CN106244838A - Niobium titanium carbon Al-alloy alterant and preparation method thereof - Google Patents

Niobium titanium carbon Al-alloy alterant and preparation method thereof Download PDF

Info

Publication number
CN106244838A
CN106244838A CN201610836489.5A CN201610836489A CN106244838A CN 106244838 A CN106244838 A CN 106244838A CN 201610836489 A CN201610836489 A CN 201610836489A CN 106244838 A CN106244838 A CN 106244838A
Authority
CN
China
Prior art keywords
niobium
titanium
powder
alloy
carbon
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
CN201610836489.5A
Other languages
Chinese (zh)
Other versions
CN106244838B (en
Inventor
肖福仁
廖波
吴大勇
乔桂英
魏腾飞
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.)
CANGZHOU DONGZHONG SPECIAL ALLOY MANUFACTURING Co.,Ltd.
Original Assignee
Yanshan University
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 Yanshan University filed Critical Yanshan University
Priority to CN201610836489.5A priority Critical patent/CN106244838B/en
Publication of CN106244838A publication Critical patent/CN106244838A/en
Application granted granted Critical
Publication of CN106244838B publication Critical patent/CN106244838B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/06Making non-ferrous alloys with the use of special agents for refining or deoxidising
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium

Abstract

The invention discloses a kind of niobium titanium carbon Al-alloy alterant and preparation method thereof.Described niobium titanium carbon Al-alloy alterant is with niobium powder, titanium valve and graphite powder as raw material, and niobium, the mass ratio of titanium are 3:7~7:3, and carbon is 0.8:1~1:1 with the atomic ratio of niobium titanium.The preparation method of niobium titanium carbon Al-alloy alterant is first the mixed material ball milling of niobium powder, titanium valve to be become niobium titanium alloy, adds the further ball milling of graphite powder and makes carbon and the further alloying of niobium titanium alloy, and forms carbide nucleus.The niobium titanium carbon Al-alloy alterant of the present invention can notable refining aluminum alloy as-cast structure, improve the plasticity of cast aluminium alloy.

Description

Niobium titanium carbon Al-alloy alterant and preparation method thereof
Technical field
The invention belongs to material science, be specifically related to a kind of niobium titanium carbon Al-alloy alterant and preparation side thereof Method.
Background technology
Aluminium alloy is one of metal material of application amount maximum, and its application amount is only below iron and steel.To metal material, tissue is thin Change is to improve the strength of materials and plasticity most efficient method.Different from ferrous materials, aluminium alloy is not because having phase transformation, it is impossible to by heat The mode thinning microstructure processed, can only pass through the means thinning microstructure such as Metamorphism treatment and thermal deformation.And Cast aluminium alloy is golden, rotten place Reason just becomes unique thinning microstructure, improves the key technology means of cast properties, and is paid attention to widely.At Metamorphism treatment In, alterant and technique have significant impact to structure refinement.At present, in Aluminum alloy modification, application preferably at most aluminum titanium boron, Aluminum strontium alterant etc..Recently, the new alterant such as the carbide of compound rare-earth, the carbide of titanium, vanadium also begins to application.Alterant Thinning microstructure it is crucial that can stable existence in the liquid phase, and interface can promote forming core as the core of heterogeneous forming core, carefully Change tissue.Another factor affecting modification effect is rotten and casting technique.Conventional aluminum titanium boron alterant is to rate of cooling The most sensitive, with the reduction of rate of cooling, the substantially roughening of its tissue, cause foundry goods different parts to produce substantially because thickness is different Histological difference.Recent studies have shown that, use aluminum titanium carbon alterant also to have good effect.
Aluminum titanium carbon is to utilize titanium, carbon to form titanium carbide, and titanium, aluminum form aluminum Tritanium/Trititanium, and titanium carbide and aluminum Tritanium/Trititanium all can be made For the core of aluminium alloy, growing up of suppression carbide, it is thus achieved that more tiny forming core points are effectively to utilize aluminum titanium carbon modification effect Key.Niobium has the characteristic similar to titanium, it is also possible to form niobium carbide and aluminum three niobium, and titanium and niobium and be substituted for each other, and is formed Titanium carbide niobium and aluminum Tritanium/Trititanium niobium.Additionally niobium has bigger atomic radius, and the diffusion in aluminum is more difficult, can effectively suppress carbide And the roughening of aluminum Tritanium/Trititanium niobium, thus reduce because casting thickness is different, cause the different impact on modification effect of rate of cooling.Cause This, preparing and obtain good modification effect niobium titanium carbon aluminum alloy modifier will become the key of refining aluminum alloy as-cast structure.
Summary of the invention
The technical issues that need to address of the present invention are to provide kind of a kind of niobium titanium carbon Al-alloy alterant and a preparation side thereof Method, makes niobium, titanium, carbon have rational ratio and structure, plays good Aluminum alloy modification effect, refining aluminum alloy solidification group Knit.
For solving above-mentioned technical problem, the technical solution adopted in the present invention is: a kind of niobium titanium carbon Al-alloy goes bad Agent, with niobium powder, titanium valve, graphite powder as raw material, described niobium powder, the mass ratio of titanium valve are 3:7~7:3;Graphite powder and niobium powder, titanium The atomic ratio of powder is 0.8:1~1:1, and above-mentioned raw materials forms niobium titanium carbon composite powder through mechanical mill alloying, wherein comprises 70- The carbide particle of the titanium carbide niobium of 80%.
The preparation method of a kind of niobium titanium carbon Al-alloy alterant, said method comprising the steps of:
Step A: be all higher than 98.0% with purity, its particle mean size niobium powder between 300 mesh~1000 mesh, titanium Powder, graphite powder are raw material;
Step B: ball milling;
Step B1: the mixed material ball milling that mass ratio is 3:7~7:3 of niobium powder, titanium valve is become niobium titanium alloy powder body;
Step B2: add graphite powder in step B1 gained niobium titanium alloy powder body, described graphite powder and niobium powder, titanium valve former Son ratio is 0.8:1~1:1, and under the protection of purity > 99.99% of argon, further ball milling makes niobium titanium alloy be formed with graphite Niobium titanium carbon composite powder, wherein comprises the carbide particle of the titanium carbide niobium of 70-80%.
Further improvement is that of the above-mentioned preparation method of the present invention: described ball milling step B1 is by niobium powder and certain proportion Titanium valve mixing after load in ball grinder, the zirconium oxide balls in ball grinder is 15:1~40:1 with the mass ratio of material, ball milling Tank is ball milling under the protection of purity > 99.99% of argon, makes niobium powder form niobium titanium alloy powder body with titanium valve.
Owing to have employed technique scheme, the technological progress that the present invention obtains is:
This invention uses the method for mechanical alloying, makes niobium titanium be initially formed alloy, forms niobium titanium carbon with carbon more multiple Close powder body, composite particles contains a certain amount of titanium carbide niobium nucleus, and due to the effect of mechanical alloying, niobium titanium carbon is combined Granule exists a large amount of defect and high mechanical energy, when adding in high-temperature liquid state aluminium alloy, due to high temperature action, niobium, titanium, Carbon energy fast reaction, on the basis of mechanical alloying forms carbide nucleus, generates tiny niobium carbide titanium, and is distributed to aluminum conjunction In gold liquid.And a small amount of niobium, titanium, carbon dissolve in aluminum alloy melt during follow-up, effectively facilitate aluminium alloy along Carbide Precipitation and coagulate Admittedly organize forming core, thinning solidification structure.
The first time mechanical milling process of the present invention achieve niobium powder, titanium valve broken, levigate, produce in making niobium, titanium granule simultaneously The raw defect such as substantial amounts of room and dislocation, in the collision process of niobium powder and titanium valve, constantly refinement produces substantial amounts of unsalted surface And the temperature rise of moment promotes niobium, Ti Alloying.
In the second time mechanical milling process of the present invention, mechanical alloying niobium titanium alloy powder and carbon dust are at mechanical mill energy The lower diffusion to niobium titanium alloy accelerating carbon of effect, forms niobium titanium carbon composite powder, and under the effect of impact temperature, forms carbon Compound nucleus, ultimately forms the aluminum alloy modifier of the niobium titanium carbon composite powder comprising certain carbide nucleus.
Detailed description of the invention
Below in conjunction with embodiment, the present invention is described in further details:
A kind of niobium titanium carbon Al-alloy alterant of the present invention is with niobium powder, titanium valve and graphite as raw material, described niobium powder, The mass ratio of titanium valve is 3:7~7:3, and graphite powder is 0.8:1~1:1 with niobium powder, the atomic ratio of titanium valve total amount.This niobium titanium carbon is multiple Close Aluminum alloy modification to be prepared by Mechanical Alloying.
Each embodiment balls grinding machine is the nanometer impact grinding that Qinhuangdao Tai Ji ring nanometer products company limited produces, ball Grinding jar is stainless cylinder of steel, and volume is 2L, abrading-ball is also zirconium oxide material, has φ 10mm, the cumulative volume of abrading-ball accounts for the volume of tank 50%~70%.
Embodiment 1
The first step: (purity is 98.0%, granularity is by niobium powder (granularity be 1000 mesh, purity be 99.2%) and titanium valve 1000 mesh) press the mass ratio mixing of 3:7, load in stainless steel jar mill, and (zirconium oxide balls is with mixed according to the ratio of grinding media to material of 39:1 Close the mass ratio of powder) in grinding jar, load zirconia ball.It is filled with purity of argon to ball grinder > 99.99%, then rush in nanometer Hit on mill, ball milling 1 hour under the rotating speed of 300r/min.
Second step: add the graphite powder (granularity identical with niobium powder and titanium valve atom summation in the ball grinder of the first step Be 325 mesh, purity be 99.1%), be filled with purity > after the argon of 99.99%, under the rotating speed of 300r/min, continue ball milling 3 little Time.
In the niobium titanium carbon Al-alloy alterant obtained, niobium, titanium mass ratio are 3:7.
Embodiment 2
The present embodiment is as follows with the difference of embodiment 1.
(granularity is that 1000 mesh, purity are for niobium powder used by the first step (granularity be 1000 mesh, purity be 99.2%) and titanium valve 98.0%) mixing for 1:1 in mass ratio, the zirconium oxide balls used is 30:1 with niobium powder, titanium valve mixed powder mass ratio, ball Consume time 1.5 hours.
Second step adds graphite powder (granularity be 320 mesh, purity be 99.1%), graphite powder amount and niobium powder and titanium valve former Son ratio is 0.9:1, and continuing Ball-milling Time is 3 hours.
In the niobium titanium carbon Al-alloy alterant obtained, niobium, titanium mass ratio are 1:1.
Embodiment 3
The present embodiment is as follows with the difference of embodiment 1.
(granularity is that 1000 mesh, purity are for niobium powder used by the first step (granularity be 1000 mesh, purity be 99.2%) and titanium valve 98.0%) pressing the mass ratio mixing of 7:3, the zirconium oxide balls used is 30:1 with niobium powder, titanium valve mixed powder mass ratio, ball Consume time 1.5 hours.
Second step adds graphite powder (granularity be 320 mesh, purity be 99.1%), graphite powder amount and niobium powder and titanium valve former Son ratio is 0.8:1, and continuing Ball-milling Time is 3.5 hours.
In the niobium titanium carbon Al-alloy alterant obtained, niobium, titanium mass ratio are 7:3.
Embodiment 4
The present embodiment is as follows with the difference of embodiment 1.
The granularity of first step niobium powder is 300 mesh, and purity is 98.0%, and the granularity of titanium valve is 320 mesh, and purity is 98.4% Ball-milling Time is 2 hours.
The Ball-milling Time of second step is 4 hours.
In the niobium titanium carbon Al-alloy alterant obtained, niobium, titanium mass ratio are 3:7.
Embodiment 5
The present embodiment is as follows with the difference of embodiment 3.
The granularity of first step niobium powder is 300 mesh, and purity is 98.0%%, and the granularity of titanium valve is 320 mesh, and purity is 98.4% Ball-milling Time be 2 hours.
The Ball-milling Time of second step is 4 hours.
Niobium, titanium mass ratio 7:3 in the niobium titanium carbon Al-alloy alterant obtained.
The result detecting above five embodiment gained samples is as follows:
First the powder body obtained by after terminating the first step carries out X-ray diffraction analysis, in the low embodiment of Ti content 1, in fact Execute example 2 and implement in 4, thing equal niobium titanium alloy solid solution mutually;And in the high enforcement of Ti content 3 with implement in 5, thing is niobium titanium mutually Solid solution and a small amount of titanium phase.Powder body obtained by after terminating second step carries out X-ray diffraction analysis, in X-ray diffraction spectrum Do not find the diffraction maximum of carbon, in the low embodiment of Ti content 1, embodiment 2 and enforcement 4, thing equal niobium titanium carbon alloy solid solution mutually And a small amount of niobium carbide titanium;With the increase of Ti content, in embodiment 2, embodiment 3, embodiment 4 and embodiment 5, niobium carbide titanium phase Amount increased.
Embodiment 6
Prepared niobium titanium carbon Al-alloy alterant is applied to A356 aluminium alloy castings and with aluminum titanium boron alterant Compare.Detailed description of the invention is as follows:
Being melted in middle hot-well formula soon by A356 aluminium alloy, fusion temperature is 690 DEG C ± 5 DEG C.Treat that aluminium alloy is completely melt also After reaching 690 DEG C ± 5 DEG C, will be compared with aluminium alloy, above-described embodiment 1 that mass percent is 1.5% is obtained to embodiment 5 Niobium titanium carbon Al-alloy alterant add in aluminum liquid.Adding Way uses aluminium foil cladding, press-in and stirs, and adds and covers Agent, logical argon is poured into a mould after giving vent to anger.Mold is the hot-die through 300 DEG C of preheatings.For silicon phase in refinement A356 aluminium alloy, it is simultaneously introduced matter Amount is than the strontium alterant being 1%.For contrasting with aluminum titanium boron alterant, same process is used to be prepared for what aluminum titanium boron alterant went bad Ingot casting, the addition mass percent that aluminum titanium boron goes bad is 2%.
Use the ingot material that above-described embodiment 1 is prepared to the niobium titanium carbon Al-alloy alterant that embodiment 5 is obtained It is respectively labeled as A, B, C, D, E, and the ingot material using aluminum titanium boron alterant to prepare is labeled as F.
Cutting metallographic specimen and tensile property sample in the part that ingot casting is identical, under the microscope, the difference of measurement goes bad After agent processes, ingot casting A, B, C, D, E, F aluminium alloy dendrite size is listed in the table below;Meanwhile, tensile yield strength and percentage elongation are also found in Following table.
As can be seen here, under conditions of niobium titanium carbon alterant addition is less than aluminum titanium boron alterant, niobium titanium carbon alterant has There is the modification effect suitable with aluminum titanium boron alterant.Niobium titanium carbon alterant when niobium titanium mass percent is 50:50, structure refinement Best results.Using niobium titanium carbon alterant compared with the performance of aluminum titanium boron alterant ingot casting, niobium titanium carbon alterant makes casting strength Slightly reduce, but plasticity dramatically increases.

Claims (3)

1. a niobium titanium carbon Al-alloy alterant, it is characterised in that: described alterant is former with niobium powder, titanium valve, graphite powder Material, described niobium powder, the mass ratio of titanium valve are 3:7~7:3;Graphite powder is 0.8:1~1:1 with niobium powder, the atomic ratio of titanium valve, on State raw material and form niobium titanium carbon composite powder through mechanical mill alloying, wherein comprise the carbide of the titanium carbide niobium of 70-80% Grain.
2. the preparation method of a niobium titanium carbon Al-alloy alterant, it is characterised in that: said method comprising the steps of:
Step A: be all higher than 98.0% with purity, its particle mean size niobium powder between 300 mesh~1000 mesh, titanium valve, stone Powdered ink is raw material;
Step B: ball milling;
Step B1: the mixed material ball milling that mass ratio is 3:7~7:3 of niobium powder, titanium valve is become niobium titanium alloy powder body;
Step B2: adding graphite powder in step B1 gained niobium titanium alloy, described graphite powder with the atomic ratio of niobium powder, titanium valve is 0.8:1~1:1, under the protection of purity > 99.99% of argon, further ball milling makes niobium titanium alloy form niobium titanium carbon with graphite Composite granule, wherein comprises the carbide particle of the titanium carbide niobium of 70-80%.
3. the preparation method of according to claim 2 niobium titanium carbon Al-alloy alterant, it is characterised in that: described ball milling Step B1 be niobium powder is mixed with a certain proportion of titanium valve after load in ball grinder, the zirconium oxide balls in ball grinder and material Mass ratio is 15:1~40:1, and ball grinder is ball milling under the protection of purity > 99.99% of argon, makes niobium powder form niobium with titanium valve Titanium alloy powder body.
CN201610836489.5A 2016-09-21 2016-09-21 Niobium titanium carbon Al-alloy alterant and preparation method thereof Active CN106244838B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610836489.5A CN106244838B (en) 2016-09-21 2016-09-21 Niobium titanium carbon Al-alloy alterant and preparation method thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610836489.5A CN106244838B (en) 2016-09-21 2016-09-21 Niobium titanium carbon Al-alloy alterant and preparation method thereof

Publications (2)

Publication Number Publication Date
CN106244838A true CN106244838A (en) 2016-12-21
CN106244838B CN106244838B (en) 2017-12-15

Family

ID=57600344

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610836489.5A Active CN106244838B (en) 2016-09-21 2016-09-21 Niobium titanium carbon Al-alloy alterant and preparation method thereof

Country Status (1)

Country Link
CN (1) CN106244838B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114453567A (en) * 2022-01-27 2022-05-10 江苏大学 High-temperature alloy solidification structure refiner and preparation method and application thereof
CN114956822A (en) * 2022-05-13 2022-08-30 咸阳职业技术学院 Erosion-resistant corrosion-resistant high-temperature atomizing nozzle and preparation method thereof

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1418973A (en) * 2002-12-18 2003-05-21 涿州市精英铝合金材料有限责任公司 Refining agent for crystalline grain of aluminium titanium carbon intermediate alloy
CN102581288A (en) * 2012-03-26 2012-07-18 燕山大学 Ultrafine niobium carbide and iron composite powder material and method for preparing same
CN104325128A (en) * 2014-09-29 2015-02-04 华中科技大学 Heat-resisting die steel material for 3D (Three-Dimensional) printing and preparation method of heat-resisting die steel material
CN104894417A (en) * 2015-04-09 2015-09-09 昌吉市吉日光有色金属合金制造有限公司 Aluminum titanium carbon intermediate alloy refinement agent and preparation technology thereof
CN105583401A (en) * 2015-12-25 2016-05-18 华中科技大学 Method for preparing composite powder for 3D printing, product and application

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1418973A (en) * 2002-12-18 2003-05-21 涿州市精英铝合金材料有限责任公司 Refining agent for crystalline grain of aluminium titanium carbon intermediate alloy
CN102581288A (en) * 2012-03-26 2012-07-18 燕山大学 Ultrafine niobium carbide and iron composite powder material and method for preparing same
CN104325128A (en) * 2014-09-29 2015-02-04 华中科技大学 Heat-resisting die steel material for 3D (Three-Dimensional) printing and preparation method of heat-resisting die steel material
CN104894417A (en) * 2015-04-09 2015-09-09 昌吉市吉日光有色金属合金制造有限公司 Aluminum titanium carbon intermediate alloy refinement agent and preparation technology thereof
CN105583401A (en) * 2015-12-25 2016-05-18 华中科技大学 Method for preparing composite powder for 3D printing, product and application

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114453567A (en) * 2022-01-27 2022-05-10 江苏大学 High-temperature alloy solidification structure refiner and preparation method and application thereof
CN114956822A (en) * 2022-05-13 2022-08-30 咸阳职业技术学院 Erosion-resistant corrosion-resistant high-temperature atomizing nozzle and preparation method thereof

Also Published As

Publication number Publication date
CN106244838B (en) 2017-12-15

Similar Documents

Publication Publication Date Title
CN108085528B (en) In-situ generated nano NbB2Method for grain refining and strengthening aluminum alloy
Reddy et al. Silicon carbide reinforced aluminium metal matrix nano composites-a review
Nie et al. Microstructure and mechanical properties of SiC nanoparticles reinforced magnesium matrix composites fabricated by ultrasonic vibration
Yang et al. Effect of multi-pass friction stir processing on microstructure and mechanical properties of Al3Ti/A356 composites
US11634333B2 (en) Boron-containing titanium-based composite powder for 3D printing and method of preparing same
EP2455503B1 (en) Grain refiner for magnesium and magnesium alloy and preparation method thereof
Miao et al. Laser powder-bed-fusion of Si3N4 reinforced AlSi10Mg composites: Processing, mechanical properties and strengthening mechanisms
Huang et al. On the interactions between molten aluminum and high entropy alloy particles during aluminum matrix composite processing
Zhang et al. Effect of hot isostatic pressing on the microstructure and properties of magnesium silicide–silicon carbide/aluminum alloy (AlSi7Cu2Mg) composites
Salarieh et al. An investigation on the microstructure and mechanical properties of Al-Zn-Mg-Cu/Ti composite produced by compocasting
Li et al. Microstructure and mechanical properties of an AlN/Mg–Al composite synthesized by Al–AlN master alloy
CN106244838B (en) Niobium titanium carbon Al-alloy alterant and preparation method thereof
US20230160038A1 (en) Metal matrix composites and methods of making and use thereof
CN114934206B (en) Multi-element aluminide reinforced aluminum-based composite material and preparation method and application thereof
CN114277277B (en) AlN/Al particle reinforced magnesium-aluminum rare earth based composite material and preparation method thereof
CN105937000B (en) A kind of aluminum alloy materials and its centre spinning method substituting QT400 ship columns
CN112481516B (en) Al-Ti-SiC intermediate alloy and preparation method and application thereof
CN108374099A (en) A kind of preparation method of long-periodic structure particle reinforced Mg-base/aluminum matrix composite
Sui et al. Effects of pouring temperature on interfacial reaction between Ti-47.5 Al-2.5 V-1Cr alloy and mold during centrifugal casting
Chen et al. Fabrication and Sc-Refinement of SiC p/A356 Composites by Vacuum Stirring Casting Method
Li et al. Synergistic Effects of B4C and Sn on the Coupled Growth Pattern and Mechanical Properties of Mg–Y–Zn–Mn Alloy Containing LPSO and W Phases
KR101080926B1 (en) The preparation method of ceramic/metal composite powders for metal materials to enhance the mechanical properties
CN105970039B (en) A kind of aluminum alloy materials and its centre spinning method for substituting QT500 loom wheel hubs
CN112921226B (en) Mg-AlN master alloy grain refiner for magnesium-aluminum alloy and preparation method thereof
CN116752008B (en) Al-Ti-Nb-B intermediate alloy and preparation method and application thereof

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant
TR01 Transfer of patent right

Effective date of registration: 20210917

Address after: 061739 Fenghuang Industrial Zone, fengfengdian Township, Cangxian County, Cangzhou City, Hebei Province

Patentee after: CANGZHOU DONGZHONG SPECIAL ALLOY MANUFACTURING Co.,Ltd.

Address before: 066004 No. 438 west section of Hebei Avenue, seaport District, Hebei, Qinhuangdao

Patentee before: Yanshan University

TR01 Transfer of patent right