CN103695721B - A kind of high strength, nickel based Alloy And Preparation Method - Google Patents
A kind of high strength, nickel based Alloy And Preparation Method Download PDFInfo
- Publication number
- CN103695721B CN103695721B CN201410018657.0A CN201410018657A CN103695721B CN 103695721 B CN103695721 B CN 103695721B CN 201410018657 A CN201410018657 A CN 201410018657A CN 103695721 B CN103695721 B CN 103695721B
- Authority
- CN
- China
- Prior art keywords
- high strength
- based alloy
- nickel based
- insulation
- 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.)
- Active
Links
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 title claims abstract description 93
- 239000000956 alloy Substances 0.000 title claims abstract description 60
- 229910045601 alloy Inorganic materials 0.000 title claims abstract description 59
- 229910052759 nickel Inorganic materials 0.000 title claims abstract description 45
- 238000002360 preparation method Methods 0.000 title claims abstract description 12
- 239000000203 mixture Substances 0.000 claims abstract description 13
- 239000000126 substance Substances 0.000 claims abstract description 10
- 239000012535 impurity Substances 0.000 claims abstract description 8
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 7
- 229910052802 copper Inorganic materials 0.000 claims abstract description 7
- 229910052742 iron Inorganic materials 0.000 claims abstract description 7
- 229910052748 manganese Inorganic materials 0.000 claims abstract description 7
- 229910052750 molybdenum Inorganic materials 0.000 claims abstract description 7
- 229910052758 niobium Inorganic materials 0.000 claims abstract description 7
- 229910052715 tantalum Inorganic materials 0.000 claims abstract description 7
- 238000009413 insulation Methods 0.000 claims description 24
- 238000001816 cooling Methods 0.000 claims description 18
- 238000005728 strengthening Methods 0.000 claims description 10
- 238000002844 melting Methods 0.000 claims description 9
- 230000008018 melting Effects 0.000 claims description 9
- 239000000463 material Substances 0.000 claims description 7
- 230000032683 aging Effects 0.000 claims description 6
- 238000005096 rolling process Methods 0.000 claims description 6
- 229910052782 aluminium Inorganic materials 0.000 claims description 5
- 238000005516 engineering process Methods 0.000 claims description 4
- 229910052684 Cerium Inorganic materials 0.000 claims description 3
- 229910001122 Mischmetal Inorganic materials 0.000 claims description 3
- 241001417490 Sillaginidae Species 0.000 claims description 3
- 238000003723 Smelting Methods 0.000 claims description 3
- GWXLDORMOJMVQZ-UHFFFAOYSA-N cerium Chemical group [Ce] GWXLDORMOJMVQZ-UHFFFAOYSA-N 0.000 claims description 3
- 238000005242 forging Methods 0.000 claims description 3
- 230000006698 induction Effects 0.000 claims description 3
- 229910052751 metal Inorganic materials 0.000 claims description 3
- 239000002184 metal Substances 0.000 claims description 3
- 239000002994 raw material Substances 0.000 claims description 3
- 238000005266 casting Methods 0.000 claims description 2
- 229910052761 rare earth metal Inorganic materials 0.000 claims description 2
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 238000007751 thermal spraying Methods 0.000 description 2
- 238000011282 treatment Methods 0.000 description 2
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- 239000004411 aluminium Substances 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910000963 austenitic stainless steel Inorganic materials 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000000265 homogenisation Methods 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 238000007669 thermal treatment Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
- 229910052727 yttrium Inorganic materials 0.000 description 1
Landscapes
- Manufacture And Refinement Of Metals (AREA)
Abstract
The present invention relates to a kind of high strength, nickel based alloy, its chemical composition contains by weight percentage: Al:3.2 ~ 6.8%, Cr:21 ~ 28%, B:3.0 ~ 4.2%, Si:1.2 ~ 1.9%, C:0.08 ~ 0.2%, Mo:1.8 ~ 2.8%, Nb:1.2 ~ 2.1%, Ta:1.0 ~ 1.8%, Ti:0.08 ~ 0.98%, Fe:3.2 ~ 5.8%, RE:0.2 ~ 0.38%, Cu:0.8 ~ 1.2%, Mn:0.002 ~ 0.08%, surplus is Ni and inevitable impurity; What by the collocation of specific alloy and preparation method, described high strength, nickel based alloy obtained that specific microtexture makes this high strength, nickel based alloy has good intensity and toughness, and has good high-temperature behavior.
Description
Technical field
The invention belongs to field of alloy material, particularly relate to a kind of high strength, nickel based Alloy And Preparation Method.
Background technology
In current industrial circle, there is the severe environmental conditions such as a large amount of abrasion and corrosions, for the requirement of machine work under adaptation extreme operating environments, often need to carry out thermal spraying treatment to the surface of component, nickel-base alloy is widely used in the thermal spraying material of piece surface owing to having good wear resistance and corrosion resistance, but in actual applications, it also has very high requirement to intensity, but when intensity improves, often to have an impact to toughness.
China Patent No. 98116301 is that a kind of applicable manufacture is for welding the nickel-base alloy wiry of super duplex or super austenitic stainless steel, point out that composition is 24.5% < Cr≤26.5%, 13.5≤Mo≤16.5%, the impurity that surplus is nickel, one or more optional assistant alloy compositions and technique are brought into, this assistant alloy composition is selected from nitrogen, aluminium and magnesium, and the electrode manufactured thus.But same, when its intensity improves, high-temperature behavior is unsatisfactory, and toughness can not meet day by day various application.
Summary of the invention
An object of the present invention is to propose a kind of high strength, nickel based alloy;
Two of object of the present invention is the preparation method proposing a kind of high strength, nickel based alloy;
For reaching this object, the present invention by the following technical solutions:
A kind of high strength, nickel based alloy, its chemical composition contains by weight percentage: Al:3.2 ~ 6.8%, Cr:21 ~ 28%, B:3.0 ~ 4.2%, Si:1.2 ~ 1.9%, C:0.08 ~ 0.2%, Mo:1.8 ~ 2.8%, Nb:1.2 ~ 2.1%, Ta:1.0 ~ 1.8%, Ti:0.08 ~ 0.98%, Fe:3.2 ~ 5.8%, RE:0.2 ~ 0.38%, Cu:0.8 ~ 1.2%, Mn:0.002 ~ 0.08%, surplus is Ni and inevitable impurity;
In the microtexture of described high strength, nickel based alloy, the area percentage of γ sosoloid shared by each cross section of alloy is 1.2 ~ 2.8%, Ni
3the area percentage of Al phase shared by each cross section of alloy is 0.8 ~ 1.1%, Ni
3the area percentage of (Al, Ti) strengthening phase shared by each cross section of alloy is 0.58 ~ 1.25%, γ ' (Ni
3al) area percentage mutually in the alloy shared by heart cross section is 0.02 ~ 0.032%;
The yield strength of described high strength, nickel based alloy is 560 ~ 610MPa, tensile strength 780 ~ 820MPa, unit elongation 42 ~ 51%, the impelling strength 98 ~ 102J/cm of 20 DEG C
2.
As preferably, the chemical composition of described high strength, nickel based alloy contains by weight percentage: Al:4.8%, Cr:26%, B:3.8%, Si:1.6%, C:0.18%, Mo:2.28%, Nb:1.91%, Ta:1.7%, Ti:0.28%, Fe:4.8%, RE:0.28%, Cu:0.98%, Mn:0.006%, surplus is Ni and inevitable impurity.
As preferably, described RE is rare earth element y.
As preferably, described RE is cerium-rich mischmetal.
A preparation method for high strength, nickel based alloy, is characterized in that, comprises the steps:
(1) melting, gets the raw materials ready according to the chemical composition of aforementioned high strength, nickel based alloy, adopts vacuum induction, the associating smelting technology of esr and vacuum consumable remelting smelts;
(2) cast, the molten metal that melting obtains is cast;
(3) forge, carry out conventional die forging;
(4) homogenizing, the homogenizing of first stage is carried out at 1120 ~ 1160 DEG C of insulation 15 ~ 22h, and then being warmed up to 1180 ~ 1190 DEG C, insulation 20 ~ 25h carries out the homogenizing of subordinate phase, and then cools to the homogenizing that 1120 ~ 1160 DEG C of insulation 18 ~ 24h carry out the phase III;
(5) ausrolling, rolling temperature is 980 ~ 1030 DEG C, and rolling pass is 5 ~ 8;
(6) aging strengthening model, carries out three step aging strengthening model by the rolled plate that step (5) obtains, and the first step is at 710 ~ 720 DEG C of insulation 6 ~ 8h, after cooling to 610 ~ 620 DEG C with the furnace with 50 ~ 60 DEG C/h subsequently, and insulation 7 ~ 9h, air cooling is to room temperature; Second step is for being heated to 660 ~ 680 DEG C of insulation 5 ~ 7h by sheet material, after cooling to 580 ~ 600 DEG C with the furnace with 55 ~ 65 DEG C/h subsequently, be incubated 5 ~ 7h, air cooling is to room temperature; 3rd step is for being heated to 600 ~ 620 DEG C of insulation 6 ~ 8h by sheet material, after cooling to 550 ~ 570 DEG C with the furnace with 45 ~ 55 DEG C/h subsequently, insulation 5 ~ 7h, air cooling, to room temperature, obtains high strength, nickel based alloy.
As preferably, the pouring temperature of described casting is 1380 ~ 1420 DEG C.
As preferably, the temperature of described melting is 1610 ~ 1720 DEG C.
effect of the present invention is:
Arranged in pairs or groups by content element being carried out to selection and concrete element, alloy property is increased dramatically;
By specific preparation method, especially specific timeliness and Homogenization Treatments, make the microtexture in alloy have reasonable layout, and not only intensity is largely increased, and toughness is also better improved;
By coordinating of concrete preparation method's thermal treatment and concrete alloying constituent and content, make microtexture obtain reasonable layout, high-temperature behavior is also largely increased.
Embodiment
embodiment 1
A kind of high strength, nickel based alloy, its chemical composition contains by weight percentage: Al:5.8%, Cr:27%, B:3.0 ~ 4.2%, Si:1.8%, C:0.18%, Mo:1.9%, Nb:1.9%, Ta:1.6%, Ti:0.71%, Fe:4.8%, Y:0.28%, Cu:0.8%, Mn:0.06%, surplus is Ni and inevitable impurity;
In the microtexture of described high strength, nickel based alloy, the area percentage of γ sosoloid shared by each cross section of alloy is 1.8%, Ni
3the area percentage of Al phase shared by each cross section of alloy is 0.98%, Ni
3the area percentage of (Al, Ti) strengthening phase shared by each cross section of alloy is 1.05%, γ ' (Ni
3al) area percentage mutually in the alloy shared by heart cross section is 0.03%;
The yield strength of described high strength, nickel based alloy is 580MPa, tensile strength 790MPa, unit elongation 46%, the impelling strength 99J/cm of 20 DEG C
2.
embodiment 2:
A kind of high strength, nickel based alloy, its chemical composition contains by weight percentage: Al:4.8%, Cr:26%, B:3.8%, Si:1.6%, C:0.18%, Mo:2.28%, Nb:1.91%, Ta:1.7%, Ti:0.28%, Fe:4.8%, RE:0.28%, Cu:0.98%, Mn:0.006%, surplus is Ni and inevitable impurity; Wherein, RE is cerium-rich mischmetal;
In the microtexture of described high strength, nickel based alloy, the area percentage of γ sosoloid shared by each cross section of alloy is 1.25%, Ni
3the area percentage of Al phase shared by each cross section of alloy is 0.88%, Ni
3the area percentage of (Al, Ti) strengthening phase shared by each cross section of alloy is 1.15%, γ ' (Ni
3al) area percentage mutually in the alloy shared by heart cross section is 0.032%;
The yield strength of described high strength, nickel based alloy is 605MPa, tensile strength 811MPa, unit elongation 43%, the impelling strength 99J/cm of 20 DEG C
2.
embodiment 3:
A preparation method for high strength, nickel based alloy, is characterized in that, comprises the steps:
(1) melting, gets the raw materials ready according to the chemical composition of aforementioned high strength, nickel based alloy, and adopt vacuum induction, the associating smelting technology of esr and vacuum consumable remelting smelts, the temperature of melting is 1640 DEG C;
(2) cast, cast to the molten metal that melting obtains, pouring temperature is 1390 DEG C;
(3) forge, carry out conventional die forging;
(4) homogenizing, carry out the homogenizing of first stage at 1120 DEG C of insulation 18h, and then be warmed up to 1185 DEG C, insulation 22h carries out the homogenizing of subordinate phase, and then cools to the homogenizing that 1130 DEG C of insulation 21h carry out the phase III;
(5) ausrolling, rolling temperature is 990 DEG C, and rolling pass is 6;
(6) aging strengthening model, carries out three step aging strengthening model by the rolled plate that step (5) obtains, and the first step is at 715 DEG C of insulation 6 ~ 8h, after cooling to 615 DEG C with the furnace with 55 DEG C/h subsequently, and insulation 8h, air cooling is to room temperature; Second step is for being heated to 670 DEG C of insulation 6h by sheet material, after cooling to 590 DEG C with the furnace with 60 DEG C/h subsequently, be incubated 6h, air cooling is to room temperature; 3rd step is for being heated to 610 DEG C of insulation 7h by sheet material, after cooling to 560 DEG C with the furnace with 50 DEG C/h subsequently, insulation 6h, air cooling, to room temperature, obtains high strength, nickel based alloy.
Claims (7)
1. a high strength, nickel based alloy, is characterized in that: its chemical composition contains by weight percentage: Al:3.2 ~ 6.8%, Cr:21 ~ 28%, B:3.0 ~ 4.2%, Si:1.2 ~ 1.9%, C:0.08 ~ 0.2%, Mo:1.8 ~ 2.8%, Nb:1.2 ~ 2.1%, Ta:1.0 ~ 1.8%, Ti:0.08 ~ 0.98%, Fe:3.2 ~ 5.8%, RE:0.2 ~ 0.38%, Cu:0.8 ~ 1.2%, Mn:0.002 ~ 0.08%, surplus is Ni and inevitable impurity;
In the microtexture of described high strength, nickel based alloy, the area percentage of γ sosoloid shared by each cross section of alloy is 1.2 ~ 2.8%, Ni
3the area percentage of Al phase shared by each cross section of alloy is 0.8 ~ 1.1%, Ni
3the area percentage of (Al, Ti) strengthening phase shared by each cross section of alloy is 0.58 ~ 1.25%, γ ' (Ni
3al) area percentage mutually in the alloy shared by heart cross section is 0.02 ~ 0.032%;
The yield strength of described high strength, nickel based alloy is 560 ~ 610MPa, tensile strength 780 ~ 820MPa, unit elongation 42 ~ 51%, the impelling strength 98 ~ 102J/cm of 20 DEG C
2.
2. high strength, nickel based alloy according to claim 1, is characterized in that: the chemical composition of described high strength, nickel based alloy contains by weight percentage: Al:4.8%, Cr:26%, B:3.8%, Si:1.6%, C:0.18%, Mo:2.28%, Nb:1.91%, Ta:1.7%, Ti:0.28%, Fe:4.8%, RE:0.28%, Cu:0.98%, Mn:0.006%, surplus is Ni and inevitable impurity.
3. high strength, nickel based alloy according to claim 1 and 2, is characterized in that: described RE is rare earth element y.
4. high strength, nickel based alloy according to claim 1 and 2, is characterized in that: described RE is cerium-rich mischmetal.
5. a preparation method for high strength, nickel based alloy described in any one of claim 1 ~ 4, is characterized in that, comprise the steps:
(1) melting, gets the raw materials ready according to the chemical composition of high strength, nickel based alloy described in any one of claim 1 ~ 4, adopts vacuum induction, the associating smelting technology of esr and vacuum consumable remelting smelts;
(2) cast, the molten metal that melting obtains is cast;
(3) forge, carry out conventional die forging;
(4) homogenizing, the homogenizing of first stage is carried out at 1120 ~ 1160 DEG C of insulation 15 ~ 22h, and then being warmed up to 1180 ~ 1190 DEG C, insulation 20 ~ 25h carries out the homogenizing of subordinate phase, and then cools to the homogenizing that 1120 ~ 1160 DEG C of insulation 18 ~ 24h carry out the phase III;
(5) ausrolling, rolling temperature is 980 ~ 1030 DEG C, and rolling pass is 5 ~ 8;
(6) aging strengthening model, carries out three step aging strengthening model by the rolled plate that step (5) obtains, and the first step is at 710 ~ 720 DEG C of insulation 6 ~ 8h, after cooling to 610 ~ 620 DEG C with the furnace with 50 ~ 60 DEG C/h subsequently, and insulation 7 ~ 9h, air cooling is to room temperature; Second step is for being heated to 660 ~ 680 DEG C of insulation 5 ~ 7h by sheet material, after cooling to 580 ~ 600 DEG C with the furnace with 55 ~ 65 DEG C/h subsequently, be incubated 5 ~ 7h, air cooling is to room temperature; 3rd step is for being heated to 600 ~ 620 DEG C of insulation 6 ~ 8h by sheet material, after cooling to 550 ~ 570 DEG C with the furnace with 45 ~ 55 DEG C/h subsequently, insulation 5 ~ 7h, air cooling, to room temperature, obtains high strength, nickel based alloy.
6. the preparation method of high strength, nickel based alloy according to claim 5, is characterized in that, the pouring temperature of described casting is 1380 ~ 1420 DEG C.
7. the preparation method of high strength, nickel based alloy according to claim 6, is characterized in that, the temperature of described melting is 1610 ~ 1720 DEG C.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410018657.0A CN103695721B (en) | 2014-01-16 | 2014-01-16 | A kind of high strength, nickel based Alloy And Preparation Method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410018657.0A CN103695721B (en) | 2014-01-16 | 2014-01-16 | A kind of high strength, nickel based Alloy And Preparation Method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103695721A CN103695721A (en) | 2014-04-02 |
| CN103695721B true CN103695721B (en) | 2016-01-20 |
Family
ID=50357380
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410018657.0A Active CN103695721B (en) | 2014-01-16 | 2014-01-16 | A kind of high strength, nickel based Alloy And Preparation Method |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103695721B (en) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104745992B (en) * | 2015-04-26 | 2016-10-05 | 北京金恒博远冶金技术发展有限公司 | The heat treatment method of engine turbine high temperature alloy |
| CN105925849B (en) * | 2016-05-04 | 2017-10-13 | 中国第一重型机械股份公司 | A kind of control method of 700 DEG C of ultra-supercritical steam turbine rotors nickel-base alloy forging |
| CN107523772B (en) * | 2016-06-22 | 2019-06-11 | 中国科学院金属研究所 | A kind of homogenization process of U720Li high temperature alloy |
| CN106636760B (en) * | 2017-01-16 | 2019-01-08 | 宁国市华成金研科技有限公司 | A kind of nickel base superalloy and its manufacturing method |
| CN110863099B (en) * | 2019-10-31 | 2021-09-21 | 河钢股份有限公司 | Heat treatment process for improving impact toughness of nickel-iron-based high-temperature alloy plate |
| CN110983111A (en) * | 2019-12-31 | 2020-04-10 | 江苏新华合金有限公司 | Nickel-based high-temperature alloy plate and preparation method thereof |
| CN112139415B (en) * | 2020-09-16 | 2022-04-19 | 江苏隆达超合金航材有限公司 | Method for producing difficult-to-deform nickel-based high-temperature alloy through compensation heating assisted free forging |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5389165A (en) * | 1991-05-14 | 1995-02-14 | Reynolds Metals Company | Low density, high strength Al-Li alloy having high toughness at elevated temperatures |
| CN102719708A (en) * | 2012-07-12 | 2012-10-10 | 丹阳市协昌合金有限公司 | Laser-cladding high-toughness high-hardness nickel-base alloy powder and preparation method thereof |
| CN103205605A (en) * | 2013-04-08 | 2013-07-17 | 武汉索力特科技有限公司 | High-temperature-oxidation-resistant casting nickel-based alloy and preparation method thereof |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP4981212B2 (en) * | 2001-01-25 | 2012-07-18 | 三菱重工業株式会社 | Ni-based alloy |
| US20070095441A1 (en) * | 2005-11-01 | 2007-05-03 | General Electric Company | Nickel-base alloy, articles formed therefrom, and process therefor |
-
2014
- 2014-01-16 CN CN201410018657.0A patent/CN103695721B/en active Active
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5389165A (en) * | 1991-05-14 | 1995-02-14 | Reynolds Metals Company | Low density, high strength Al-Li alloy having high toughness at elevated temperatures |
| CN102719708A (en) * | 2012-07-12 | 2012-10-10 | 丹阳市协昌合金有限公司 | Laser-cladding high-toughness high-hardness nickel-base alloy powder and preparation method thereof |
| CN103205605A (en) * | 2013-04-08 | 2013-07-17 | 武汉索力特科技有限公司 | High-temperature-oxidation-resistant casting nickel-based alloy and preparation method thereof |
Also Published As
| Publication number | Publication date |
|---|---|
| CN103695721A (en) | 2014-04-02 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN103695721B (en) | A kind of high strength, nickel based Alloy And Preparation Method | |
| CN103725924B (en) | A kind of nickelalloy and preparation method thereof | |
| CN104451339A (en) | Low-nickel aging strengthening type iron-nickel based corrosion resistant alloy and preparation method thereof | |
| CN103447348A (en) | Manufacturing method of stainless steel wire | |
| CN104195458A (en) | Stainless steel hot rolled plate with low relative permeability and preparation method thereof | |
| CN107460370A (en) | A kind of low-cost high-strength high-ductility metastable β Titanium-alloy and preparation method thereof | |
| CN104131237A (en) | Economic type diphasic stainless steel with good toughness and weldability and manufacturing method thereof | |
| CN100529130C (en) | High-hardness titanium alloy and method for producing same | |
| CN103882318A (en) | Molybdenum-saving type multi-component microalloy shock-resistant fire-resistant steel and preparation method of steel | |
| CN101637850A (en) | Argon tungsten-arc welding wire used in HR3C stainless steel welding | |
| CN103614638A (en) | High-niobium Q460-grade fire-resistant steel and manufacturing method thereof | |
| CN103252593A (en) | Oxidation-resistant low-expansion high-temperature alloy welding wire for gas shielded welding | |
| JP2017510704A5 (en) | ||
| CN103540859B (en) | High heat-resistant stainless steel coffee pot material and preparation method thereof | |
| CN107974639A (en) | A kind of complex alloy wear-resistant steel ball of high tenacity and preparation method thereof | |
| CN105238957A (en) | High-property nickel-base superalloy and production method thereof | |
| CN104694779B (en) | A kind of B30 materials and preparation method thereof | |
| CN102409258A (en) | Boron-containing high strength hydrogen embrittlement resistant alloy and structural homogeneity control method thereof | |
| CN114561517A (en) | Low-density high-ductility steel and preparation method and application thereof | |
| CN102965543A (en) | High-strength titanium alloy with wide adjustable performance range | |
| JP6575756B2 (en) | Method for producing precipitation strengthened stainless steel | |
| CN104651685A (en) | Aluminum magnesium alloy material and preparation method thereof | |
| CN104152805A (en) | Alloy steel and thermal treatment method thereof | |
| CN103725923B (en) | A kind of nickel-base alloy of aluminum strengthening and preparation method thereof | |
| CN103726002B (en) | A kind of heat treating method of high-intensity nickel alloy |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CB03 | Change of inventor or designer information |
Inventor after: Wang Jiancong Inventor after: Sun Xiaohui Inventor before: Zhang Xia |
|
| CB03 | Change of inventor or designer information | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20171227 Address after: 529500 Yangjiang Hi-tech Zone Port Industrial Park, seaport three cross road, Guangdong Province, 1 Patentee after: Yangjiang Yi Chuan Metal Technology Co. Ltd. Address before: 523000, Guangdong, Humen Town, South Village, Naval Battle Road, No. A28 Patentee before: Zhang Xia |
|
| TR01 | Transfer of patent right | ||
| CB03 | Change of inventor or designer information |
Inventor after: Wang Jiancong Inventor after: Wu Lianquan Inventor after: Sun Xiaohui Inventor before: Wang Jiancong Inventor before: Sun Xiaohui |
|
| CB03 | Change of inventor or designer information |