CN113969380A - Manufacturing method of nuclear-grade nickel-based alloy high-performance bar, bar and application - Google Patents

Manufacturing method of nuclear-grade nickel-based alloy high-performance bar, bar and application Download PDF

Info

Publication number
CN113969380A
CN113969380A CN202010718980.4A CN202010718980A CN113969380A CN 113969380 A CN113969380 A CN 113969380A CN 202010718980 A CN202010718980 A CN 202010718980A CN 113969380 A CN113969380 A CN 113969380A
Authority
CN
China
Prior art keywords
forging
temperature
bar
nuclear
based alloy
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CN202010718980.4A
Other languages
Chinese (zh)
Other versions
CN113969380B (en
Inventor
欧新哲
马天军
赵欣
胡仁民
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Baowu Special Metallurgy Co Ltd
Original Assignee
Baowu Special Metallurgy Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Baowu Special Metallurgy Co Ltd filed Critical Baowu Special Metallurgy Co Ltd
Priority to CN202010718980.4A priority Critical patent/CN113969380B/en
Publication of CN113969380A publication Critical patent/CN113969380A/en
Application granted granted Critical
Publication of CN113969380B publication Critical patent/CN113969380B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/10Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of nickel or cobalt or alloys based thereon
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/03Alloys based on nickel or cobalt based on nickel
    • C22C19/05Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/051Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
    • C22C19/055Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 20% but less than 30%
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F22STEAM GENERATION
    • F22BMETHODS OF STEAM GENERATION; STEAM BOILERS
    • F22B1/00Methods of steam generation characterised by form of heating method
    • F22B1/02Methods of steam generation characterised by form of heating method by exploitation of the heat content of hot heat carriers
    • F22B1/04Methods of steam generation characterised by form of heating method by exploitation of the heat content of hot heat carriers the heat carrier being hot slag, hot residues, or heated blocks, e.g. iron blocks

Abstract

The invention discloses a method for manufacturing a nuclear-grade nickel-based alloy high-performance bar, which comprises the following steps: graded high temperature diffusion annealing: high-temperature diffusion is carried out in two stages; the forging adopts a composite forging method of quick forging and precision forging; adopting rapid forging cogging, controlling pass deformation amount to be 40-60% and forging temperature to be 1200-1230 ℃; forging by adopting a precision forging rapid forging method, controlling the pass deformation by 30-40%, gradually forging to obtain a finished bar, and rapidly cooling after the final forging temperature is 1000-1050 ℃; performing heat treatment on the finished bar, wherein the heat treatment temperature is 1140-: dx (0.25-0.35) min/mm, followed by rapid cooling. Also disclosed are bars, and uses of the bars. The invention effectively improves the high-temperature performance, especially the long-term durability, of the UNS N06625 alloy bar by optimizing and adjusting the proportion of C and Ti elements and simultaneously adopting a graded high-temperature diffusion, quick forging and finish forging composite forging method and the heat treatment of the finished bar.

Description

Manufacturing method of nuclear-grade nickel-based alloy high-performance bar, bar and application
Technical Field
The invention belongs to the technical field of nickel-based alloy, and particularly relates to a method for manufacturing a nickel-based alloy bar for nuclear-grade high-temperature long-time use.
Background
Nuclear power is advanced clean energy, is an important component of the national energy strategy, and is one of the most important measures for realizing the national energy-saving and emission-reducing targets. The modular high-temperature gas cooled reactor nuclear power station has the characteristics of high safety, simple system, high power generation efficiency, wide application, economic competitiveness and the like, and is one of the fourth generation advanced nuclear reactor types required by the future energy market.
The UNS N06625 nickel-based alloy is a Ni-Cr-Mo solid solution strengthening type nickel-based corrosion-resistant alloy with high Mo content, has good comprehensive performance, and is widely applied to the field of petrochemical industry. The alloy contains high Cr and Ni elements, high Mo and Nb elements and high alloying degree, so that the steel ingot is easy to segregate during solidification, has high deformation resistance in processing and is easy to crack. The traditional UNS N06625 alloy bar is mainly applied to the traditional fields of petrochemical industry and the like, the high-temperature strength and the high-temperature long-term endurance strength of the material are not generally required in the industry, and the bar meeting the requirements can be produced by adopting a conventional forging process.
However, the temperature of helium at the inlet of a steam generator in a high-temperature gas-cooled reactor nuclear power station is up to 750 ℃, so that the long-term working temperature of parts in a steam generator inlet chamber and a heat exchange assembly also reaches 750 ℃, the manufacturing of the parts puts higher requirements on the room temperature performance, 750 ℃ instantaneous performance and 750 ℃ long-term durability of materials compared with the traditional application field, and the performance of bars produced by adopting a conventional forging process cannot meet the harsh requirements of the high-temperature gas-cooled reactor steam generator.
Disclosure of Invention
The technical problem to be solved by the invention is to overcome the defects of the prior art and provide a method for manufacturing a high-performance bar suitable for manufacturing a high-temperature gas-cooled reactor steam generator.
The technical scheme of the invention is that the manufacturing method of the nuclear-grade nickel-based alloy high-performance bar comprises the following steps of high-temperature diffusion annealing and forging:
a. graded high temperature diffusion annealing: first-stage high-temperature diffusion temperature: 1110 ℃ -1130 ℃, heat preservation time: d is multiplied by (0.03-0.05) h/mm, D is the diameter of the steel ingot, and the unit is mm; then directly heating to the second stage at 1200-1250 ℃, and keeping the temperature for: d is multiplied by (0.08-0.10) h/mm, D is the diameter of the steel ingot, and the unit is mm;
b. the forging adopts a composite forging method of quick forging and precision forging; firstly, adopting rapid forging cogging, controlling pass deformation amount to be 40-60% and forging temperature to be 1200-1230 ℃; secondly, forging by adopting a precision forging rapid forging method, controlling the pass deformation to be 30-40%, gradually forging the finished bar material, and rapidly cooling by water after the final forging temperature is 1000-1050 ℃;
c. performing heat treatment on the finished bar, wherein the heat treatment temperature is 1140-: d x (0.25-0.35) min/mm, D being the diameter of the bar in mm, followed by rapid water cooling.
And carrying out long-time homogenization treatment on the cast ingot by adopting a graded high-temperature diffusion method, and eliminating intermetallic laves phases of low-temperature eutectic in the steel ingot solidification process and redistribution of Mo and Nb easily-segregated elements, so that the structure and the components of the forged rod are more uniform.
The above contents are mutually restricted, and are all indispensable, and are an organic whole. Any one of the bars cannot reach the comprehensive performance index due to unreasonable design.
According to the method for manufacturing the high-performance rod of the nuclear-grade nickel-based alloy, the high-temperature diffusion temperature of the first stage in the step a is preferably 1115-1125 ℃, and the heat preservation time is preferably Dx (0.04-0.05) h/mm. More preferably, the first-stage high-temperature diffusion temperature is 1119-.
According to the manufacturing method of the nuclear grade nickel base alloy high-performance bar, the temperature of the second-stage high-temperature diffusion in the step a is preferably 1225-.
According to the manufacturing method of the nuclear grade nickel base alloy high-performance bar, the cooling mode in the step b is preferably water cooling.
According to the manufacturing method of the nuclear grade nickel base alloy high-performance bar, the cooling mode in the step c is preferably water cooling.
The invention also provides a nuclear grade nickel-based alloy high-performance bar prepared by the method,
the weight percentage of the chemical components is as follows: 0.03-0.04%, P is less than or equal to 0.010%, S is less than or equal to 0.010%, Cr: 20.0-23.0%, Ni is more than or equal to 58.0%, Mo: 8.5-9.5%, Nb: 3.3-3.8%, Al: 0.35-0.50%, and the balance of inevitable impurities; and Ti/C is 9.0-13.0.
On the basis of the distribution ratio of the chemical composition of the existing UNS N06625 alloy, the proportion of C and Ti elements is adjusted, the content of C element is reduced to 0.03-0.04%, and Ti/C is 9.0-13.0. Forming the optimized component proportion.
The high-performance bar of the nuclear-grade nickel-based alloy has the Ti content of 0.27-0.52 percent. More preferably, the Ti content is 0.36% to 0.52%.
According to the high-performance bar of the nuclear-grade nickel-based alloy, preferably, the bar has the following properties: the tensile strength at the high temperature of 750 ℃ is more than or equal to 530MPa, the yield strength is more than or equal to 250MPa, and the elongation is more than or equal to 90 percent.
According to the high-performance bar of the nuclear-grade nickel-based alloy, the bar is further extrapolated by 10 at 750 DEG C5The hour endurance strength is more than or equal to 90 MPa. The impact energy at room temperature of 750 ℃ aged for 5000 hours is more than or equal to 45J.
The invention also discloses application of the nuclear-grade nickel-based alloy high-performance bar in a high-temperature gas cooled reactor nuclear power station component. The temperature of helium at the inlet of a steam generator in a high-temperature gas cooled reactor nuclear power station is up to 750 ℃, so that the long-term working temperature of parts in a steam generator inlet chamber and a heat exchange assembly is up to 750 ℃, the manufacturing of the parts has higher requirements on the room temperature performance, 750 ℃ instantaneous performance and 750 ℃ long-term lasting performance of materials, and the bar disclosed by the invention can meet the requirements.
The technical principle of the invention is as follows:
1. the long-term service temperature of the high-temperature gas-cooled reactor is 750 ℃, which is in the sensitization temperature range of UNS N06625. When the temperature is kept for a long time, a large amount of secondary carbides are precipitated from grain boundaries, and the carbides cause embrittlement of the grain boundaries, so that the service life of the alloy is shortened. The Ti element in the alloy has strong affinity with the C, more stable high-temperature primary TiC is formed in the structure by regulating the proportion of the C element to the Ti element, and the precipitation of the C element in a grain boundary is reduced, so that the precipitation of secondary carbide when the alloy is used at the high temperature of 750 ℃ for a long time is avoided, the binding force of the grain boundary is improved, and the lasting life of the alloy is prolonged.
2. 625 alloy contains a large amount of Nb and Mo easy segregation elements, and during solidification, a brittle intermetallic laves phase of 1100-1120 ℃ low-temperature eutectic can be formed in an as-cast structure, and meanwhile, micro segregation of Nb and Mo can be formed. On one hand, the intermetallic laves phase of the low-temperature eutectic can be partially dissolved in the subsequent high-temperature forging, and can be solidified into a crack source after the forging, so that the alloy can be broken when being used at high temperature for a long time, and the lasting life of the alloy is shortened. On the other hand, micro-segregation of Nb and Mo causes structural unevenness, thereby reducing the alloy life. Therefore, there is a need to improve the longevity of alloys by eliminating these brittle intermetallic laves phases and microsegregation by reasonable high temperature diffusion methods.
3. As is known, the size and uniformity of grain size have important influence on the high-temperature endurance life of the alloy, and the grain size is generally considered to be within the range of 3-5 grade, so that the short-time strength of the alloy can be ensured, and the alloy has better endurance life. Under the condition of a certain component proportion, the main factors influencing the grain size of the alloy are deformation, temperature and a final heat treatment system. Based on this, controlling the amount of deformation, temperature and final heat treatment regime in bar manufacturing is critical to obtaining a reasonable grain size structure.
The invention has the following beneficial effects:
on the basis of the unchanged chemical composition system of the existing UNS N06625 alloy, the invention effectively improves the UNS N06625 alloy by optimizing and adjusting the proportioning of C and Ti elements, simultaneously adopting a graded high-temperature diffusion, quick forging and finish forging composite forging method and heat treatment of finished bars and four organically integrated matching processesThe high-temperature performance, especially the long-term durability, of the gold bar meets the following requirements: the tensile strength at high temperature of 750 ℃ is more than or equal to 530MPa, the yield strength is more than or equal to 250MPa, the elongation is more than or equal to 90 percent, and particularly the extrapolation rate is 10 percent at 750 DEG C5The hour endurance strength is more than or equal to 90MPa, and the impact energy at room temperature of long-term aging (5000 hours) at 750 ℃ is more than or equal to 45J.
The use of the alloy in a high-temperature long-term environment at 750 ℃ is widened, and the alloy is particularly suitable for manufacturing high-temperature components of a high-temperature gas cooled reactor steam generator.
Drawings
FIG. 1 is a comparison of room temperature impact toughness after extended use at elevated temperatures for pre-and post-optimized bars of the present invention.
Detailed Description
Example 1
The method for manufacturing the nuclear-grade nickel-based alloy high-performance bar comprises the following steps:
step 1: adopting a vacuum induction and electroslag remelting mode to smelt steel ingots, wherein the components meet the optimized components, and the weight percentage of the chemical components is C: 0.03%, P is less than or equal to 0.010%, S is less than or equal to 0.010%, Cr: 20.0-23.0%, Ni is more than or equal to 58.0%, Mo: 8.5-9.5%, Nb: 3.3-3.8%, Al: 0.35 to 0.50%, 9.0% Ti/C, and the balance unavoidable impurities. The diameter of the steel ingot is 510 mm.
Step 2: and carrying out long-time homogenization treatment on the cast ingot by adopting a graded high-temperature diffusion method. The grading high-temperature diffusion process comprises the following steps: first-stage high-temperature diffusion temperature: the temperature is 1120 ℃, and the heat preservation time is 25.5 h. Then directly heating to the second stage at 1230 ℃, and keeping the temperature for 51 h.
And step 3: and (3) performing composite forging of quick forging and finish forging. Heating the steel ingot after high-temperature diffusion to 1200 ℃ in a heating furnace, forging the steel ingot to a 390mm octagonal shape on a quick forging press once, then heating the steel ingot to 1200 ℃ in the furnace, forging the steel ingot on a finish forging machine twice to a finished bar with the diameter of 240mm, wherein the finish forging temperature is 1000 ℃, and then rapidly cooling the steel ingot by water.
And 4, step 4: carrying out heat treatment on the finished bar, wherein the heat treatment temperature is 1140 ℃, and the heat preservation time is as follows: 84min, then rapidly water-cooling.
And (3) performing 750 ℃ high-temperature mechanical property test on the finished forged rod after heat treatment: tensile strength: 560MPa, yield strength: 260MPa, elongation: 98%, extrapolated 105 hour endurance at 750 ℃: 95MPa, long-term aging (5000 hours) at 750 ℃ and impact energy at room temperature: 58J.
Example 2
The method for manufacturing the nuclear-grade nickel-based alloy high-performance bar comprises the following steps:
step 1: adopting a vacuum induction and electroslag remelting mode to smelt steel ingots, wherein the components meet the optimized components, and the weight percentage of the chemical components is C: 0.04%, P is less than or equal to 0.010%, S is less than or equal to 0.010%, Cr: 20.0-23.0%, Ni is more than or equal to 58.0%, Mo: 8.5-9.5%, Nb: 3.3-3.8%, Al: 0.35 to 0.50%, 13.0% Ti/C, and the balance unavoidable impurities. The diameter of the steel ingot is 510 mm.
Step 2: and carrying out long-time homogenization treatment on the cast ingot by adopting a graded high-temperature diffusion method. The grading high-temperature diffusion process comprises the following steps: first-stage high-temperature diffusion temperature: the temperature is 1120 ℃, and the heat preservation time is 25.5 h. Then directly heating to the second stage at 1230 ℃, and keeping the temperature for 51 h.
And step 3: and (3) performing composite forging of quick forging and finish forging. Heating the steel ingot after high-temperature diffusion to 1210 ℃ in a heating furnace, forging the steel ingot to a 250mm octagonal shape in one step on a quick forging press, then heating the steel ingot to 1210 ℃ in the furnace, forging the steel ingot in three steps on a finish forging machine to obtain a finished bar with the diameter of 110mm, wherein the finish forging temperature is 1050 ℃, and then rapidly cooling the steel ingot by water.
And 4, step 4: carrying out heat treatment on the finished bar, wherein the heat treatment temperature is 1160 ℃, and the heat preservation time is as follows: 27.5min, then rapidly water-cooled.
And (3) performing 750 ℃ high-temperature mechanical property test on the finished forged rod after heat treatment: tensile strength: 565MPa, yield strength: 265MPa, elongation: 98%, extrapolated 105 hour endurance at 750 ℃: 94MPa, long-term aging (5000 hours) at 750 ℃ and impact energy at room temperature: 60J.
Example 3
The method for manufacturing the nuclear-grade nickel-based alloy high-performance bar comprises the following steps:
step 1: adopting a vacuum induction and electroslag remelting mode to smelt steel ingots, wherein the components meet the optimized components, and the weight percentage of the chemical components is C: 0.035%, P is less than or equal to 0.010%, S is less than or equal to 0.010%, Cr: 20.0-23.0%, Ni is more than or equal to 58.0%, Mo: 8.5-9.5%, Nb: 3.3-3.8%, Al: 0.35 to 0.50%, Ti/C of 11.0, and the balance being unavoidable impurities. The diameter of the steel ingot is 660 mm.
Step 2: and carrying out long-time homogenization treatment on the cast ingot by adopting a graded high-temperature diffusion method. The grading high-temperature diffusion process comprises the following steps: first-stage high-temperature diffusion temperature: 1120 ℃ and the heat preservation time is 33 h. Then directly heating to the second stage at 1230 ℃, and keeping the temperature for 66 h.
And step 3: and (3) performing composite forging of quick forging and finish forging. Heating the steel ingot after high-temperature diffusion to 1230 ℃ in a heating furnace, forging to 480mm octagonal in one step on a quick forging press, then heating to 1200 ℃ in the furnace, forging for the second time on a finish forging machine, forging finished bars with the diameter of 300mm in 2 passes, and then rapidly cooling by water.
And 4, step 4: carrying out heat treatment on the finished bar, wherein the heat treatment temperature is 1150 ℃, and the heat preservation time is as follows: 90min, then rapidly water-cooling.
And (3) performing 750 ℃ high-temperature mechanical property test on the finished forged rod after heat treatment: tensile strength: 570MPa, yield strength: 270MPa, elongation: 95%, extrapolated 105 hours permanent strength at 750 ℃: impact work at room temperature of 96MPa and 750 ℃ long-term aging (5000 hours): 61.
the invention effectively improves the high-temperature performance, especially the long-term durability, of the UNS N06625 alloy bar by optimizing and adjusting the proportion of C and Ti elements and simultaneously adopting a graded high-temperature diffusion, quick forging and finish forging composite forging method and the heat treatment of the finished bar.

Claims (10)

1. A manufacturing method of a nuclear-grade nickel-based alloy high-performance bar comprises high-temperature diffusion annealing and forging, and is characterized in that: the method comprises the following steps:
a. graded high temperature diffusion annealing: first-stage high-temperature diffusion temperature: 1110 ℃ -1130 ℃, heat preservation time: d is multiplied by (0.03-0.05) h/mm, and D is the diameter of the steel ingot; then directly heating to the second stage at 1200-1250 ℃, and keeping the temperature for: d is multiplied by (0.08-0.10) h/mm, and D is the diameter of the steel ingot;
b. the forging adopts a composite forging method of quick forging and precision forging; firstly, adopting rapid forging cogging, controlling pass deformation amount to be 40-60% and forging temperature to be 1200-1230 ℃; secondly, forging by adopting a precision forging rapid forging method, controlling the pass deformation to be 30-40%, gradually forging the finished bar material, and rapidly cooling by water after the final forging temperature is 1000-1050 ℃;
c. performing heat treatment on the finished bar, wherein the heat treatment temperature is 1140-: d x (0.25-0.35) min/mm, D being the diameter of the bar, followed by rapid water cooling.
2. The method for manufacturing the high-performance bar of the nuclear-grade nickel-based alloy according to claim 1, wherein the method comprises the following steps: the high-temperature diffusion temperature of the first stage in the step a is 1115-1125 ℃, and the heat preservation time is Dx (0.04-0.05) h/mm.
3. The method for manufacturing the high-performance bar of the nuclear-grade nickel-based alloy according to claim 1, wherein the method comprises the following steps: the second-stage high-temperature diffusion temperature in the step a is 1225-1235 ℃, and the heat preservation time Dx (0.09-0.10) h/mm.
4. The method for manufacturing the high-performance bar of the nuclear-grade nickel-based alloy according to claim 1, wherein the method comprises the following steps: and the cooling mode of the step b is water cooling.
5. The method for manufacturing the high-performance bar of the nuclear-grade nickel-based alloy according to claim 1, wherein the method comprises the following steps: and c, cooling by water.
6. The nuclear grade nickel-based alloy high-performance bar prepared by the method of claim 1, which is characterized in that:
the weight percentage of the chemical components is as follows: 0.03-0.04%, P is less than or equal to 0.010%, S is less than or equal to 0.010%, Cr: 20.0-23.0%, Ni is more than or equal to 58.0%, Mo: 8.5-9.5%, Nb: 3.3-3.8%, Al: 0.35-0.50%, and the balance of inevitable impurities; and Ti/C is 9.0-13.0.
7. The nuclear grade nickel-based alloy high-performance bar according to claim 6, wherein: the properties of the bar are as follows: the tensile strength at the high temperature of 750 ℃ is more than or equal to 530MPa, the yield strength is more than or equal to 250MPa, and the elongation is more than or equal to 90 percent.
8. The nuclear grade nickel-based alloy high-performance bar according to claim 7, wherein: the bars were extrapolated 10 at 750 ℃5The hour endurance strength is more than or equal to 90 MPa.
9. The nuclear grade nickel-based alloy high-performance bar according to claim 7, wherein: the impact energy at room temperature of 750 ℃ aged for 5000 hours is more than or equal to 45J.
10. Use of the nuclear grade nickel base alloy high performance rod of claim 6 in a high temperature gas cooled reactor nuclear power plant component.
CN202010718980.4A 2020-07-23 2020-07-23 Manufacturing method of nuclear-grade nickel-based alloy high-performance bar, bar and application Active CN113969380B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202010718980.4A CN113969380B (en) 2020-07-23 2020-07-23 Manufacturing method of nuclear-grade nickel-based alloy high-performance bar, bar and application

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202010718980.4A CN113969380B (en) 2020-07-23 2020-07-23 Manufacturing method of nuclear-grade nickel-based alloy high-performance bar, bar and application

Publications (2)

Publication Number Publication Date
CN113969380A true CN113969380A (en) 2022-01-25
CN113969380B CN113969380B (en) 2022-07-15

Family

ID=79585418

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202010718980.4A Active CN113969380B (en) 2020-07-23 2020-07-23 Manufacturing method of nuclear-grade nickel-based alloy high-performance bar, bar and application

Country Status (1)

Country Link
CN (1) CN113969380B (en)

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0953653A1 (en) * 1998-04-20 1999-11-03 Crucible Materials Corporation Method for producing forged iron-nickel-base superalloys
US20020053376A1 (en) * 2000-09-13 2002-05-09 Hitachi Metals, Ltd. Manufacturing process of nickel-based alloy having improved high temperature sulfidation-corrosion resistance
WO2010023210A1 (en) * 2008-08-26 2010-03-04 Aubert & Duval Process for preparing a nickel-based superalloy part and part thus prepared
CN103695826A (en) * 2013-12-20 2014-04-02 钢铁研究总院 Fine-grain forging method for large-size GH690 nickel-based alloy bar billet
CN105925849A (en) * 2016-05-04 2016-09-07 中国第重型机械股份公司 Control method for nickel-based alloy forgings for 700-DEG C ultra-supercritical steam turbine rotor
CN109280788A (en) * 2018-11-28 2019-01-29 陕西宝锐金属有限公司 A kind of technique preventing GH625 alloy pipe weld stress corrosion cracking
CN110747418A (en) * 2019-12-05 2020-02-04 北京钢研高纳科技股份有限公司 GH4738 alloy, homogenizing method thereof, turbine disc forging and gas turbine
CN110952053A (en) * 2019-12-20 2020-04-03 南京工程学院 Short-flow homogenization cogging process of Nb-containing solid solution strengthened nickel-based superalloy, alloy device and application of alloy device
CN111471897A (en) * 2020-05-08 2020-07-31 华能国际电力股份有限公司 Preparation and forming process of high-strength nickel-based high-temperature alloy

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0953653A1 (en) * 1998-04-20 1999-11-03 Crucible Materials Corporation Method for producing forged iron-nickel-base superalloys
US20020053376A1 (en) * 2000-09-13 2002-05-09 Hitachi Metals, Ltd. Manufacturing process of nickel-based alloy having improved high temperature sulfidation-corrosion resistance
WO2010023210A1 (en) * 2008-08-26 2010-03-04 Aubert & Duval Process for preparing a nickel-based superalloy part and part thus prepared
CN103695826A (en) * 2013-12-20 2014-04-02 钢铁研究总院 Fine-grain forging method for large-size GH690 nickel-based alloy bar billet
CN105925849A (en) * 2016-05-04 2016-09-07 中国第重型机械股份公司 Control method for nickel-based alloy forgings for 700-DEG C ultra-supercritical steam turbine rotor
CN109280788A (en) * 2018-11-28 2019-01-29 陕西宝锐金属有限公司 A kind of technique preventing GH625 alloy pipe weld stress corrosion cracking
CN110747418A (en) * 2019-12-05 2020-02-04 北京钢研高纳科技股份有限公司 GH4738 alloy, homogenizing method thereof, turbine disc forging and gas turbine
CN110952053A (en) * 2019-12-20 2020-04-03 南京工程学院 Short-flow homogenization cogging process of Nb-containing solid solution strengthened nickel-based superalloy, alloy device and application of alloy device
CN111471897A (en) * 2020-05-08 2020-07-31 华能国际电力股份有限公司 Preparation and forming process of high-strength nickel-based high-temperature alloy

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
李红梅等: "均匀化处理对铸态GH625合金组织的影响", 《材料热处理学报》 *
欧新哲等: "固溶处理对UNSN06625合金组织和力学性能的影响", 《金属功能材料》 *

Also Published As

Publication number Publication date
CN113969380B (en) 2022-07-15

Similar Documents

Publication Publication Date Title
WO2021174726A1 (en) Nickel-based deformed high-temperature alloy having high aluminum content and preparation method therefor
CN108315599B (en) A kind of high cobalt nickel base superalloy and preparation method thereof
EP4245873A1 (en) Creep-resistant, long-service-life, nickel-based deformation superalloy and method for preparation thereof and application thereof
JP2778705B2 (en) Ni-based super heat-resistant alloy and method for producing the same
WO2020249115A1 (en) Composite-strengthened corrosion-resistant superalloy and preparation processing therefor
US6811746B2 (en) Zirconium alloy having excellent corrosion resistance and mechanical properties for nuclear fuel cladding tube
CN109136652B (en) Nickel-based alloy large-section bar for nuclear power key equipment and manufacturing method thereof
CN105821250A (en) High-strength nickel-base superalloy and manufacturing method thereof
CN104109780A (en) Nickel-based high-temperature alloy and manufacturing method thereof
CN104630597A (en) Iron-nickel-chromium-based superalloy and manufacturing method thereof
CN106636848A (en) Preparation method of abrasion-proof and corrosion-resistant nickel-based alloy wire
CN110268078A (en) High temperature resistant to damage superalloy, the product manufactured by the alloy and the method for manufacturing the alloy
CN107841657B (en) High-strength and high-toughness Ni-Cr-Mo-based casting alloy
CN114231765A (en) Preparation method and application of high-temperature alloy bar
JP2014070230A (en) METHOD FOR PRODUCING Ni-BASED SUPERALLOY
CN111647790B (en) Preparation method and application of high-strength high-toughness iron-nickel-chromium-based heat-resistant alloy
CN114622133A (en) Heat-resistant steel for ultra-supercritical steam turbine rotor forging and preparation method thereof
CN106086581B (en) 700 DEG C of ultra supercritical unit iron nickel base alloy rotor heat treatment methods
CN111961923A (en) High-plasticity easy-processing cobalt-based wrought superalloy and preparation method thereof
CN106929710A (en) Ultra-supercritical steam turbine rotor high-strength and high ductility heat-resisting alloy and preparation method thereof
CN115354195B (en) Crack-resistant nickel-based superalloy, and preparation method and application thereof
CN113969380B (en) Manufacturing method of nuclear-grade nickel-based alloy high-performance bar, bar and application
JP2014109053A (en) Austenitic heat resistant steel and turbine component
CN1322156C (en) Titanium three-aluminum base alloy and method for preparing same
CN108330335A (en) A kind of high temperature heat-resisting and its manufacturing process

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant