.24 9.70 0.273155 0.156 0.467 0.260 0.013 0.010 0.017 1.33 11.41 0.774156 0.178 0.369 0.255 0.044 0.008 0.016 1.61 11.40 0.164157 0.252 0.152 0.712 0.011 0.003 0.018 0.682 10.44 0.103158 0.142 0.347 0.586 0.022 0.006 0.012 1.40 9.52 0.280159 0.196 0.345 0.841 0.045 0.005 0.006 0.742 12.19 0.904160 0.175 0.277 0.416 0.047 0.006 0.012 1.51 11.75 0.648______________________________________
TABLE 14__________________________________________________________________________(Continued from Table 13) (mass %) Invention steelsNo. W Zr Ta Hf Ti N O CS MPa VE J TO .mu.m__________________________________________________________________________151 0.904 0.036 0.671 0.089 0.079 0.325 0.005 215 98.9 39152 0.366 0.044 0.112 0.999 0.098 0.218 0.011 204 82.1 27153 1.495 0.021 0.217 0.142 0.022 0.156 0.006 208 118.6 50154 1.280 0.034 0.025 0.175 0.048 0.412 0.010 245 99.2 24155 0.608 0.054 0.305 0.302 0.013 0.258 0.010 186 96.2 19156 1.040 0.048 0.121 0.709 0.026 0.175 0.018 199 90.2 42157 1.498 0.085 0.352 0.574 0.010 0.235 0.019 201 121.9 39158 0.271 0.085 0.012 0.101 0.074 0.309 0.007 163 83.2 18159 0.248 0.066 0.014 0.962 0.056 0.475 0.005 153 75.5 27160 0.324 0.097 0.066 0.854 0.015 0.211 0.015 239 109.8 14__________________________________________________________________________ CS: Creep rupture strength at 650.degree. C., 150 thousand hours; VE: Charpy impact absorption energy at 0.degree. C. after aging at 700.degree C. for 3000 hours; TO: Oxidation scale thickness after 650.degree. C., 10 thousand hour hightemperature oxidation
TABLE 15______________________________________Comparison steels (mass %)No. C Si Mn P S Nb V Cr Mo______________________________________161 0.042 0.232 0.535 0.012 0.007 0.012 0.565 8.85 0.54162 0.076 0.025 0.512 0.014 0.008 0.018 0.554 9.02 0.53163 0.099 0.056 0.498 0.011 0.002 0.017 0.512 9.05 0.50164 0.122 0.101 0.446 0.034 0.002 0.012 0.776 9.00 0.50165 0.087 0.087 0.335 0.044 0.001 0.014 0.898 9.01 0.50166 0.078 0.099 0.323 0.007 0.001 0.011 0.999 9.043 0.49167 0.065 0.022 0.898 0.006 0.001 0.019 0.117 12.01 0.22168 0.223 0.045 0.991 0.003 0.002 0.017 2.565 12.02 0.87169 0.206 0.130 0.567 0.011 0.001 0.072 1.555 12.50 0.51170 0.197 0.124 0.532 0.010 0.001 0.015 1.889 11.44 0.55171 0.112 0.187 0.500 0.009 0.008 0.011 1.990 11.08 0.66172 0.188 0.291 0.502 0.016 0.001 0.009 1.156 10.56 0.48173 0.055 0.029 0.499 0.018 0.008 0.002 0.331 10.98 0.52174 0.042 0.067 0.561 0.011 0.002 0.005 0.505 10.43 0.44______________________________________
TABLE 16__________________________________________________________________________(Continued from Table 15) Comparison steels (mass %)No. W Zr Ta Hf Ti N O CS MPa VE J TO (.mu.m)__________________________________________________________________________161 0.87 0.006 -- -- -- 0.007 0.012 78 71 860162 0.80 -- 0.65 -- -- 0.045 0.015 90 74 450163 0.87 -- -- 0.21 -- 0.511 0.011 187 8 25164 0.86 -- -- -- 0.025 0.862 0.006 202 14 30165 0.11 0.007 -- -- -- 0.165 0.005 61 80 45166 1.93 0.008 0.088 0.35 -- 0.144 0.002 50 6 20167 0.99 0.007 -- -- 0.041 0.330 0.002 120 80 20168 0.88 0.004 -- 0.21 0.026 0.221 0.002 105 13 40169 0.88 -- 0.36 -- -- 0.280 0.004 190 11 30170 0.67 0.118 0.27 0.15 0.053 0.155 0.006 220 4 15171 0.77 -- 1.80 0.90 0.081 0.129 0.012 230 8 15172 1.23 -- -- 1.70 0.011 0.444 0.019 205 9 5173 1.21 0.007 -- -- 0.112 0.313 0.008 208 6 30174 1.44 0.003 0.54 0.28 0.019 0.189 0.002 36 3 40__________________________________________________________________________ CS: Creep rupture strength at 650.degree. C., 150 thousand hours; VE: Charpy impact absorption energy at 0.degree. C. after aging at 700.degree C. for 3000 hours; TO: Oxidation scale thickness after 650.degree. C., 10 thousand hour hightemperature oxidation
The present invention provides a high-nitrogen ferritic heat-resisting steel with high V content exhibiting a high rupture strength after prolonged creep and superior high-temperature oxidation resistance and, as such, can be expected to make a major contribution to industrial progress.

Number	Date	Country
205629	Jan 1984	DEX
795471	May 1958	GBX

High-nitrogen ferritic heat-resisting steel with high vanadium content and method of production thereof

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