CN106623424A - Preparing method of multi-layer corrosion resistant lightweight aluminum titanium composite plate - Google Patents
Preparing method of multi-layer corrosion resistant lightweight aluminum titanium composite plate Download PDFInfo
- Publication number
- CN106623424A CN106623424A CN201611118497.2A CN201611118497A CN106623424A CN 106623424 A CN106623424 A CN 106623424A CN 201611118497 A CN201611118497 A CN 201611118497A CN 106623424 A CN106623424 A CN 106623424A
- Authority
- CN
- China
- Prior art keywords
- aluminium
- titanium
- pure
- composite panel
- clad
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21B—ROLLING OF METAL
- B21B1/00—Metal-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
- B21B1/38—Metal-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 sheets of limited length, e.g. folded sheets, superimposed sheets, pack rolling
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21B—ROLLING OF METAL
- B21B9/00—Measures for carrying out rolling operations under special conditions, e.g. in vacuum or inert atmosphere to prevent oxidation of work; Special measures for removing fumes from rolling mills
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/16—Changing 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
- C22F1/18—High-melting or refractory metals or alloys based thereon
- C22F1/183—High-melting or refractory metals or alloys based thereon of titanium or alloys based thereon
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21B—ROLLING OF METAL
- B21B1/00—Metal-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
- B21B1/38—Metal-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 sheets of limited length, e.g. folded sheets, superimposed sheets, pack rolling
- B21B2001/386—Plates
Landscapes
- 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)
- Laminated Bodies (AREA)
Abstract
The invention belongs to the technical field of layer-shaped composite material preparation, and relates to a preparing method of a multi-layer corrosion resistant lightweight aluminum titanium composite plate. The method comprises the process steps of surface treatment of a surface to be composited of a pure aluminum and LY12 aluminum alloy plate, pure aluminum and aluminum alloy plate riveting assembling, pure aluminum and aluminum plate hot-rolling-bonding, leveling and cutting size of a composite aluminum plate, pure titanium plate annealing treatment, surface treatment of a composite surface of a composite aluminum plate and a pure titanium plate, riveting assembling of the composite plate and the pure titanium plate, rolling compositing of an aluminum titanium composite plate and leveling and cutting size of the aluminum titanium composite plate. The prepared multi-layer aluminum titanium composite plate has good corrosion resistance and high strength, achieves the lightweight property, and has a wide application prospect.
Description
Technical field
The invention belongs to laminar composite preparing technical field, and in particular to a kind of multilayer corrosion-proof lightweight aluminium titanium composite panel
Preparation method.
Background technology
Aluminum laminate titanium composite panel has the high temperature resistant of low-gravity, high-termal conductivity and the titanium of aluminium, corrosion resistant feature concurrently, therefore,
Aluminium-titanium composite panel can be widely applied to the fields such as Aeronautics and Astronautics and petrochemical industry.Preparing the method for laminated composite plate at present has solid
Liquid is compound, Explosion composite, thermal diffusion are compound and Rolling compund.The low cost of solid-liquid complex method, the bond strength of compound interface
Height, but for preparing during aluminium titanium composite panel, can only in the pure aluminum or aluminum alloy that titanium plate Coating a layer thickness is 0.5～2mm,
It is difficult to prepare the lightweight aluminium titanium composite panel that one layer of thin titanium layer is combined in surface of aluminum plate；The interface bond strength of Explosion composite method
Height, for preparing during aluminium titanium composite panel, can as needed adjust the thickness of titanium layer and aluminium lamination, but the cost of Explosion composite method
It is very high, limit its extensive application；Thermal diffusion complex method is adapted to mate with additive method and is used together, and thermal diffusion is used alone
When complex method prepares aluminium titanium composite panel, interface bond strength is very low；Rolling compund is that a kind of inexpensive, efficient stratiform is answered
The preparation method of plywood, but when high strength alumin ium alloy plate and the direct assembly of titanium plate are rolled, pass deformation is little, interface cohesion
Intensity is relatively low, it is difficult to prepare high performance aluminium titanium composite panel.Therefore need to be improved on the basis of existing process method,
Develop a kind of low cost, high efficiency, the preparation method of the high-performance aluminum laminate titanium composite panel of high interfacial bonding strength.
The present invention prepares the Problems Existing of aluminium titanium composite panel for Rolling compund method, there is provided a kind of " fine aluminium-LY12 aluminium
The preparation method of alloy-fine aluminium-pure titanium " multilayer composite sheet." fine aluminium-LY12 is prepared initially with large deformation composite technique for rolling
Aluminium alloy-fine aluminium " clad aluminium, then clad aluminium is combined with each other with Titanium board using large deformation composite technique for rolling, from
And prepare " the pure titanium of fine aluminium-LY12 aluminium alloy-fine aluminiums-" multilayer composite sheet.In multilayer aluminum titanium composite panel, the aluminum layer of outer layer
The good performance of corrosion resistance is played in the medium of respective contact respectively with pure titanium layer；Middle duralumin layer (LY12 aluminium alloys) rises and carries
The effect of high intensity；Middle aluminum layer can be realized respectively preferably combining with duralumin layer and pure titanium layer, as duralumin layer and
Excessive layer between pure titanium layer, can prevent crackle and cracking occur in large deformation Rolling compund plus man-hour interface, improve interface cohesion
Intensity.
The content of the invention
It is an object of the invention to provide a kind of preparation side of " the pure titanium of fine aluminium-LY12 aluminium alloy-fine aluminiums-" multilayer composite sheet
Method, it is characterised in that comprise the steps：
(1) surface treatment on pure aluminum plate and LY12 aluminium alloy plates surface to be composite：Select the pure aluminum plate through annealing
With LY12 aluminium alloy plates, pure aluminum plate and LY12 aluminium alloy plates surface to be composite are polished using the method for mechanical grinding, it
Sheet material is stored in dry environment afterwards, and was used within 24 hours；
The riveting assembly of (2) three layers of aluminium sheet：Three aluminium sheets are carried out into four sides riveting assembly, assemble pattern is " fine aluminium-LY12
Block pure aluminum plate of aluminium alloy-fine aluminium ", i.e., two is clipped in the middle LY12 aluminium alloy plates；
(3) aluminum plate hot rolling is combined：One group of " fine aluminium-LY12 aluminium alloys-fine aluminium " sheet material for having organized base is put into nitrogen protection
Heated in atmosphere heating furnace, then carried out single pass great-deformation hot-rolled compound；
(4) smoothing of clad aluminium and cutting is sized：" fine aluminium-LY12 aluminium alloys-fine aluminium " composite plate after hot rolling is carried out
Smoothing process, and carry out cutting being sized；
(5) annealing of Titanium board：Titanium board is made annealing treatment；
(6) surface treatment on clad aluminium and Titanium board surface to be composite：Take clad aluminium and through the pure of annealing
Titanium plate, is polished clad aluminium and Titanium board surface to be composite using the method for mechanical grinding, is then stored in sheet material
In dry environment, and used within 24 hours.
(7) the riveting assembly of clad aluminium and Titanium board：Clad aluminium and Titanium board are carried out into four sides riveting assembly, assembly
Mode is " clad aluminium-pure titanium-pure titanium-clad aluminium ", i.e., including pure titanium layer, aluminium lamination outside, is applied between two Titanium boards
Last layer talcum powder, prevents the bonding between Titanium board；
(8) aluminium titanium composite panel Rolling compund：One group of " clad aluminium-pure titanium-pure titanium-clad aluminium " sheet material of base will have been organized
It is put into nitrogen protection atmosphere heating furnace and is heated, then carries out single pass large deformation Rolling compund；
(9) aluminium titanium composite panel smoothing：One group of aluminium titanium composite panel after by rolling is taken apart, and to individual aluminium titanium composite panel school is carried out
It is flat；
(10) cut and be sized：Aluminium titanium composite panel after smoothing is cut and is sized, obtain finished product sheet material.
The thickness of pure aluminum plate is 0.5～1mm in the step (1), and the thickness of LY12 aluminium alloy plates is 9～12mm.
420～460 DEG C of clad aluminium heating-up temperature in the step (3), is incubated 1～5 hour, and pass deformation is 60%
～75%.
The thickness of Titanium board is 0.5～1mm in the step (5), and annealing process is：Vacuum≤1 × 10-2Pa, annealing
Temperature is 650～750 DEG C, is incubated 1～1.5 hour, along with the furnace cooling.
420～460 DEG C of aluminium titanium composite panel heating-up temperature in the step (8), is incubated 1～5 hour, and single pass large deformation is rolled
The compound pass deformation of system is 60%～75%.
Beneficial effects of the present invention are：1. fine aluminium meal, LY12 aluminium alloy plates and Titanium board are compounded in using rolling mill practice
Together, multilayer aluminum titanium composite panel is prepared, both with good corrosion resistance and higher intensity, lightweight is realized again, will be had
Have broad application prospects；2. it is 1～2mm multilayer aluminum titanium composite panels to be suitable for producing aluminium titanium composite panel, particularly thickness in batches
The preparation processing of thin plate.
Description of the drawings
Fig. 1 is the preparation technology flow chart of multilayer corrosion-proof lightweight aluminium titanium composite panel.
Specific embodiment
The invention provides a kind of preparation method of multilayer corrosion-proof lightweight aluminium titanium composite panel, below by accompanying drawing and specifically real
The present invention will be further described to apply mode.
Embodiment 1
Preparation technology flow chart according to Fig. 1, thickness is as follows for the preparation process of 1mm aluminium titanium composite panels：
(1) surface treatment on pure aluminum plate and LY12 aluminium alloy plates surface to be composite：Select the pure aluminum plate through annealing
With LY12 aluminium alloy plates, pure aluminum plate specification be 1050 × 1050 × 1mm, aluminium alloy LY12 plate gauges lattice be 1050 × 1050 ×
12mm；Pure aluminum plate and LY12 aluminium alloy plates surface to be composite are polished using the method for mechanical grinding, and is cleaned out, beaten
Sheet material after mill is preserved in a dry environment, and is used within 24 hours；
The riveting assembly of (2) three layers of aluminium sheet：Three aluminium sheets are carried out into four sides riveting assembly, assemble pattern is " fine aluminium-LY12
Block pure aluminum plate of aluminium alloy-fine aluminium ", i.e., two is clipped in the middle LY12 aluminium alloy plates；
(3) aluminum plate hot rolling is combined：One group of " fine aluminium-LY12 aluminium alloys-fine aluminium " sheet material for having organized base is put into nitrogen protection
It is heated to 460 DEG C in atmosphere heating furnace, is incubated 1 hour, then carry out great-deformation hot-rolled compound, the deflection of single pass is
75%, after rolling, clad aluminium thickness is 3.5mm；
(4) smoothing of clad aluminium and cutting is sized, and " fine aluminium-LY12 aluminium alloys-fine aluminium " after hot rolling is combined
Plate carries out smoothing process, and cuts and be sized to 900 × 1000mm；
(5) annealing of Titanium board：The specification of Titanium board is 900 × 1000 × 0.5mm, and annealing process is：Vacuum
≤1×10-2Pa, annealing temperature is 750 DEG C, is incubated 1 hour, along with the furnace cooling；
(6) surface treatment on clad aluminium and Titanium board surface to be composite：The clad aluminium and pure of annealing of learning from else's experience
Titanium plate, is polished clad aluminium and Titanium board surface to be composite with the method for mechanical grinding, is afterwards stored in sheet material dry
In dry environment, and used within 24 hours；
(7) assembly of clad aluminium and Titanium board：Clad aluminium and Titanium board are carried out into four sides riveting assembly, assemble pattern
For " clad aluminium-pure titanium-pure titanium-clad aluminium ", i.e., including pure titanium layer, aluminium lamination outside, between two Titanium boards one is coated
Layer talcum powder, prevents the bonding between Titanium board；
(8) aluminium titanium composite panel Rolling compund：One group of " clad aluminium-pure titanium-pure titanium-clad aluminium " sheet material of base will have been organized
It is put into nitrogen protection atmosphere heating furnace and is heated to 460 DEG C, be incubated 1 hour, then carries out large deformation Rolling compund, single pass
Deflection is 75%.After rolling, the gross thickness of assembly " clad aluminium-pure titanium-pure titanium-clad aluminium " is changed into 2mm, individual
Compound plate thickness is 1mm；
(9) aluminium titanium composite panel smoothing：One group of aluminium titanium composite panel after by rolling is taken apart, then to single thickness for 1mm's
Aluminium titanium composite panel is smoothed；
(10) cut and be sized, the aluminium titanium composite panel after smoothing is cut and is sized, obtain finished product sheet material.
Embodiment 2
Preparation technology flow chart according to Fig. 1, thickness is as follows for the preparation process of 2mm aluminium titanium composite panels：
(1) surface treatment on pure aluminum plate and LY12 aluminium alloy plates surface to be composite：Select the pure aluminum plate through annealing
With LY12 aluminium alloy plates, pure aluminum plate specification be 1050 × 1050 × 0.5mm, aluminium alloy LY12 plate gauges lattice be 1050 × 1050 ×
9mm；Pure aluminum plate and LY12 aluminium alloy plates surface to be composite are polished using the method for mechanical grinding, and is cleaned out, beaten
Sheet material after mill is preserved in a dry environment, and is used within 24 hours；
The riveting assembly of (2) three layers of aluminium sheet：Three aluminium sheets are carried out into four sides riveting assembly, assemble pattern is " fine aluminium-LY12
Block pure aluminum plate of aluminium alloy-fine aluminium ", i.e., two is clipped in the middle LY12 aluminium alloy plates；
(3) aluminum plate hot rolling is combined：One group of " fine aluminium-LY12 aluminium alloys-fine aluminium " sheet material for having organized base is put into nitrogen protection
It is heated to 420 DEG C in atmosphere heating furnace, is incubated 5 hours, then carry out great-deformation hot-rolled compound, the deflection of single pass is
60%, after rolling, clad aluminium thickness is 4mm；
(4) smoothing of clad aluminium and cutting is sized, and " fine aluminium-LY12 aluminium alloys-fine aluminium " after hot rolling is combined
Plate carries out smoothing process, and cuts and be sized to 900 × 1000mm；
(5) annealing of Titanium board：The specification of Titanium board is 900 × 1000 × 1mm, and annealing process is：Vacuum≤1
×10-2Pa, annealing temperature is 650 DEG C, is incubated 1.5 hours, along with the furnace cooling；
(6) surface treatment on clad aluminium and Titanium board surface to be composite：The clad aluminium and pure of annealing of learning from else's experience
Titanium plate, is polished clad aluminium and Titanium board surface to be composite with the method for mechanical grinding, is afterwards stored in sheet material dry
In dry environment, and used within 24 hours；
(7) assembly of clad aluminium and Titanium board：Clad aluminium and Titanium board are carried out into four sides riveting assembly, assemble pattern
For " clad aluminium-pure titanium-pure titanium-clad aluminium ", i.e., including pure titanium layer, aluminium lamination outside, between two Titanium boards one is coated
Layer talcum powder, prevents the bonding between Titanium board；
(8) aluminium titanium composite panel Rolling compund：One group of " clad aluminium-pure titanium-pure titanium-clad aluminium " sheet material of base will have been organized
It is put into nitrogen protection atmosphere heating furnace and is heated to 420 DEG C, be incubated 5 hours, then carries out large deformation Rolling compund, single pass
Deflection is 60%.After rolling, the gross thickness of assembly " clad aluminium-pure titanium-pure titanium-clad aluminium " is changed into 4mm, individual
Aluminium titanium composite panel thickness is 2mm；
(9) aluminium titanium composite panel smoothing：One group of aluminium titanium composite panel after by rolling is taken apart, then to single thickness for 2mm's
Aluminium titanium composite panel is smoothed；
(10) cut and be sized, the aluminium titanium composite panel after smoothing is cut and is sized, obtain finished product sheet material.
Claims (5)
1. a kind of preparation method of multilayer corrosion-proof lightweight aluminium titanium composite panel, it is characterised in that comprise the steps：
(1) surface treatment on pure aluminum plate and LY12 aluminium alloy plates surface to be composite：Select through annealing pure aluminum plate and
LY12 aluminium alloy plates, are polished pure aluminum plate and LY12 aluminium alloy plates surface to be composite with the method for mechanical grinding, then will
Sheet material is stored in dry environment, and is used within 24 hours；
The riveting assembly of (2) three layers of aluminium sheet：Three aluminium sheets are carried out into four sides riveting assembly, assemble pattern is for " fine aluminium-LY12 aluminium is closed
Block pure aluminum plate of gold-fine aluminium ", i.e., two is clipped in the middle LY12 aluminium alloy plates；
(3) aluminum plate hot rolling is combined：One group of " fine aluminium-LY12 aluminium alloys-fine aluminium " sheet material for having organized base is put into nitrogen protection atmosphere
Heated in heating furnace, then carried out single pass great-deformation hot-rolled compound；
(4) smoothing of clad aluminium and cutting is sized：" fine aluminium-LY12 aluminium alloys-fine aluminium " composite plate after hot rolling is smoothed
Process, and carry out cutting being sized；
(5) annealing of Titanium board：Titanium board is made annealing treatment；
(6) surface treatment on clad aluminium and Titanium board surface to be composite：Clad aluminium and the Titanium board through annealing are taken,
Clad aluminium and Titanium board surface to be composite are polished using the method for mechanical grinding, then sheet material is stored in and is dried ring
In border, and used within 24 hours；
(7) the riveting assembly of clad aluminium and Titanium board：Clad aluminium and Titanium board are carried out into four sides riveting assembly, assemble pattern
For " clad aluminium-pure titanium-pure titanium-clad aluminium ", last layer talcum powder is applied between two Titanium boards, prevented between Titanium board
Bonding；
(8) aluminium titanium composite panel Rolling compund：One group of " clad aluminium-pure titanium-pure titanium-clad aluminium " sheet material for having organized base is put into
Heated in nitrogen protection atmosphere heating furnace, then carried out single pass large deformation Rolling compund；
(9) aluminium titanium composite panel smoothing：One group of aluminium titanium composite panel after by rolling is taken apart, and individual aluminium titanium composite panel is smoothed；
(10) cut and be sized：Aluminium titanium composite panel after smoothing is cut and is sized, obtain multilayer corrosion-proof lightweight aluminium titanium composite panel material.
2. the preparation method of a kind of multilayer corrosion-proof lightweight aluminium titanium composite panel according to claim 1, it is characterised in that described
The thickness of pure aluminum plate is 0.5～1mm in step (1), and the thickness of LY12 aluminium alloy plates is 9～12mm.
3. the preparation method of a kind of multilayer corrosion-proof lightweight aluminium titanium composite panel according to claim 1, it is characterised in that described
In step (3) clad aluminium heating-up temperature be 420～460 DEG C, temperature retention time be 1～5 hour, pass deformation be 60%～
75%.
4. the preparation method of a kind of multilayer corrosion-proof lightweight aluminium titanium composite panel according to claim 1, it is characterised in that described
The thickness of Titanium board is 0.5～1mm in step (5), and annealing process is：Vacuum≤1 × 10-2Pa, annealing temperature be 650～
750 DEG C, 1～1.5 hour is incubated, along with the furnace cooling.
5. a kind of preparation method of multilayer corrosion-proof lightweight aluminium titanium composite panel according to claim 1, it is characterised in that step
(8) 420～460 DEG C of aluminium titanium composite panel heating-up temperature in, temperature retention time is 1～5 hour, the road of single pass large deformation Rolling compund
Secondary deflection is 60%～75%.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611118497.2A CN106623424B (en) | 2016-12-07 | 2016-12-07 | A kind of preparation method of multilayer corrosion-proof lightweight aluminium titanium composite panel |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611118497.2A CN106623424B (en) | 2016-12-07 | 2016-12-07 | A kind of preparation method of multilayer corrosion-proof lightweight aluminium titanium composite panel |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106623424A true CN106623424A (en) | 2017-05-10 |
| CN106623424B CN106623424B (en) | 2018-06-15 |
Family
ID=58819927
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611118497.2A Active CN106623424B (en) | 2016-12-07 | 2016-12-07 | A kind of preparation method of multilayer corrosion-proof lightweight aluminium titanium composite panel |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106623424B (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110033947A (en) * | 2019-05-13 | 2019-07-19 | 南通海星电子股份有限公司 | A kind of high intensity electronic light foil and its manufacturing process |
| CN111906144A (en) * | 2020-07-17 | 2020-11-10 | 太原理工大学 | Method for improving interface bonding strength of titanium/aluminum composite board |
| CN111922077A (en) * | 2020-07-16 | 2020-11-13 | 太原理工大学 | Hole-pattern rolling forming method for metal laminated composite plate |
| CN113172962A (en) * | 2021-05-28 | 2021-07-27 | 太原理工大学 | High-conductivity corrosion-resistant layered composite board |
| CN113305171A (en) * | 2021-05-12 | 2021-08-27 | 北京科技大学 | Preparation method of titanium/aluminum laminated composite thin plate strip |
| CN114346626A (en) * | 2021-12-14 | 2022-04-15 | 常州市常蒸蒸发器有限公司 | Production method of roll-bond evaporator for new energy equipment |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2000273598A (en) * | 1999-03-24 | 2000-10-03 | Kobe Steel Ltd | Manufacture of high strength coil cold rolled titanium alloy sheet excellent in workability |
| CN101450542A (en) * | 2007-11-28 | 2009-06-10 | 北京有色金属研究总院 | Laminar titanium aluminum composite plate and preparation method thereof |
| CN101574861A (en) * | 2009-06-08 | 2009-11-11 | 昆明理工大学 | Titanium-coated aluminium laminated composite plate and preparation method thereof |
| CN101758070A (en) * | 2010-01-25 | 2010-06-30 | 洛阳铜一金属材料发展有限公司 | Production method of aluminum-titanium compounded metal plate strip |
| CN104209697A (en) * | 2013-06-04 | 2014-12-17 | 北京有色金属研究总院 | Method for manufacturing laminated titanium-aluminum composite board |
-
2016
- 2016-12-07 CN CN201611118497.2A patent/CN106623424B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2000273598A (en) * | 1999-03-24 | 2000-10-03 | Kobe Steel Ltd | Manufacture of high strength coil cold rolled titanium alloy sheet excellent in workability |
| CN101450542A (en) * | 2007-11-28 | 2009-06-10 | 北京有色金属研究总院 | Laminar titanium aluminum composite plate and preparation method thereof |
| CN101574861A (en) * | 2009-06-08 | 2009-11-11 | 昆明理工大学 | Titanium-coated aluminium laminated composite plate and preparation method thereof |
| CN101758070A (en) * | 2010-01-25 | 2010-06-30 | 洛阳铜一金属材料发展有限公司 | Production method of aluminum-titanium compounded metal plate strip |
| CN104209697A (en) * | 2013-06-04 | 2014-12-17 | 北京有色金属研究总院 | Method for manufacturing laminated titanium-aluminum composite board |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110033947A (en) * | 2019-05-13 | 2019-07-19 | 南通海星电子股份有限公司 | A kind of high intensity electronic light foil and its manufacturing process |
| CN111922077A (en) * | 2020-07-16 | 2020-11-13 | 太原理工大学 | Hole-pattern rolling forming method for metal laminated composite plate |
| CN111922077B (en) * | 2020-07-16 | 2022-03-18 | 太原理工大学 | Hole-pattern rolling forming method for metal laminated composite plate |
| CN111906144A (en) * | 2020-07-17 | 2020-11-10 | 太原理工大学 | Method for improving interface bonding strength of titanium/aluminum composite board |
| CN111906144B (en) * | 2020-07-17 | 2022-02-22 | 太原理工大学 | Method for improving interface bonding strength of titanium/aluminum composite board |
| CN113305171A (en) * | 2021-05-12 | 2021-08-27 | 北京科技大学 | Preparation method of titanium/aluminum laminated composite thin plate strip |
| CN113172962A (en) * | 2021-05-28 | 2021-07-27 | 太原理工大学 | High-conductivity corrosion-resistant layered composite board |
| CN114346626A (en) * | 2021-12-14 | 2022-04-15 | 常州市常蒸蒸发器有限公司 | Production method of roll-bond evaporator for new energy equipment |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106623424B (en) | 2018-06-15 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106623424B (en) | A kind of preparation method of multilayer corrosion-proof lightweight aluminium titanium composite panel | |
| CN110181227B (en) | Method for preparing aluminum/magnesium/aluminum composite board by three-dimensional layer interface | |
| CN105798062B (en) | A kind of method of oblique ripple roll Rolling compund strip | |
| CN105170652B (en) | A kind of preparation method of multi-layer heterogeneous metal composite strip in razor-thin | |
| WO2019148961A1 (en) | Method for preparing titanium-steel composite plate | |
| CN110548776A (en) | Method for preparing aluminum-magnesium-aluminum three-layer metal composite plate by prefabricating cross corrugated interface | |
| CN103935103B (en) | Preparation method of graphene/metal composite panel | |
| CN105618479B (en) | A kind of method of herringbone corrugating roll Rolling compund strip | |
| CN104209697B (en) | The preparation method of a kind of laminar titanium aluminum composite plate | |
| CN109177426B (en) | Hot-pressing compounding method of aluminum-magnesium interlayer composite board | |
| CN106180729A (en) | A kind of method preparing Metal Packaging intermetallic compound base lamination composite armour | |
| CN104907334A (en) | Machining method for preparing Al/Mg/Al alloy composite board by rolling | |
| CN104438322A (en) | Method for preparing metal layered micro-gradient composite material | |
| CN106424741A (en) | Preparation method of SiC particle enhanced intermetallic compound based laminated composite material Ti/Al3Ti | |
| CN115739998A (en) | Ultrasonic-assisted interface micro-melting warm-rolling compounding method for magnesium/titanium composite board with large thickness ratio | |
| US20040137260A1 (en) | Copper clad aluminum core composite material suitable for making a cellular telephone transmission tower antenna | |
| CN106563696A (en) | Manufacturing method for laminated composite metal board with slot holes in internal layer | |
| CN112828037B (en) | Method for preparing ultrathin aluminum-magnesium layered composite material by low-temperature rolling | |
| CN113733687A (en) | Manufacturing method of high-strength honeycomb composite board | |
| CN112644108A (en) | Fe-Al intermetallic compound micro-laminated composite material and preparation method thereof | |
| CN110496859B (en) | Welding-free sheath hot rolling compounding method | |
| CN113305171B (en) | Preparation method of titanium/aluminum laminated composite thin plate strip | |
| CN114292995A (en) | Aluminum-magnesium composite board and preparation method thereof | |
| CN105172308A (en) | Preparing method for titanium-aluminum-stainless-steel composite plate | |
| JP2890102B2 (en) | Manufacturing method of metal honeycomb sandwich plate |
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 | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20190611 Address after: 101407 No. 11 Xingke East Street, Yanqi Economic Development Zone, Huairou District, Beijing Patentee after: Research Institute of engineering and Technology Co., Ltd. Address before: No. 2, Xinjie street, Xicheng District, Beijing, Beijing Patentee before: General Research Institute for Nonferrous Metals |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20210825 Address after: 101407 No. 11 Xingke East Street, Yanqi Economic Development Zone, Huairou District, Beijing Patentee after: Youyan metal composite technology Co.,Ltd. Address before: 101407 No. 11 Xingke East Street, Yanqi Economic Development Zone, Huairou District, Beijing Patentee before: YOUYAN ENGINEERING TECHNOLOGY RESEARCH INSTITUTE Co.,Ltd. |