CN106364054A - Metal composite plate - Google Patents
Metal composite plate Download PDFInfo
- Publication number
- CN106364054A CN106364054A CN201610775624.XA CN201610775624A CN106364054A CN 106364054 A CN106364054 A CN 106364054A CN 201610775624 A CN201610775624 A CN 201610775624A CN 106364054 A CN106364054 A CN 106364054A
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- CN
- China
- Prior art keywords
- layer
- plate
- thickness
- composite metal
- metal plate
- 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
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/01—Layered products comprising a layer of metal all layers being exclusively metallic
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/18—Layered products comprising a layer of metal comprising iron or steel
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/20—Layered products comprising a layer of metal comprising aluminium or copper
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/06—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the heating method
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/10—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the pressing technique, e.g. using action of vacuum or fluid pressure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/04—Interconnection of layers
- B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2250/00—Layers arrangement
- B32B2250/03—3 layers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/546—Flexural strength; Flexion stiffness
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/558—Impact strength, toughness
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Laminated Bodies (AREA)
Abstract
The invention discloses a metal composite plate, which comprises a plate coating layer and a base plate layer, wherein the plate coating layer comprises composite two layers of coating layers; the two layers of coating layers are respectively a stainless steel plate layer and a titanium plate layer; the thickness of the stainless steel plate layer is 1.5mm; the thickness of the titanium plate layer is 1.5mm; the base plate layer is made of a base plate material which is one of galvanized iron, stainless steel, carbon steel, copper, aluminum or aluminum alloy; the thickness of the base plate layer is 2mm. The metal composite plate is simple in structure and has the characteristics of bending resistance and high compression strength.
Description
Technical field
The present invention relates to a kind of metallic composite technical field, specifically a kind of composite metal plate.
Background technology
At present, the now domestic metallic composite reaching metallurgical binding, great majority are multiple using Rolling compund and blast
Conjunction method is produced, Rolling compund material coating thickness 1mm about, gross thickness 3mm about；Explosion composite coating
Thickness is more than 2mm.On market, gross thickness is more than 6mm, and the composite of below coating 2mm seldom, is primarily due to routine side
Method is difficult to produce or high cost.Rolling compund method can prepare the metallic composite of below coating 2mm, but typically
Gross thickness is less than 3mm, very big to produce the thick composite plate early stage equipment investment of 6～8mm；Explosion composite method
Gross thickness can be produced and be more than 6mm composite, but coating thickness minimum can only achieve 2mm.In answering of thin coating thickness basic unit
Close on the market of product of metal material field or blank out.For this reason, practitioner improves the preparation side of metallic composite one after another
Method is it is therefore necessary to develop a kind of composite metal plate of the simple thickness ultrathin of structure.
Content of the invention
The technical problem to be solved in the present invention is to provide a kind of structure simply, the composite metal plate of thickness ultrathin, the present invention
Composite metal plate, its final finished thickness be 5.5 ~ 6.5mm.
For solving above-mentioned technical problem, the technical solution used in the present invention is that this composite metal plate, including cladding plate layer and base
Flaggy, described cladding plate layer includes compound two-layer coating, and two-layer coating is rustless steel flaggy and titanium plate layer respectively, and Stainless Steel layer covers
The thickness of layer is 1.5mm, and the thickness of titanium plate layer coating is 1.5mm, described substrate layer be baseplate material be galvanized iron, rustless steel,
One of carbon steel, copper, aluminum or aluminum alloy, the thickness of described substrate layer is 2mm.
Further improvement is that, between described coating and basic unit, be provided with one layer of polymeric laminate.
Further improvement is that, described polymeric laminate is flaky texture.
Further improvement is that, described polymeric laminate is polyolefin adhesive film.
Further improvement is that, the thickness of this composite metal plate is 5.5 ~ 6.5mm.
Present invention technical problem also to be solved is to provide a kind of structure simply, the composite metal plate preparation of thickness ultrathin
Method.
For solving above-mentioned technical problem, the technical solution used in the present invention is, the preparation method of this composite metal plate, including
Following steps:
1) preparation of cladding plate layer: by two-layer coating Stainless Steel flaggy and titanium plate layer by the compound titanium-stainless made of hot-rolling mill calendering
Steel cladding plate layer；
2) cladding plate and substrate are combined: be combined into through roll-in tourelle roll-in after cladding plate, substrate and polymeric laminate are overlapped
Composite metal plate；
3) composite metal plate is carried out Tempering and Quenching and make product with forming technology.
Further improvement is that, titanium plate is all passed through with after grinder buffing and steel brush polishing with stainless two surfaces again
Hot-rolling mill calendering is compound.
Further improvement is that, after first passing through correcting device during by cladding plate, polymeric laminate and superimposed substrate so as to overlap
Two ends more smooth.
Further improvement is that, the rolling speed of roll-in tourelle is 1.0 ~ 2.0m, the temperature of roll-in be 200 DEG C (±
10 DEG C), the pressure of roll-in is 4mpa.
Further improvement is that, through roll-in tourelle roll-in three times after cladding plate, substrate and polymeric laminate are overlapped
After be combined into composite metal plate.
The invention has the advantages that and effect: the structure of this composite metal plate is simple, has bend resistance, compressive resistance high
Feature.
Specific embodiment
Embodiment: composite metal plate, including cladding plate layer and substrate layer；Described cladding plate layer includes compound two-layer coating, and two
Layer coating is rustless steel flaggy and titanium plate layer respectively, and the thickness of Stainless Steel layer coating is 1.5mm, and the thickness of titanium plate layer coating is
1.5mm, described substrate layer is one of galvanized iron, rustless steel, carbon steel, copper, aluminum or aluminum alloy for baseplate material, described substrate
The thickness of layer is 2mm, is provided with one layer of polymeric laminate between described coating and basic unit, and described polymeric laminate is flake knot
Structure, described polymeric laminate is polyolefin adhesive film, and the thickness of this composite metal plate is 6mm.
The preparation method of this composite metal plate, comprises the following steps:
1) preparation of cladding plate layer: by two-layer coating Stainless Steel flaggy and titanium plate layer by the compound titanium-stainless made of hot-rolling mill calendering
Steel cladding plate layer；
2) cladding plate and substrate are combined: after cladding plate, substrate and polymeric laminate are overlapped after roll-in tourelle roll-in three times
It is combined into composite metal plate；
3) composite metal plate is carried out Tempering and Quenching and make product with forming technology；Wherein, first titanium plate and stainless two
Individual surface is all combined by hot-rolling mill calendering with after grinder buffing and steel brush polishing again；Cladding plate do not embroidered guiding principle flaggy face, high score
Correcting device is first passed through so as to the two ends after overlapping are more smooth when sub- glued membrane and superimposed substrate；The rolling speed of roll-in tourelle
Spend for 2.0m, the temperature of roll-in is 200 DEG C (± 10 DEG C), the pressure of roll-in is 4mpa.
Ultimate principle, principal character and the advantage of the present invention have been shown and described above.The technical staff of the industry should
Understand, the present invention is not restricted to the described embodiments, the simply explanation present invention's described in above-described embodiment and description is former
Reason, without departing from the spirit and scope of the present invention, the present invention also has various changes and modifications, these changes and improvements
Both fall within scope of the claimed invention.Claimed scope is by appending claims and its equivalent circle.
Fixed.
Claims (5)
1. a kind of composite metal plate, including cladding plate layer and substrate layer；It is characterized in that, described cladding plate layer includes compound two-layer and covers
Layer, two-layer coating is rustless steel flaggy and titanium plate layer respectively, and the thickness of Stainless Steel layer coating is 1.5mm, the thickness of titanium plate layer coating
Spend for 1.5mm, described substrate layer is one of galvanized iron, rustless steel, carbon steel, copper, aluminum or aluminum alloy for baseplate material, described
The thickness of substrate layer is 2mm.
2. the composite metal plate according to claim 1 is it is characterised in that be provided with a floor height between described coating and basic unit
Molecule glued membrane.
3. according to claim 2 composite metal plate it is characterised in that described polymeric laminate be flaky texture.
4. according to claim 3 composite metal plate it is characterised in that described polymeric laminate be polyolefin adhesive film.
5. according to claim 4 composite metal plate it is characterised in that this composite metal plate thickness be 5.5 ~ 6.5mm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610775624.XA CN106364054A (en) | 2016-08-31 | 2016-08-31 | Metal composite plate |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610775624.XA CN106364054A (en) | 2016-08-31 | 2016-08-31 | Metal composite plate |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106364054A true CN106364054A (en) | 2017-02-01 |
Family
ID=57901892
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610775624.XA Pending CN106364054A (en) | 2016-08-31 | 2016-08-31 | Metal composite plate |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106364054A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108312667A (en) * | 2018-03-30 | 2018-07-24 | 广州金纪金属制造有限公司 | Composite metal plate and its production technology |
| CN109457165A (en) * | 2018-12-28 | 2019-03-12 | 宁波逾明新材料有限公司 | A kind of titanium-stainless composite material and its use composite plate made of the composite material |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2688491Y (en) * | 2003-10-08 | 2005-03-30 | 柏智勇 | Composite metal materials |
| CN101269556A (en) * | 2007-03-22 | 2008-09-24 | 马金富 | Bi-metal composite panel and process technique |
| CN203427395U (en) * | 2013-08-08 | 2014-02-12 | 江苏金谷不锈钢有限公司 | Stainless steel composite plate |
| CN104859219A (en) * | 2015-04-21 | 2015-08-26 | 杜双双 | Composite plate and production method thereof |
| CN104859218A (en) * | 2015-04-21 | 2015-08-26 | 杜双双 | Thin-coat metal composite plate and production method thereof |
-
2016
- 2016-08-31 CN CN201610775624.XA patent/CN106364054A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2688491Y (en) * | 2003-10-08 | 2005-03-30 | 柏智勇 | Composite metal materials |
| CN101269556A (en) * | 2007-03-22 | 2008-09-24 | 马金富 | Bi-metal composite panel and process technique |
| CN203427395U (en) * | 2013-08-08 | 2014-02-12 | 江苏金谷不锈钢有限公司 | Stainless steel composite plate |
| CN104859219A (en) * | 2015-04-21 | 2015-08-26 | 杜双双 | Composite plate and production method thereof |
| CN104859218A (en) * | 2015-04-21 | 2015-08-26 | 杜双双 | Thin-coat metal composite plate and production method thereof |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108312667A (en) * | 2018-03-30 | 2018-07-24 | 广州金纪金属制造有限公司 | Composite metal plate and its production technology |
| CN109457165A (en) * | 2018-12-28 | 2019-03-12 | 宁波逾明新材料有限公司 | A kind of titanium-stainless composite material and its use composite plate made of the composite material |
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| C06 | 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: 20170201 |
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| RJ01 | Rejection of invention patent application after publication |