CN104878248B - High temperature alloy 625H and its manufacturing process - Google Patents

High temperature alloy 625H and its manufacturing process Download PDF

Info

Publication number
CN104878248B
CN104878248B CN201510107892.XA CN201510107892A CN104878248B CN 104878248 B CN104878248 B CN 104878248B CN 201510107892 A CN201510107892 A CN 201510107892A CN 104878248 B CN104878248 B CN 104878248B
Authority
CN
China
Prior art keywords
high temperature
temperature
alloy
refining
composition
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.)
Active
Application number
CN201510107892.XA
Other languages
Chinese (zh)
Other versions
CN104878248A (en
Inventor
华大凤
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.)
Jiangsu Xinhua Alloy Co., Ltd
Original Assignee
JIANGSU XINHUA ALLOY ELECTRIC APPARATUS 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 JIANGSU XINHUA ALLOY ELECTRIC APPARATUS CO Ltd filed Critical JIANGSU XINHUA ALLOY ELECTRIC APPARATUS CO Ltd
Priority to CN201510107892.XA priority Critical patent/CN104878248B/en
Publication of CN104878248A publication Critical patent/CN104878248A/en
Application granted granted Critical
Publication of CN104878248B publication Critical patent/CN104878248B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Manufacture And Refinement Of Metals (AREA)
  • Heat Treatment Of Steel (AREA)

Abstract

The invention discloses high temperature alloy 625H, and it is formulated count by weight percentage, and concrete content composition includes:C:≤0.04%~0.05%;Si:≤0.20%;Mn:≤0.10%;P:≤0.015%;S:≤0.005%;Cr:22.50~23.00%;Ti:0.20%~0.30%;AL:0.30%~0.40%;Mo:9.50%~10.00%;Nb+Ta:3.65%~4.15%;Fe:≤0.50%;Cu:≤0.05%;Co:≤0.05%;Ni:≥60.00%.Influence of the proportionate relationship to alloy UNS N06625 between Nb, Ti, Al element is found by special chemical composition design and collocation, to reach overcritical(750℃)Environment, not less than high-temperature duration life under 178MPa more than 1000 hours.

Description

High temperature alloy 625H and its manufacturing process
Technical field
The present invention relates to high-temperature alloy material preparing technical field, is made more particularly to high temperature alloy 625H and its technique Method.
Background technology
UNS N06625 alloys are ni-base wrought superalloy, are the solution strengthening types that element is need to strengthen based on molybdenum, niobium Wrought superalloy, there is excellent corrosion resistance and inoxidizability.It is widely used in manufacture aerial motor spare part, aerospace Structure member, chemical industry equipment and nuclear power generating equipment parts etc..In order to promote nuclear industry to develop, national grinding to a variety of heap-type Hair, the material that China's forth generation nuclear power HTGR material has been selected based on UNS N06625 substantially, but in this material On the basis of propose and higher want summing target.In order to meet it at 750 DEG C, high-temperature duration life is small more than 1000 under 178MPa When technical indicator, and be able to can be reached at 750 DEG C by this research and development, high-temperature duration life is more than 100000 under 75.3MPa The technical indicator of hour.
The content of the invention
In order to overcome the above-mentioned deficiencies of the prior art, above-mentioned technical indicator is reached, the present invention is by special chemical into setting up separately Influence of the proportionate relationship to alloy UNS N06625 between Nb, Ti, Al element is found in meter and collocation, to reach overcritical(750 ℃)Environment, not less than high-temperature duration life under 178MPa more than 1000 hours.
The technical solution adopted in the present invention is:High temperature alloy 625H, it is formulated count by weight percentage, concrete content Composition includes:
C:≤0.04%~0.05% Si:≤0.20% Mn:≤0.10%
P:≤0.015% S:≤0.005% Cr:22.50~23.00%;
Ti:0.20%~0.30% AL :0.30%~0.40% Mo: 9.50%~10.00% Nb+Ta:3.65% ~4.15% Fe:≤0.50% Cu:≤0.05%
Co:≤0.05% Ni:≥60.00%.
Further, on the basis of including above-mentioned content, high temperature alloy 625H also needed to add zirconium in the later stage of melting Zr and rare earth alloy are to lift the performance of material.
A kind of technique for manufacturing above-mentioned high temperature alloy 625H, using the smelting process of vacuum metling+electroslag duplex(VIM+ ESR), i.e. the technique of vacuum induction melting (VIM)+inert atmosphere protection electroslag remelting (ESR) duplex, and by forging and heat Processing heat processing technique requirement is controlled and improved;Comprise the following steps:
A. vacuum induction furnace smelting:By above-mentioned ingredient composition, vacuum induction furnace smelting is put into;
B. electroslag refining;
C. forge:1130 DEG C of starting forging temperature, final forging temperature >=900 DEG C;
D. ultrasound detection;
E. it is heat-treated:>=1093 DEG C of solid solution+>=+700 DEG C of age-hardenings of 982 DEG C of stabilizing annealings;
F. ultrasound detection;
G. line sampling;
H. performance test:Including its composition, room temperature tensile properties, 750 DEG C of tensile properties, metallographic, 750 DEG C of high-temperature and durables Can detection;
I. car light grinding finished product.
Further, the refining temperature in the step B:1520--1560 DEG C, refining time is more than 45min, tapping temperature Spend for 1540-1580 DEG C.
Compared with prior art, the beneficial effects of the invention are as follows:Arranged in pairs or groups and controlled using suitable chemical element C, Nb, Ti, Al The value volume and range of product of its hardening constituent is made, increases solid solution element Mo, Cr, Ni constituent content, limits Fe, Cu, Co element, strictly Control S, Pb, Se, Bi, Hg constituent content, increase Zr, rare earth trace element effect;Using the smelting of vacuum metling+electroslag duplex Sweetening process(VIM+ESR)To improve steel degree of purity and degasifying effect;Control hot-working(Forging and heat treatment)Temperature come To suitable metallurgical structure.
Using new recipe configuration high temperature alloy 625H, i.e.,:C:≤0.04%~0.05%; Si:≤0.20%; Mn:≤ 0.10%; P:≤0.015%; S:≤0.005%; Cr:22.50~23.00%; Ti :0.20%~0.30%; AL :0.30%~ 0.40%; Mo: 9.50%~10.00% Nb+Ta:3.65%~4.15% Fe:≤0.50% ; Cu:≤0.05% ; Co:≤ 0.05% ; Ni:≥60.00%.And zirconium Zr and rare earth alloy are added to lift the performance of material in the melting later stage.So that it is compared Different UNS N06625 possess higher yield strength and high temperature endurance performance under 750 DEG C of high temperature.
Material of the present invention is the various parts raw material of the HTGR of forth generation nuclear power field.At present in system The evaporator and in-pile component of the high temperature gas-cooled reactor project of forth generation nuclear power are largely using the steam manufactured by UNS N06625 materials Pipe, support mandrel, container plate etc..Nuclear power as clean energy resource is that China gives priority to and promotion project, forth generation high temperature HTGR is due to its small volume, power is big, safety coefficient is high as the national emphasis studied.And in petrochemical industry, military project etc. Field can all use the material of this trade mark, be obviously improved mechanical property and high temperature endurance performance research and development 625H necessarily more added with Its popularity of the promotion of power uses.
Embodiment
In order to deepen the understanding of the present invention, with reference to embodiment, the present invention is further described, and the embodiment is only used In explaining the present invention, protection scope of the present invention is not formed and limited.
High temperature alloy 625H, it is formulated count by weight percentage, and concrete content composition includes:
C:≤0.04%~0.05% Si:≤0.20% Mn:≤0.10%
P:≤0.015% S:≤0.005% Cr:22.50~23.00%;
Ti:0.20%~0.30% AL :0.30%~0.40% Mo: 9.50%~10.00% Nb+Ta:3.65% ~4.15% Fe:≤0.50% Cu:≤0.05%
Co:≤0.05% Ni:≥60.00%.
The formula also also needs to add in the later stage of melting on the basis of including above-mentioned content in its high temperature alloy 625H Zirconium Zr and rare earth alloy are to lift the performance of material.
A kind of technique for manufacturing above-mentioned high temperature alloy 625H, using the smelting process of vacuum metling+electroslag duplex(VIM+ ESR), i.e. the technique of vacuum induction melting (VIM)+inert atmosphere protection electroslag remelting (ESR) duplex, and by forging and heat Processing heat processing technique requirement is controlled and improved;Comprise the following steps:
A. vacuum induction furnace smelting:By above-mentioned ingredient composition, vacuum induction furnace smelting is put into;
B. electroslag refining;
C. forge:1130 DEG C of starting forging temperature, final forging temperature >=900 DEG C;
D. ultrasound detection;
E. it is heat-treated:>=1093 DEG C of solid solution+>=+700 DEG C of age-hardenings of 982 DEG C of stabilizing annealings;
F. ultrasound detection;
G. line sampling;
H. performance test:Including its composition, room temperature tensile properties, 750 DEG C of tensile properties, metallographic, 750 DEG C of high-temperature and durables Can detection;
I. car light grinding finished product.
In step B, its refining temperature:1520--1560 DEG C, refining time is more than 45min, tapping temperature 1540- 1580 DEG C, there is preferable performance.
Now the principle of composition designed by 625H of the present invention is described further with effect:First, chemical composition is carried out Analysis, alloy composition contrast are shown in Table 1;
The alloy composition of table 1 contrasts
Secondly, its mechanical property is analyzed, is shown in Table 2;
Table 2 is heat-treated reference value
Combined, the performance of chemical element, analyzed by above table:
(1)The effect of carbon:Carbon forms carbide dispersion with Nb, Ti element in 625H alloys and is distributed in transgranular reinforcing work With.
(2)The effect of chromium:The key element of high temperature alloy high-temperature oxidation resistance and anti-corrosion capability, in the guarantor that high temperature is formed Oxide-film is protected mainly by Cr2O3Composition.With Cr2O3Based on oxide-film it is finer and close, tack is also stronger, it is ensured that alloy exists It is long-term use of under high temperature.
(3)The effect of silicon:Silicon produces SiO2 after high-temperature oxydation, is distributed in the interface of oxide-film and parent metal, can To prevent oxygen from penetrating into, low-alloyed oxidation rate drops.Silicon and rare earth element simultaneously in the presence of, silicon improves the effect of antioxygenic property It is more notable.Improve the compactness of oxidation-resistant film.
(4)The effect of manganese and iron:Low-alloyed antioxygenic property can drop in manganese and iron, increase oxidation rate, a small amount of manganese and sulphur Hot-short and influence of the high-temperature and durable sulphur to its retention time can be reduced by forming MnS.
(5)The effect of nickel:Nickel forms face-centered cubic lattice with other alloys, i.e. austenite lattice, high temperature is not undergone phase transition, Therefore its stability is good at high temperature.Nickel is parent in nickel base superalloy, and the characteristic of itself plays a leading role.Nickel is Ovshinsky Body element, good combination property can be provided, solid solution can be formed with chromium under the good high temperature of stability, most have comparison high Elevated temperature strength, there is high plasticity, good process industrial art performance in normal temperature.
(6)The effect of rare earth element:A small amount of rare earth is added in high temperature alloy can significantly improve the combination property of alloy, because It is separated out in grain boundaries to purify crystal boundary with oxidizing substance formation compound, and can improve intensity in crystal grain thinning.
(7)The effect of aluminium:The essential element of γ ' phases is formed, aluminium can form Ni3Al with nickel in nickel chromium triangle system high temperature alloy An important factor for phase is raising inoxidizability, and alloy high-temp intensity can be improved and improve creep rupture strength.
(8)The effect of titanium:The essential element of γ ' phases is formed, Ni3Al can be promoted to form and formed Ni3(Al, Ti), carry High γ ' phases reinforcing degree.
(9)The effect of niobium:Carbide forms NbC, crystal grain thinning.A large amount of Nb form γ ' '(Ni3Nb)It is Main hardening constituent, γ ' is dissolved on a small quantity and mutually promotes γ ' precipitations, delay growing up for γ ', improve intensity.
(10)The effect of molybdenum:Its solution strengthening effect improves heat resistance in high temperature alloy.
(11)S、 P:It is the intensity and creep rupture life of inevitable objectionable impurities elements, particularly S to material in material Influence and its seriously require its control 0.005%, a small amount of P can improve creep rupture strength.
Embodiment
Test objective:By for being not added with common the 625 of C, AL, Ti, to the 625-1 of increase AL, Ti composition, to increase C Content, and the 625-2 of Cr, Mo, Nb content is adjusted, 4 groups are devised altogether to the 625H for adjusting AL, Ti, Nb content and ratio again Implement experiment to implement;
Object:Referring to table 3, it is more than 99% simple metal material as raw material from Ni, Cr, Mo, Nb, Mn, AL, Ti, Zr content Manufactured, remaining element controls in proportion;
Making step:Completed by above-mentioned A to I steps, i.e., according to 4 groups of embodiment design ingredient compositions of the present invention, vacuum sense Stove is answered to smelt(Refining temperature:1520--1560℃;Refining time:More than 45 minutes, 1540--1580 DEG C of tapping temperature)→ electricity Slag refining → forging(1130 DEG C of starting forging temperature, final forging temperature >=900 DEG C)→ ultrasound detection → heat treatment(1140 DEG C of solid solutions+990 DEG C+700 DEG C of age-hardenings of stabilizing annealing)→ ultrasound detection → line sampling → performance test(Composition, room temperature tensile, 750 DEG C Stretching, metallographic, 750 DEG C of high-temperature and durables)→ car light grinds finished product;
Table 3 is embodied composition and carries out its preparing materials
Mechanics Performance Testing:Require that ASME SB-446 requirements have carried out mechanical property to this four groups of samples respectively according to American Standard It can test, test result is as shown in table 4:
4 four groups of mechanical property contrasts of table
Raising alloy strength that can be different degrees of by increasing alloying element, but improve intensity unobvious.It is but logical Cross increase AL, Ti content and control Al:Ti content=1:1, increase Nb content form NbC and promote γ ' mutually to separate out and can significantly change Kind 750 DEG C yield strength, and its elongation will remote super other alloying component collocation.Certainly, this and final heat treatment It is related.+ 700 DEG C of age-hardenings of+990 DEG C of stabilizing annealings are dissolved by rational 1140 DEG C of heat treatment temperature, be dissolved+ Stabilizing annealing can allow the composition of alloy and precipitated phase to be uniformly distributed elimination harmful phase, and 700 DEG C of timeliness promotes a small amount of γ ' phases Separate out and improve alloy yield strength at 750 DEG C.
Grain size detects:As shown in table 5;
5 four groups of grain size contrasts of table
As can be seen from Table 5, be dissolved in same heat treatment temperature+Stabilizing Heat Treatment when, the high crystal grain of carbon content Grow up slower, grain size≤5.0 grade should be controlled as requested.
Duration running detects:It is shown in Table 6;
The duration running of table 6 contrasts
It is raw from table 3 to table 6 as can be seen that by composition collocation reasonable in design by a series of excellent processing technologys The 625H alloys that output is come can reach overcritical under suitable heat treatment process system(750℃), high temperature is held under 178MPa The long life-span was more than 1000 hours.The alloy of this composition mainly obtains suitable metallographic structure by composition collocation and production technology (4.0-5.0 level grain sizes, increase hardening constituent and precipitated phase), yield strength and elongation under 750 DEG C of environment are improved, so as to Reach requirement of the high-temperature duration life more than 1000 hours under 178MPa.It is thus the HTGR of forth generation nuclear power field Various parts high-quality raw material are provided, and more high-quality guarantee will be provided in civilian goods high temperature alloy field.
Using a kind of novel high-temperature alloy 625H designed by the present invention, the High Temperature Gas of forth generation nuclear power field disclosure satisfy that The high temperature endurance performance requirement of the exotic material of cold dome is overcritical(750℃), high-temperature duration life exceedes under 178MPa 1000 hours.
What embodiments of the invention were announced is preferred embodiment, but is not limited thereto, the ordinary skill people of this area Member, easily according to above-described embodiment, understand the spirit of the present invention, and make different amplification and change, but as long as not departing from this The spirit of invention, all within the scope of the present invention.

Claims (1)

1. high temperature alloy 625H, it is formulated count by weight percentage, and concrete content composition includes:
C:≤0.04%~0.05% Si:≤0.20% Mn:≤0.10%
P:≤0.015% S:≤0.005% Cr:22.50~23.00%;
Ti:0.20%~0.30% AL :0.30%~0.40% Mo: 9.50%~10.00% Nb+Ta:3.65%~ 4.15% Fe:≤0.50% Cu:≤0.05%
Co:≤0.05% Ni:≥60.00%;On the basis of including above-mentioned content, high temperature alloy 625H is molten In the later stage of refining, also need to add zirconium Zr and rare earth alloy to lift the performance of material;
High temperature alloy 625H technique, using the smelting process ESR of vacuum metling VIM+electroslag duplex, wherein VIM is vacuum sense Answer melting, ESR is inert atmosphere protection electroslag remelting, and by forge and be heat-treated heat processing technique requirement be controlled and Improve;Comprise the following steps:
A. vacuum induction furnace smelting:By above-mentioned ingredient composition, vacuum induction furnace smelting is put into;
B. electroslag refining, refining temperature:1520--1560 DEG C, refining time is more than 45min, and tapping temperature is 1540-1580 DEG C;
C. forge:1130 DEG C of starting forging temperature, final forging temperature >=900 DEG C;
D. ultrasound detection;
E. it is heat-treated:>=1093 DEG C of solid solution+>=+700 DEG C of age-hardenings of 982 DEG C of stabilizing annealings;
F. ultrasound detection;
G. line sampling;
H. performance test:Including its composition, room temperature tensile properties, 750 DEG C of tensile properties, metallographic, 750 DEG C of high temperature endurance performance inspections Survey;
I. car light grinding finished product.
CN201510107892.XA 2015-03-12 2015-03-12 High temperature alloy 625H and its manufacturing process Active CN104878248B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510107892.XA CN104878248B (en) 2015-03-12 2015-03-12 High temperature alloy 625H and its manufacturing process

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510107892.XA CN104878248B (en) 2015-03-12 2015-03-12 High temperature alloy 625H and its manufacturing process

Publications (2)

Publication Number Publication Date
CN104878248A CN104878248A (en) 2015-09-02
CN104878248B true CN104878248B (en) 2017-12-01

Family

ID=53945918

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201510107892.XA Active CN104878248B (en) 2015-03-12 2015-03-12 High temperature alloy 625H and its manufacturing process

Country Status (1)

Country Link
CN (1) CN104878248B (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107841657B (en) * 2017-09-30 2020-03-31 中国科学院金属研究所 High-strength and high-toughness Ni-Cr-Mo-based casting alloy
CN110453164B (en) * 2019-08-14 2020-12-22 河北工业大学 Processing method for enhancing oxidation resistance of forged Ni-Cr-Co-based alloy
CN111139414B (en) * 2019-11-27 2021-09-07 北京钢研高纳科技股份有限公司 Stabilizing treatment process of precipitation hardening type nickel-based high-temperature alloy
CN112941370B (en) * 2019-12-10 2022-11-01 中国科学院金属研究所 Method for controlling delta phase precipitation in Nb-containing nickel-based superalloy
CN112176223B (en) * 2020-09-03 2022-01-28 太原钢铁(集团)有限公司 Method for controlling performance of nickel-based alloy wire
CN113584331A (en) * 2021-06-30 2021-11-02 江西恒大高新技术股份有限公司 Preparation method of aluminum-doped Inconel625 alloy applied to oxygen-containing high-temperature chlorine corrosion environment
CN113584381B (en) * 2021-07-05 2023-03-07 重庆材料研究院有限公司 High-strength copper-containing Ni-Fe-Cr-based age-hardening corrosion-resistant alloy and electroslag remelting method thereof
CN115233012B (en) * 2022-07-19 2023-08-11 山西太钢不锈钢股份有限公司 Manufacturing method of nickel-based superalloy hot rolled plate
CN115369289B (en) * 2022-08-29 2024-02-09 江西宝顺昌特种合金制造有限公司 Inconel625 forging for underwater flowmeter and preparation method thereof

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104233001B (en) * 2013-06-08 2016-08-24 上海丰渠特种合金有限公司 A kind of UNS N06625 high temperature alloy and preparation method thereof
CN103316949A (en) * 2013-06-25 2013-09-25 浙江国邦钢业有限公司 Corrosion-resistant alloy tube manufacturing process and corrosion-resistant alloy seamless steel tube
CN103484803A (en) * 2013-10-12 2014-01-01 钢铁研究总院 Processing technique of nickel-based heat-resisting alloy boiler pipe

Also Published As

Publication number Publication date
CN104878248A (en) 2015-09-02

Similar Documents

Publication Publication Date Title
CN104878248B (en) High temperature alloy 625H and its manufacturing process
CN108315599B (en) A kind of high cobalt nickel base superalloy and preparation method thereof
WO2018151222A1 (en) Ni-BASED HEAT-RESISTANT ALLOY AND METHOD FOR MANUFACTURING SAME
CN102628127A (en) High-strength corrosion-resisting nickel base alloy and manufacturing method thereof
CN111876653A (en) Preparation method of pure austenitic stainless steel
CN105821250A (en) High-strength nickel-base superalloy and manufacturing method thereof
CN109136652B (en) Nickel-based alloy large-section bar for nuclear power key equipment and manufacturing method thereof
CN104789815A (en) High-resistant chromium-nickel electric heating alloy and preparation process thereof
CN104532097A (en) High-strength high-corrosion-resistant nickel-based high-temperature alloy and solution and aging heat treatment method thereof
CN114196854B (en) High-strength and difficult-to-deform nickel-based high-temperature alloy and preparation method thereof
CN104630597A (en) Iron-nickel-chromium-based superalloy and manufacturing method thereof
CN111057937A (en) Electrothermal alloy iron-chromium-aluminum wire material and preparation method thereof
CN102041450A (en) Ferrite heat resisting steel and manufacture method thereof
CN111118348A (en) Preparation method of electrothermal alloy nickel-chromium wire
CN101654764A (en) Iron-nickel based highly elastic alloy, capillary pipe thereof and method for manufacturing capillary pipe
CN105238957A (en) High-property nickel-base superalloy and production method thereof
CN108193144B (en) High-strength spring wire with high elastic modulus and preparation method thereof
CN114231765A (en) Preparation method and application of high-temperature alloy bar
CN110106397B (en) High-temperature-resistant bolt alloy material and manufacturing method of bolt
EP4276209A1 (en) High-aluminum austenitic alloy having excellent high-temperature anticorrosion capabilities and creep resistance
WO2017056674A1 (en) Low thermal expansion super-heat-resistant alloy and method for producing same
CN111394663A (en) Heat-resistant iron-based alloy and preparation method thereof
CN103469051A (en) Duplex stainless steel master alloy and preparation method thereof
CN113088761B (en) Ultrahigh-strength corrosion-resistant alloy and manufacturing method thereof
CN112410517B (en) Method for eliminating delta ferrite in austenitic stainless steel

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
EXSB Decision made by sipo to initiate substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant
CP01 Change in the name or title of a patent holder

Address after: 225700, No. 19, Zhang Guo Town, Xinghua, Jiangsu, Taizhou

Patentee after: Jiangsu Xinhua Alloy Co., Ltd

Address before: 225700, No. 19, Zhang Guo Town, Xinghua, Jiangsu, Taizhou

Patentee before: Jiangsu Xinhua Alloy Electric Apparatus Co., Ltd.

CP01 Change in the name or title of a patent holder