EP4578565A1 - Steel tube exhibiting excellent fatigue characteristics against hydrogen and production method therefor, and steel material and production method therefor - Google Patents

Steel tube exhibiting excellent fatigue characteristics against hydrogen and production method therefor, and steel material and production method therefor Download PDF

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Publication number
EP4578565A1
EP4578565A1 EP23872574.1A EP23872574A EP4578565A1 EP 4578565 A1 EP4578565 A1 EP 4578565A1 EP 23872574 A EP23872574 A EP 23872574A EP 4578565 A1 EP4578565 A1 EP 4578565A1
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European Patent Office
Prior art keywords
less
steel
temperature
steel pipe
hydrogen
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EP23872574.1A
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German (de)
French (fr)
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EP4578565A4 (en
Inventor
Naho INOUE
Hiroshi Okano
Yoshihiro Nishihara
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JFE Steel Corp
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JFE Steel Corp
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Publication of EP4578565A1 publication Critical patent/EP4578565A1/en
Publication of EP4578565A4 publication Critical patent/EP4578565A4/en
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/60Ferrous alloys, e.g. steel alloys containing lead, selenium, tellurium, or antimony, or more than 0.04% by weight of sulfur
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21BROLLING OF METAL
    • B21B17/00Tube-rolling by rollers of which the axes are arranged essentially perpendicular to the axis of the work, e.g. "axial" tube-rolling
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D11/00Continuous casting of metals, i.e. casting in indefinite lengths
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    • C21D1/00General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
    • C21D1/18Hardening; Quenching with or without subsequent tempering
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    • C21D1/00General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
    • C21D1/18Hardening; Quenching with or without subsequent tempering
    • C21D1/19Hardening; Quenching with or without subsequent tempering by interrupted quenching
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    • C21D1/00General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
    • C21D1/18Hardening; Quenching with or without subsequent tempering
    • C21D1/25Hardening, combined with annealing between 300 degrees Celsius and 600 degrees Celsius, i.e. heat refining ("Vergüten")
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    • C21D1/00General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
    • C21D1/26Methods of annealing
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    • C21D8/00Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment
    • C21D8/02Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/0221Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
    • C21D8/0226Hot rolling
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    • C21D8/00Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment
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    • C21D8/0247Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
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    • C21D8/00Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment
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    • C21D9/00Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
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    • C21D9/085Cooling or quenching
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    • C21D2211/00Microstructure comprising significant phases
    • C21D2211/001Austenite
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    • C21D2211/00Microstructure comprising significant phases
    • C21D2211/008Martensite

Definitions

  • the present invention relates to a steel pipe with a good fatigue property in hydrogen, a method for producing the steel pipe, a steel material, and a method for producing the steel material.
  • An austenitic stainless steel such as SUS 316L, which is more resistant to hydrogen embrittlement than low-alloy steels, has been used for a steel structure used in a high-pressure hydrogen gas environment.
  • an austenitic stainless steel such as SUS 316L
  • SUS 316L is high in steel material cost and has low strength, and when designed to withstand a high hydrogen pressure, has a large wall thickness and results in an increased price of a structure for hydrogen itself.
  • a steel for a high-pressure hydrogen environment described in Patent Literature 1 is a steel used in a high-pressure hydrogen environment, in which Ca/S is less than 1.5 or 11 or more to reduce the diffusible hydrogen concentration ratio and suppress embrittlement due to diffusible hydrogen.
  • a low-alloy high-strength steel described in Patent Literature 3 is a Cr-Mo high-strength low-alloy steel with good elongation and reduction in area characteristics even in a 45-MPa hydrogen atmosphere and with excellent high-pressure hydrogen environment embrittlement resistance provided by tempering at a relatively high temperature of 560°C to 580°C to adjust the grain size number after tempering to 8.4 or more and the tensile strength in a very narrow range of 900 to 950 MPa.
  • Patent Literature 4 proposes a low-alloy steel for a high-pressure hydrogen gas environment.
  • adding V increasing the Mo content as compared with existing steels, increasing the tempering temperature, and utilizing a V-Mo carbide improve the carbide form at a grain boundary and greatly improve hydrogen environment embrittlement resistance.
  • NPL 1 Matsunaga et al., Int J Hydrogen Energy, Vol. 40 (2015), pp. 5739-5748
  • Non Patent Literature 1 it is known that the fatigue life of a material decreases in a high-pressure hydrogen environment. This means that the service life of a line pipe material decreases when the line pipe material is designed based on a conventional natural gas line pipe.
  • the related art described above can suppress the occurrence of hydrogen-induced cracking in a sour environment but cannot sufficiently increase fatigue strength in hydrogen gas, that is, there is a problem in that it is difficult to achieve both the suppression of the occurrence of hydrogen-induced cracking in a sour environment and high fatigue strength in hydrogen gas, which more easily affects the service life
  • a steel pipe with a good fatigue property in hydrogen in a high-pressure hydrogen gas environment which is suitable for a steel structure used in a high-pressure hydrogen gas environment, such as a line pipe for 100% hydrogen gas or a natural gas containing hydrogen at a hydrogen partial pressure of 1 MPa or more (natural gas is a gas containing hydrocarbons, such as methane and ethane, as main components), a method for producing the steel pipe, a steel material, and a method for producing the steel material.
  • the present invention has been further studied based on such new findings, and the gist of the present invention is as follows:
  • the present invention can provide a steel pipe and a steel material with a very good fatigue property in a high-pressure hydrogen gas environment and is industrially very useful.
  • An implementation method for a steel pipe is more specifically described as a first embodiment, and then an implementation method for a steel material is more specifically described as a second embodiment.
  • the C content is an element necessary to increase strength. The effect is insufficient at less than 0.10%.
  • the C content is 0.10% or more.
  • the C content is preferably 0.13% or more.
  • the C content is more preferably 0.15% or more, still more preferably 0.18% or more.
  • more than 0.45% may result in a quenching crack at the time of quenching, causes the formation of a coarse carbide, and results in a degradation of the fatigue property in hydrogen.
  • the C content is 0.45% or less.
  • the C content is preferably 0.43% or less.
  • the C content is more preferably 0.40% or less, still more preferably 0.38% or less.
  • Si is contained as a deoxidizer in steelmaking and as an element for ensuring hardenability, but the effects are insufficient at less than 0.01%, so that the Si content is 0.01% or more.
  • the Si content is preferably 0.1% or more.
  • the Si content is more preferably 0.15% or more.
  • more than 2.0% results in an embrittled grain boundary, a decrease in the low-temperature toughness, and a degradation of the fatigue property in hydrogen.
  • the Si content is 2.0% or less.
  • the Si content is preferably 1.5% or less.
  • the Si content is preferably 1.0% or less, more preferably 0.8% or less.
  • B is an element for ensuring hardenability
  • the B content when B is contained, the B content may be 0% or more, but the above effect is difficult to ensure at less than 0.0005%, so that the B content is preferably 0.0005% or more.
  • more than 0.005% results in lower toughness.
  • the B content when B is contained, the B content is 0.005% or less.
  • the B content is preferably 0.004% or less.
  • the B content is more preferably 0.003% or less, still more preferably 0.002% or less.
  • Austenite remaining in a steel pipe may increase the amount of hydrogen in the steel and increase hydrogen embrittlement sensitivity. Furthermore, when austenite is transformed into martensite by stress loading during use, hydrogen cracking is likely to occur because martensite is very hard, and cracking may occur from the martensite portion.
  • retained austenite is 3% or less to reduce the fatigue crack growth rate. Retained austenite is preferably 2% or less, more preferably 1% or less. The retained austenite may be 0%.
  • an electric-resistance-welded pipe or a UOE steel pipe can be produced by performing the treatment so as to have the same thermal history.
  • a steel pipe according to the present invention can be produced by sequentially performing the following steps (1) to (3).
  • the temperature in the following description is the temperature at the center of the plate thickness of a steel raw material or a steel pipe.
  • the average cooling rate means the temperature at a quarter thickness position from the inner surface of a steel pipe.
  • the temperature at the center of the plate thickness and the temperature at the quarter thickness position from the inner surface of a steel pipe are estimated from the surface temperature of the steel pipe measured with a radiation thermometer using heat-transfer calculation or the like in consideration of the heat transfer coefficient of the steel material.
  • the average cooling rate from 550°C to 50°C is preferably 12°C/s or less, more preferably 10°C/s or less. Although the lower limit is not particularly limited, the average cooling rate from 550°C to 50°C is preferably 1°C/s or more.
  • the cooling method is not particularly limited, and an arbitrary method, such as water cooling, oil cooling, or air cooling, can be used alone or in combination, but water cooling or oil cooling is preferred from 800°C to 550°C, and air cooling is preferred from 550°C to 50°C.
  • Group B cooling to 50°C or less at an average cooling rate of 10°C/s or more from 800°C to 300°C and at an average cooling rate of 5°C/s or less from 300°C to 50°C at the quarter thickness position from the inner surface of a steel pipe.
  • an average cooling rate of less than 10°C/s from 800°C to 300°C at the quarter thickness position from the inner surface of a steel pipe the predetermined carbide density cannot be achieved, and the fatigue property deteriorates.
  • the cooling stop temperature is more than 50°C, a desired carbide density cannot be achieved, the transformation is not completed, and a desired steel microstructure cannot be formed after tempering. Thus, quenching is performed to a temperature of 50°C or less.
  • the cooling stop temperature is preferably 45°C or less, more preferably 40°C or less. Although the lower limit is not particularly limited, the cooling stop temperature is preferably 25°C or more.
  • Tempering temperature 400°C or more and Ac 1 temperature or lower
  • Heating at an average heating rate of 0.01°C/s or more and a tempering temperature of 400°C or more can result in a decrease in austenite, a decrease in hydrogen in the steel, and a predetermined carbide density.
  • the tempering temperature is preferably 450°C or more, more preferably 500°C or more.
  • heating to a temperature higher than the Ac 1 temperature may result in an increase in austenite and hydrogen in the steel.
  • the tempering temperature is the Ac 1 temperature or lower, preferably (Ac 1 temperature - 30) °C or lower.
  • the upper limit of the average heating rate during tempering is preferably, but not limited to, 1°C/s or less.
  • tempering time is less than 60 minutes.
  • the tempering time is preferably 50 minutes or less.
  • An excessively short tempering time results in no decrease in austenite and the amount of hydrogen in a steel material, so that the tempering time is preferably 10 minutes or more, more preferably 20 minutes or more.
  • Each element symbol in the formula represents the element content (% by mass) of the steel and is 0 for an element not contained.
  • dehydrogenation treatment for removing hydrogen from steel materials
  • the holding time R (s) is preferably determined from the plate thickness or the wall thickness t (mm) of a steel material or a steel pipe and the hydrogen diffusion coefficient D (rmn 2 ⁇ s -1 ) in the steel at room temperature using the following formula (A).
  • the hydrogen diffusion coefficient varies depending on a component contained and the metallic microstructure and a value within a range from, for example, 1 x 10 -5 to 5 x 10 -3 mm 2 /s, more preferably 5 x 10 -4 mm 2 /s or less may be adopted.
  • the dehydrogenation treatment step is performed before pipe production or welding for connecting steel pipes.
  • the dehydrogenation treatment is preferably performed at a high temperature because the hydrogen diffusion coefficient D at a high temperature is small and hydrogen is released quickly.
  • the calculation may be performed using a diffusion coefficient D' (diffusion coefficient at corresponding temperature) at the holding temperature for the value of D in the formula (A).
  • the dehydrogenation treatment temperature is preferably 550°C or less.
  • the dehydrogenation treatment temperature T is more preferably 500°C or less.
  • the dehydrogenation treatment temperature T is still more preferably 400°C or less, most preferably 300°C or less.
  • the dehydrogenation treatment temperature T is preferably room temperature or higher for the reason that the dehydrogenation treatment at a temperature lower than room temperature increases the treatment time and cost.
  • the dehydrogenation treatment temperature T is more preferably 50°C or more.
  • the dehydrogenation treatment temperature T is still more preferably 100°C or more, most preferably 150°C or more.
  • the dehydrogenation treatment temperature T herein is the temperature of the atmosphere in the dehydrogenation treatment step.
  • the room temperature refers to 20°C ⁇ 10°C.
  • heating if conducted, takes time for the temperature Tc at the center of the plate thickness of a steel material or a steel pipe to reach the temperature of the atmosphere in the dehydrogenation treatment step (dehydrogenation treatment temperature T), so even if the holding time R (s) is satisfied at the ambient temperature, the dehydrogenation treatment may be insufficient if the dehydrogenation treatment temperature T (ambient temperature) has not been reached at the center of the plate thickness.
  • At least the former can appropriately control the amount of hydrogen in the steel material in the surface layer portion of the steel material or the steel pipe, and when the latter is also performed, the amount of hydrogen in the steel material from the surface layer portion to the center of the plate thickness of the steel material or the steel pipe can be appropriately controlled.
  • the temperature Tc at the center of the plate thickness may be actually measured with a thermocouple or the like or may be predicted using a finite element method or the like.
  • the scale on the steel surface inhibits dehydrogenation and is therefore preferably removed before dehydrogenation treatment.
  • the scale removal method may be, for example, but is not limited to, physical cleaning by high-pressure cleaning or a chemical method using a scale remover.
  • the thickness of scale to be removed is not particularly limited, the scale removal effect can be obtained when the scale is removed by approximately 100 ⁇ m.
  • a steel material according to the present invention is more specifically described below.
  • the chemical composition, metallic microstructure, and crack growth rate of the steel material are the same as those described for the steel pipe, and the steps other than the rolling step and the cooling step (the casting step, the heating step, the reheating and quenching step, the tempering step, and the dehydrogenation treatment step) in the production method are performed in the same manner as described for the steel pipe.
  • the rolling step and the cooling step are performed as described below.
  • a steel raw material heated in the heating step as described in the method for producing a steel pipe is hot-rolled using a hot-rolling mill under the following conditions.
  • Finish rolling temperature 820°C or more
  • a finish rolling temperature of less than 820°C results in excessively large rolling force and a higher risk of occurrence of rolling trouble.
  • the finish rolling temperature is 820°C or more.
  • the finish rolling temperature is preferably 850°C or more, more preferably 900°C or more.
  • the upper limit of the finish rolling temperature is not particularly limited, an excessively high temperature tends to result in a nonuniform metallic microstructure, so that the finish rolling temperature is preferably 1200°C or less.
  • the finish rolling temperature is more preferably 1150°C or less, still more preferably 1100°C or less.
  • a steel material with the chemical composition described above is hot-rolled, then heated, and held at a temperature of the Ac 3 temperature or higher and 1000°C or less, and is cooled under the cooling conditions of the following Group A or Group B.
  • the temperature is preferably held for 10 minutes or more, more preferably 15 minutes or more, still more preferably 20 minutes or more.
  • the upper limit is not particularly limited, the temperature is preferably held for 60 minutes or less, more preferably 45 minutes or less.
  • Heating temperature after hot rolling Ac 3 temperature or higher and 1000°C or less
  • a heating temperature lower than the Ac 3 temperature in the cooling step results in ferrite remaining in the steel after cooling, a decrease in the strength of a steel material, and a degradation of the fatigue property.
  • the heating temperature is the Ac 3 temperature or higher.
  • the heating temperature is preferably the Ac 3 temperature + 30°C or more, more preferably the Ac 3 temperature + 50°C or more.
  • the Ac 3 temperature + 30°C or more or the Ac 3 temperature + 50°C or more is not applied to a composition system in which the Ac 3 temperature + 30°C or the Ac 3 temperature + 50°C exceeds 1000°C.
  • a heating temperature of more than 1000°C may result in coarse austenite grains and a decrease in the impact absorbed energy and toughness of the material after heat treatment.
  • Steel materials with a good fatigue property in hydrogen gas have the above chemical composition and include various types, such as a sheet, a plate, and a steel pipe, with high fatigue crack growth resistance in hydrogen gas, or may be steel materials for a hydrogen pipeline formed into a predetermined shape.
  • the steel pipes were heated and held at 950°C for steel pipes with a Ac 3 temperature of 950°C or less or at 1000°C for steel pipes with a Ac 3 temperature of more than 950°C, were then water-cooled under the conditions shown in Table 2-3, and were then tempered under the conditions shown in Table 2-3.
  • the metallic microstructure and mechanical properties were evaluated. The evaluation method is described below.
  • the tempering temperature was arbitrarily adjusted so that the materials had a tensile strength in the range of 520 MPa to 700 MPa.
  • the ambient temperature that is, the dehydrogenation treatment temperature T, was kept at 50°C for 3 hours, followed by natural cooling.
  • test specimen taken from a steel material with plate thickness of 10 mm or less was ground from the surface by 0.5 mm resulting in test specimen thickness of 2 mm, 5 mm, 8 mm, or 9 mm, respectively, and for a test specimen taken from a steel material with plate thickness other than these, a test specimen with a thickness of 10 mm was taken from a position of t/2 (t: sheet thickness), and the front and back sides of a crack growth portion were mirror-polished.
  • Tables 2-1, 2-2, and 2-3 show the results.
  • a carbide measurement method for a steel material is described below.
  • a test specimen was cut out from a cross section parallel to the thickness direction from the center position of the plate thickness of a steel material and was subjected to nital etching, and a carbide was observed by SEM.
  • Ten fields were randomly selected and observed at an acceleration voltage of 15 kV and a magnification of 20000 times.
  • Tables 2-1, 2-2, and 2-3 show the average value of the 10 fields as the number of carbides, with Y indicating that the number of carbides with a diameter of 200 nm or more is 20 pieces/10 ⁇ m 2 or less, and N indicating that the number of carbides with a diameter of 200 nm or more is more than 20 pieces/10 ⁇ m 2 .
  • a method for measuring the amount of austenite in a steel material is described below.
  • a sample for metallic microstructure observation was taken from the center of the sheet width in the center in the longitudinal direction of each of the steel materials and the steel pipes thus produced, a cross section parallel to the longitudinal direction was buffed as an observation surface, the surface layer was then removed by chemical polishing using picric acid etching, and X-ray diffractometry was performed. More specifically, a Co-K ⁇ radiation source was used for an incident X-ray, and the area fraction of retained austenite was calculated from the intensity ratios of the (200), (211), and (220) planes of ferrite to the (200), (220), and (311) planes of austenite.
  • the amount of hydrogen remaining in the steel was measured by thermal desorption analysis method using a low-temperature programmed hydrogen analyzer ⁇ gas chromatograph type> (JTF-20AL).
  • the thermal desorption analysis was performed in the temperature range of room temperature to 400°C at a heating rate of 200°C/h, and the sum total thereof was taken as the amount of hydrogen.
  • the specimen has a cylindrical shape with 30 mm in length and 7 ⁇ in diameter in the longitudinal direction of the steel pipe at the quarter thickness position of the steel plate and at the quarter thickness position from the inner surface of the steel pipe.
  • the amount of hydrogen is the amount of H shown in Tables 1-1 and 1-2, and the amount before being subjected to a high-pressure hydrogen fatigue test explained in aging described later.
  • the examples of the present invention all satisfied the condition that the fatigue crack growth rate in hydrogen gas was 1.0 x 10 -6 m/cycle or less.
  • Table 2-1 Steel material No. Steel pipe No.
  • Example 2 All satisfied the condition that the crack growth rate da/dN in hydrogen gas was 1.0 x 10 -6 m/cycle or less. Among them, the crack propagation characteristics were better when the reheating and quenching steps were performed under more suitable conditions.
  • Table 3 Billet No. Steel pipe No.
  • Example 14 14, 43, and 97 in Example 1 was performed at a dehydrogenation treatment temperature T (ambient temperature) of 50°C for a holding time of 3 hours, in the present example, the dehydrogenation treatment of the steel pipes Nos. 14D, 43D, and 97D was performed at a dehydrogenation treatment temperature T (ambient temperature) of 50°C so that the holding time tc after the temperature Tc at the center of the plate thickness reached 50°C satisfied the formula (A).
  • T ambient temperature
  • the dehydrogenation treatment temperature T (ambient temperature) was 50°C, and the holding time tc satisfied the formula (A) at a dehydrogenation treatment temperature T of 50°C, but the holding time tc after the temperature Tc at the center of the plate thickness reached 50°C did not satisfy the formula (A).
  • the dehydrogenation treatment temperature T (ambient temperature) was 50°C, but neither the holding time t at the ambient temperature nor the holding time tc after the temperature Tc at the center of the plate thickness reached 50°C did not satisfied the formula (A).
  • Dehydrogenation holding time t is Y
  • Dehydrogenation holding time t is 50°C and the holding time t satisfies the formula (A)
  • “Dehydrogenation holding time t is N” means that the dehydrogenation treatment temperature T (ambient temperature) is 50°C, but the holding time t does not satisfy the formula (A).
  • Holding time tc at center temperature of steel plate thickness Tc is Y
  • the holding time tc after the temperature Tc at the center of the plate thickness reaches 50°C satisfies the formula (A)
  • “Holding time tc at steel material center temperature Tc is N” means that the temperature Tc at the center of the plate thickness reaches 50°C, but the holding time tc after Tc reaches 50°C does not satisfy the formula (A).
  • the examples of the present invention all satisfied the condition that the crack growth rate da/dN in hydrogen gas was 1.0 x 10 -6 m/cycle or less. Among them, a steel pipe subjected to the dehydrogenation treatment under more suitable conditions had better crack propagation characteristics. [Table 4] Billet No. Steel pipe No.

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Abstract

To provide a steel pipe with a good fatigue property in hydrogen in a high-pressure hydrogen gas environment, which is suitable for a steel structure used in a high-pressure hydrogen gas environment, such as a line pipe for 100% hydrogen gas or a natural gas containing hydrogen at a hydrogen partial pressure of 1 MPa or more (natural gas is a gas containing hydrocarbons, such as methane and ethane, as main components), a method for producing the steel pipe, a steel material, and a method for producing the steel material.The steel pipe with a good fatigue property in hydrogen has a specific chemical composition and a specific microstructure and has a crack growth rate da/dN of 1.0 x 10<sup>-6</sup> m·cycle<sup>-1</sup> or less at a stress intensity factor range of 20 MPa √m in hydrogen of 1 MPa or more.

Description

    Technical Field
  • The present invention relates to a steel pipe with a good fatigue property in hydrogen, a method for producing the steel pipe, a steel material, and a method for producing the steel material.
  • Background Art
  • There is a line pipe for transporting natural gas as an existing energy infrastructure. Such a steel material has been required to suppress the occurrence of hydrogen-induced cracking in a sour environment. On the other hand, in recent years, hydrogen has attracted a great deal of attention worldwide as a clean energy source for the construction of a decarbonizing society. Thus, for the purpose of transporting a large amount of hydrogen gas, construction of a hydrogen gas transportation network that pressure-feeds natural gas partially mixed with hydrogen or hydrogen gas as an alternative through a natural gas line pipe has been studied. The transport pressure in such a pipeline operation is assumed to be a high pressure of 1 to 40 MPa, and line pipes are placed in a high-pressure hydrogen gas exposure environment. A steel material used in such an environment has a concern about the occurrence of "hydrogen embrittlement" in which hydrogen enters the steel and degrades its characteristics. Thus, it is necessary to have not only high toughness and sour resistance required for conventional line pipes but also hydrogen embrittlement resistance required in a hydrogen gas environment.
  • An austenitic stainless steel, such as SUS 316L, which is more resistant to hydrogen embrittlement than low-alloy steels, has been used for a steel structure used in a high-pressure hydrogen gas environment. However, an austenitic stainless steel, such as SUS 316L, is high in steel material cost and has low strength, and when designed to withstand a high hydrogen pressure, has a large wall thickness and results in an increased price of a structure for hydrogen itself. Thus, there has been a strong demand for a low-alloy steel material that can withstand a high-pressure hydrogen gas environment at a lower cost for a steel structure for hydrogen.
  • In response to such a demand, for example, a steel for a high-pressure hydrogen environment described in Patent Literature 1 is a steel used in a high-pressure hydrogen environment, in which Ca/S is less than 1.5 or 11 or more to reduce the diffusible hydrogen concentration ratio and suppress embrittlement due to diffusible hydrogen.
  • Patent Literature 2 discloses that a low-alloy high-strength steel adjusted to have a specific chemical composition is used in the tensile strength range of 900 to 950 MPa in the atmosphere to increase the reduction in area and elongation as compared with JIS G 3128 SHY685NS in a 45-MPa hydrogen atmosphere and improve high-pressure hydrogen environment embrittlement resistance characteristics.
  • A low-alloy high-strength steel described in Patent Literature 3 is a Cr-Mo high-strength low-alloy steel with good elongation and reduction in area characteristics even in a 45-MPa hydrogen atmosphere and with excellent high-pressure hydrogen environment embrittlement resistance provided by tempering at a relatively high temperature of 560°C to 580°C to adjust the grain size number after tempering to 8.4 or more and the tensile strength in a very narrow range of 900 to 950 MPa.
  • Patent Literature 4 proposes a low-alloy steel for a high-pressure hydrogen gas environment. In the low-alloy steel described in Patent Literature 4, adding V, increasing the Mo content as compared with existing steels, increasing the tempering temperature, and utilizing a V-Mo carbide improve the carbide form at a grain boundary and greatly improve hydrogen environment embrittlement resistance.
  • Patent Literature 5 proposes a steel for a high-pressure hydrogen gas storage container with high hydrogen resistance. According to the technique described in Patent Literature 5, stress relief annealing for an extended period after normalizing treatment in the production of a steel plate finely and densely disperses and precipitates an MC carbide (Mo, V)C and improves the hydrogen resistance, such as hydrogen embrittlement resistance, of the steel.
  • Patent Literature 6 proposes a steel material for high-pressure hydrogen storage. Patent Literature 6 proposes a steel material with a metallic microstructure composed of 90% or more by area of a bainite-based microstructure in which cementite with an average grain size of 50 nm or less and an average aspect ratio of 3 or less is dispersedly precipitated in the bainite.
  • Citation List Patent Literature
    • PTL 1: Japanese Unexamined Patent Application Publication No. 2005-2386
    • PTL 2: Japanese Unexamined Patent Application Publication No. 2009-46737
    • PTL 3: Japanese Unexamined Patent Application Publication No. 2009-275249
    • PTL 4: Japanese Unexamined Patent Application Publication No. 2009-74122
    • PTL 5: Japanese Unexamined Patent Application Publication No. 2010-37655
    • PTL 6: Japanese Unexamined Patent Application Publication No. 2012-107332
    Non Patent Literature
  • NPL 1: Matsunaga et al., Int J Hydrogen Energy, Vol. 40 (2015), pp. 5739-5748
  • Summary of Invention Technical Problem
  • With respect to the pressure in a line pipe, due to fluctuations during operation or periodical shutdown, stress is repeatedly applied to a structure like the line pipe. Thus, when designing a steel structure, such as a line pipe, it is essential to consider fatigue fracture. However, as described in Non Patent Literature 1, it is known that the fatigue life of a material decreases in a high-pressure hydrogen environment. This means that the service life of a line pipe material decreases when the line pipe material is designed based on a conventional natural gas line pipe. The related art described above can suppress the occurrence of hydrogen-induced cracking in a sour environment but cannot sufficiently increase fatigue strength in hydrogen gas, that is, there is a problem in that it is difficult to achieve both the suppression of the occurrence of hydrogen-induced cracking in a sour environment and high fatigue strength in hydrogen gas, which more easily affects the service life
  • In view of the problems of the related art, it is an object of the present invention to provide a steel pipe with a good fatigue property in hydrogen in a high-pressure hydrogen gas environment, which is suitable for a steel structure used in a high-pressure hydrogen gas environment, such as a line pipe for 100% hydrogen gas or a natural gas containing hydrogen at a hydrogen partial pressure of 1 MPa or more (natural gas is a gas containing hydrocarbons, such as methane and ethane, as main components), a method for producing the steel pipe, a steel material, and a method for producing the steel material.
  • The phrase "a good fatigue property in hydrogen in a high-pressure hydrogen environment", as used herein, means that the crack growth rate da/dN at a stress intensity factor range of 20 MPa √m is 1.0 x 10-6 m·cycle-1 or less, as determined by a fatigue test in accordance with ASTM E647 at a frequency of 1 Hz, a repetitive waveform of a sine wave, a control method of load control, and a stress ratio of R = 0.1, in both environments of hydrogen gas at room temperature (20°C ± 10°C) and at a pressure of 1 MPa or more and a natural gas (the main components are hydrocarbons, such as methane and ethane) mixed atmosphere containing hydrogen at a hydrogen partial pressure of 1 MPa or more. The natural gas containing hydrogen at a hydrogen partial pressure of 1 MPa or more, for example, has a hydrogen concentration of 30% or less by volume and a pressure of 30 MPa or less as the entire gas.
  • When the crack growth rate da/dN in a hydrogen environment is 1.0 x 10-6 m·cycle-1 or less, it is possible to design a structural steel for hydrogen in a plate thickness range that is possible in the production process. Solution to Problem
  • From the above perspective, the present inventors have conducted extensive studies on the conditions to be satisfied by various steel materials in hydrogen gas and have found a novel steel pipe and a novel steel material with a good fatigue property in hydrogen.
  • The present invention has been further studied based on such new findings, and the gist of the present invention is as follows:
    1. [1] A steel pipe with a good fatigue property in hydrogen, the steel pipe having a chemical composition comprising:
      • on a mass percent basis,
      • C: 0.10% to 0.45%,
      • Si: 0.01% to 2.0%,
      • Mn: 0.3% to 2.0%,
      • Al: 0.01% to 0.15%,
      • N: 0.0005% to 0.008%,
      • P: 0.015% or less,
      • S: 0.0015% or less,
      • O: 0.01% or less,
      • H: 0.0010% or less,
      • Cu: 0% to 2.5%,
      • Ni: 0% to 2.5%,
      • Cr: 0% to 2.5%,
      • Mo: 0% to 2.0%,
      • Nb: 0% to 0.5%,
      • V: 0% to 0.5%,
      • Ti: 0% to 0.5%,
      • W: 0% to 2.5%,
      • B: 0% to 0.005%,
      • Sn: 0% to 0.3%,
      • Sb: 0% to 0.3%,
      • Ca: 0% to 0.01%,
      • Mg: 0% to 0.01%, and
      • REM: 0% to 0.005%,
      • the remainder being Fe and incidental impurities,
      • wherein retained austenite constitutes 3% or less,
      • the number of carbides with a diameter of 200 nm or more is 20 pieces/10 µm2 or less, and
      • a crack growth rate da/dN at a stress intensity factor range of 20 MPa √m in hydrogen of 1 MPa or more is 1.0 x 10-6 m·cycle-1 or less.
    2. [2] A method for producing a steel pipe, the method comprising:
      • a casting step of casting a steel raw material with the chemical composition according to [1] at a casting speed of 1.8 m/min or less;
      • a heating step of heating at 1350°C or less;
      • a hot rolling step of rolling the steel raw material heated in the heating step at a finish rolling temperature of 820°C or more to form a steel pipe shape;
      • a cooling step of holding a steel pipe obtained in the hot rolling step at a temperature of an Ac3 temperature or higher and 1000°C or less, and a cooling condition is the following Group A or Group B; and
      • a tempering step of tempering the steel pipe obtained in the cooling step at 400°C or more and an Ac1 temperature or lower for less than 60 minutes,
      • Group A:
        cooling the steel pipe to 50°C or less at an average cooling rate of 15°C/s or more from 800°C to 550°C at a quarter thickness position from an inner surface of the steel pipe and at an average cooling rate of 15°C/s or less from 550°C to 50°C at the quarter thickness position from the inner surface of the steel pipe, and
      • Group B:
        cooling the steel pipe to 50°C or less at an average cooling rate of 10°C/s or more from 800°C to 300°C at the quarter thickness position from the inner surface of the steel pipe and at an average cooling rate of 5°C/s or less from 300°C to 50°C at the quarter thickness position from the inner surface of the steel pipe.
    3. [3] The method for producing a steel pipe according to [2], comprising, before the tempering step, a quenching step of reheating to an Ac3 temperature or higher and 1000°C or less, and a cooling condition is the following Group A or Group B,
      • Group A:
        cooling the steel pipe to 50°C or less at an average cooling rate of 15°C/s or more from 800°C to 550°C at a quarter thickness position from an inner surface of the steel pipe and at an average cooling rate of 15°C/s or less from 550°C to 50°C at the quarter thickness position from the inner surface of the steel pipe, and
      • Group B:
        cooling the steel pipe to 50°C or less at an average cooling rate of 10°C/s or more from 800°C to 300°C at the quarter thickness position from the inner surface of the steel pipe and at an average cooling rate of 5°C/s or less from 300°C to 50°C at the quarter thickness position from the inner surface of the steel pipe.
    4. [4] The method for producing a steel pipe according to [2] or [3], wherein the casting speed is 1.0 m/min or less.
    5. [5] A steel material with a good fatigue property in hydrogen, the steel material having a chemical composition comprising:
      • on a mass percent basis,
      • C: 0.10% to 0.45%,
      • Si: 0.01% to 2.0%,
      • Mn: 0.3% to 2.0%,
      • Al: 0.01% to 0.15%,
      • N: 0.0005% to 0.008%,
      • P: 0.015% or less,
      • S: 0.0015% or less,
      • O: 0.01% or less,
      • H: 0.0010% or less,
      • Cu: 0% to 2.5%,
      • Ni: 0% to 2.5%,
      • Cr: 0% to 2.5%,
      • Mo: 0% to 2.0%,
      • Nb: 0% to 0.5%,
      • V: 0% to 0.50,
      • Ti: 0% to 0.5%,
      • W: 0% to 2.5%,
      • B: 0% to 0.005%,
      • Sn: 0% to 0.3%,
      • Sb: 0% to 0.3%,
      • Ca: 0% to 0.01%,
      • Mg: 0% to 0.01%, and
      • REM: 0% to 0.005%,
      • the remainder being Fe and incidental impurities,
      • wherein retained austenite constitutes 3% or less,
      • the number of carbides with a diameter of 200 nm or more is 20 pieces/10 µm2 or less, and
      • a crack growth rate da/dN at a stress intensity factor range of 20 MPa √m in hydrogen of 1 MPa or more is 1.0 x 10-6 m·cycle-1 or less.
    6. [6] A method for producing a steel material, the method comprising:
      • a casting step of casting a steel raw material with the chemical composition according to [5] at a casting speed of 1.8 m/min or less;
      • a heating step of heating at 1350°C or less;
      • a hot rolling step of rolling the steel raw material heated in the heating step at a finish rolling temperature of 820°C or more;
      • a cooling step of holding a steel material obtained in the hot rolling step at a temperature of an Ac3 temperature or higher and 1000°C or less, and a cooling condition is the following Group A or Group B; and
      • a tempering step of tempering the steel material obtained in the cooling step at 400°C or more and an Ac1 temperature or lower for less than 60 minutes,
      • Group A:
        cooling the steel material to 50°C or less at an average cooling rate of 15°C/s or more from 800°C to 550°C at a quarter thickness position from a surface of the steel material and at an average cooling rate of 15°C/s or less from 550°C to 50°C at the quarter thickness position from the surface of the steel material, and
      • Group B:
        cooling the steel material to 50°C or less at an average cooling rate of 10°C/s or more from 800°C to 300°C at the quarter thickness position from the surface of the steel material and at an average cooling rate of 5°C/s or less from 300°C to 50°C at the quarter thickness position from the surface of the steel material.
    7. [7] The method for producing a steel material according to [6], comprising, before the tempering step, a quenching step of reheating to an Ac3 temperature or higher and 1000°C or less, and a cooling condition is the following Group A or Group B,
      • Group A:
        cooling the steel material to 50°C or less at an average cooling rate of 15°C/s or more from 800°C to 550°C at a quarter thickness position from a surface of the steel material and at an average cooling rate of 15°C/s or less from 550°C to 50°C at the quarter thickness position from the surface of the steel material, and
      • Group B:
        cooling the steel material to 50°C or less at an average cooling rate of 10°C/s or more from 800°C to 300°C at the quarter thickness position from the surface of the steel material and at an average cooling rate of 5°C/s or less from 300°C to 50°C at the quarter thickness position from the surface of the steel material.
    8. [8] The method for producing a steel material according to [6] or [7], wherein the casting speed is 1.0 m/min or less. Advantageous Effects of Invention
  • The present invention can provide a steel pipe and a steel material with a very good fatigue property in a high-pressure hydrogen gas environment and is industrially very useful.
  • Description of Embodiments
  • Next, a method for implementing the present invention is more specifically described.
  • An implementation method for a steel pipe is more specifically described as a first embodiment, and then an implementation method for a steel material is more specifically described as a second embodiment.
  • First Embodiment [Chemical Composition]
  • The reasons for limiting the chemical composition of a steel pipe (including a steel material) according to the present invention are described below. Unless otherwise specified, "%" in the following description refers to "% by mass".
  • C: 0.10% to 0.45%
  • C is an element necessary to increase strength. The effect is insufficient at less than 0.10%. Thus, the C content is 0.10% or more. The C content is preferably 0.13% or more. The C content is more preferably 0.15% or more, still more preferably 0.18% or more. On the other hand, more than 0.45% may result in a quenching crack at the time of quenching, causes the formation of a coarse carbide, and results in a degradation of the fatigue property in hydrogen. Thus, the C content is 0.45% or less. The C content is preferably 0.43% or less. The C content is more preferably 0.40% or less, still more preferably 0.38% or less.
  • Si: 0.01% to 2.0%
  • Si is contained as a deoxidizer in steelmaking and as an element for ensuring hardenability, but the effects are insufficient at less than 0.01%, so that the Si content is 0.01% or more. The Si content is preferably 0.1% or more. The Si content is more preferably 0.15% or more. On the other hand, more than 2.0% results in an embrittled grain boundary, a decrease in the low-temperature toughness, and a degradation of the fatigue property in hydrogen. Thus, the Si content is 2.0% or less. The Si content is preferably 1.5% or less. The Si content is preferably 1.0% or less, more preferably 0.8% or less.
  • Mn: 0.3% to 2.0%
  • Mn is contained as an element for ensuring hardenability, but the effect is insufficient at less than 0.3%, so that the Mn content is 0.3% or more. The Mn content is preferably 0.4% or more. The Mn content is more preferably 0.5% or more. The Mn content is still more preferably 0.6% or more. On the other hand, more than 2.0% results in a decrease in grain boundary strength and low-temperature toughness. Furthermore, a high Mn content may result in an increase in austenite stability, an amount of retained austenite exceeding a specified amount, and an increase in the amount of hydrogen in the steel. Furthermore, the hardness of a surface layer portion or a center segregation zone increases during cooling (accelerated cooling or quenching) after hot rolling, and the fatigue property in hydrogen deteriorates. Thus, the Mn content is 2.0% or less. The Mn content is preferably 1.5% or less, more preferably 1.3% or less. The Mn content is most preferably 1.0% or less.
  • Al: 0.01% to 0.15%
  • Al is contained as a deoxidizer and at the same time has an effect of pinning an austenite grain as a fine precipitate of an Al nitride during heating and suppressing coarsening of grains, but the effects are insufficient at less than 0.01%. Thus, the Al content is 0.01% or more. The Al content is preferably 0.02% or more. The Al content is more preferably 0.03% or more. On the other hand, a content of more than 0.15% results in a steel with lower cleanliness and toughness and a degradation of the fatigue property in hydrogen. Thus, the Al content is 0.15% or less. The Al content is preferably 0.13% or less. The Al content is more preferably 0.10% or less, still more preferably 0.08% or less.
  • N: 0.0005% to 0.008%
  • N is contained because N forms a fine precipitate by forming a nitride with Nb, Ti, Al, or the like and has an effect of pinning an austenite grain during heating, thereby suppressing coarsening of the grain and improving low-temperature toughness. The effect of refining the microstructure is insufficient at a content of less than 0.0005%, so that the N content is 0.0005% or more. The N content is preferably 0.001% or more. The N content is more preferably 0.0025% or more. On the other hand, a content of more than 0.008% results in an increase in the amount of solute N, a base material and a weld heat-affected zone with lower toughness, and a degradation of the fatigue property in hydrogen. Thus, the N content is 0.008% or less. The N content is preferably 0.007% or less. The N content is more preferably 0.006% or less, still more preferably 0.005% or less.
  • P: 0.015% or less
  • An impurity element P is likely to segregate at a grain boundary, and more than 0.015% results in lower bonding strength between adjacent crystal grains, a decrease in the low-temperature toughness, and a degradation of the fatigue property in hydrogen. Thus, the P content is 0.015% or less. The P content is preferably 0.013% or less, more preferably 0.010% or less. The lower limit is preferably, but not limited to, 0.001% or more due to an increase in cost.
  • S: 0.0015% or less
  • An impurity element S is likely to segregate at a grain boundary and form a non-metallic inclusion MnS. More than 0.0015% results in lower bonding strength between adjacent crystal grains, an increase in the amount of inclusion, a decrease in the low-temperature toughness, and a degradation of the fatigue property in hydrogen. Thus, the S content is 0.0015% or less. The S content is preferably 0.0013% or less. The S content is more preferably 0.0010% or less, still more preferably 0.0008% or less. The lower limit is preferably, but not limited to, 0.0001% or more due to an increase in cost.
  • O: 0.01% or less
  • O forms an oxide with Al or the like and affects the workability of the material, and a lower O content is better. A content of more than 0.01% results in an increase in the amount of inclusion and lower workability. Further, as the amount of inclusion increases, the fatigue property in hydrogen deteriorates. Thus, the O content is 0.01% or less. The O content is preferably 0.009% or less. The O content is more preferably 0.008% or less. The lower limit is preferably, but not limited to, 0.0001% or more due to an increase in cost. The O content is more preferably 0.002% or more.
  • H: 0.0010% or less
  • H may be introduced into a steel material in various steps during production, and a large amount of H introduced increases the risk of cracking after solidification and accelerates fatigue crack growth. A large amount of H introduced also increases the crack growth rate, and it is therefore important to decrease the amount of hydrogen in the steel material. The effects do not cause a problem at 0.0010% or less, and the H content is therefore 0.0010% or less, preferably 0.0005% or less, more preferably 0.0002% or less. On the other hand, less than 0.00001% causes an increase in cost, so that 0.00001% or more is preferred. The H content is preferably 0.0001% or more. The amount of hydrogen is the amount of residual hydrogen after forming of a steel material, a steel pipe, UOE, or the like.
  • In the present invention, the remainder of the chemical composition is preferably a steel composition composed of Fe and incidental impurities but, depending on the desired characteristics, it is preferable to further appropriately contain one or two or more of Cu: 0% to 2.5%, Ni: 0% to 2.5%, Cr: 0% to 2.5%, Mo: 0% to 2.0%, Nb: 0% to 0.5%, V: 0% to 0.5%, Ti: 0% to 0.5%, W: 0% to 2.5%, B: 0% to 0.005%, Sn: 0% to 0.3%, Sb: 0% to 0.3%, Ca: 0% to 0.01%, Mg: 0% to 0.01%, and REM: 0% to 0.005% individually or simultaneously.
  • Cu: 0% to 2.5%
  • Cu has an effect of improving the hardenability. Thus, when Cu is contained, the Cu content may be 0% or more, but the above effect is difficult to ensure at less than 0.05%, so that the Cu content is preferably 0.05% or more. On the other hand, more than 2.5% is likely to cause hot cracking during heating of a steel billet. Thus, when Cu is contained, the Cu content is 2.5% or less. The Cu content is preferably 2.3% or less. The Cu content is more preferably 2.0% or less, still more preferably 1.8% or less.
  • Ni: 0% to 2.5%
  • Ni has an effect of improving the hardenability similarly to Cu and further has an effect of improving the toughness. Thus, when Ni is contained, the Ni content may be 0% or more, but the above effect is difficult to ensure at less than 0.05%, so that the Ni content is preferably 0.05% or more. On the other hand, more than 2.5% results in low economic efficiency. Thus, when Ni is contained, the Ni content is 2.5% or less. The Ni content is preferably 2.3% or less, more preferably 2.0% or less, preferably 1.8% or less.
  • Cr: 0% to 2.5%
  • Cr is contained as an element for ensuring hardenability, and when Cr is contained, the Cr content may be 0% or more, but the above effect is difficult to ensure at less than 0.1%, so that the Cr content is preferably 0.1% or more. On the other hand, a content of more than 2.5% results in lower toughness and low economic efficiency. Thus, when Cr is contained, the Cr content is 2.5% or less. The Cr content is preferably 2.3% or less. The Cr content is more preferably 2.0% or less, still more preferably 1.8% or less, most preferably 1.5% or less.
  • Mo: 0% to 2.0%
  • Mo has an effect of improving the hardenability, and when Mo is contained, the Mo content may be 0% or more, but the above effect is difficult to ensure at less than 0.05%, so that the Mo content is preferably 0.05% or more. On the other hand, a content of more than 2.0% results in low economic efficiency. Thus, when Mo is contained, the Mo content is 2.0% or less. The Mo content is preferably 1.8% or less. The Mo content is more preferably 1.5% or less, still more preferably 1.2% or less.
  • Nb: 0% to 0.5%
  • Nb has an effect of improving the hardenability, pins an austenite grain as a fine precipitate of a Nb-based carbide/nitride/carbonitride during heating, and suppresses coarsening of the grain. Thus, when Nb is contained, the Nb content may be 0% or more, but the above effect is difficult to ensure at less than 0.005%, so that the Nb content is preferably 0.005% or more. The Nb content is more preferably 0.01% or more. On the other hand, a content of more than 0.5% may result in precipitation of a coarse Nb carbonitride and lower toughness. Thus, when Nb is contained, the Nb content is 0.5% or less. The Nb content is preferably 0.4% or less. The Nb content is preferably 0.3% or less, and the Nb content is preferably 0.2% or less.
  • V: 0% to 0.5%
  • V has an effect of improving the hardenability, pins an austenite grain as a fine precipitate of a V carbide during heating, and suppresses coarsening of the grain. Thus, when V is contained, the V content may be 0% or more, but the above effect is difficult to ensure at less than 0.005%, so that the V content is preferably 0.005% or more. On the other hand, a content of more than 0.5% may result in precipitation of a coarse V carbonitride and lower toughness. Thus, when V is contained, the V content is 0.5% or less. The V content is preferably 0.4% or less. The V content is more preferably 0.3% or less, still more preferably 0.2% or less.
  • Ti: 0% to 0.5%
  • Ti has an effect of improving the hardenability and has an effect of pinning an austenite grain as a fine precipitate of a Ti-based carbide/nitride/carbonitride during heating and suppressing the growth of the grain. Thus, when Ti is contained, the Ti content may be 0% or more, but the above effect is difficult to ensure at less than 0.005%, so that the Ti content is preferably 0.005% or more. The Ti content is preferably 0.01% or more. On the other hand, a content of more than 0.5% tends to result in the formation of a coarse angular nitride and results in lower toughness. Thus, when Ti is contained, the Ti content is 0.5% or less. The Ti content is preferably 0.4% or less. The Ti content is more preferably 0.3% or less, still more preferably 0.2% or less.
  • W: 0% to 2.5%
  • W has an effect of improving the hardenability, and when W is contained, the W content may be 0% or more, but the above effect is difficult to ensure at less than 0.05%, so that the W content is preferably 0.05% or more. On the other hand, more than 2.5% results in low economic efficiency. Thus, when W is contained, the W content is 2.5% or less. The W content is preferably 2.3% or less. The W content is more preferably 2.0% or less, still more preferably 1.8% or less.
  • B: 0% to 0.005%
  • B is an element for ensuring hardenability, and when B is contained, the B content may be 0% or more, but the above effect is difficult to ensure at less than 0.0005%, so that the B content is preferably 0.0005% or more. On the other hand, more than 0.005% results in lower toughness. Thus, when B is contained, the B content is 0.005% or less. The B content is preferably 0.004% or less. The B content is more preferably 0.003% or less, still more preferably 0.002% or less.
  • Sn: 0% to 0.3%
  • Sn has an effect of increasing the corrosion resistance of a steel pipe. Thus, when Sn is contained, the Sn content may be 0% or more, but the above effect is difficult to ensure at less than 0.005%, so that the Sn content is preferably 0.005% or more. The Sn content is more preferably 0.01% or more. On the other hand, a content of more than 0.3% results in a decrease in high-temperature ductility and an increase in the possibility of cracking during casting. Thus, when Sn is contained, the Sn content is 0.3% or less. The Sn content is preferably 0.25% or less. The Sn content is more preferably 0.2% or less, still more preferably 0.15% or less.
  • Sb: 0% to 0.3%
  • Sb has an effect of increasing the corrosion resistance of a steel pipe. Thus, when Sb is contained, the Sb content may be 0% or more, but the above effect is difficult to ensure at less than 0.005%, so that the Sb content is preferably 0.005% or more. The Sb content is more preferably 0.01% or more. On the other hand, a content of more than 0.3% results in a decrease in high-temperature ductility and a decrease in hot rollability. Thus, when Sb is contained, the Sb content is 0.3% or less. The Sb content is preferably 0.25% or less. The Sb content is more preferably 0.2% or less, still more preferably 0.15% or less.
  • Ca: 0% to 0.01%
  • Ca forms CaS and has an effect of controlling the form of a sulfide inclusion to CaS, which is a spherical inclusion less likely to be ductile by rolling, instead of MnS, which is an inclusion likely to be ductile by rolling. Thus, when Ca is contained, the Ca content may be 0% or more, but the above effect is difficult to ensure at less than 0.0005%, so that the Ca content is preferably 0.0005% or more. The Ca content is more preferably 0.001% or more. On the other hand, a content of more than 0.01% results in lower cleanliness and a degradation of the material property, such as toughness. Thus, when Ca is contained, the Ca content is 0.01% or less. The Ca content is preferably 0.005% or less. The Ca content is more preferably 0.003% or less, still more preferably 0.002% or less.
  • Mg: 0% to 0.01%
  • Mg may be used as a pig iron desulfurization material. Thus, when Mg is contained, the Mg content may be 0% or more, but the above effect is difficult to ensure at less than 0.0005%, so that the Mg content is preferably 0.0005% or more. The Mg content is more preferably 0.001% or more. On the other hand, a content of more than 0.01% results in lower cleanliness. Thus, when Mg is contained, the Mg content is 0.01% or less. The Mg content is preferably 0.005% or less. The Mg content is more preferably 0.004% or less, still more preferably 0.003% or less.
  • REM: 0% to 0.005%
  • REM forms a sulfide as REM(O, S) in steel, thereby reducing the amount of solute S at a grain boundary and improving SR cracking resistance characteristics. Thus, when REM is contained, the REM content may be 0% or more, but the above effect is difficult to ensure at less than 0.0005%, so that the REM content is preferably 0.0005% or more. On the other hand, a content of more than 0.005% results in significant accumulation of a REM sulfide in a sedimental zone and a deterioration of the material property. Thus, when REM is contained, the REM content is 0.005% or less. The REM content is preferably 0.003% or less. The REM content is more preferably 0.001% or less. REM is an abbreviation of Rare Earth Metal and refers to a rare-earth metal.
  • In the chemical composition of a steel plate and a steel pipe, the remainder other than the above components (elements) is composed of Fe and an incidental impurity element.
  • A preferred metallic microstructure of a steel pipe according to the present invention is more specifically described.
  • Retained austenite: 3% or less
  • Austenite remaining in a steel pipe may increase the amount of hydrogen in the steel and increase hydrogen embrittlement sensitivity. Furthermore, when austenite is transformed into martensite by stress loading during use, hydrogen cracking is likely to occur because martensite is very hard, and cracking may occur from the martensite portion. In the present invention, retained austenite is 3% or less to reduce the fatigue crack growth rate. Retained austenite is preferably 2% or less, more preferably 1% or less. The retained austenite may be 0%.
  • Number of carbide with diameter of 200 nm or more: 20 pieces/10 µm2 or less
  • In a steel pipe according to the present invention, a number of coarsened carbides equal to or greater than a predetermined number adversely affect the fatigue property in hydrogen. Thus, the number of carbides with a diameter of 200 nm or more is 20 pieces/10 µm2 or less, preferably 15 pieces/10 µm2 or less, more preferably 10 pieces/10 µm2 or less, still more preferably 5 pieces/10 µm2 or less. The lower limit is preferably as small as possible and may be 0 pieces/10 µm2. The diameter refers to a value calculated from 2√(A/2 x B/2) using a long side A and a short side B passing through the center. Carbides refer to, for example, intermetallic compounds including cementite, ε-carbide, χ-carbide, Fe7C3, and the like.
  • Furthermore, carbides with a diameter of less than 200 nm uniformly dispersed in a grain at intervals of 100 nm or more contribute to an improvement in strength without adversely affecting the fatigue property in hydrogen, so that carbides with a diameter of less than 200 nm dispersed in a grain are preferably 10 pieces/10 µm2 or more. As for the upper limit, the number of carbides with a diameter of less than 200 nm dispersed in a grain is preferably 100 pieces/10 µm2 or less for the reason that coarsening proceeds when the number of precipitates is too large. The precipitation of carbides is affected by the conditions of a cooling step and a tempering step after hot rolling described later, and it is therefore important to control these conditions.
  • Crack growth rate da/dN at stress intensity factor of 20 MPa √m in hydrogen with pressure of 1 MPa or more: 1.0 x 10-6 m·cycle-1 or less
  • The fatigue crack growth rate is an important parameter in the design of a steel pipe used for a line pipe or a gas container and is necessary to obtain a service life in which the safety of a destructive structural member is ensured. In a destructive structural member, it is difficult to eliminate cracks and crack initiation sites, and a crack occurs inevitably and propagates under repeated stress. The crack growth rate is low when the stress applied to a crack tip is small, and increases as the stress to the crack tip increases. In a hydrogen environment, hydrogen enters a steel pipe and makes a crack more likely to propagate. The degree of acceleration of the crack growth rate by hydrogen is greatly affected by the microstructure and precipitates of the material. In a crack growth test in hydrogen at 1 MPa or more, when the crack growth rate da/dN at a stress intensity factor range of 20 MPa √m is 1.0 x 10-6 m·cycle-1 or less determined in a fatigue test in accordance with ASTM E647 at a frequency of 1 Hz, a repetitive waveform of a sine wave, a control method of load control, and a stress ratio of R = 0.1, the service life of a steel structure in a high-pressure hydrogen environment can also be sufficiently ensured. Thus, in a crack growth test in hydrogen at 1 MPa or more, the crack growth rate da/dN at a stress intensity factor of 20 MPa √m is 1.0 x 10-6 m·cycle-1 or less. The crack growth rate da/dN at a stress intensity factor of 20 MPa √m is preferably 0.9 x 10-6 m·cycle-1 or less, more preferably 0.8 x 10-6 m·cycle-1 or less, still more preferably 0.7 x 10-6 m·cycle-1 or less. The closer the lower limit is to the result in the atmosphere, the better it is considered, and the crack growth rate da/dN at a stress intensity factor of 20 MPa √m is preferably 0.05 x 10-6 m·cycle-1 or more.
  • The plate thickness of a steel pipe is preferably, but not limited to, 5 mm or more. The plate thickness is preferably 30 mm or less.
  • A steel pipe according to the present invention may be a seamless steel pipe, an electric-resistance-welded pipe, a UOE steel pipe, or the like, and a method for producing a seamless steel pipe is more specifically described as an example.
  • A steel pipe with a good fatigue property in hydrogen gas according to the present invention has the chemical composition described above and satisfies the crack growth rate in hydrogen, and a method for producing the steel pipe is more specifically described below.
  • It is needless to say that an electric-resistance-welded pipe or a UOE steel pipe can be produced by performing the treatment so as to have the same thermal history.
  • A steel pipe according to the present invention can be produced by sequentially performing the following steps (1) to (3).
    1. (1) A step of casting a steel raw material after component adjustment
    2. (2) A hot rolling and cooling (accelerated cooling) step of heating and rolling a cast material to form a steel pipe shape (including a case of conducting reheating and quenching before a tempering step)
    3. (3) A step of tempering a steel pipe produced in the above step
  • Each of the steps is described below. Unless otherwise specified, the temperature in the following description is the temperature at the center of the plate thickness of a steel raw material or a steel pipe. The average cooling rate means the temperature at a quarter thickness position from the inner surface of a steel pipe. The temperature at the center of the plate thickness and the temperature at the quarter thickness position from the inner surface of a steel pipe are estimated from the surface temperature of the steel pipe measured with a radiation thermometer using heat-transfer calculation or the like in consideration of the heat transfer coefficient of the steel material.
  • [Casting Step] Casting speed: 1.8 m/min or less
  • A lower casting speed results in a decrease in the hydrogen concentration and inclusions in the steel, and the effects are remarkable at 1.8 m/min or less, so that the casting speed is 1.8 m/min or less, preferably 1.5 m/min or less, more preferably 1.0 /min or less, still more preferably 0.5 m/min or less, most preferably 0.1 m/min or less. Although the lower limit is not particularly limited, the casting speed may be more than 0 m/min.
  • Heating Step
  • To perform hot rolling, a steel raw material with the chemical composition described above is heated. The steel raw material can be, for example, but is not limited to, a slab, a billet, or the like produced by an ordinary continuous casting method.
  • Heating temperature: 1350°C or less
  • A heating temperature of more than 1350°C in the heating step results in prior austenite grains with an excessively large average grain size and a degradation of various characteristics, so that the heating temperature is 1350°C or less. The heating temperature is preferably 1300°C or less, more preferably 1250°C or less, most preferably 1200°C or less. On the other hand, the heating temperature is preferably lowered to reduce the amount of hydrogen in the steel, but an excessively low heating temperature results in a decrease in the finish rolling temperature and makes rolling difficult. Thus, the heating temperature is preferably 950°C or more. The heating temperature is more preferably 1000°C or more. Although the heating time is not particularly specified, an excessively long heating time increases the risk of increasing the amount of hydrogen introduced into a steel pipe, so that 180 minutes or less is preferred. The heating time is more preferably 150 minutes or less, still more preferably 120 minutes or less. Although the lower limit is not particularly limited, the heating time is preferably 30 minutes or more, more preferably 60 minutes or more.
  • Rolling Step
  • The steel raw material heated in the heating step is rolled into a steel pipe shape under the following conditions. The rolling can be hot rolling including piercing rolling, such as an ordinary Mannesmann-plug mill process or Mannesmann-mandrel mill process.
  • Finish rolling temperature: 820°C or more
  • A finish rolling temperature of less than 820°C results in excessively large rolling force and a higher risk of occurrence of rolling trouble. Thus, the finish rolling temperature is 820°C or more. The finish rolling temperature is preferably 850°C or more, more preferably 900°C or more. On the other hand, although the upper limit of the finish rolling temperature is not particularly limited, an excessively high temperature tends to result in a nonuniform metallic microstructure, so that the finish rolling temperature is preferably 1200°C or less. The finish rolling temperature is more preferably 1150°C or less, still more preferably 1100°C or less.
  • [Cooling Step (Accelerated Cooling step)]
  • In the cooling step, a steel material with the chemical composition described above is heated and held at a temperature of the Ac3 temperature or higher and 1000°C or less as it is or after being processed into a steel pipe, and is cooled under the cooling conditions of the following Group A or Group B. The temperature is preferably held for 10 minutes or more, more preferably 15 minutes or more, still more preferably 20 minutes or more. Although the upper limit is not particularly limited, the temperature is preferably held for 60 minutes or less, more preferably 45 minutes or less.
  • Heating temperature after processing into steel pipe: Ac3 temperature or higher and 1000°C or less
  • A heating temperature lower than the Ac3 temperature in the cooling step results in ferrite remaining in the steel after cooling, a decrease in the strength of a steel pipe, and a degradation of the fatigue property in hydrogen. Thus, the heating temperature is the Ac3 temperature or higher. The heating temperature is preferably the Ac3 temperature + 30°C or more, more preferably the Ac3 temperature + 50°C or more. However, the Ac3 temperature + 30°C or more or the Ac3 temperature + 50°C or more is not applied to a composition system in which the Ac3 temperature + 30°C or the Ac3 temperature + 50°C exceeds 1000°C. On the other hand, a heating temperature of more than 1000°C may result in coarse austenite grains and a decrease in the impact absorbed energy and toughness of the material after heat treatment. Thus, the heating temperature is 1000°C or less. The heating temperature is preferably 950°C or less, more preferably 900°C or less. However, 950°C or less or 900°C or less described above is not applied to a composition system in which 950°C or 900°C is lower than the Ac3 temperature. In the cooling process, when the temperature after the completion of rolling satisfies the heating conditions, cooling may be performed as it is, or the completion of rolling may be followed by superheating again and cooling. When a steel plate is cooled by air cooling once, the steel plate may be heated again to a temperature of the Ac3 temperature or higher and 1000°C or less and may be cooled under the cooling conditions of the following Group A or Group B. In the present invention, the Ac3 temperature (°C) is calculated using the following formula. Ac3 (°C) = 910 - 203[C]1/2 - 30[Mn] + 44.7[Si] + 700[P] + 100[Al] + 31.5[Mo] - 11[Cr] - 15.2[Ni] - 20[Cu] + 104[V]
  • In the formula, [M] denotes the element M content (% by mass).
  • Average Cooling Rate
  • Group A:
    cooling to 50°C or less at an average cooling rate of 15°C/s or more from 800°C to 550°C and at an average cooling rate of 15°C/s or less from 550°C to 50°C at the quarter thickness position from the inner surface of a steel pipe
  • The predetermined carbide density cannot be achieved at an average cooling rate of less than 15°C/s from 800°C to 550°C at the quarter thickness position from the inner surface of a steel pipe. Furthermore, although the microstructure is not particularly limited, to achieve a predetermined fatigue property in hydrogen, bainite or martensite preferably constitutes 90% or more by area. At an average cooling rate of less than 15°C/s, it is difficult for bainite to constitute 90% or more by area, and the formation of martensite may be affected depending on the chemical composition. Thus, the average cooling rate at the quarter thickness position from the inner surface of a steel pipe is 15°C/s or more. From the perspective of reducing variations in microstructure, the average cooling rate is preferably 17°C/s or more. The average cooling rate from 800°C to 550°C is more preferably 20°C/s or more, most preferably 22°C/s or more. On the other hand, to reduce variations in grain size, the average cooling rate is preferably 50°C/s or less, more preferably 45°C/s or less, still more preferably 40°C/s or less. Furthermore, cooling to 50°C or less at an average cooling rate of 15°C/s or less from 550°C to 50°C can decrease retained austenite and reduce the amount of hydrogen in the steel. Thus, the average cooling rate from 550°C to 50°C is 15°C/s or less. The average cooling rate from 550°C to 50°C is preferably 12°C/s or less, more preferably 10°C/s or less. Although the lower limit is not particularly limited, the average cooling rate from 550°C to 50°C is preferably 1°C/s or more. The cooling method is not particularly limited, and an arbitrary method, such as water cooling, oil cooling, or air cooling, can be used alone or in combination, but water cooling or oil cooling is preferred from 800°C to 550°C, and air cooling is preferred from 550°C to 50°C.
  • Group B:
    cooling to 50°C or less at an average cooling rate of 10°C/s or more from 800°C to 300°C and at an average cooling rate of 5°C/s or less from 300°C to 50°C at the quarter thickness position from the inner surface of a steel pipe
  • At an average cooling rate of less than 10°C/s from 800°C to 300°C at the quarter thickness position from the inner surface of a steel pipe, the predetermined carbide density cannot be achieved, and the fatigue property deteriorates. Furthermore, at an average cooling rate of less than 10°C/s, it is difficult for martensite to constitute 90% or more by area, and the formation of bainite may be affected depending on the chemical composition. Thus, the average cooling rate at the quarter thickness position from the inner surface of a steel pipe is 10°C/s or more. From the perspective of reducing variations in microstructure, the average cooling rate from 800°C to 300°C is preferably 12°C/s or more, more preferably 15°C/s or more, still more preferably 17°C/s or more. Although the upper limit is not particularly limited, the average cooling rate is preferably 60°C/s or less. Furthermore, cooling to 50°C or less at an average cooling rate of 5°C/s or less from 300°C to 50°C can reduce the amount of hydrogen in the steel. Thus, the average cooling rate from 300°C to 50°C is 5°C/s or less. The average cooling rate from 300°C to 50°C is preferably 1°C/s or less. The lower limit is preferably, but not limited to, 0.1°C/s or more. The cooling method is not particularly limited, and an arbitrary method, such as water cooling, oil cooling, or air cooling, can be used alone or in combination, but water cooling or oil cooling is preferred from 800°C to 300°C, and air cooling is preferred from 300°C to 50°C.
  • [Reheating and Quenching Step (Suitable Conditions)] Reheating temperature before quenching: Ac3 temperature or higher and 1000°C or less
  • When the temperature at the center of the plate thickness is lower than the Ac3 temperature, non-transformed austenite partially remains, and a desired steel microstructure cannot be formed after hot rolling, quenching, and tempering described later. Thus, the heating temperature before quenching at the time of reheating is the Ac3 temperature or higher, preferably higher than the Ac3 temperature. To suppress an excessive increase in the initial austenite grain size and improve the production efficiency, the heating temperature before quenching is preferably 1000°C or less, more preferably 980°C or less, still more preferably 960°C or less, most preferably 950°C or less. A reheating temperature before quenching on the low temperature side in the range of the Ac3 temperature or higher can result in a decrease in the initial austenite grain size and a decrease in the crack growth rate in hydrogen.
  • Average cooling rate during quenching: the following Group A or Group B
  • Group A:
    cooling to 50°C or less at an average cooling rate of 15°C/s or more from 800°C to 550°C and at an average cooling rate of 15°C/s or less from 550°C to 50°C at the quarter thickness position from the inner surface of a steel pipe
    The predetermined carbide density cannot be achieved at an average cooling rate of less than 15°C/s from 800°C to 550°C at the quarter thickness position from the inner surface of a steel pipe. At an average cooling rate of less than 15°C/s, it is difficult for bainite to constitute 90% or more by area, and the formation of martensite may be affected depending on the chemical composition. Thus, the average cooling rate at the quarter thickness position from the inner surface of a steel pipe is 15°C/s or more. From the perspective of reducing variations in microstructure, the average cooling rate is preferably 17°C/s or more, more preferably 20°C/s or more, still more preferably 22°C/s or more. On the other hand, to reduce variations in grain size, the average cooling rate is preferably 50°C/s or less, more preferably 47°C/s or less, still more preferably 45°C/s or less. Furthermore, cooling to 50°C or less at an average cooling rate of 15°C/s or less from 550°C to 50°C can decrease retained austenite and reduce the amount of hydrogen in the steel. Thus, the average cooling rate from 550°C to 50°C is 15°C/s or less. The average cooling rate from 550°C to 50°C is preferably 12°C/s or less, more preferably 10°C/s or less. Although the lower limit is not particularly limited, the average cooling rate from 550°C to 50°C is preferably 1°C/s or more. The cooling method is not particularly limited, and an arbitrary method, such as water cooling, oil cooling, or air cooling, can be used alone or in combination, but water cooling or oil cooling is preferred from 800°C to 550°C, and air cooling is preferred from 550°C to 50°C.
  • Group B:
    cooling to 50°C or less at an average cooling rate of 10°C/s or more from 800°C to 300°C and at an average cooling rate of 5°C/s or less from 300°C to 50°C at the quarter thickness position from the inner surface of a steel pipe
    At an average cooling rate of less than 10°C/s from 800°C to 300°C at the quarter thickness position from the inner surface of a steel pipe, the predetermined carbide density cannot be achieved, and the fatigue property deteriorates. Furthermore, at an average cooling rate of less than 10°C/s, it is difficult for martensite to constitute 90% or more by area, and the formation of bainite may be affected depending on the chemical composition. Thus, the average cooling rate at the quarter thickness position from the inner surface of a steel pipe is 10°C/s or more. From the perspective of reducing variations in microstructure, the average cooling rate is preferably 17°C/s or more, more preferably 20°C/s or more, still more preferably 25°C/s or more. On the other hand, although the average cooling rate may have any upper limit, when the average cooling rate is more than 60°C/s, a large amount of hard microstructure is formed on the surface of a steel plate, a steel microstructure with the microstructure intended in the present invention is not formed, and the fatigue property in hydrogen deteriorates, so that the average cooling rate is preferably 60°C/s or less. Furthermore, cooling to 50°C or less at an average cooling rate of 5°C/s or less from 300°C to 50°C can reduce the amount of hydrogen in the steel. Thus, the average cooling rate from 300°C to 50°C is 5°C/s or less. The average cooling rate is preferably 3°C/s or less, more preferably 1°C/s or less. The lower limit is preferably, but not limited to, 0.1°C/s or more. The cooling method is not particularly limited, and an arbitrary method, such as water cooling, oil cooling, or air cooling, can be used alone or in combination, but water cooling or oil cooling is preferred from 800°C to 300°C, and air cooling is preferred from 300°C to 50°C.
  • Cooling stop temperature during quenching: 50°C or less
  • When the cooling stop temperature is more than 50°C, a desired carbide density cannot be achieved, the transformation is not completed, and a desired steel microstructure cannot be formed after tempering. Thus, quenching is performed to a temperature of 50°C or less. The cooling stop temperature is preferably 45°C or less, more preferably 40°C or less. Although the lower limit is not particularly limited, the cooling stop temperature is preferably 25°C or more.
  • Tempering Step Tempering temperature: 400°C or more and Ac1 temperature or lower
  • Heating at an average heating rate of 0.01°C/s or more and a tempering temperature of 400°C or more can result in a decrease in austenite, a decrease in hydrogen in the steel, and a predetermined carbide density. The tempering temperature is preferably 450°C or more, more preferably 500°C or more. On the other hand, heating to a temperature higher than the Ac1 temperature may result in an increase in austenite and hydrogen in the steel. Thus, the tempering temperature is the Ac1 temperature or lower, preferably (Ac1 temperature - 30) °C or lower. The upper limit of the average heating rate during tempering is preferably, but not limited to, 1°C/s or less. An excessively long tempering time results in coarsening of a carbide and adversely affects hydrogen embrittlement, so that the tempering time is less than 60 minutes. The tempering time is preferably 50 minutes or less. An excessively short tempering time results in no decrease in austenite and the amount of hydrogen in a steel material, so that the tempering time is preferably 10 minutes or more, more preferably 20 minutes or more.
  • In the present invention, the Ac1 temperature (°C) may be determined by any method, for example, by Ac1 = 723 - 14Mn + 22Si - 14.4Ni + 23.3Cr. Each element symbol in the formula represents the element content (% by mass) of the steel and is 0 for an element not contained.
  • Dehydrogenation Treatment Step
  • Hydrogen originally present in a steel material increases the acceleration of fatigue crack growth and decreases the fatigue life and the fatigue limit stress in hydrogen. Thus, dehydrogenation treatment (for removing hydrogen from steel materials) may be performed to release hydrogen remaining after production. In the dehydrogenation treatment, holding a product at a high temperature for a certain period before use can reduce the amount of hydrogen in the steel, and a steel plate with high fatigue resistance in a high-pressure hydrogen gas environment can be produced. The holding time R (s) is preferably determined from the plate thickness or the wall thickness t (mm) of a steel material or a steel pipe and the hydrogen diffusion coefficient D (rmn2·s-1) in the steel at room temperature using the following formula (A). R t 2 / D
    Figure imgb0001
  • The hydrogen diffusion coefficient varies depending on a component contained and the metallic microstructure and a value within a range from, for example, 1 x 10-5 to 5 x 10-3 mm2/s, more preferably 5 x 10-4 mm2/s or less may be adopted. The dehydrogenation treatment step is performed before pipe production or welding for connecting steel pipes. The dehydrogenation treatment is preferably performed at a high temperature because the hydrogen diffusion coefficient D at a high temperature is small and hydrogen is released quickly. At a high temperature, the calculation may be performed using a diffusion coefficient D' (diffusion coefficient at corresponding temperature) at the holding temperature for the value of D in the formula (A). On the other hand, an excessively high temperature in the dehydrogenation step results in a significant decrease in the material strength, and the dehydrogenation treatment temperature is preferably 550°C or less. The dehydrogenation treatment temperature T is more preferably 500°C or less. The dehydrogenation treatment temperature T is still more preferably 400°C or less, most preferably 300°C or less. Furthermore, the dehydrogenation treatment temperature T is preferably room temperature or higher for the reason that the dehydrogenation treatment at a temperature lower than room temperature increases the treatment time and cost. The dehydrogenation treatment temperature T is more preferably 50°C or more. The dehydrogenation treatment temperature T is still more preferably 100°C or more, most preferably 150°C or more. The dehydrogenation treatment temperature T herein is the temperature of the atmosphere in the dehydrogenation treatment step. The room temperature refers to 20°C ± 10°C.
  • In particular, heating, if conducted, takes time for the temperature Tc at the center of the plate thickness of a steel material or a steel pipe to reach the temperature of the atmosphere in the dehydrogenation treatment step (dehydrogenation treatment temperature T), so even if the holding time R (s) is satisfied at the ambient temperature, the dehydrogenation treatment may be insufficient if the dehydrogenation treatment temperature T (ambient temperature) has not been reached at the center of the plate thickness. Thus, it is preferable to hold for R (s) or more after the temperature Tc at the center of the plate thickness reaches the target dehydrogenation treatment temperature T. Furthermore, to achieve a predetermined crack growth rate in hydrogen gas, it is necessary to appropriately adjust the amount of hydrogen in a steel material in a surface layer portion and at the center of the plate thickness, and for this purpose, it is preferable to hold the steel material at the dehydrogenation treatment temperature T for R (s) or more defined by the formula (A), and it is further preferable to hold the steel material for the holding time R (s) or more after the temperature Tc at the center of the plate thickness reaches the target dehydrogenation treatment temperature T. In other words, at least the former can appropriately control the amount of hydrogen in the steel material in the surface layer portion of the steel material or the steel pipe, and when the latter is also performed, the amount of hydrogen in the steel material from the surface layer portion to the center of the plate thickness of the steel material or the steel pipe can be appropriately controlled. The temperature Tc at the center of the plate thickness may be actually measured with a thermocouple or the like or may be predicted using a finite element method or the like.
  • Furthermore, the scale on the steel surface inhibits dehydrogenation and is therefore preferably removed before dehydrogenation treatment. The scale removal method may be, for example, but is not limited to, physical cleaning by high-pressure cleaning or a chemical method using a scale remover. Although the thickness of scale to be removed is not particularly limited, the scale removal effect can be obtained when the scale is removed by approximately 100 µm.
  • Second Embodiment
  • A steel material according to the present invention is more specifically described below. The chemical composition, metallic microstructure, and crack growth rate of the steel material are the same as those described for the steel pipe, and the steps other than the rolling step and the cooling step (the casting step, the heating step, the reheating and quenching step, the tempering step, and the dehydrogenation treatment step) in the production method are performed in the same manner as described for the steel pipe. The rolling step and the cooling step are performed as described below.
  • Rolling Step
  • A steel raw material heated in the heating step as described in the method for producing a steel pipe is hot-rolled using a hot-rolling mill under the following conditions.
  • Finish rolling temperature: 820°C or more
  • A finish rolling temperature of less than 820°C results in excessively large rolling force and a higher risk of occurrence of rolling trouble. Thus, the finish rolling temperature is 820°C or more. The finish rolling temperature is preferably 850°C or more, more preferably 900°C or more. On the other hand, although the upper limit of the finish rolling temperature is not particularly limited, an excessively high temperature tends to result in a nonuniform metallic microstructure, so that the finish rolling temperature is preferably 1200°C or less. The finish rolling temperature is more preferably 1150°C or less, still more preferably 1100°C or less.
  • Cooling Step (Accelerated Cooling Step)
  • In the cooling step, a steel material with the chemical composition described above is hot-rolled, then heated, and held at a temperature of the Ac3 temperature or higher and 1000°C or less, and is cooled under the cooling conditions of the following Group A or Group B. The temperature is preferably held for 10 minutes or more, more preferably 15 minutes or more, still more preferably 20 minutes or more. Although the upper limit is not particularly limited, the temperature is preferably held for 60 minutes or less, more preferably 45 minutes or less.
  • Heating temperature after hot rolling: Ac3 temperature or higher and 1000°C or less
  • A heating temperature lower than the Ac3 temperature in the cooling step results in ferrite remaining in the steel after cooling, a decrease in the strength of a steel material, and a degradation of the fatigue property. Thus, the heating temperature is the Ac3 temperature or higher. The heating temperature is preferably the Ac3 temperature + 30°C or more, more preferably the Ac3 temperature + 50°C or more. However, the Ac3 temperature + 30°C or more or the Ac3 temperature + 50°C or more is not applied to a composition system in which the Ac3 temperature + 30°C or the Ac3 temperature + 50°C exceeds 1000°C. On the other hand, a heating temperature of more than 1000°C may result in coarse austenite grains and a decrease in the impact absorbed energy and toughness of the material after heat treatment. Thus, the heating temperature is 1000°C or less, more preferably 950°C or less, still more preferably 900°C or less. However, 950°C or less or 900°C or less described above is not applied to a composition system in which 950°C or 900°C is lower than the Ac3 temperature. In the cooling process, when the temperature after the completion of rolling satisfies the heating conditions, cooling may be performed as it is, or the completion of rolling may be followed by superheating again and cooling. When a steel material is cooled by air cooling once, the steel sheet may be heated again to a temperature of the Ac3 temperature or higher and 1000°C or less and may be cooled under the cooling conditions of the following Group A or Group B (in this case, referred to as quenching). In the present invention, the Ac3 temperature (°C) is calculated using the following formula. Ac3 (°C) = 910 - 203[C]1/2 - 30[Mn] + 44.7[Si] + 700[P] + 100[Al] + 31.5[Mo] - 11[Cr] - 15.2[Ni] - 20[Cu] + 104[V]
  • In the formula, [M] denotes the element M content (% by mass).
  • Average Cooling Rate
  • Group A:
    cooling to 50°C or less at an average cooling rate of 15°C/s or more from 800°C to 550°C and at an average cooling rate of 15°C/s or less from 550°C to 50°C at the quarter thickness position from the surface of a steel material
    The predetermined carbide density cannot be achieved at an average cooling rate of less than 15°C/s from 800°C to 550°C at the quarter thickness position from the surface of a steel material. Furthermore, although the microstructure is not particularly limited, to achieve a predetermined fatigue property in hydrogen, bainite or martensite preferably constitutes 90% or more by area. At an average cooling rate of less than 15°C/s, it is difficult for bainite to constitute 90% or more by area, and the formation of martensite may be affected depending on the chemical composition. Thus, the average cooling rate at the quarter thickness position from the surface of a steel material is 15°C/s or more. From the perspective of reducing variations in microstructure, the average cooling rate is preferably 17°C/s or more, more preferably 20°C/s or more, still more preferably 22°C/s or more. On the other hand, to suppress variations in grain size, the average cooling rate is 50°C/s or less, preferably 47°C/s or less, more preferably 45°C/s or less. Furthermore, cooling to 50°C or less at an average cooling rate of 15°C/s or less from 550°C to 50°C can decrease retained austenite and reduce the amount of hydrogen in the steel. Thus, the average cooling rate from 550°C to 50°C is 15°C/s or less. Although the lower limit is not particularly limited, the average cooling rate from 550°C to 50°C is preferably 1°C/s or more. The cooling method is not particularly limited, and an arbitrary method, such as water cooling, oil cooling, or air cooling, can be used alone or in combination, but water cooling or oil cooling is preferred from 800°C to 550°C, and air cooling is preferred from 550°C to 50°C.
  • Group B:
    cooling to 50°C or less at an average cooling rate of 10°C/s or more from 800°C to 300°C and at an average cooling rate of 5°C/s or less from 300°C to 50°C at the quarter thickness position from the surface of a steel material
  • At an average cooling rate of less than 10°C/s from 800°C to 300°C at the quarter thickness position from the surface of a steel material, the predetermined carbide density cannot be achieved, and the fatigue property deteriorates. Furthermore, at an average cooling rate of less than 10°C/s, it is difficult for martensite to constitute 90% or more by area, and the formation of bainite may be affected depending on the chemical composition. Thus, the average cooling rate at the quarter thickness position from the surface of a steel material is 10°C/s or more. From the perspective of reducing variations in microstructure, 12°C/s or more is more preferred. The average cooling rate is still more preferably 15°C/s or more, still more preferably 17°C/s or more. On the other hand, although the average cooling rate may have any upper limit, when the average cooling rate is more than 60°C/s, a large amount of hard microstructure is formed on the surface of a steel plate, a steel microstructure with the microstructure intended in the present invention is not formed, and the fatigue property in hydrogen deteriorates, so that the average cooling rate is preferably 60°C/s or less. Furthermore, cooling to 50°C or less at an average cooling rate of 5°C/s or less from 300°C to 50°C can reduce the amount of hydrogen in the steel. Thus, the average cooling rate from 300°C to 50°C is 5°C/s or less. The average cooling rate is preferably 1°C/s or less, more preferably 0.8°C/s or less. The lower limit is preferably, but not limited to, 0.1°C/s or more. The cooling method is not particularly limited, and an arbitrary method, such as water cooling, oil cooling, or air cooling, can be used alone or in combination, but water cooling or oil cooling is preferred from 800°C to 300°C, and air cooling is preferred from 300°C to 50°C.
  • In a case of steel sheet (thin plate), it is preferable to coil the steel sheet, although coiling is not necessary for a steel plate.
  • Steel materials with a good fatigue property in hydrogen gas according to the present invention have the above chemical composition and include various types, such as a sheet, a plate, and a steel pipe, with high fatigue crack growth resistance in hydrogen gas, or may be steel materials for a hydrogen pipeline formed into a predetermined shape.
  • Under the above conditions, a steel pipe and a steel material with a good fatigue property in hydrogen satisfying a predetermined crack growth rate in hydrogen can be produced.
  • EXAMPLE 1
  • Examples that have verified the advantages of the present invention are described below. The examples are preferred examples of the present invention, and the present invention is not limited to these examples. A production method and characterization of a seamless steel pipe for an actual steel structure were studied in the examples.
  • Billets with the chemical compositions shown in the steel pipes Nos. 1 to 29 (billets Nos. A to AC) and 40 to 87 (billets Nos. AN to CI) in Tables 1-1 and 1-2 were produced at a casting speed of 0.6 m/min and were heated to 1250°C and expanded to produce seamless steel pipes. The steel pipes were produced under the conditions that expansion was finished at 820°C or more. The steel pipes were heated and held at 950°C for steel pipes with a Ac3 temperature of 950°C or less or at 1000°C for steel pipes with a Ac3 temperature of more than 950°C, were then water-cooled under the conditions shown in Tables 2-1 and 2-2, and were then tempered. The metallic microstructure and mechanical properties were evaluated. Furthermore, slabs with the chemical compositions shown in steel materials Nos. 30 to 39 (slabs Nos. AD to AM) of Tables 1-1 and 1-2 were produced at a casting speed of 0.6 m/min, were heated to 1250°C, and were then rolled using a hot-rolling mill at 820°C or more. The steel materials were heated and held at 950°C for steel materials with a Ac3 temperature of 950°C or less or at 1000°C for steel materials with a Ac3 temperature of more than 950°C, were then water-cooled under the conditions shown in Tables 2-1 and 2-2, were then tempered, and were evaluated for the metallic microstructure and mechanical properties in the same manner as the steel pipes. After tempering, Nos. 2, 5, 14, 15, 43, and 63 to 69 were also subjected to dehydrogenation treatment. In the dehydrogenation treatment, the ambient temperature, that is, the dehydrogenation treatment temperature T, was kept at 50°C for 3 hours, followed by natural cooling. The evaluation method is described below. The tempering temperature was arbitrarily adjusted so that the materials had a tensile strength in the range of 520 to 700 MPa.
  • Furthermore, billets with the chemical compositions shown in the steel pipes Nos. 88 to 101 (billets Nos. AO1 to BB1) in Table 2-3 were produced at various casting speeds and were heated to 1250°C and expanded to produce seamless steel pipes. The chemical compositions of the billets Nos. AO1 to BB1 are the same as the chemical compositions of Nos. AO to BB shown in Table 1-2. The steel pipes were produced under the conditions that expansion was finished at 820°C or more. The steel pipes were heated and held at 950°C for steel pipes with a Ac3 temperature of 950°C or less or at 1000°C for steel pipes with a Ac3 temperature of more than 950°C, were then water-cooled under the conditions shown in Table 2-3, and were then tempered under the conditions shown in Table 2-3. The metallic microstructure and mechanical properties were evaluated. The evaluation method is described below. The tempering temperature was arbitrarily adjusted so that the materials had a tensile strength in the range of 520 MPa to 700 MPa. In the dehydrogenation treatment, the ambient temperature, that is, the dehydrogenation treatment temperature T, was kept at 50°C for 3 hours, followed by natural cooling.
  • The fatigue crack propagation characteristics were evaluated by a fatigue crack growth test. A compact tension (CT) test specimen (a test specimen close to a square with a notch at one end portion) according to ASTM E 647 was taken from each steel material so that the load direction was parallel to the rolling direction, and a fatigue test was performed at a frequency of 1 Hz, a repetitive waveform of a sine wave, and a stress ratio of R = 0.1. The length of a fatigue crack was measured by a compliance method using a clip gauge to determine the fatigue crack propagation rate in 5-MPa high-pressure hydrogen gas. It was performed at room temperature (20°C ± 10°C). A test specimen taken from a steel material with plate thickness of 10 mm or less was ground from the surface by 0.5 mm resulting in test specimen thickness of 2 mm, 5 mm, 8 mm, or 9 mm, respectively, and for a test specimen taken from a steel material with plate thickness other than these, a test specimen with a thickness of 10 mm was taken from a position of t/2 (t: sheet thickness), and the front and back sides of a crack growth portion were mirror-polished. At this time, the fatigue crack growth rate (m/cycle) in a stress intensity factor range ΔK = 20 (MPa·m1/2) as a stable growth region where the Paris law holds was evaluated as a measure of central tendency. Tables 2-1, 2-2, and 2-3 show the results.
  • Furthermore, a carbide measurement method for a steel material is described below. A test specimen was cut out from a cross section parallel to the thickness direction from the center position of the plate thickness of a steel material and was subjected to nital etching, and a carbide was observed by SEM. Ten fields were randomly selected and observed at an acceleration voltage of 15 kV and a magnification of 20000 times. Tables 2-1, 2-2, and 2-3 show the average value of the 10 fields as the number of carbides, with Y indicating that the number of carbides with a diameter of 200 nm or more is 20 pieces/10 µm2 or less, and N indicating that the number of carbides with a diameter of 200 nm or more is more than 20 pieces/10 µm2. Furthermore, a method for measuring the amount of austenite in a steel material is described below.
  • A sample for metallic microstructure observation was taken from the center of the sheet width in the center in the longitudinal direction of each of the steel materials and the steel pipes thus produced, a cross section parallel to the longitudinal direction was buffed as an observation surface, the surface layer was then removed by chemical polishing using picric acid etching, and X-ray diffractometry was performed. More specifically, a Co-Kα radiation source was used for an incident X-ray, and the area fraction of retained austenite was calculated from the intensity ratios of the (200), (211), and (220) planes of ferrite to the (200), (220), and (311) planes of austenite.
  • Hydrogen Thermal Desorption Analysis
  • The amount of hydrogen remaining in the steel was measured by thermal desorption analysis method using a low-temperature programmed hydrogen analyzer <gas chromatograph type> (JTF-20AL). The thermal desorption analysis was performed in the temperature range of room temperature to 400°C at a heating rate of 200°C/h, and the sum total thereof was taken as the amount of hydrogen. The specimen has a cylindrical shape with 30 mm in length and 7Φ in diameter in the longitudinal direction of the steel pipe at the quarter thickness position of the steel plate and at the quarter thickness position from the inner surface of the steel pipe. The amount of hydrogen is the amount of H shown in Tables 1-1 and 1-2, and the amount before being subjected to a high-pressure hydrogen fatigue test explained in aging described later.
  • Steel pipes are also subjected to the various tests in the same manner as the steel materials described above.
  • The examples of the present invention all satisfied the condition that the fatigue crack growth rate in hydrogen gas was 1.0 x 10-6 m/cycle or less.
  • The steel pipes Nos. 94 and 101, in which the casting speed in Table 2-3 was outside the scope of the present invention, included coarse inclusions, had a fatigue crack growth rate in hydrogen gas outside the scope of the present invention, and were comparative examples.
    Figure imgb0002
    Figure imgb0003
    [Table 2-1]
    Steel material No. Steel pipe No. Cooling step Tempering step Carbide Amount of residual y (%) Crack growth rate in hydrogen at ΔK=20 (MPa·m1/2) 10-6 m/cycle Notes
    A B Cooling stop temperature (°C)
    Average cooling rate from 800°C to 550°C (°C/s) Average cooling rate from 550°C to 50°C (°C/s) Average cooling rate from 800°C to 300°C (°C/s) Average cooling rate from 300°C to 50°C (°C/s) Temperature (°C) Time (min)
    - 1 - - 14 4 39 633 20 Y 0 0.788 Inventive example
    - 2 15 5 - - 32 620 30 Y 0 0.640 Inventive example
    - 3 16 6 - - 25 614 30 Y 0 0.455 Inventive example
    - 4 16 4 - - 26 627 30 Y 0 0.512 Inventive example
    - 5 18 9 - - 25 596 30 Y 2 0.213 Inventive example
    - 6 19 5 - - 25 653 30 Y 0 0.180 Inventive example
    - 7 19 4 - - 25 629 30 Y 0 0.106 Inventive example
    - 8 20 5 - - 33 638 30 Y 0 0.661 Inventive example
    - 9 18 3 - - 25 635 50 Y 2 0.211 Inventive example
    - 10 19 4 - - 25 642 30 Y 1 0.169 Inventive example
    - 11 26 5 - - 32 639 30 Y 1 0.637 Inventive example
    - 12 19 6 - - 25 613 30 Y 0 0.078 Inventive example
    - 13 18 4 - - 25 638 30 Y 0 0.188 Inventive example
    - 14 19 5 - - 25 626 30 Y 0 0.097 Inventive example
    - 15 17 6 - - 25 631 30 Y 0 0.385 Inventive example
    - 16 16 8 - - 25 625 30 Y 0 0.491 Inventive example
    - 17 - - 13 3 41 616 30 Y 0 0.815 Inventive example
    - 18 18 4 - - 25 619 30 Y 0 0.282 Inventive example
    - 19 16 2 - - 25 642 30 Y 0 0.444 Inventive example
    - 20 16 3 - - 28 611 30 Y 0 0.551 Inventive example
    - 21 19 6 - - 25 634 30 Y 1 0.128 Inventive example
    - 22 17 8 - - 25 624 30 Y 1 0.411 Inventive example
    - 23 18 5 - - 25 678 40 Y 0 0.280 Inventive example
    - 24 17 4 - - 25 650 30 Y 0 0.315 Inventive example
    - 25 18 3 - - 25 631 30 Y 0 0.249 Inventive example
    - 26 19 3 - - 25 620 30 Y 1 0.125 Inventive example
    - 27 18 5 - - 25 593 30 Y 1 0.310 Inventive example
    - 28 18 4 - - 25 667 30 Y 0 0.210 Inventive example
    - 29 23 3 - - 29 648 30 Y 2 0.585 Inventive example
    30 - - - 13 2 41 631 30 Y 0 0.813 Inventive example
    31 - 15 3 - - 30 608 30 Y 1 0.597 Inventive example
    32 - - - 14 3 37 646 30 Y 0 0.743 Inventive example
    33 - 16 4 - - 27 624 30 Y 0 0.548 Inventive example
    34 - 16 5 - - 25 651 20 Y 1 0.476 Inventive example
    35 - - - 14 4 35 613 30 Y 1 0.694 Inventive example
    36 - 19 7 - - 25 615 30 Y 0 0.146 Inventive example
    37 - - - 13 3 41 633 30 Y 0 0.826 Inventive example
    38 - 16 5 - - 25 618 30 Y 0 0.502 Inventive example
    39 - 16 4 - - 25 689 30 Y 0 0.483 Inventive example
    - 40 - - 14 3 38 653 30 Y 1 0.766 Inventive example
    Underline: outside the scope of the present invention. γ: austenite
    [Table 2-2]
    Steel material No. Steel pipe No. Cooling step Tempering step Carbide Amount of residual γ (%) Crack growth rate in hydrogen at ΔK=20 (MPa m12) 10-6 m/cycle Notes
    A B Cooling stop temperature (°C)
    Average cooling rate from 800°C to 550°C (°C/s) Average cooling rate from 550°C to 50°C (°C/s) Average cooling rate from 800°C to 300°C (°C/s) Average cooling rate from 300°C to 50°C (°C/s) Temperature (°C) Time (min)
    - 41 18 6 - - 25 614 40 Y 1 0.286 Inventive example
    - 42 - - 14 4 35 643 30 Y 0 0.695 Inventive example
    - 43 15 4 - - 31 663 30 Y 0 0.620 Inventive example
    - 44 - - 14 3 37 653 30 Y 0 0.741 Inventive example
    - 45 18 5 - - 25 611 30 Y 0 0.252 Inventive example
    - 46 17 6 - - 25 665 30 Y 0 0.421 Inventive example
    - 47 18 6 - - 25 653 30 Y 0 0.273 Inventive example
    - 48 18 7 - - 25 667 30 Y 1 0.299 Inventive example
    - 49 - - 14 3 37 672 30 Y 0 0.731 Inventive example
    - 50 - - 13 3 41 606 40 Y 0 0.825 Inventive example
    - 51 18 6 - - 25 674 30 Y 0 0.308 Inventive example
    - 52 - - 13 3 41 663 30 Y 0 0.829 Inventive example
    - 53 - - 14 4 35 629 30 Y 0 0.703 Inventive example
    - 54 18 8 - - 25 687 50 Y 1 0.267 Inventive example
    - 55 16 6 - - 27 616 20 Y 0 0.542 Inventive example
    - 56 18 7 - - 25 647 30 Y 0 0.267 Inventive example
    - 57 18 8 - - 25 681 30 Y 0 0.272 Inventive example
    - 58 15 6 - - 32 689 30 Y 0 0.647 Inventive example
    - 59 - - 13 2 42 619 30 Y 0 0.842 Inventive example
    - 60 - - 14 3 40 636 30 Y 3 0.791 Inventive example
    - 61 16 5 - - 26 657 40 Y 0 0.524 Inventive example
    - 62 16 6 - - 25 624 30 Y 0 0.450 Inventive example
    - 63 - - 13 3 44 635 30 Y 2 0.880 Inventive example
    - 64 - - 9 2 25 647 30 N 0 1.123 Comparative example
    - 65 - - 9 1 25 647 30 N 0 1.046 Comparative example
    - 66 - - 14 4 40 757 30 Y 4 1.995 Comparative example
    - 67 17 16 - - 33 737 30 Y 4 1.642 Comparative example
    - 68 20 9 - - 26 647 80 N 0 1305 Comparative example
    - 69 - - 12 3 25 647 70 N 0 1.029 Comparative example
    - 70 16 6 - - 48 613 30 N 0 2.375 Comparative example
    - 71 18 7 - - 37 655 30 N 0 1834 Comparative example
    - 72 18 8 - - 50 655 20 Y 0 2513 Comparative example
    - 73 15 5 - - 25 651 30 Y 1 1.243 Comparative example
    - 74 - - 13 3 46 613 30 Y 4 2.316 Comparative example
    - 75 - - 14 4 33 632 30 Y 4 1.642 Comparative example
    - 76 16 5 - - 41 639 40 Y 0 2.047 Comparative example
    - 77 16 6 - - 25 640 30 Y 0 1206 Comparative example
    - 78 - - 13 2 41 636 30 Y 0 2.050 Comparative example
    - 79 - - 14 3 37 601 40 Y 0 1827 Comparative example
    - 80 18 5 - - 42 613 30 Y 2 2106 Comparative example
    - 81 - - 13 2 28 620 30 Y 0 1.395 Comparative example
    - 82 - - 14 4 33 637 30 Y 0 1.666 Comparative example
    - 83 18 6 - - 30 635 30 Y 0 1.492 Comparative example
    - 84 - - 14 4 35 615 30 Y 0 1735 Comparative example
    - 85 15 5 - - 30 657 30 Y 2 1.495 Comparative example
    - 86 22 5 - - 55 620 30 N 1 1.223 Comparative example
    - 87 - - 15 3 43 630 30 Y 0 0.892 Inventive example
    Underline: outside the scope of the present invention. γ: austenite
    [Table 2-3]
    Billet No. Steel pipe No. Casting speed (m/min) Cooling step Tempering step Carbide Amount of residual γ (%) Crack growth rate in hydrogen at ΔK=20 (MPa·m1/2) 10-6 m/cycle Notes
    A B Cooling stop temperature (°C)
    Average cooling rate from 800°C to 550°C (°C/s) Average cooling rate from 550°C to 50°C (°C/s) Average cooling rate from 800°C to 300°C (°C/s) Average cooling rate from 300°C to 50°C (°C/s) Temperature (°C) Time (min)
    AO1 88 0.8 18 6 - - 25 614 40 Y 1 0.255 Inventive example
    Figure imgb0004
    AP1
    89 1.2 - - 14 4 35 643 30 Y 0 0.839 Inventive example
    AQ1 90 1.5 15 4 - - 31 663 30 Y 0 0.918 Inventive example
    AR1 91 1.5 - - 14 3 37 653 30 Y 0 0.882 Inventive example
    AS1 92 1.8 18 5 - - 25 611 30 Y 0 0.902 Inventive example
    AT1 93 1.8 17 6 - - 25 665 30 Y 0 0.911 Inventive example
    AU1 94 20 18 6 - - 25 653 30 Y 0 1.190 Comparative example
    AV1 95 0.8 18 7 - - 25 667 30 Y 1 0.252 Inventive example
    AW1 96 1.2 - - 14 3 37 672 30 Y 0 0.839 Inventive example
    AX1 97 1.5 - - 13 3 41 606 40 Y 0 0.892 Inventive example
    AY1 98 1.5 18 6 - - 25 674 30 Y 0 0.914 Inventive example
    AZ1 99 1.8 - - 13 3 41 663 30 Y 0 0.958 Inventive example
    BA1 100 1.8 - - 14 4 35 629 30 Y 0 0.961 Inventive example
    BB1 101 2.0 18 8 - - 25 687 50 Y 1 1.090 Comparative example
    Underline: outside the scope
    of the present invention.
    γ: austenite
  • EXAMPLE 2
  • Examples in which the advantages of the present invention have been verified are described below. In the following Examples, steel pipes were produced under the following production conditions and were characterized. Steel pipes with the same chemical composition as the billets Nos. Q and BC shown in Tables 1-1 and 1-2 and AS1 shown in Table 2-3 were subjected to up to the cooling step under predetermined conditions, were reheated under the conditions shown in Table 3 after the cooling step (before the tempering step), were subjected to the quenching step, and were characterized. The steel pipes Nos. 17A to 17C shown in Table 3 were the steel pipes No. 17 shown in Tables 1-1 and 2-1 subjected to the reheating step. The steel pipes Nos. 55A to 55C were the steel pipes No. 55 shown in Tables 1-2 and 2-2 subjected to the reheating step, and the steel pipes Nos. 92A and 92B were the steel pipes No. 92 shown in Table 2-3 subjected to the reheating step. The examples of Example 2 all satisfied the condition that the crack growth rate da/dN in hydrogen gas was 1.0 x 10-6 m/cycle or less. Among them, the crack propagation characteristics were better when the reheating and quenching steps were performed under more suitable conditions. [Table 3]
    Billet No. Steel pipe No. Cooling step Reheating step Cooling step Tempering step Carbide Amount of residual Y (%) Crack growth rate in hydrogen at ΔK=20 (MPa·m1/2) 10-6 m/cycle Notes
    A B Cooling stop temperature (°C) A B Cooling stop temperature (°C)
    Average cooling rate from 800°C to 550°C (°C/s) Average cooling rate from 550°C to 50°C (°C/s) Average cooling rate from 800°C to 300°C (°C/s) Average cooling rate from 300°C to 50°C (°C/s) Reheating temperature (°C) Average cooling rate from 800°C to 550°C (°C/s) Average cooling rate from 550°C to 50°C (°C/s) Average cooling rate from 800°C to 300°C (°C/s) Average cooling rate from 300°C to 50°C (°C/s) Temperature (°C) Time (min)
    Q 17 - - 13 3 41 - - - - - - 616 30 Y 0 0.815 Inventive example
    Q 17A - - 13 3 41 890 - - 13 3 36 616 30 Y 0 0.723 Inventive example
    Q 17B - - 13 3 41 950 - - 13 3 38 616 30 Y 0 0.756 Inventive example
    Q 17C - - 13 3 41 1000 - - 13 3 49 616 30 Y 0 0.978 Inventive example
    BC 55 16 6 - - 27 - - - - - - 616 20 Y 0 0.542 Inventive example
    BC 55A 16 6 - - 27 960 16 6 - - 25 616 20 Y 0 0.492 Inventive example
    BC 55B 16 6 - - 27 980 16 6 - - 25 616 20 Y 0 0.508 Inventive example
    BC 55C 16 6 - - 27 1000 16 6 - - 35 616 20 Y 0 0.695 Inventive example
    AS1 92 18 5 - - 25 - - - - - - 611 30 Y 0 0.902 Inventive example
    AS1 92A 18 5 - - 25 920 18 5 - - 25 611 30 Y 0 0.816 Inventive example
    AS1 92B 18 5 - - 25 950 18 5 - - 25 611 30 Y 0 0.838 Inventive example
    γ: austenite
  • EXAMPLE 3
  • Examples in which the advantages of the present invention have been verified are described below. In the following Examples, steel pipes were produced under the following production conditions and were characterized. The billets Nos. N and AQ shown in Tables 1-1 and 1-2 and AX1 shown in Table 2-3 were used, up to the tempering step was performed under the same conditions as the steel pipes Nos. 14 and 43 shown in Tables 2-1 and 2-2 and the steel pipe No. 97 shown in Table 2-3, and the characteristics were evaluated while the dehydrogenation treatment conditions were changed. Table 4 shows the results. Although the dehydrogenation treatment of the steel pipes Nos. 14, 43, and 97 in Example 1 was performed at a dehydrogenation treatment temperature T (ambient temperature) of 50°C for a holding time of 3 hours, in the present example, the dehydrogenation treatment of the steel pipes Nos. 14D, 43D, and 97D was performed at a dehydrogenation treatment temperature T (ambient temperature) of 50°C so that the holding time tc after the temperature Tc at the center of the plate thickness reached 50°C satisfied the formula (A). For the steel pipes Nos. 14E, 43E, and 97E, the dehydrogenation treatment temperature T (ambient temperature) was 50°C, and the holding time tc satisfied the formula (A) at a dehydrogenation treatment temperature T of 50°C, but the holding time tc after the temperature Tc at the center of the plate thickness reached 50°C did not satisfy the formula (A). For the steel pipes Nos. 14F and 97F, the dehydrogenation treatment temperature T (ambient temperature) was 50°C, but neither the holding time t at the ambient temperature nor the holding time tc after the temperature Tc at the center of the plate thickness reached 50°C did not satisfied the formula (A).
  • In Table 4, "Dehydrogenation holding time t is Y" means that the dehydrogenation treatment temperature T (ambient temperature) is 50°C and the holding time t satisfies the formula (A), and "Dehydrogenation holding time t is N" means that the dehydrogenation treatment temperature T (ambient temperature) is 50°C, but the holding time t does not satisfy the formula (A). Furthermore, "Holding time tc at center temperature of steel plate thickness Tc is Y" means that the holding time tc after the temperature Tc at the center of the plate thickness reaches 50°C satisfies the formula (A), and "Holding time tc at steel material center temperature Tc is N" means that the temperature Tc at the center of the plate thickness reaches 50°C, but the holding time tc after Tc reaches 50°C does not satisfy the formula (A).
  • Investigation of the fatigue crack propagation characteristics was evaluated by the fatigue crack growth test described in Example 1.
  • The examples of the present invention all satisfied the condition that the crack growth rate da/dN in hydrogen gas was 1.0 x 10-6 m/cycle or less. Among them, a steel pipe subjected to the dehydrogenation treatment under more suitable conditions had better crack propagation characteristics. [Table 4]
    Billet No. Steel pipe No. Dehydrogenation holding time t Holding time tc at center temperature of steel plate thickness TC Carbide Amount of residual γ (%) Crack growth rate in hydrogen at ΔK=20 (MPa·m1/2) 10-6 m/cycle Notes
    N 14D Y Y Y 0 0.087 Inventive example
    N 14E Y N Y 0 0.099 Inventive example
    N 14F N N Y 0 0.337 Inventive example
    AQ 430 Y Y Y 0 0.543 Inventive example
    AQ 43E Y N Y 0 0.650 Inventive example
    AX1 97D Y Y Y 0 0.772 Inventive example
    AX1 97E Y N Y 0 0.888 Inventive example
    AX1 97F N N Y 0 0.913 Inventive example
    γ: austenite

Claims (8)

  1. A steel pipe with a good fatigue property in hydrogen, the steel pipe having a chemical composition comprising:
    on a mass percent basis,
    C: 0.10% to 0.45%,
    Si: 0.01% to 2.0%,
    Mn: 0.3% to 2.0%,
    Al: 0.01% to 0.15%,
    N: 0.0005% to 0.008%,
    P: 0.015% or less,
    S: 0.0015% or less,
    O: 0.01% or less,
    H: 0.0010% or less,
    Cu: 0% to 2.5%,
    Ni: 0% to 2.5%,
    Cr: 0% to 2.5%,
    Mo: 0% to 2.0%,
    Nb: 0% to 0.5%,
    V: 0% to 0.5%,
    Ti: 0% to 0.5%,
    W: 0% to 2.5%,
    B: 0% to 0.005%,
    Sn: 0% to 0.3%,
    Sb: 0% to 0.3%,
    Ca: 0% to 0.01%,
    Mg: 0% to 0.01%, and
    REM: 0% to 0.005%,
    the remainder being Fe and incidental impurities,
    wherein retained austenite constitutes 3% or less,
    the number of carbides with a diameter of 200 nm or more is 20 pieces/10 µm2 or less, and
    a crack growth rate da/dN at a stress intensity factor range of 20 MPa √m in hydrogen of 1 MPa or more is 1.0 x 10-6 m·cycle-1 or less.
  2. A method for producing a steel pipe, the method comprising:
    a casting step of casting a steel raw material with the chemical composition according to Claim 1 at a casting speed of 1.8 m/min or less;
    a heating step of heating at 1350°C or less;
    a hot rolling step of rolling the steel raw material heated in the heating step at a finish rolling temperature of 820°C or more to form a steel pipe shape;
    a cooling step of holding a steel pipe obtained in the hot rolling step at a temperature of an Ac3 temperature or higher and 1000°C or less, and a cooling condition is the following Group A or Group B; and
    a tempering step of tempering the steel pipe obtained in the cooling step at 400°C or more and an Ac1 temperature or lower for less than 60 minutes,
    Group A:
    cooling the steel pipe to 50°C or less at an average cooling rate of 15°C/s or more from 800°C to 550°C at a quarter thickness position from an inner surface of the steel pipe and at an average cooling rate of 15°C/s or less from 550°C to 50°C at the quarter thickness position from the inner surface of the steel pipe, and
    Group B:
    cooling the steel pipe to 50°C or less at an average cooling rate of 10°C/s or more from 800°C to 300°C at the quarter thickness position from the inner surface of the steel pipe and at an average cooling rate of 5°C/s or less from 300°C to 50°C at the quarter thickness position from the inner surface of the steel pipe.
  3. The method for producing a steel pipe according to Claim 2, comprising, before the tempering step, a quenching step of reheating to an Ac3 temperature or higher and 1000°C or less, and a cooling condition is the following Group A or Group B,
    Group A:
    cooling the steel pipe to 50°C or less at an average cooling rate of 15°C/s or more from 800°C to 550°C at a quarter thickness position from an inner surface of the steel pipe and at an average cooling rate of 15°C/s or less from 550°C to 50°C at the quarter thickness position from the inner surface of the steel pipe, and
    Group B:
    cooling the steel pipe to 50°C or less at an average cooling rate of 10°C/s or more from 800°C to 300°C at the quarter thickness position from the inner surface of the steel pipe and at an average cooling rate of 5°C/s or less from 300°C to 50°C at the quarter thickness position from the inner surface of the steel pipe.
  4. The method for producing a steel pipe according to Claim 2 or 3, wherein the casting speed is 1.0 m/min or less.
  5. A steel material with a good fatigue property in hydrogen, the steel material having a chemical composition comprising:
    on a mass percent basis,
    C: 0.10% to 0.45%,
    Si: 0.01% to 2.0%,
    Mn: 0.3% to 2.0%,
    Al: 0.01% to 0.15%,
    N: 0.0005% to 0.008%,
    P: 0.015% or less,
    S: 0.0015% or less,
    O: 0.01% or less,
    H: 0.0010% or less,
    Cu: 0% to 2.5%,
    Ni: 0% to 2.5%,
    Cr: 0% to 2.5%,
    Mo: 0% to 2.0%,
    Nb: 0% to 0.5%,
    V: 0% to 0.5%,
    Ti: 0% to 0.5%,
    W: 0% to 2.5%,
    B: 0% to 0.005%,
    Sn: 0% to 0.3%,
    Sb: 0% to 0.3%,
    Ca: 0% to 0.01%,
    Mg: 0% to 0.01%, and
    REM: 0% to 0.005%,
    the remainder being Fe and incidental impurities,
    wherein retained austenite constitutes 3% or less,
    the number of carbides with a diameter of 200 nm or more is 20 pieces/10 µm2 or less, and
    a crack growth rate da/dN at a stress intensity factor range of 20 MPa √m in hydrogen of 1 MPa or more is 1.0 x 10-6 m·cycle-1 or less.
  6. A method for producing a steel material, the method comprising:
    a casting step of casting a steel raw material with the chemical composition according to Claim 5 at a casting speed of 1.8 m/min or less;
    a heating step of heating at 1350°C or less;
    a hot rolling step of rolling the steel raw material heated in the heating step at a finish rolling temperature of 820°C or more;
    a cooling step of holding a steel material obtained in the hot rolling step at a temperature of an Ac3 temperature or higher and 1000°C or less, and a cooling condition is the following Group A or Group B; and
    a tempering step of tempering the steel material obtained in the cooling step at 400°C or more and an Ac1 temperature or lower for less than 60 minutes,
    Group A:
    cooling the steel material to 50°C or less at an average cooling rate of 15°C/s or more from 800°C to 550°C at a quarter thickness position from a surface of the steel material and at an average cooling rate of 15°C/s or less from 550°C to 50°C at the quarter thickness position from the surface of the steel material, and
    Group B:
    cooling the steel material to 50°C or less at an average cooling rate of 10°C/s or more from 800°C to 300°C at the quarter thickness position from the surface of the steel material and at an average cooling rate of 5°C/s or less from 300°C to 50°C at the quarter thickness position from the surface of the steel material.
  7. The method for producing a steel material according to Claim 6, comprising, before the tempering step, a quenching step of reheating to an Ac3 temperature or higher and 1000°C or less, and a cooling condition is the following Group A or Group B,
    Group A:
    cooling the steel material to 50°C or less at an average cooling rate of 15°C/s or more from 800°C to 550°C at a quarter thickness position from a surface of the steel material and at an average cooling rate of 15°C/s or less from 550°C to 50°C at the quarter thickness position from the surface of the steel material, and
    Group B:
    cooling the steel material to 50°C or less at an average cooling rate of 10°C/s or more from 800°C to 300°C at the quarter thickness position from the surface of the steel material and at an average cooling rate of 5°C/s or less from 300°C to 50°C at the quarter thickness position from the surface of the steel material.
  8. The method for producing a steel material according to Claim 6 or 7, wherein the casting speed is 1.0 m/min or less.
EP23872574.1A 2022-09-29 2023-09-28 STEEL PIPE WITH EXCELLENT FATISFACTION PROPERTIES TO HYDROGEN AND MANUFACTURING METHOD FOR IT, AS WELL AS STEEL MATERIAL AND MANUFACTURING METHOD FOR IT Pending EP4578565A4 (en)

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PCT/JP2023/035556 WO2024071354A1 (en) 2022-09-29 2023-09-28 Steel tube exhibiting excellent fatigue characteristics against hydrogen and production method therefor, and steel material and production method therefor

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JP2005002386A (en) 2003-06-10 2005-01-06 Sumitomo Metal Ind Ltd Steel for high pressure hydrogen environment, steel pipe and method for producing the same
JP5020572B2 (en) * 2006-08-31 2012-09-05 新日本製鐵株式会社 High strength thin steel sheet with excellent delayed fracture resistance after forming
JP5094272B2 (en) 2007-08-21 2012-12-12 株式会社日本製鋼所 Low alloy high strength steel with excellent high pressure hydrogen environment embrittlement resistance and method for producing the same
JP4251229B1 (en) 2007-09-19 2009-04-08 住友金属工業株式会社 Low alloy steel for high pressure hydrogen gas environment and container for high pressure hydrogen
JP5201625B2 (en) 2008-05-13 2013-06-05 株式会社日本製鋼所 High strength low alloy steel with excellent high pressure hydrogen environment embrittlement resistance and method for producing the same
JP5353501B2 (en) 2008-07-09 2013-11-27 新日鐵住金株式会社 High temperature hydrogen gas storage steel container having excellent hydrogen resistance and method for producing the same
JP5849609B2 (en) 2010-10-28 2016-01-27 Jfeスチール株式会社 Steel for high-pressure hydrogen storage
IN2014DN09191A (en) * 2012-06-20 2015-07-10 Nippon Steel & Sumitomo Metal Corp
CN105102653B (en) * 2013-03-29 2018-05-08 杰富意钢铁株式会社 The manufacture method of hydrogen steel structure, hydrogen storage vessel and hydrogen pipeline
CN105102657B (en) * 2013-03-29 2017-03-15 杰富意钢铁株式会社 Steel and hydrogen container and their manufacture method
JP5928394B2 (en) * 2013-03-29 2016-06-01 Jfeスチール株式会社 Steel structure for hydrogen excellent in hydrogen embrittlement resistance in high-pressure hydrogen gas, hydrogen pressure accumulator, and method for producing hydrogen line pipe
MX385708B (en) * 2014-02-27 2025-03-18 Jfe Steel Corp HIGH STRENGTH HOT-ROLLED STEEL SHEET AND METHOD FOR MANUFACTURING SAME.
JP6222041B2 (en) * 2014-10-30 2017-11-01 Jfeスチール株式会社 Ultra-thick steel plate with excellent HIC resistance and manufacturing method thereof
KR102120616B1 (en) * 2015-09-17 2020-06-08 제이에프이 스틸 가부시키가이샤 Steel structure for hydrogen gas with excellent hydrogen embrittlement resistance in high pressure hydrogen gas and method of producing the same
JP6451874B2 (en) * 2016-10-17 2019-01-16 Jfeスチール株式会社 High strength seamless steel pipe for oil well and method for producing the same
WO2019069771A1 (en) * 2017-10-03 2019-04-11 新日鐵住金株式会社 Steel sheet and method for producing steel sheet
JP6989004B2 (en) * 2018-12-26 2022-01-05 Jfeスチール株式会社 Method for manufacturing high-pressure hydrogen gas environmental steel, high-pressure hydrogen gas environmental steel structure, and high-pressure hydrogen gas environmental steel
WO2020166638A1 (en) * 2019-02-13 2020-08-20 日本製鉄株式会社 Steel pipe for fuel injection line, and fuel injection line employing same
KR20230145592A (en) * 2021-03-30 2023-10-17 제이에프이 스틸 가부시키가이샤 Steel pipe for high-pressure hydrogen, container for high-pressure hydrogen, and manufacturing method of the steel pipe

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