CN108620436B - A kind of titanium aluminum copper clad material and preparation method thereof - Google Patents

A kind of titanium aluminum copper clad material and preparation method thereof Download PDF

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CN108620436B
CN108620436B CN201810374921.2A CN201810374921A CN108620436B CN 108620436 B CN108620436 B CN 108620436B CN 201810374921 A CN201810374921 A CN 201810374921A CN 108620436 B CN108620436 B CN 108620436B
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titanium
copper
roll
aluminum
aluminium
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CN108620436A (en
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谢敬佩
苌清华
陈艳芳
马窦琴
毛爱霞
赵海丽
王爱琴
王文焱
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Henan University of Science and Technology
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21BROLLING OF METAL
    • B21B1/00Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations
    • B21B1/46Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations for rolling metal immediately subsequent to continuous casting
    • B21B1/463Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations for rolling metal immediately subsequent to continuous casting in a continuous process, i.e. the cast not being cut before rolling
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00Layered products comprising a layer of metal
    • B32B15/01Layered products comprising a layer of metal all layers being exclusively metallic
    • B32B15/013Layered products comprising a layer of metal all layers being exclusively metallic one layer being formed of an iron alloy or steel, another layer being formed of a metal other than iron or aluminium
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00Layered products comprising a layer of metal
    • B32B15/20Layered products comprising a layer of metal comprising aluminium or 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
    • 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
    • C22F1/16Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of other metals or alloys based thereon
    • C22F1/18High-melting or refractory metals or alloys based thereon
    • C22F1/183High-melting or refractory metals or alloys based thereon of titanium or alloys based thereon

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Metal Rolling (AREA)

Abstract

The present invention relates to a kind of titanium aluminum copper clad materials and preparation method thereof, belong to technical field of composite material manufacturing.Titanium aluminum copper clad material of the invention includes the titanium layer, aluminium layer, layers of copper set gradually.The preparation method of titanium aluminum copper clad material of the invention include the following steps: by titanium plate and copper sheet interval setting make to form gap between titanium plate and copper sheet, molten aluminum is cast into the gap between titanium plate and copper sheet, rolling to get.Titanium aluminum copper clad material of the invention combines the performance of titanium, three kinds of aluminium, copper metals, both realizes replacing copper with aluminium, realizes with aluminium section titanium, can show the advantages such as titanium-the highly conductive of Solder for Al-Cu Joint Welding composite plate, high thermal conductivity, corrosion-resistant, at low cost.

Description

A kind of titanium aluminum copper clad material and preparation method thereof
Technical field
The present invention relates to a kind of titanium aluminum copper clad materials and preparation method thereof, belong to technical field of composite material manufacturing.
Background technique
With being constantly progressive for science and technology, the material of single component has been difficult to meet modern industry comprehensive to material The requirement of energy, more and more fields start largely to use composite material.Double metallic composite material is as one in composite material Kind, it not only can satisfy and the complexity of material required in design, while also the comprehensive performance of composite material can be made to embody. Therefore, extensive concern of the bimetallic material increasingly by countries in the world.
Copper has many advantages, such as that high conductivity, high thermal conductivity, contact resistance are low, intensity is high, corrosion-resistant, diamagnetism, specious, At present often by fields such as vessel, electric power facility, ocean shippings.But copper content in the earth's crust only has 0.01wt%, leads to state Border copper processing persistently rises.Simultaneously as China's copper ore resource is deficient, a large amount of import copper products will cause capital outflow, influence Domestic economy development.Therefore, the research of the substitute of copper product seems significant.
Aluminium content in the earth's crust is high, and use scope is only second to steel, and has light weight, cheap, thermally conductive and lead Electrically the advantages that good, easy processing.But since aluminium hardness is small, tensile strength is low, it is difficult directly in the high occasion of some hardness requirements It connects and replaces copper.In the occasion less high to hardness requirement, the composite material of aluminium and copper has a good application prospect.Titanium has height Tensile strength and corrosion resistance, but titanium price is relatively higher.Designing and manufacturing titanium-Solder for Al-Cu Joint Welding composite material will be able to have The institute of three's basis material is advantageous, obtains that a kind of cost performance is very high, composite material of function admirable.
The currently used complex method of 3-layer composite material is Hot rolling, though Hot rolling can be realized the system of composite material It is standby, but the method processing technology is complicated, needing for trilaminate material to be stacked together, it is compound to carry out heating rolling, and needs not Interface cohesion is realized in disconnected rolling back and forth.Rolling is easy to destroy the interface that composite plate is formed back and forth, reduces bond strength.Meanwhile This method is difficult the width of control interface binder course and the type of intermetallic compound.
Producing 3-layer composite material, there are also the modes such as Explosion composite, but Explosion composite is difficult to realize the homogenization at interface, Although many fire points can be disposed, interface discontinuously will affect the bond strength of composite plate, meanwhile, Explosion composite environment It is poor, the SO for having pollution to atmosphere can be generated2Equal gases.
Metallurgical bonding is also to produce a kind of mode of composite plate, can make to realize that metallurgical interface combines, continuously nothing is split at interface Line.Application publication number is that the Chinese invention patent of CN102205346A discloses a kind of preparation side of copper-aluminum-copper composite board Method, this method are oppositely arranged vertically by showing two blocks the copper alloy of cleaning pretreatment, and the molten aluminum after fusing is poured into two pieces Alloy blank is obtained between copper alloy, alloy blank is heat-treated, then rolling copper aluminum bronze three-layer composite board.Due to this Method preparation is copper aluminum bronze three-layer composite board, and what it is positioned at aluminium two sides is copper sheet, and composite board can not be made to have the characteristic of titanium.
Summary of the invention
The purpose of the present invention is to provide one kind can integrate titanium, aluminium, three kinds of metallic characters of copper titanium aluminum copper clad material.
The object of the invention is also to provide the preparation methods of above-mentioned titanium aluminum copper clad material.
To achieve the above object, the technical solution of titanium aluminum copper clad material of the invention is:
A kind of titanium aluminum copper clad material, including the titanium layer, aluminium layer, layers of copper set gradually.
Titanium aluminum copper clad material of the invention combines the performance of titanium, three kinds of aluminium, copper metals, both realizes replacing copper with aluminium, It is realized again with aluminium section titanium, the advantages such as titanium-the highly conductive of Solder for Al-Cu Joint Welding composite plate, high thermal conductivity, corrosion-resistant, at low cost can be shown.
The ratio between the titanium layer, aluminium layer, copper layer thickness are 0.5-1:2-4:1.5-3.
Titanium plate uses TA1 titanium.Aluminium layer uses 1060 aluminium.Copper sheet uses T2 copper.
Above-mentioned copper layer thickness is 1.5-3mm.Titanium layer is with a thickness of 0.5-1mm.Aluminum layer thickness is 2-4mm.
The technical solution of the preparation method of titanium aluminum copper clad material of the invention is as follows:
A kind of preparation method of titanium aluminum copper clad material includes the following steps: titanium plate and the setting of copper sheet interval making titanium plate Form gap between copper sheet, molten aluminum be cast into the gap between titanium plate and copper sheet, rolling to get.
The molten aluminum is semisolid molten aluminum.It is poured using semisolid molten aluminum, molten aluminum is easy molding, is convenient for subsequent rolling When formed meet need aluminium layer, avoid using liquid aluminium liquid be easy flowing, be not easy the problem of rolling.
The rolling is heat transfer, and revolving speed when heat transfer close to the roll of titanium plate is lower than the roll close to copper sheet Revolving speed.If influencing whether the interface cohesion of titanium plate and aluminium and copper sheet and aluminium using identical slewing rate.Asymmetrical rolling energy Enough guarantee that inside the aluminium layer of composite plate be not in stratum.
The heat transfer is to be rolled simultaneously using the first roll close to titanium plate and the second roll close to copper sheet.It is close The ratio between the roll of titanium plate and revolving speed of roll of close copper sheet are 1:1.2-1.5.The velocity of rotation of roll close to titanium plate is 0.3-1m/min。
During the rolling, roll is used as crystallizer simultaneously.Lead to cooling water inside roll, molten aluminum is promoted to solidify in time.
It is compound using anaerobic during the rolling.The compound destruction that can reduce oxide to interface of anaerobic.
It is above-mentioned to be set to parallel interval setting.
The titanium plate is before the setting of interval by annealing.The annealing temperature of the titanium plate annealing is 200 DEG C ~300 DEG C.
Annealing is the stress for removing plate.
The copper sheet is before the setting of interval by annealing.The temperature of the copper sheet annealing is 100 DEG C~200 DEG C.
Annealing is the stress for removing plate.
It is surface-treated after titanium plate annealing and before the setting of interval, the surface treatment is first to remove surface impurity and oil Rouge, then with pickling descale.
It is surface-treated after copper sheet annealing and before the setting of interval, the surface treatment is first to remove surface impurity and oil Rouge, then with pickling descale.
Above-mentioned copper plate thickness is 1.5-3mm.Titanium plate thickness is 0.5-1mm.Aluminum layer thickness is 2-4mm.
It is made annealing treatment after rolling, the temperature of annealing is 230-250 DEG C.Annealing herein is to remove rolling Stress prevents composite board from cracking, and improves the cycling processability of composite board.
Molten aluminum is obtained using 1060 aluminium meltings.Molten aluminum removes the foreign gas in aluminium using refining.Titanium plate uses TA1 titanium. Copper sheet uses T2 copper.
Two interfacial thicknesses of the titanium aluminum copper clad material of above method production are between 1~2 μm.
The beneficial effects of the present invention are:
Titanium aluminum copper clad material of the invention can combine three kinds of titanium, aluminium, copper materials, substantially increase material Overall performance.
Titanium aluminum copper clad material of the invention can be realized the titanium aluminum bronze richness produced deteriorate material interface it is continuous, without splitting Line, clean, free from admixture, the combination of interlayer reach metallurgical bonding.Simple production process, the compound straight free from admixture of board interface influence.
Specific embodiment
Technical solution of the present invention is described further combined with specific embodiments below.
Embodiment 1
The titanium aluminum copper clad material of the present embodiment includes the titanium layer, aluminium layer and layers of copper of successively compound setting.The thickness of titanium layer For 0.5mm.Aluminium layer with a thickness of 2mm.Layers of copper with a thickness of 1.5mm.Aluminium layer is 1060 aluminium.Titanium layer is TA1 titanium.Layers of copper is T2 Copper.
The composite board manufacturing device that uses when the titanium aluminum copper clad material preparation of the present embodiment, including two be arranged in parallel Roll and the casting container that is arranged in above two rolls disposed in parallel.Two rolls disposed in parallel are respectively first Roll and second roll.Gap is provided between first roll and second roll.Two rolls are respectively by two different drivings Mechanism driving is different to facilitate the revolving speed for adjusting two rolls.
The roll surface of first roll and second roll is along axial equal length.First roll is corresponding with titanium plate, is used to titanium Plate is set up thereon.Second roll is corresponding with copper sheet, for setting up thereon copper sheet.Casting container includes the appearance for containing aluminum fluid Device ontology and the molten aluminum discharging gate that vessel lower end is set.Molten aluminum discharging gate includes the material receiving end being connected with vessel And the discharge end far from material receiving end.In the present embodiment, vessel is that section is rectangular tubular structure.Specifically, container Ontology upper and lower opening, section in the horizontal direction are rectangle.The roll surface of length and roll of the rectangle on roll axial direction is long It spends equal.
The preparation method of the titanium aluminum copper clad material of the present embodiment, includes the following steps:
1) annealing 1h will be carried out at 300 DEG C with a thickness of the progress of the TA1 titanium plate of 0.5mm, surface then is carried out to titanium plate Processing, the step of surface treatment include: that the dirt and grease on titanium plate surface are first brushed away with steel brush, then with mass fraction are 20% Hydrochloric acid cleaning removes surface scale.Titanium plate after surface treatment is wound on the first unwinding device.
2) by with a thickness of the T2 copper sheet of 1.5mm in 200 DEG C of annealing 1h;Then copper sheet is surface-treated, surface The step of processing includes: the dirt and grease that copper sheet surface is first brushed away with steel brush, then is cleaned with the hydrochloric acid that mass fraction is 20% Remove surface scale.Copper sheet after surface treatment is wound on the second unwinding device.
3) by 1060 aluminium, melting forms molten aluminum at 700 DEG C, then carries out refining degasification to molten aluminum under anaerobic.
4) first roll and second roll are arranged in parallel, there are gap, the gaps between first roll and second roll Width be 4mm;One end of titanium plate on first unwinding device is bypassed into first roll, by the copper sheet on the second unwinding device One end bypasses second roll, and one end of the titanium plate around first roll and one end of the copper sheet around second roll is arranged in parallel And the gap for being used to accommodate molten aluminum is formed between, it is 2mm for accommodating the width in the gap of molten aluminum;
Then the molten aluminum after refining in step 3) is cast into the gap of the receiving molten aluminum between aluminium sheet and copper sheet, simultaneously Rotate first roll and second roll, the velocity of rotation of first roll is 0.3m/min, and the revolving speed of second roll is 0.36m/ The speed adjustment control of min, molten aluminum casting are so that the discharging speed for the titanium aluminum copper composite plate that roll-in is formed is 0.5m/min.By It is higher than copper in the tensile strength of titanium, and the heating conduction of titanium is lower than copper, the revolving speed of the corresponding roll of copper sheet is corresponding higher than titanium plate Roll revolving speed, can guarantee that finally formed composite board internal is not in stratum.
While rolling, the composite plate that rolling obtains is pulled using wrap-up, while being wound.It has wound Cheng Hou forms compound coiled sheet, compound coiled sheet is carried out at 230 DEG C annealing 0.5h to get.
Embodiment 2
The titanium aluminum copper clad material of the present embodiment includes the titanium layer, aluminium layer and layers of copper of successively compound setting.The thickness of titanium layer For 0.8mm.Aluminium layer with a thickness of 3.2mm.Layers of copper with a thickness of 2.4mm.Aluminium layer is 1060 aluminium.Titanium layer is TA1 titanium.Layers of copper is T2 Copper.
The preparation method of the titanium aluminum copper clad material of the present embodiment, includes the following steps:
1) annealing 1h will be carried out at 300 DEG C with a thickness of the progress of the TA1 titanium plate of 0.8mm, surface then is carried out to titanium plate Processing, the step of surface treatment include: that the dirt and grease on titanium plate surface are first brushed away with steel brush, then with mass fraction are 20% Hydrochloric acid cleaning removes surface scale.Titanium plate after surface treatment is wound on the first unwinding device.
2) by with a thickness of the T2 copper sheet of 2.4mm in 200 DEG C of annealing 1h;Then copper sheet is surface-treated, surface The step of processing includes: the dirt and grease that copper sheet surface is first brushed away with steel brush, then is cleaned with the hydrochloric acid that mass fraction is 20% Remove surface scale.Copper sheet after surface treatment is wound on the second unwinding device.
3) by 1060 aluminium, melting forms molten aluminum at 700 DEG C, then carries out refining degasification to molten aluminum under anaerobic.
4) first roll and second roll are arranged in parallel, there are gap, the gaps between first roll and second roll Width be 6.4mm;One end of titanium plate on first unwinding device is bypassed into first roll, by the copper sheet on the second unwinding device One end bypass second roll, make one end of the titanium plate around first roll with bypass that one end of copper sheet of second roll is parallel sets The gap for accommodating molten aluminum is set and formed between, is 3.2mm for accommodating the width in the gap of molten aluminum;
Then the molten aluminum after refining in step 3) is cast into the gap of the receiving molten aluminum between aluminium sheet and copper sheet, simultaneously Rotate first roll and second roll, the velocity of rotation of first roll is 0.5m/min, and the revolving speed of second roll is 0.6m/ The speed adjustment control of min, molten aluminum casting are so that the discharging speed for the titanium aluminum copper composite plate that roll-in is formed is 1m/min.Due to The tensile strength of titanium is higher than copper, and the heating conduction of titanium is lower than copper, and it is corresponding that the revolving speed of the corresponding roll of copper sheet is higher than titanium plate The revolving speed of roll can guarantee that finally formed composite board internal is not in stratum.
While rolling, the composite plate that rolling obtains is pulled using wrap-up, while being wound.It has wound Cheng Hou forms compound coiled sheet, compound coiled sheet is carried out at 240 DEG C annealing 0.5h to get.
Embodiment 3
The titanium aluminum copper clad material of the present embodiment includes the titanium layer, aluminium layer and layers of copper of successively compound setting.The thickness of titanium layer For 1mm.Aluminium layer with a thickness of 4mm.Layers of copper with a thickness of 3mm.Aluminium layer is 1060 aluminium.Titanium layer is TA1 titanium.Layers of copper is T2 copper.
The preparation method of the titanium aluminum copper clad material of the present embodiment, includes the following steps:
1) annealing 1h will be carried out at 200 DEG C with a thickness of the progress of the TA1 titanium plate of 1mm, then titanium plate is carried out at surface Reason, the step of surface treatment include: the dirt and grease on titanium plate surface are first brushed away with steel brush, then with mass fraction for 20% salt Acid cleaning removes surface scale.Titanium plate after surface treatment is wound on the first unwinding device.
2) by with a thickness of the T2 copper sheet of 3mm in 100 DEG C of annealing 1h;Then copper sheet is surface-treated, at surface The step of reason includes: the dirt and grease that copper sheet surface is first brushed away with steel brush, then is cleaned and removed with the hydrochloric acid that mass fraction is 20% Remove surface scale.Copper sheet after surface treatment is wound on the second unwinding device.
3) by 1060 aluminium, melting forms molten aluminum at 700 DEG C, then carries out refining degasification to molten aluminum under anaerobic.
4) first roll and second roll are arranged in parallel, there are gap, the gaps between first roll and second roll Width be 8mm;One end of titanium plate on first unwinding device is bypassed into first roll, by the copper sheet on the second unwinding device One end bypasses second roll, and one end of the titanium plate around first roll and one end of the copper sheet around second roll is arranged in parallel And the gap for being used to accommodate molten aluminum is formed between, it is 4mm for accommodating the width in the gap of molten aluminum;
Then the molten aluminum after refining in step 3) is cast into the gap of the receiving molten aluminum between aluminium sheet and copper sheet, simultaneously First roll and second roll are rotated, the velocity of rotation of first roll is 1m/min, and the revolving speed of second roll is 1.2m/min, The speed adjustment control of molten aluminum casting is so that the discharging speed for the titanium aluminum copper composite plate that roll-in is formed is 1.5m/min.Due to titanium Tensile strength be higher than copper, and the heating conduction of titanium is lower than copper, and the revolving speed of the corresponding roll of copper sheet is higher than that titanium plate is corresponding to roll The revolving speed of roller can guarantee that finally formed composite board internal is not in stratum.
While rolling, the composite plate that rolling obtains is pulled using wrap-up, while being wound.It has wound Cheng Hou forms compound coiled sheet, compound coiled sheet is carried out at 250 DEG C annealing 0.5h to get.
Test example
Bond strength test:
Each three groups of titanium aluminum copper clad material in Example 1-3 are used as sample, are combined strength test, test result As shown in table 1.
The bond strength of titanium aluminum copper clad material in 1 embodiment 1-3 of table
As can be seen from Table 1, titanium aluminum copper clad material produced by the present invention, bond strength are excellent.

Claims (4)

1. a kind of preparation method of titanium aluminum copper clad material, which comprises the steps of: set titanium plate and copper sheet interval Setting makes to form gap between titanium plate and copper sheet, and molten aluminum is cast into the gap between titanium plate and copper sheet, rolling to get;
The molten aluminum is semisolid molten aluminum;
The rolling is heat transfer, and revolving speed when heat transfer close to the roll of titanium plate is lower than turning for the roll close to copper sheet The ratio between speed, the roll close to titanium plate and revolving speed of roll close to copper sheet are 1:1.2-1.5;
It is made annealing treatment after the rolling, the temperature of annealing is 230-250 DEG C.
2. the preparation method of titanium aluminum copper clad material according to claim 1, it is characterised in that: the roll of close titanium plate Velocity of rotation is 0.3-1m/min.
3. the preparation method of titanium aluminum copper clad material according to claim 1, it is characterised in that: the titanium plate and copper sheet exist It is made annealing treatment before the setting of interval.
4. the preparation method of titanium aluminum copper clad material according to claim 1, it is characterised in that: the preparation method is resulting The ratio between titanium layer, aluminium layer, thickness of layers of copper are 0.5-1:2-4:1.5-3.
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Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102205346A (en) * 2011-04-28 2011-10-05 上海交通大学 Method for preparing copper-aluminum-copper compound board
WO2012012389A1 (en) * 2010-07-19 2012-01-26 Ems Engineered Materials Solutions, Llc A metallic composite material
CN102671944A (en) * 2011-12-25 2012-09-19 河南科技大学 Device for forming three-layer metal composite plate by cast-rolling compounding by brazing method
CN202621550U (en) * 2012-04-17 2012-12-26 红光电气集团有限公司 Processing equipment for cold rolling manufacture of copper-aluminum composite plate strips
CN105170652A (en) * 2015-08-31 2015-12-23 东北大学 Preparation method for multilayer dissimilar metal composite ultra-thin strip

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20020006526A1 (en) * 1999-10-11 2002-01-17 Polese Frank J. Aluminum silicon carbide and copper clad material and manufacturing process

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2012012389A1 (en) * 2010-07-19 2012-01-26 Ems Engineered Materials Solutions, Llc A metallic composite material
CN102205346A (en) * 2011-04-28 2011-10-05 上海交通大学 Method for preparing copper-aluminum-copper compound board
CN102671944A (en) * 2011-12-25 2012-09-19 河南科技大学 Device for forming three-layer metal composite plate by cast-rolling compounding by brazing method
CN202621550U (en) * 2012-04-17 2012-12-26 红光电气集团有限公司 Processing equipment for cold rolling manufacture of copper-aluminum composite plate strips
CN105170652A (en) * 2015-08-31 2015-12-23 东北大学 Preparation method for multilayer dissimilar metal composite ultra-thin strip

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