JPS6363605B2 - - Google Patents

Description

[Detailed description of the invention]

The present invention relates to a method for manufacturing high-strength oil country tubular goods having excellent stress corrosion cracking resistance. In recent years, due to the deterioration of the energy situation, there has been a marked tendency for oil and natural gas wells to become deeper.
Deep wells over 6000m deep, some over 10000m deep, have appeared. Furthermore, due to similar circumstances, it is becoming increasingly difficult to extract oil and natural gas in a harsh corrosive environment containing humid hydrogen sulfide, as well as corrosive components such as carbon dioxide gas and chloride ions. As oil and natural gas are drilled in such harsh environments, the oil country tubular goods used in this process are now required to have high strength and excellent corrosion resistance, especially stress corrosion cracking resistance. . As a general anti-corrosion measure for oil country tubular goods, it is known to introduce a corrosion suppressant called an inhibitor, but this method is often not effective for use in, for example, offshore oil wells. From this point of view, consideration has recently begun to be given to the use of high-grade corrosion-resistant high-alloy steels such as stainless steel and Incoloy and Hastelloy (both trade names) for the production of oil country tubular goods. Regarding the corrosion behavior of H ₂ S―CO ₂ ―Cl ^- in an oil well environment, the details have not yet been fully elucidated, and furthermore, it does not have the high strength required for oil country tubular goods for deep wells. is the current situation. Therefore, from the above-mentioned point of view, the present inventors investigated deep wells and severe corrosive environments, especially H ₂ S―CO ₂ -
As a result of conducting research to manufacture oil country tubular goods with high strength and excellent stress corrosion cracking resistance that can sufficiently withstand oil drilling in the Cl ^- oil well environment, we found that (a) H ₂ S―CO ₂ - The main type of corrosion in a Cl ^- environment is stress corrosion cracking, but the behavior of stress corrosion cracking in this case is completely different from that of general austenitic stainless steel. In other words, whereas general stress corrosion cracking is deeply related to the presence of Cl ^- , in the oil well environment mentioned above, the influence of H ₂ S is greater than that of Cl ^- . (b) Steel pipes used for practical use as oil country tubular goods are generally
Cold working is performed to improve strength, but cold working significantly reduces the resistance to stress corrosion cracking. (c) The elution rate (corrosion rate) of steel in an H ₂ S—CO ₂ —Cl ⁻ environment depends on the contents of Cr, Ni, Mo, and W, and is affected by the surface film made of these components. Corrosion resistance is maintained and these components are
It also increases its resistance to stress corrosion cracking, with Mo being 10 times more effective than Cr, and Mo being 10 times more effective than W.
It has twice the effect of
Mo and W satisfy the following conditional expressions: Cr (%) + 10Mo (%) + 5W (%) ≧110%, 8%≦Mo (%) + 1/2W (%)≦12%, and the Ni content is 30～
60%, and the Cr content is 15 to 30%, H ₂ S—, which is extremely corrosive, even if it is a cold-worked material.
It is possible to obtain a surface film that exhibits excellent resistance to stress corrosion cracking in a CO ₂ - Cl ^- oil well environment, especially in a harsh environment of 200°C or higher. (d) Ni has the effect of increasing stress corrosion cracking resistance not only on the surface film but also on the structure. (e) When N is included as an alloy component in the range of 0.05 to 0.3%, the strength of the pipe material is further improved. (f) If the S content as an unavoidable impurity is reduced to 0.0007% or less, the hot workability of the pipe material will be significantly improved. (g) When the P content as an unavoidable impurity is reduced to 0.003% or less, the susceptibility to hydrogen cracking significantly decreases. (h) Cu: 2% or less and Co: 2 as alloy components
% or less, the corrosion resistance is further improved. (i) Rare earth elements: 0.10% or less as alloy components;
Y: 0.20% or less, Mg: 0.10% or less, Ti: 0.5%
When one or more of the following and Ca: 0.10% or less is contained, hot workability is further improved. (j) However, in order to ensure the desired high strength,
First, to the alloy of the above composition, preferably 1050 ~
This material is heated to a temperature within the temperature range of 1250°C to completely dissolve intermetallic compounds and carbides, and then hot worked under conditions where the wall thickness reduction rate below the recrystallization temperature is 10% or more. Hot working is to form fine recrystallized grains in the post-process heat treatment to ensure high strength and good ductility. (℃) and the same empirical formula: 16Mo (%) +
Heat treatment is performed at a temperature between the upper limit temperature (°C) calculated by 10W (%) + 10Cr (%) + 777 for 2 hours or less to form fine recrystallized grains as described above, and in this case If there is undissolved carbide that degrades corrosion resistance, it will be dissolved in solid solution, and eventually the pipe material after the above heat treatment will contain 10 to 60% carbide.
It is necessary to perform cold working at a wall thickness reduction rate of % to strengthen the process. The findings shown in (a) to (j) above were obtained. Therefore, this invention was made based on the above knowledge, and includes C: 0.05% or less, Si: 1.0%.
% or less, Mn: 2.0% or less, P: 0.030% or less, preferably for the purpose of further improving hydrogen cracking resistance, P: 0.003% or less, S: 0.005% or less, preferably for the purpose of further improving hot workability. So S: 0.0007%
Below, sol.Al: 0.5% or less, Ni: 30-60%, Cr:
Contains 15-30%, Mo: 12% or less and W: 24
% or less, and if necessary, N: 0.05 to 0.3%, Cu: 2% or less,
Co: 2% or less, rare earth elements: 0.10% or less, Y:
0.20% or less, Mg: 0.10% or less, Ti: 0.5% or less,
and Ca: 0.10% or less, and the remainder is Fe and unavoidable impurities.
) and satisfies the following conditions: Cr (%) + 10Mo (%) + 5W (%) ≧110%, 8%≦Mo (%) + 1/2W (%)≦12%. , hot working under the condition that the wall thickness reduction rate below the recrystallization temperature is 10% or more, and then the lower limit temperature (℃) calculated by 260logC (%) + 1300 and 16Mo (%) + 10W (%) + 10Cr (%) +777
After heat treatment at a temperature between the upper limit temperature (℃) calculated for 2 hours or less, cold working at a wall thickness reduction rate of 10 to 60% improves stress corrosion cracking resistance. This method is characterized by a method for manufacturing high-strength oil country tubular goods with excellent properties. Next, in the method for manufacturing oil country tubular goods of this invention,
The reason why the component composition, heat treatment conditions, and wall thickness reduction rates in hot working and cold working are limited as described above will be explained below. A Component composition (a) C The lower the C content, the more the precipitation of carbides will be suppressed, so the heating temperature and heat treatment temperature during hot working can be lowered, and this will improve the strength after cold working. It works more effectively as the temperature rises. Therefore, C
It is desirable that the content be as low as possible, but C
If the content exceeds 0.05%, intergranular stress corrosion cracking is likely to occur, so the upper limit value should be
It was set at 0.05%. (b) Si Si is a necessary component as a deoxidizing component, but
If the content exceeds 1.0%, hot workability will deteriorate, so the upper limit value should be set.
It was set at 1.0%. (c) Mn Mn component has a deoxidizing effect like Si,
Furthermore, since this component has almost no effect on stress corrosion cracking resistance, its upper limit was set at a rather high value of 2.0%. (d) P The P component as an unavoidable impurity has the effect of increasing stress corrosion cracking susceptibility when its content exceeds 0.030%.
It is necessary to set it at 0.030% to keep stress corrosion cracking susceptibility to a low level. It has also been found that as the P content is reduced, hydrogen cracking resistance rapidly improves after reaching 0.003%. If necessary, the P content is preferably 0.0030% or less. (e) S The S component as an unavoidable impurity has the effect of deteriorating hot workability when its content exceeds 0.005%, so the upper limit value must be set.
It is necessary to set it at 0.005% to prevent deterioration of hot workability. In this way, the S component has the effect of deteriorating hot workability when its content increases, but by decreasing its content, 0.0007
On the contrary, if the S content is reduced to 0.0007% or less, the hot workability will be further improved, so if hot working under severe conditions is required, it is desirable to reduce the S content to 0.0007% or less. (f) Al Al is effective as a deoxidizing component like Si and Mn, and even if it is included up to 0.5% in sol.Al content, it will not impair the properties of the pipe material. .0.5 in Al content
% or less. (g) Ni Ni has the effect of improving the stress corrosion cracking resistance of pipe materials, but if its content is less than 30%, the desired excellent stress corrosion cracking resistance cannot be secured; Even if the content exceeds 30%, no further improvement effect on stress corrosion cracking resistance appears, and the content was set at 30% to 60%, taking economic efficiency into account. (h) Cr The Cr component is a component that significantly improves stress corrosion cracking resistance when coexisting with Ni, Mo, and W components, but hot workability is not improved even if its content is less than 15%. On the contrary, in order to secure the desired stress corrosion cracking resistance, the content of Mo and W must be increased by that amount, which is economically disadvantageous, so the lower limit The value was set at 15%. On the other hand, if the S content exceeds 30%, deterioration of hot workability cannot be avoided no matter how much the S content is reduced, so the upper limit was set at 30%. (i) Mo and W As mentioned above, these components have an equal effect on improving stress corrosion cracking resistance when coexisting with Ni and Cr, but each
Even if Mo: 12% and W: 24% are contained, the environmental temperature is 200℃ or higher H ₂ S—CO ₂
- In the corrosive environment of Cl ^- , no further improvement effect appeared, and in consideration of economic efficiency, the respective contents were determined to be Mo: 12% or less and W: 24% or less. Also, regarding the content of Mo and W,
The reason why the conditional expression: Mo (%) + 1/2 W (%) is specified is because the atomic weight of W is about twice that of Mo, and the effect is about 1/2, which is equivalent, so this value is If it is less than 8%, the desired stress corrosion cracking resistance cannot be obtained, especially under the adverse environment above 200°C.On the other hand, even if this value is increased beyond 12%, as mentioned above, there will be substantially unnecessary stress corrosion cracking resistance. Since the amount of Mo and W contained is uneconomical, the value of Mo (%) + 1/2 W (%) was set at 8 to 12%. (j) N Since the N component has the effect of improving strength through solid solution strengthening, it is included as necessary when particularly high strength is required, but if the content is 0.05
If the content is less than 0.3%, the desired strength improvement effect cannot be obtained; on the other hand, if the content exceeds 0.3%,
Since melting and ingot making are difficult, its content was set at 0.05 to 0.3%. (k) Cu and Co These components have a uniform effect of improving the corrosion resistance of pipe materials, and Co has a solid solution strengthening effect. However, if Cu exceeds 2%, hot workability will deteriorate, while Co content will not improve further even if it exceeds 2%. each value
Cu: 2% and Co: 2% were set. (l) Rare earth elements, Y, Mg, Ti, and Ca These components have a uniform effect to further improve hot workability, so they can be used as needed when hot working is carried out under severe conditions. Rare earth elements: 0.10
%, Y: 0.20%, Mg: 0.10%, Ti: 0.5%,
and Ca: Even if the content exceeds 0.10%, there is no improvement effect on hot workability, and even a deterioration phenomenon appears.
Y: 0.20% or less, Mg: 0.10% or less, Ti: 0.5
% or less, and Ca: 0.10% or less. (m) Cr (%) + 10Mo (%) + 5W (%) Figure 1 shows stress corrosion cracking resistance under severe corrosive environments. Cr (%) + 10Mo (%) + 5W
(%) and the relationship between Ni content. That is, Cr-Ni-Mo system, Cr-
Ni-W steel and Cr-Ni-Mo-W steel are melted, cast, and forged to form a slab with a thickness of 50 mm, which is then heated to 1200°C and hot rolled. In this hot rolling, the processing rate is reduced to 30°C from the time when the plate thickness reaches 10mm, that is, from the time when the temperature reaches 1000℃ where recrystallization does not proceed.
The plate material was hot-rolled to a thickness of 7 mm as a percentage, and then this plate material was held at a temperature of 1000℃ for 30 minutes, water-cooled, and then cold-worked at a processing rate of 22% for the purpose of improving strength. , from the resulting steel plate, perpendicular to the rolling direction, thickness: 2 mm ×
Cut out a test piece with width: 10mm x length: 75mm,
For this test piece, using the three-point support beam jig shown in Fig. 2, a tensile stress equivalent to 0.2% proof stress was applied to the test piece S, and 10
_H2S and 10 atm _{of CO2}
20% NaCl solution saturated with _CO2 (temperature: 300
A stress corrosion cracking test was carried out by immersing the test piece in 1,000-hour immersion temperature (°C) for 1000 hours, and after the test, the presence or absence of cracking in the test piece was observed. Based on these results,
Conditional expression independently set by the inventors: Cr (%)
It has become clear that there is a relationship between +10Mo (%) +5W (%) and Ni content with respect to stress corrosion cracking resistance, as shown in Figure 1. In FIG. 1, the ◯ mark indicates no cracking, and the x mark indicates cracking. From the results shown in Figure 1, Cr (%)
It is clear that the desired excellent stress corrosion cracking resistance cannot be obtained when the value of +10Mo (%) +5W (%) is less than 110% and the Ni content is less than 30%. In addition, in the alloy of this invention, B, Sn, Pb, and Zn are each contained at 0.1 as unavoidable impurities.
Even if the content is within the range of % or less, the properties of the alloy of the present invention will not be impaired in any way. B. Hot working conditions The reason why the wall thickness reduction rate below the recrystallization temperature during hot working is set at 10% or more is because this wall thickness reduction rate is
This is because if it is less than 10%, it will not be possible to sufficiently form fine recrystallized grains, which are essential for imparting the desired high strength and excellent ductility to the pipe material, in the post-process heat treatment. In addition, during hot working, it is desirable that the heating temperature be 1050 to 1250°C.
This is because if the heating temperature is less than 1050℃, the deformation resistance during hot working becomes too high, making the processing itself difficult, and undissolved intermetallic compounds and carbides remain, deteriorating toughness and corrosion resistance. On the other hand, if the heating temperature exceeds 1250°C, the deformability in hot conditions will be significantly reduced, making hot working difficult. C Heat treatment conditions As mentioned above, this heat treatment is performed to sufficiently form fine recrystallized grains, but the formation of fine recrystallized grains in this case is 260logC (%) + 1300
The lower limit temperature (℃) calculated by 16Mo (%) +
This is done by maintaining the temperature between the upper limit temperature (%) calculated by 10W (%) + 10Cr (%) + 777 for 2 hours or less. The formula for calculating the lower limit temperature: 260logC (%) + 1300 and the formula for calculating the upper limit temperature: 16Mo (%) + 10W (%) + 10Cr (%)
+777 has been determined empirically based on the results of numerous tests, and the formation of the specified fine recrystallization cannot be sufficiently achieved below the above lower limit temperature, while the heat treatment temperature is lower than the above upper limit temperature. If the temperature exceeds 2 hours or the holding time exceeds 2 hours, the crystal grains will become coarse and the effects brought about by hot working will disappear, making it impossible to secure the desired high strength and high toughness. Therefore, the heat treatment conditions were limited as described above. In this case, if undissolved intermetallic compounds and carbides remain, this will cause deterioration of corrosion resistance, but by setting the heat treatment temperature to the above-mentioned lower limit temperature or higher, they can be completely dissolved. D. Cold working conditions In addition, in this invention, as described above, cold working is performed after heat treatment to improve the strength, but if the cold working is less than 10% in wall thickness reduction rate, the desired strength cannot be secured. On the other hand, cold working with a wall thickness reduction rate of more than 60% will result in significant deterioration of ductility and toughness. It is. By applying the above component composition and manufacturing conditions, we manufacture oil country tubular goods that have high strength with a 0.2% proof stress of 85 Kgf/mm ² or more, as well as excellent ductility and toughness, as well as excellent stress corrosion cracking resistance. It is possible to do so. Next, the method for manufacturing oil country tubular goods of the present invention will be specifically explained using examples and comparing with comparative examples. Example Molten metal having the composition shown in Table 1 was heated in a normal electric furnace and for the purpose of desulfurization and N addition.
Diameter: 500 mm after melting using an Ar-oxygen decarburization furnace (AOD furnace) and, if necessary, an electroslag melting furnace (ESR furnace) for the purpose of dephosphorization.
It is cast into a φ ingot, and then hot forged at a temperature of 1200℃ to create a diameter of 150mm.
A billet of φ is formed, and in this case, for the purpose of evaluating hot workability, it is observed whether or not cracks occur in the billet.
Hot extrusion processing is performed under the hot processing conditions shown in the table to form a raw tube with an outer diameter of 60 mmφ and a wall thickness of 4 mm.
Subsequently, the alloy tube materials 1 to 27 of the present invention were obtained by heat treatment and cold working under the heat treatment conditions (cooling after treatment was all water cooling) and wall thickness reduction rate shown in Table 1, respectively. , Comparative alloy tube material 1~
9 and conventional alloy tube materials 1 to 4 were manufactured, respectively. In addition, Comparative Alloy Tube Materials 1 to 9 have the content of any one of the constituent components or any of the manufacturing conditions (indicated with an asterisk in Table 1) of the present invention. The tube material 1 was manufactured under conditions outside the range, and all conventional alloy tube materials have known compositions.

【table】

【table】

【table】

[Table] JIS/SUS316, same 2 is JIS/SUS310S, same 3
The composition is equivalent to Incoloy 800, and the composition corresponding to Incoloy 4 is JIS/SUS329J1. Next, the resulting alloy tube materials 1 to 1 of the present invention
27, comparative alloy pipe materials 1 to 9, and conventional alloy pipe material 1
From ~4, cut out a test piece with a length of 20 mm,
Cut off a section corresponding to 60° along the length of this test piece, pass a bolt through this test piece as shown in the front view in Figure 3, tighten it with a nut, and attach it to the outside surface of the tube. A tensile stress equivalent to 0.2% proof stress is applied to the specimen S in this state, and H ₂ S
A stress corrosion cracking test was conducted by immersion in H ₂ S - 10 atm CO ₂ - 20% NaCl solution (liquid temperature: 300°C) at partial pressures of 0.1 atm, 1 atm, and 20 atm, respectively, for 1000 hours. The presence or absence of stress corrosion cracking was investigated. The results are shown in Table 2 together with the presence or absence of cracking during hot forging, the tensile test results, and the impact test results. In Table 2, the ○ marks indicate those with no cracks, while the x marks indicate those with cracks. From the results shown in Table 2, comparative alloy tube materials 1 to
No. 9 is inferior in at least one of hot workability, stress corrosion cracking resistance, and strength, whereas alloy tube materials 1 to 27 of the present invention are
Both have excellent hot workability and stress corrosion cracking resistance, and also have high strength and good hot workability, but have relatively low strength and poor stress corrosion cracking resistance. It is clear that this material has even better characteristics than conventional alloy tube materials 1 to 4, which are inferior. As mentioned above, oil country tubular goods manufactured by the method of the present invention have particularly high strength and excellent stress corrosion cracking resistance, so they can be used in petroleum and natural products in harsh environments where these properties are required. It exhibits extremely excellent performance not only in gas extraction, but also when used as geothermal well pipes.

[Brief explanation of drawings]

Figure 1 shows the stress corrosion cracking resistance of alloys.
Figures 2 and 3 are diagrams showing the relationship between the combined content and Cr (%) + 10Mo (%) + 5W (%), and Figures 2 and 3 are diagrams showing the stress corrosion cracking test for plate-shaped and tubular specimens, respectively. be.

Claims (1)

[Claims] 1 C: 0.05% or less, Si: 1.0% or less, Mn: 2.0%
Below, P: 0.030% or less, S: 0.005% or less, sol.
Contains Al: 0.5% or less, Ni: 30 to 60%, Cr: 15 to 30%, one or two of Mo: 12% or less and W: 24% or less, and the rest is Fe. It has a composition (weight% or more) consisting of unavoidable impurities, and Cr (%) + 10Mo (%) + 5W (%) ≧110%, 8%≦Mo (%) + 1/2W (%)≦12%, An alloy that satisfies the conditions is hot-worked under the condition that the wall thickness reduction rate below the recrystallization temperature is 10% or more, and then the lower limit temperature (℃) calculated by 260logC (%) + 1300 and 16Mo (% )+10W(%)+10Cr(%)+777
Stress corrosion cracking resistance characterized by heat treatment at a temperature between the upper limit temperature (°C) calculated for 2 hours or less, and then cold working at a wall thickness reduction rate of 10 to 60%. A manufacturing method for high-strength oil country tubular goods with excellent properties. 2 C: 0.05% or less, Si: 1.0% or less, Mn: 2.0%
Below, P: 0.030% or less, S: 0.005% or less, sol.
Contains Al: 0.5% or less, Ni: 30 to 60%, Cr: 15 to 30%, one or two of Mo: 12% or less and W: 24% or less, and further Cu: 2 %
One or two of the following and Co: 2% or less
It has a composition (more than % by weight) containing seeds and the rest is Fe and unavoidable impurities, and Cr (%) + 10Mo (%) + 5W (%) ≧110%, 8%≦Mo (%) + 1/ 2W (%) ≦ 12%, an alloy that satisfies the conditions is hot worked under the condition that the wall thickness reduction rate below the recrystallization temperature is 10% or more, and then the lower limit calculated by 260logC (%) + 1300 Temperature (℃) and 16Mo (%) + 10W (%) + 10Cr (%) + 777
Stress corrosion cracking resistance characterized by heat treatment at a temperature between the upper limit temperature (°C) calculated for 2 hours or less, and then cold working at a wall thickness reduction rate of 10 to 60%. A manufacturing method for high-strength oil country tubular goods with excellent properties. 3 C: 0.05% or less, Si: 1.0% or less, Mn: 2.0%
Below, P: 0.030% or less, S: 0.005% or less, sol.
Contains Al: 0.5% or less, Ni: 30 to 60%, Cr: 15 to 30%, one or two of Mo: 12% or less and W: 24% or less, and further rare earth elements: A composition containing one or more of the following: 0.10% or less, Y: 0.20% or less, Mg: 0.10% or less, Ti: 0.5% or less, and Ca: 0.10% or less, with the remainder consisting of Fe and inevitable impurities. (more than weight%) and satisfies the following conditions: Cr (%) + 10Mo (%) + 5W (%) ≧110%, 8%≦Mo (%) + 1/2W (%)≦12% is hot-worked under conditions where the wall thickness reduction rate below the recrystallization temperature is 10% or more, and then the lower limit temperature (℃) calculated by 260logC (%) + 1300 and 16Mo (%) + 10W (%) +10Cr(%)+777
Stress corrosion cracking resistance characterized by heat treatment at a temperature between the upper limit temperature (°C) calculated for 2 hours or less, and then cold working at a wall thickness reduction rate of 10 to 60%. A manufacturing method for high-strength oil country tubular goods with excellent properties. 4 C: 0.05% or less, Si: 1.0% or less, Mn: 2.0%
Below, P: 0.030% or less, S: 0.005% or less, sol.
Contains Al: 0.5% or less, Ni: 30 to 60%, Cr: 15 to 30%, one or two of Mo: 12% or less and W: 24% or less, and further Cu: 2 %
One or two of the following and Co: 2% or less
Species, rare earth elements: 0.10% or less, Y: 0.20% or less, Mg: 0.10% or less, Ti: 0.5% or less, and
Contains one or more of Ca: 0.10% or less, with the remainder consisting of Fe and unavoidable impurities (weight%), and Cr (%) + 10Mo (%) + 5W (%) )≧110%, 8%≦Mo(%)+1/2W(%)≦12%, An alloy that satisfies the following conditions is hot-heated under the condition that the wall thickness reduction rate below the recrystallization temperature is 10% or more. After processing, the lower limit temperature (℃) calculated by 260logC (%) + 1300 and 16Mo (%) + 10W (%) + 10Cr (%) + 777
Stress corrosion cracking resistance characterized by heat treatment at a temperature between the upper limit temperature (°C) calculated for 2 hours or less, and then cold working at a wall thickness reduction rate of 10 to 60%. A manufacturing method for high-strength oil country tubular goods with excellent properties. 5 C: 0.05% or less, Si: 1.0% or less, Mn: 2.0%
Below, P: 0.030% or less, S: 0.005% or less, sol.
Al: 0.5% or less, N: 0.05-0.3%, Ni: 30-60
%, Cr: 15 to 30%, Mo: 12% or less, W: 24% or less, and the remainder is Fe and unavoidable impurities (weight%). Cr (%) + 10Mo (%) + 5W (%) ≧ 110%, 8% ≦ Mo (%) + 1/2W (%) ≦ 12%, and below the recrystallization temperature. Hot working is performed under the condition that the wall thickness reduction rate is 10% or more, and then the lower limit temperature (℃) calculated from 260logC (%) + 1300 and 16Mo (%) + 10W (%) + 10Cr (%) + 777
Stress corrosion cracking resistance characterized by heat treatment at a temperature between the upper limit temperature (°C) calculated for 2 hours or less, and then cold working at a wall thickness reduction rate of 10 to 60%. A manufacturing method for high-strength oil country tubular goods with excellent properties. 6 C: 0.05% or less, Si: 1.0% or less, Mn: 2.0%
Below, P: 0.030% or less, S: 0.005% or less, sol.
Al: 0.5% or less, N: 0.05-0.3%, Ni: 30-60
%, Cr: 15 to 30%, Mo: 12% or less and W: 24% or less, and Cu: 2% or less and Co: 2% or less. Contains one or two types, with the remainder consisting of Fe and unavoidable impurities (weight %),
And, an alloy that satisfies the following conditions: Cr (%) + 10Mo (%) + 5W (%) ≧110%, 8%≦Mo (%) + 1/2W (%)≦12%, is processed at a temperature below the recrystallization temperature. Hot working is performed under the condition that the thickness reduction rate is 10% or more, and then the lower limit temperature (℃) calculated from 260logC (%) + 1300 and 16Mo (%) + 10W (%) + 10Cr (%) + 777
Stress corrosion cracking resistance characterized by heat treatment at a temperature between the upper limit temperature (°C) calculated for 2 hours or less, and then cold working at a wall thickness reduction rate of 10 to 60%. A manufacturing method for high-strength oil country tubular goods with excellent properties. 7 C: 0.05% or less, Si: 1.0% or less, Mn: 2.0%
Below, P: 0.030% or less, S: 0.005% or less, sol.
Al: 0.5% or less, N: 0.05-0.3%, Ni: 30-60
%, Cr: 15 to 30%, Mo: 12% or less and W: 24% or less, further containing rare earth elements: 0.10% or less, Y: 0.20%
Below, Mg: 0.10% or less, Ti: 0.5% or less, and
Contains one or more of Ca: 0.10% or less, with the remainder consisting of Fe and unavoidable impurities (weight%), and Cr (%) + 10Mo (%) + 5W (%) ≧110%, 8%≦Mo(%)+1/2W(%)≦12%, Alloys that satisfy the following conditions are hot worked under conditions where the wall thickness reduction rate below the recrystallization temperature is 10% or more. Then, the lower limit temperature (℃) calculated by 260logC (%) + 1300 and 16Mo (%) + 10W (%) + 10Cr (%) + 777
Stress corrosion cracking resistance characterized by heat treatment at a temperature between the upper limit temperature (°C) calculated for 2 hours or less, and then cold working at a wall thickness reduction rate of 10 to 60%. A manufacturing method for high-strength oil country tubular goods with excellent properties. 8 C: 0.05% or less, Si: 1.0% or less, Mn: 2.0%
Below, P: 0.030% or less, S: 0.005% or less, sol.
Al: 0.5% or less, N: 0.05-0.3%, Ni: 30-60
%, Cr: 15 to 30%, Mo: 12% or less and W: 24% or less, and Cu: 2% or less and Co: 2% or less. 1 or 2 types, rare earth elements: 0.10% or less, Y: 0.20% or less, Mg: 0.10% or less, Ti: 0.5
% or less, and one or more of Ca: 0.10% or less, with the remainder consisting of Fe and unavoidable impurities (wt%), and Cr (%) + 10Mo (%) ) + 5W (%) ≧ 110%, 8% ≦ Mo (%) + 1/2W (%) ≦ 12%, the alloy that satisfies the following conditions has a wall thickness reduction rate of 10% or more below the recrystallization temperature. After hot working under the following conditions, the lower limit temperature (℃) calculated from 260logC (%) + 1300 and 16Mo (%) + 10W (%) + 10Cr (%) + 777
Stress corrosion cracking resistance characterized by heat treatment at a temperature between the upper limit temperature (°C) calculated for 2 hours or less, and then cold working at a wall thickness reduction rate of 10 to 60%. A manufacturing method for high-strength oil country tubular goods with excellent properties.