CN107653384A - A kind of preparation method of in-situ preparation nickel aluminide enhancing Cu-base composites - Google Patents

A kind of preparation method of in-situ preparation nickel aluminide enhancing Cu-base composites Download PDF

Info

Publication number
CN107653384A
CN107653384A CN201710767764.7A CN201710767764A CN107653384A CN 107653384 A CN107653384 A CN 107653384A CN 201710767764 A CN201710767764 A CN 201710767764A CN 107653384 A CN107653384 A CN 107653384A
Authority
CN
China
Prior art keywords
preparation
base composites
aluminium
nickel aluminide
intermediate 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.)
Pending
Application number
CN201710767764.7A
Other languages
Chinese (zh)
Inventor
宋宏婷
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to CN201710767764.7A priority Critical patent/CN107653384A/en
Publication of CN107653384A publication Critical patent/CN107653384A/en
Pending legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/02Making non-ferrous alloys by melting
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/02Making non-ferrous alloys by melting
    • C22C1/03Making non-ferrous alloys by melting using master alloys
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/10Alloys containing non-metals
    • C22C1/1036Alloys containing non-metals starting from a melt
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/10Alloys containing non-metals
    • C22C1/1036Alloys containing non-metals starting from a melt
    • C22C1/1057Reactive infiltration
    • C22C1/1063Gas reaction, e.g. lanxide
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C32/00Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ
    • C22C32/0047Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with carbides, nitrides, borides or silicides as the main non-metallic constituents
    • C22C32/0068Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with carbides, nitrides, borides or silicides as the main non-metallic constituents only nitrides
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C9/00Alloys based on copper
    • 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
    • C22F1/08Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of copper or alloys based thereon

Abstract

A kind of preparation method of in-situ preparation nickel aluminide enhancing Cu-base composites, belongs to metal material field, preparation method is as follows:Prepared by matrix material, prepared by alloy material, fusion smelting, the step such as in-situ preparation, and the copper alloy of preparation has the advantages that conductive effect is high, mechanical property is strong.

Description

A kind of preparation method of in-situ preparation nickel aluminide enhancing Cu-base composites
Technical field
The present invention relates to financial field of smelting, a kind of specifically in-situ preparation nickel aluminide enhancing Cu-base composites Preparation method.
Background technology
Copper alloy(copper alloy )The alloy being made up of using fine copper the one or more of other elements of matrix addition. Fine copper is also known as red copper in Zi Hong Se ﹐.Fine copper density is that 8.96 ﹐ fusing points are that there is 1083 DEG C ﹐ excellent Dao electricity ﹑ Dao Re ﹑ to prolong Malleability and corrosion resistance.It is mainly used in making and generates electricity Ji ﹑ Mu Xian ﹑ electricity Lan ﹑ Kai and close electrotechnical apparatus and the heat exchange such as Zhuan Zhi ﹑ transformers The heat conduction equipments such as the flat plate collector of Qi ﹑ Guan Dao ﹑ solar heat collectors.Conventional copper alloy is divided into Huang Tong ﹑ Qing Tong ﹑ copper-nickel alloys 3 Major class.
And strengthened adding ceramics into metal at present, it has been effectively combined ceramics and metal a little, preparation Metal has the advantages that rigidity is big, intensity is high, processing characteristics is good.Existing ceramics enhancing is mainly aluminium, is being difficult to obtain on copper To application, essentially consist among in-situ preparation process, enhancing ceramics are difficult to generate, and use machinery generation ceramal, its copper Alloy property is again bad.
The content of the invention
It is an object of the invention to:For above-mentioned problem, there is provided a kind of in-situ preparation nickel aluminide enhancing is copper-based multiple The preparation method of condensation material, physical property enhancing is carried out to copper using metallic compound, preparation method is as follows:
Step 1: it is prepared by matrix material, the raw material that described matrix material is made up of fine aluminium, fine copper;
Step 2 weighs nickel powder and mixed successively with absolute ethyl alcohol and propyl alcohol, then mechanical agitation respectively, is then heated to ethanol and third Alcoholic solution all volatilizees, and obtains nickel powder;
It is placed in Step 3: matrix material in step 1 is put into crucible in melting resistance furnace, while indifferent gas is filled with into stove Body is protected, and melting 5 ~ 20 minutes, is subsequently added into described alloy gross mass under conditions of being 700 ~ 950 DEG C in smelting temperature 0.01% ~ 2.1% carbon trichloride refines 5 ~ 20 minutes;
Step 4: the nickel powder that addition step 2 obtains in crucible melting 5 ~ 20 minutes under conditions of 700 ~ 950 DEG C, so It is applied to afterwards using water cooling ultrasonic head in melting matrix alloy, continual application ultrasonic wave 1 ~ 10 minute;Stand 5 ~ 20 Skimmed after minute, finally casting obtains nickel aluminide enhancing Cu-base composites;
Step 5: the composite after above-mentioned processing is subjected to hot extrusion;
Step 6:Hot rolling treatment is carried out more than recrystallization temperature;
Step 7:Alloy after step 6 is subjected to solution treatment.
As an improvement, described fine aluminium be using the purified aluminum after vacuum heat-treating method, purity be at least 99.99% with On.
As an improvement, the application frequency of ultrasonic wave is 20 ~ 80 KHzs, amplitude is 20 ~ 50 microns.
As an improvement, the weight of aluminium is accounted between 10%-15% in matrix material.
As an improvement, described step is a kind of to add intermediate alloy, described intermediate alloy is aluminum bronze intermediate alloy, aluminium manganese The raw material of intermediate alloy composition.
As an improvement, described aluminum bronze intermediate alloy aluminium and the mass ratio of copper are 1:1, the matter of aluminium manganese intermediate alloy aluminium and manganese Amount is than being 1:1.
As an improvement, the weight ratio that intermediate alloy raw material accounts for matrix material is 20%.
As an improvement, described inert gas is helium, one or two kinds of mixtures of argon gas.
As an improvement, described inert gas carries out the pre-heat treatment before addition.
As an improvement, contain nitrogen in described inert gas, and described nitrogen and nickel production nickel oxide, described inertia Chemical reaction generation nickel oxide occurs for the nickel in the nitrogen and melt in gas, and the nickel oxide produced is dispersed in matrix In, described nickel oxide is three nickel of nitridation, contains certain ammonia preferably in inert gas in inert gas, specifically Content volume number is in 10%-50%.
Composite technology prepared by the present invention is simple, single sintering cleaning, it is prepared reinforcing copper have good electrical and Mechanical property.The relative density for the reinforcing copper products that the present invention is prepared is up to 99%, and conductance is up to 95%, and hardness is up to 141HV, tensile strength are up to 403MPa, have very excellent combination property.
Embodiment
In order to make the purpose , technical scheme and advantage of the present invention be clearer, with reference to embodiments, to the present invention It is further elaborated.It should be appreciated that the specific embodiments described herein are merely illustrative of the present invention, it is not used to Limit the present invention.
Specific embodiment 1:A kind of in-situ preparation nickel aluminide strengthens Cu-base composites, and preparation method is as follows:
Step 1: it is prepared by matrix material, the raw material that described matrix material is made up of fine aluminium, fine copper;
Step 2 weighs nickel powder and mixed successively with absolute ethyl alcohol and propyl alcohol, then mechanical agitation respectively, is then heated to ethanol and third Alcoholic solution all volatilizees, and obtains nickel powder;
It is placed in Step 3: matrix material in step 1 is put into crucible in melting resistance furnace, while indifferent gas is filled with into stove Body is protected, and melting 12 minutes, is subsequently added into described alloy gross mass under conditions of being 1000 DEG C in smelting temperature 0.05% carbon trichloride refines 5 ~ 20 minutes;
Step 4: the nickel powder that addition step 2 obtains in crucible melting 12 minutes under conditions of 820 DEG C, then using water Cold ultrasonic head is applied in melting matrix alloy, continual application ultrasonic wave 1 ~ 10 minute;Stand 5 ~ 20 minutes it After skim, finally casting obtain nickel aluminide enhancing Cu-base composites;
Step 5: the composite after above-mentioned processing is subjected to hot extrusion;
Step 6:Hot rolling treatment is carried out more than recrystallization temperature;
Step 7:Alloy after step 6 is subjected to solution treatment.
Described fine aluminium is to be at least more than 99.99% using the purified aluminum after vacuum heat-treating method, purity.Ultrasonic wave Application frequency be 20-80 KHzs, amplitude be 20 ~ 50 microns.The weight of aluminium accounts for 10% in matrix material.Described step One kind adds intermediate alloy, and described intermediate alloy is aluminum bronze intermediate alloy, the raw material of aluminium manganese intermediate alloy composition.Described aluminium The mass ratio of copper intermediate alloy aluminium and copper is 1:1, the mass ratio of aluminium manganese intermediate alloy aluminium and manganese is 1:1.Intermediate alloy raw material accounts for The weight ratio of matrix material is 20%.
Described inert gas is helium, one or two kinds of mixtures of argon gas.Inert gas carries out pre- before addition Heat treatment.Contain nitrogen, described nitrogen and nickel production nickel oxide in described inert gas.
Specific embodiment 2:A kind of in-situ preparation nickel aluminide strengthens Cu-base composites, and preparation method is as follows:
Step 1: it is prepared by matrix material, the raw material that described matrix material is made up of fine aluminium, fine copper;
Step 2 weighs nickel powder and mixed successively with absolute ethyl alcohol and propyl alcohol, then mechanical agitation respectively, is then heated to ethanol and third Alcoholic solution all volatilizees, and obtains nickel powder;
It is placed in Step 3: matrix material in step 1 is put into crucible in melting resistance furnace, while indifferent gas is filled with into stove Body is protected, and melting 11 minutes, is subsequently added into the six of described alloy gross mass 1% under conditions of being 800 DEG C in smelting temperature Chloroethanes refines 5-20 minutes;
Step 4: the nickel powder that addition step 2 obtains in crucible melting 5 ~ 20 minutes under conditions of 700 ~ 950 DEG C, so It is applied to afterwards using water cooling ultrasonic head in melting matrix alloy, continual application ultrasonic wave 1 ~ 10 minute;Stand 5 ~ 20 Skimmed after minute, finally casting obtains nickel aluminide enhancing Cu-base composites;
Step 5: the composite after above-mentioned processing is subjected to hot extrusion;
Step 6:Hot rolling treatment is carried out more than recrystallization temperature;
Step 7:Alloy after step 6 is subjected to solution treatment.
Described fine aluminium is to be at least more than 99.99% using the purified aluminum after vacuum heat-treating method, purity.Ultrasonic wave Application frequency be 20 ~ 80 KHzs, amplitude be 20 ~ 50 microns.The weight of aluminium accounts for 15% in matrix material.Described step A kind of rapid addition intermediate alloy, described intermediate alloy are aluminum bronze intermediate alloy, the raw material of aluminium manganese intermediate alloy composition.Described The mass ratio of aluminum bronze intermediate alloy aluminium and copper is 1:1, the mass ratio of aluminium manganese intermediate alloy aluminium and manganese is 1:1.Intermediate alloy raw material The weight ratio for accounting for matrix material is 20%.
Described inert gas is helium, one or two kinds of mixtures of argon gas.Inert gas carries out pre- before addition Heat treatment.Contain nitrogen, described nitrogen and nickel production nickel oxide in described inert gas.
Specific embodiment 1:A kind of in-situ preparation nickel aluminide strengthens Cu-base composites, and preparation method is as follows:
Step 1: it is prepared by matrix material, the raw material that described matrix material is made up of fine aluminium, fine copper;
Step 2 weighs nickel powder and mixed successively with absolute ethyl alcohol and propyl alcohol, then mechanical agitation respectively, is then heated to ethanol and third Alcoholic solution all volatilizees, and obtains nickel powder;
It is placed in Step 3: matrix material in step 1 is put into crucible in melting resistance furnace, while indifferent gas is filled with into stove Body is protected, and melting 15 minutes, is subsequently added into described alloy gross mass 1.5% under conditions of being 800 DEG C in smelting temperature Carbon trichloride refines 5 ~ 20 minutes;
Step 4: the nickel powder that addition step 2 obtains in crucible melting 5-20 minutes under conditions of 900 DEG C, then use Water cooling ultrasonic head is applied in melting matrix alloy, continual application ultrasonic wave 1-20 minutes;Stand 5 ~ 20 minutes Skim afterwards, finally casting obtains nickel aluminide enhancing Cu-base composites;
Step 5: the composite after above-mentioned processing is subjected to hot extrusion;
Step 6:Hot rolling treatment is carried out more than recrystallization temperature;
Step 7:Alloy after step 6 is subjected to solution treatment.
Described fine aluminium is to be at least more than 99.99% using the purified aluminum after vacuum heat-treating method, purity.Ultrasonic wave Application frequency be 20 ~ 80 KHzs, amplitude be 20 ~ 50 microns.The weight of aluminium accounts for 12% in matrix material.Described step A kind of rapid addition intermediate alloy, described intermediate alloy are aluminum bronze intermediate alloy, the raw material of aluminium manganese intermediate alloy composition.Described The mass ratio of aluminum bronze intermediate alloy aluminium and copper is 1:1, the mass ratio of aluminium manganese intermediate alloy aluminium and manganese is 1:1.Intermediate alloy raw material The weight ratio for accounting for matrix material is 20%.
Described inert gas is helium, one or two kinds of mixtures of argon gas.Inert gas carries out pre- before addition Heat treatment.Contain nitrogen, described nitrogen and nickel production nickel oxide in described inert gas.
Specific embodiment 1:A kind of in-situ preparation nickel aluminide strengthens Cu-base composites, and preparation method is as follows:
Step 1: it is prepared by matrix material, the raw material that described matrix material is made up of fine aluminium, fine copper;
Step 2 weighs nickel powder and mixed successively with absolute ethyl alcohol and propyl alcohol, then mechanical agitation respectively, is then heated to ethanol and third Alcoholic solution all volatilizees, and obtains nickel powder;
It is placed in Step 3: matrix material in step 1 is put into crucible in melting resistance furnace, while indifferent gas is filled with into stove Body is protected, and melting 20 minutes, is subsequently added into described alloy gross mass 0.01% under conditions of being 700 DEG C in smelting temperature Carbon trichloride refining 5-20 minutes;
Step 4: the nickel powder that addition step 2 obtains in crucible melting 5 ~ 20 minutes under conditions of 700 ~ 950 DEG C, so It is applied to afterwards using water cooling ultrasonic head in melting matrix alloy, continual application ultrasonic wave 1 ~ 10 minute;Stand 5 ~ 20 Skimmed after minute, finally casting obtains nickel aluminide enhancing Cu-base composites;
Step 5: the composite after above-mentioned processing is subjected to hot extrusion;
Step 6:Hot rolling treatment is carried out more than recrystallization temperature;
Step 7:Alloy after step 6 is subjected to solution treatment.
Described fine aluminium is to be at least more than 99.99% using the purified aluminum after vacuum heat-treating method, purity.Ultrasonic wave Application frequency be 20 ~ 80 KHzs, amplitude be 20 ~ 50 microns.The weight of aluminium accounts for 15% in matrix material.Described step A kind of rapid addition intermediate alloy, described intermediate alloy are aluminum bronze intermediate alloy, the raw material of aluminium manganese intermediate alloy composition.Described The mass ratio of aluminum bronze intermediate alloy aluminium and copper is 1:1, the mass ratio of aluminium manganese intermediate alloy aluminium and manganese is 1:1.Intermediate alloy raw material The weight ratio for accounting for matrix material is 20%.
Described inert gas is helium, one or two kinds of mixtures of argon gas.Inert gas carries out pre- before addition Heat treatment.Contain nitrogen, described nitrogen and nickel production nickel oxide in described inert gas.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all essences in the present invention All any modification, equivalent and improvement made within refreshing and principle etc., should be included in the scope of the protection.

Claims (10)

1. a kind of preparation method of in-situ preparation nickel aluminide enhancing Cu-base composites, it is characterised in that preparation method is as follows:
Step 1: it is prepared by matrix material, the raw material that described matrix material is made up of fine aluminium, fine copper;
Step 2 weighs nickel powder and mixed successively with absolute ethyl alcohol and propyl alcohol, then mechanical agitation respectively, is then heated to ethanol and third Alcoholic solution all volatilizees, and obtains nickel powder;
It is placed in Step 3: matrix material in step 1 is put into crucible in melting resistance furnace, while indifferent gas is filled with into stove Body is protected, and melting 5 ~ 20 minutes, is subsequently added into described alloy gross mass under conditions of being 700 ~ 950 DEG C in smelting temperature 0.01% ~ 2.1% carbon trichloride refines 5 ~ 20 minutes;
Step 4: the nickel powder that addition step 2 obtains in crucible melting 5 ~ 20 minutes under conditions of 700 ~ 950 DEG C, so It is applied to afterwards using water cooling ultrasonic head in melting matrix alloy, continual application ultrasonic wave 1 ~ 10 minute;Stand 5 ~ 20 Skimmed after minute, finally casting obtains nickel aluminide enhancing Cu-base composites;
Step 5: the composite after above-mentioned processing is subjected to hot extrusion;
Step 6:Hot rolling treatment is carried out more than recrystallization temperature;
Step 7:Alloy after step 6 is subjected to solution treatment.
2. the preparation method of in-situ preparation nickel aluminide enhancing Cu-base composites according to claim 1, it is characterised in that Described fine aluminium is to be at least more than 99.99% using the purified aluminum after vacuum heat-treating method, purity.
3. the preparation method of in-situ preparation nickel aluminide enhancing Cu-base composites according to claim 2, it is characterised in that The application frequency of ultrasonic wave is 20 ~ 80 KHzs, amplitude is 20 ~ 50 microns.
4. the preparation method of in-situ preparation nickel aluminide enhancing Cu-base composites according to claim 3, it is characterised in that The weight of aluminium is accounted between 10%-15% in matrix material.
5. the preparation method of in-situ preparation nickel aluminide enhancing Cu-base composites according to claim 4, it is characterised in that Described step is a kind of to add intermediate alloy, and described intermediate alloy is aluminum bronze intermediate alloy, the original of aluminium manganese intermediate alloy composition Material.
6. the preparation method of in-situ preparation nickel aluminide enhancing Cu-base composites according to claim 5, it is characterised in that Described aluminum bronze intermediate alloy aluminium and the mass ratio of copper are 1:1, the mass ratio of aluminium manganese intermediate alloy aluminium and manganese is 1:1.
7. in-situ preparation nickel aluminide according to claim 6 strengthens Cu-base composites, it is characterised in that intermediate alloy is former The weight ratio that material accounts for matrix material is 20%.
8. in-situ preparation nickel aluminide according to claim 7 strengthens Cu-base composites, it is characterised in that described inertia Gas is helium, one or two kinds of mixtures of argon gas.
9. in-situ preparation nickel aluminide according to claim 8 strengthens Cu-base composites, it is characterised in that described is lazy Property gas carries out the pre-heat treatment before addition.
10. in-situ preparation nickel aluminide according to claim 9 strengthens Cu-base composites, it is characterised in that described is lazy Property gas in contain nitrogen, described nitrogen and nickel production nickel oxide.
CN201710767764.7A 2017-08-31 2017-08-31 A kind of preparation method of in-situ preparation nickel aluminide enhancing Cu-base composites Pending CN107653384A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710767764.7A CN107653384A (en) 2017-08-31 2017-08-31 A kind of preparation method of in-situ preparation nickel aluminide enhancing Cu-base composites

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710767764.7A CN107653384A (en) 2017-08-31 2017-08-31 A kind of preparation method of in-situ preparation nickel aluminide enhancing Cu-base composites

Publications (1)

Publication Number Publication Date
CN107653384A true CN107653384A (en) 2018-02-02

Family

ID=61128893

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201710767764.7A Pending CN107653384A (en) 2017-08-31 2017-08-31 A kind of preparation method of in-situ preparation nickel aluminide enhancing Cu-base composites

Country Status (1)

Country Link
CN (1) CN107653384A (en)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5295531A (en) * 1976-02-06 1977-08-11 Olin Corp Precipitation hardened spinodal copper based alloy and method of obtaining it
CN1865465A (en) * 2006-06-19 2006-11-22 东北大学 Method and device for preparing gradient composite material using high intensity gradient magnetic field
CN103328665A (en) * 2010-12-13 2013-09-25 日本精线株式会社 Copper alloy and method for producing copper alloy
CN104878272A (en) * 2015-04-03 2015-09-02 中国科学院兰州化学物理研究所 Nickel aluminum/copper oxide high-temperature self-lubricating composite material and preparation method thereof

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5295531A (en) * 1976-02-06 1977-08-11 Olin Corp Precipitation hardened spinodal copper based alloy and method of obtaining it
CN1865465A (en) * 2006-06-19 2006-11-22 东北大学 Method and device for preparing gradient composite material using high intensity gradient magnetic field
CN103328665A (en) * 2010-12-13 2013-09-25 日本精线株式会社 Copper alloy and method for producing copper alloy
CN104878272A (en) * 2015-04-03 2015-09-02 中国科学院兰州化学物理研究所 Nickel aluminum/copper oxide high-temperature self-lubricating composite material and preparation method thereof

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
陶世平: "Cu-Ni-Al合金相图富Cu端合金的析出相表征", 《金属热处理》 *

Similar Documents

Publication Publication Date Title
CN102031399B (en) Method for preparing Cu-Fe alloy under action of magnetic field
CN106521250B (en) A kind of preparation method of big current-carrying heat-resistant aluminum alloy wire
CN105063403A (en) Preparation method of copper matrix graphene alloy
CN105063402A (en) Preparation method of aluminum base graphene alloy
CN102862003A (en) Silver-free copper based solder and preparation method thereof
CN106591639A (en) Electroconductive Al alloy material and preparation method thereof
CN104962789B (en) Aluminium alloy material used for preparing high temperature resistant brazed aluminium/steel composite sheet material prepared from aluminium-silicon brazing filler metal, and preparation method thereof
CN110273081A (en) A kind of Cu-Fe-Ti electrical conductivity alloy and preparation method thereof
CN103255319A (en) Al-Yb-Zr heatproof aluminium alloy and its heat treatment technology
CN104762520A (en) High-strength high-conductivity Cu-Fe-Ag in-situ composite material prepared by using directional solidification and method for preparing same
CN102634691B (en) Manufacturing method of high-strength and high-corrosion-resistance cupronickel alloy
CN101456122A (en) High-conductivity high silicon aluminum base alloy and manufacture method thereof
CN111636011A (en) High-strength high-conductivity copper-nickel-silicon alloy with good formability and preparation method thereof
CN102839304B (en) Aluminum alloy tube for camping tent support and preparation method thereof
CN107653384A (en) A kind of preparation method of in-situ preparation nickel aluminide enhancing Cu-base composites
CN107815559A (en) A kind of in-situ preparation nickel aluminide strengthens Cu-base composites
CN107090557A (en) A kind of aluminium alloy and preparation method for being used to prepare inexpensive high temperature resistant brazed aluminum/steel composite strip
CN102198570B (en) Heating welding flux of copper-coated steel/steel grounding network
CN101733621A (en) Method for preparing Cu-Cr-Zr alloy plate by modifying
CN103390820B (en) A kind of containing Sc, Ni aluminium alloy and copper connection terminal and preparation method thereof
CN103773991B (en) High-strength conductive copper rod material and preparation method thereof
CN102220524A (en) Preparation method of aluminum-nickel-titanium-carbon intermediate alloy
CN110527856B (en) Preparation method of high-surface-quality and high-strength nickel alloy strip
CN110257664B (en) Copper-based composite material and preparation method thereof
CN110592430B (en) TiAl alloy plate thermo-electric coupling non-sheath preparation method

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
RJ01 Rejection of invention patent application after publication

Application publication date: 20180202

RJ01 Rejection of invention patent application after publication