CN108327356A - Composite plate, compound board manufacturing apparatus and composite board manufacture method - Google Patents
Composite plate, compound board manufacturing apparatus and composite board manufacture method Download PDFInfo
- Publication number
- CN108327356A CN108327356A CN201810350304.9A CN201810350304A CN108327356A CN 108327356 A CN108327356 A CN 108327356A CN 201810350304 A CN201810350304 A CN 201810350304A CN 108327356 A CN108327356 A CN 108327356A
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- plate
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- 239000002131 composite material Substances 0.000 title claims abstract description 111
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 40
- 150000001875 compounds Chemical class 0.000 title claims abstract description 18
- 238000000034 method Methods 0.000 title claims abstract description 13
- 239000000758 substrate Substances 0.000 claims abstract description 58
- 239000000853 adhesive Substances 0.000 claims abstract description 18
- 230000001070 adhesive effect Effects 0.000 claims abstract description 18
- 238000003490 calendering Methods 0.000 claims description 18
- 230000015572 biosynthetic process Effects 0.000 claims description 12
- 239000005038 ethylene vinyl acetate Substances 0.000 claims description 6
- 229920001200 poly(ethylene-vinyl acetate) Polymers 0.000 claims description 6
- 229910000838 Al alloy Inorganic materials 0.000 claims description 4
- 229910052782 aluminium Inorganic materials 0.000 claims description 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 4
- 238000004080 punching Methods 0.000 abstract description 7
- 239000010410 layer Substances 0.000 description 12
- 230000035882 stress Effects 0.000 description 12
- 239000002905 metal composite material Substances 0.000 description 8
- 238000001816 cooling Methods 0.000 description 7
- 238000005452 bending Methods 0.000 description 6
- 238000009413 insulation Methods 0.000 description 6
- 238000000465 moulding Methods 0.000 description 6
- 238000005516 engineering process Methods 0.000 description 5
- 239000011229 interlayer Substances 0.000 description 5
- 238000000576 coating method Methods 0.000 description 4
- 238000010924 continuous production Methods 0.000 description 4
- 238000010438 heat treatment Methods 0.000 description 4
- 239000011248 coating agent Substances 0.000 description 3
- 239000002994 raw material Substances 0.000 description 3
- 239000000243 solution Substances 0.000 description 3
- 230000032683 aging Effects 0.000 description 2
- 238000005520 cutting process Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000007613 environmental effect Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 230000000930 thermomechanical effect Effects 0.000 description 2
- 238000005299 abrasion Methods 0.000 description 1
- 238000005034 decoration Methods 0.000 description 1
- 235000013399 edible fruits Nutrition 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 239000003292 glue Substances 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 239000004922 lacquer Substances 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000005022 packaging material Substances 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
- 239000011120 plywood Substances 0.000 description 1
- 231100000167 toxic agent Toxicity 0.000 description 1
- 239000003440 toxic substance Substances 0.000 description 1
- 230000001988 toxicity Effects 0.000 description 1
- 231100000419 toxicity Toxicity 0.000 description 1
Classifications
-
- 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
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
- B32B3/26—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
- B32B3/28—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer characterised by a layer comprising a deformed thin sheet, i.e. the layer having its entire thickness deformed out of the plane, e.g. corrugated, crumpled
-
- 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
- B32B15/016—Layered products comprising a layer of metal all layers being exclusively metallic all layers being formed of aluminium or aluminium alloys
-
- 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
- B32B37/08—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the cooling 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
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/12—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by using adhesives
- B32B37/1284—Application of adhesive
-
- 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
- B32B38/00—Ancillary operations in connection with laminating processes
-
- 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
- B32B38/00—Ancillary operations in connection with laminating processes
- B32B38/0012—Mechanical treatment, e.g. roughening, deforming, stretching
-
- 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
- B32B43/00—Operations specially adapted for layered products and not otherwise provided for, e.g. repairing; Apparatus therefor
- B32B43/003—Cutting
-
- 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
- B32B7/10—Interconnection of layers at least one layer having inter-reactive properties
-
- 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
- B32B38/00—Ancillary operations in connection with laminating processes
- B32B2038/0052—Other operations not otherwise provided for
- B32B2038/006—Relieving internal or residual stresses
-
- 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
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Laminated Bodies (AREA)
Abstract
A kind of composite plate of present invention offer, compound board manufacturing apparatus and composite board manufacture method are related to composite board technical field, and composite plate includes substrate, middle layer and panel, and middle layer includes core plate, and core plate has the first end face and second end face being oppositely arranged；First end face is equipped with multigroup first protrusion, and one end that each first protrusion protrudes from first end face is third end face, and third end face is plane；The third end face of each first protrusion is Nian Jie with panel；Second end face is equipped with multigroup second protrusion, and one end that each second protrusion protrudes from second end face is the 4th end face, and the 4th end face is plane；4th end face of each second protrusion is and substrate bonding.The second protrusion and the bond area of substrate can be expanded, improve adhesive strength, and can balanced bond area, prevent punching shear caused by unbalanced stress, improve Wind-Pressure Resistance deformability.
Description
Technical field
The present invention relates to composite board technical fields, more particularly, to a kind of composite plate, a kind of compound board manufacturing apparatus, with
And a kind of composite board manufacture method.
Background technology
Metal composite decorative plate has the lacquer type organic coating class decorative cover using roll coating process coating, and coating is smooth, decorates
Property good and no color differnece.Metal composite decorative plate can be widely applied for various fields, such as：Building, municipal works, decoration,
The fields such as machinery and furniture can be used in making roof boarding, wallboard, partition panel, movable plank house and high-grade packaging material.
Existing metal composite decorative plate is made of panel, core plate and substrate, is wherein spaced and is set on the upper surface of core plate
There are multiple hemispherical hollow boss, wherein panel is Nian Jie with multiple hemispherical hollow boss respectively, under substrate and new edition
Surface bonding can form metal composite decorative plate.
Since hemispherical hollow boss only top can form point contact with panel, by panel, core plate and base
Plate carries out compound tense, needs to oppress hemispherical protrusion downwards using panel, so that the top of hemispherical protrusion shrivels, shrivels
The top down recess of hemispherical protrusion afterwards, hollow boss can form line with panel and contact, and contact position by the line
Set bonding.The problem of this metal composite decorative plate is, hollow boss and panel be bonded, the bonding plane by line contact position
Product is smaller, and adhesive strength is poor, and be easy to causeing metal composite decorative plate unbalance stress causes metal composite decorative plate to deform
Be easily peeled off.
Invention content
The purpose of the present invention is to provide a kind of composite plates, are bonded with solving metal composite decorative plate in the prior art
The poor technical problem of intensity.
Composite plate provided by the invention, including substrate, middle layer and panel, the substrate, the middle layer and the face
Plate is bonded successively；
The middle layer includes core plate, and the core plate has the first end face and second end face being oppositely arranged；
The first end face is arranged towards the panel, and the first end face is raised equipped with multigroup first, and multigroup first
Protrusion is arranged along the first direction uniform intervals of core plate；Every group first protrusion includes multiple first protrusions, multiple first protrusions
Second direction uniform intervals along core plate are arranged, and the first direction is vertical with the second direction；
The outer profile of each first protrusion is truncated cone-shaped, and each first protrusion is convex towards the panel
Go out, each first protrusion all has the first cavity, and first cavity forms the first opening with the second end face, and every
One end that a first protrusion protrudes from the first end face is third end face, and the third end face is plane；
The radius of the third end face is 1.5-6 millimeters, and the height that each first protrusion protrudes from first end face is equal
It is 1.5-5 millimeters；
The third end face of each first protrusion is Nian Jie with the panel；
The second end face is arranged towards the substrate, and the second end face is raised equipped with multigroup second, and multigroup second
Protrusion is arranged along the first direction uniform intervals of core plate；Every group second protrusion includes multiple second protrusions, multiple second protrusions
Second direction uniform intervals along core plate are arranged；
The outer profile of each second protrusion is truncated cone-shaped, and each second protrusion is convex towards the substrate
Go out, each second protrusion all has the second cavity, and second cavity forms the second opening with the first end face, and every
One end that a second protrusion protrudes from the second end face is the 4th end face, and the 4th end face is plane；
The radius of 4th end face is 1.5-6 millimeters, and the height that each second protrusion protrudes from second end face is equal
It is 1.5-5 millimeters；
4th end face of each second protrusion with the substrate bonding；
Along the first direction of the core plate, first protrusion and second protrusion are arranged alternately successively, and adjacent the
Centre-to-centre spacing between one protrusion and the second protrusion is 9-18 millimeters；Along the second direction of the core plate, first protrusion and institute
It states the second protrusion to be arranged alternately successively, the centre-to-centre spacing between the adjacent first protrusion and the second protrusion is 9-18 millimeters；
The basal plane and panel are made of aluminium alloy, and the core plate is made of aluminum.
Further, the thickness of the substrate is 0.3-0.6 millimeters, and the thickness of the panel is 0.5-1.0 millimeters, institute
The thickness for stating core plate is 0.3-0.6 millimeters, and the thickness of the composite plate is 3-10 millimeters.
Further, first protrusion and second protrusion are made of calendering technology.
Further, the third end face of each first protrusion is be bonded by adhesive linkage with the panel, and each described the
4th end face of two protrusions is be bonded by adhesive linkage with the substrate, and the adhesive linkage is by ethylene-vinyl acetate copolymer system
At.
Further, the middle layer includes multiple core plates；
Multiple core plates stack gradually, be located at multiple core plate one end it is multiple first protrusion third end faces with it is described
Panel be bonded, be located at multiple core plate other ends it is multiple second protrusion the 4th end faces with the substrate bonding.
Further, the middle layer further includes the first closure member and the second closure member；
The first closure member setting is in second opening, for closing second opening；
The second closure member setting is in first opening, for closing first opening.
Further, the outer profile of first closure member is truncated cone-shaped, first closure member and the first end face
Bonding, and one end of first closure member protrusion and the first end face is the 5th end face, the 5th end face is plane, and
5th end face is Nian Jie with the panel；
The outer profile of second closure member is truncated cone-shaped, and second closure member is Nian Jie with the second end face, and institute
It is the 6th end face to state the second closure member and protrude from one end of the second end face, and the 6th end face is plane, and the described 6th
End face is Nian Jie with the panel.
Further, the radius of the 5th end face is less than the radius of the third end face, the radius of the 6th end face
Less than the radius of the 4th end face.
The present invention also aims to provide a kind of compound board manufacturing apparatus, for manufacturing composite plate of the present invention,
Including calender stack, feed component and composite component；
The calender stack includes the upper roller being oppositely arranged and lower roll；
The outer surface of the upper roller is equipped with multigroup convex die head, and multigroup convex die head is along the circumferential equal of the upper roller
Even interval setting, convex die head described in every group includes multiple convex die heads, axial direction of multiple convex die heads along the upper roller
Uniform intervals are arranged, and each convex die head is truncated cone-shaped；
The outer surface of the lower roll is equipped with multigroup lower punch head, and multigroup lower punch head is along the circumferential equal of the lower roll
Even interval setting, lower punch head described in every group includes multiple lower punch heads, axial direction of multiple lower punch heads along the lower roll
Uniform intervals are arranged, and each lower punch head is truncated cone-shaped；
When the upper roller and lower roll rotate, along the axial direction of the upper roller, the convex die head and the lower punch head are handed over
For setting, for the first protrusion of calendering formation and the second protrusion on core plate；
The feed component is used to the panel, the core plate and the substrate being delivered to the composite component；
The composite component is used to the panel, the core plate and the core plate being complex as composite plate.
The present invention also aims to provide a kind of composite board manufacture method, for manufacturing composite plate of the present invention,
Include the following steps：
Calendering formation step：Using calender stack of the present invention, the first protrusion of calendering formation and second on core plate
Protrusion；
It is fed step：The panel, the core plate and the substrate are delivered to the composite component；
Composite steps：The panel, the core plate and the substrate are complex as composite plate.
Composite plate provided by the invention, including substrate, middle layer and panel, substrate, middle layer and panel are bonded successively；In
Interbed includes core plate, and core plate has the first end face and second end face being oppositely arranged；First end face is arranged towards panel, first end
Face is equipped with multigroup first protrusion, and multigroup first protrusion is arranged along the first direction uniform intervals of core plate；Every group first protrusion is
Including multiple first protrusions, multiple first protrusions are arranged along the second direction uniform intervals of core plate, and first direction and described the
Two directions are vertical；The outer profile of each first protrusion is truncated cone-shaped, and each first protrusion is protruded towards panel, and each first
Protrusion all has the first cavity, and the first cavity forms the first opening with second end face, and each first protrusion protrudes from first end
The one end in face is third end face, and third end face is plane；The radius of third end face is 1.5-6 millimeters, and each first protrusion is convex
Height for first end face is 1.5-5 millimeters；The third end face of each first protrusion is Nian Jie with panel；Second end face
It is arranged towards substrate, second end face is equipped with multigroup second protrusion, first direction uniform intervals of multigroup second protrusion along core plate
Setting；Every group second protrusion includes multiple second protrusions, and multiple second protrusions are arranged along the second direction uniform intervals of core plate；
The outer profile of each second protrusion is truncated cone-shaped, and each second protrusion is protruded towards substrate, and each second protrusion all has
Second cavity, the second cavity forms the second opening with first end face, and one end that each second protrusion protrudes from second end face is equal
For the 4th end face, the 4th end face is plane；The radius of 4th end face is 1.5-6 millimeters, and each second protrusion protrudes from second end
The height in face is 1.5-5 millimeters；4th end face of each second protrusion is and substrate bonding；Along the first direction of core plate,
One protrusion and the second protrusion are arranged alternately successively, and the centre-to-centre spacing between the adjacent first protrusion and the second protrusion is 9-18 millimeters；
Along the second direction of core plate, the first protrusion and the second protrusion are arranged alternately successively, between the adjacent first protrusion and the second protrusion
Centre-to-centre spacing be 9-18 millimeters；Basal plane and panel are made of aluminium alloy, and core plate is made of aluminum.Due to the first end face of core plate
Be respectively equipped in second end face first protrusion and second protrusion, first protrusion third end face be plane, it is each first protrusion
Third end face it is Nian Jie with panel, the first protrusion and the bond area of panel can be expanded, improve adhesive strength；Second protrusion
The 4th end face be plane, the 4th end face of each second protrusion and substrate bonding can expand the second protrusion and substrate
Bond area improves adhesive strength；And since the first protrusion and the second protrusion are arranged alternately, can balanced bond area, prevent
Only punching shear caused by unbalanced stress improves Wind-Pressure Resistance deformability.
Description of the drawings
It, below will be to specific in order to illustrate more clearly of the specific embodiment of the invention or technical solution in the prior art
Embodiment or attached drawing needed to be used in the description of the prior art are briefly described, it should be apparent that, in being described below
Attached drawing is some embodiments of the present invention, for those of ordinary skill in the art, before not making the creative labor
It puts, other drawings may also be obtained based on these drawings.
Fig. 1 is the structural schematic diagram of composite plate provided in an embodiment of the present invention；
Fig. 2 is the structural schematic diagram of the composite plate provided in an embodiment of the present invention with multiple core plates；
Fig. 3 is the sectional view of composite plate provided in an embodiment of the present invention；
Fig. 4 is the sectional view of the composite plate with the first closure member and the second closure member provided in an embodiment of the present invention；
Fig. 5 is the side view of the calender stack in compound board manufacturing apparatus provided in an embodiment of the present invention；
Fig. 6 is the front view of the calender stack in compound board manufacturing apparatus provided in an embodiment of the present invention.
Icon：1- panels；2- core plates；21- first end faces；The first protrusions of 22-；The second protrusions of 23-；24- second
Opening；25- second end faces；26- first is open；The first closure members of 27-；The second closure members of 28-；3- substrates；4- upper rollers；
The convex die heads of 41-；5- lower rolls；51- lower punch heads.
Specific implementation mode
Technical scheme of the present invention is clearly and completely described below in conjunction with attached drawing, it is clear that described implementation
Example is a part of the embodiment of the present invention, instead of all the embodiments.Based on the embodiments of the present invention, ordinary skill
The every other embodiment that personnel are obtained without making creative work, shall fall within the protection scope of the present invention.
In the description of the present invention, it should be noted that such as occur term "center", "upper", "lower", "left", "right",
"vertical", "horizontal", "inner", "outside" etc., indicated by orientation or positional relationship be orientation based on ... shown in the drawings or position
Relationship is merely for convenience of description of the present invention and simplification of the description, and not indicating or implying the indicated device or element must have
There is specific orientation, with specific azimuth configuration and operation, therefore is not considered as limiting the invention.In addition, as occurred
Term " first ", is used for description purposes only " second ", is not understood to indicate or imply relative importance.Wherein, term
" first position " and " second position " is two different positions.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " installation ", " phase
Even ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or be integrally connected；It can
Can also be electrical connection to be mechanical connection；It can be directly connected, can also indirectly connected through an intermediary, Ke Yishi
Connection inside two elements.For the ordinary skill in the art, above-mentioned term can be understood at this with concrete condition
Concrete meaning in invention.
The present invention provides a kind of composite plate, compound board manufacturing apparatus and composite board manufacture methods, and multiple realities are given below
Example is applied composite plate provided by the invention, compound board manufacturing apparatus and composite board manufacture method is described in detail.
Embodiment 1
Composite plate provided in this embodiment, as shown in Figures 1 to 4, including substrate 3, middle layer and panel 1, substrate 3, in
Interbed and panel 1 are bonded successively；Middle layer includes core plate 2, and core plate 2 has the first end face 21 and second end face being oppositely arranged
25；First end face 21 is arranged towards panel 1, and first end face 21 is equipped with multigroup first protrusion 22, and multigroup first protrusion 22 is along core
The first direction uniform intervals of plate 2 are arranged；Every group of first protrusion 22 includes multiple first protrusions 22, the multiple first raised 22 edges
The second direction uniform intervals of core plate 2 are arranged, and first direction is vertical with second direction；The outer profile of each first protrusion 22 is equal
For truncated cone-shaped, each first protrusion 22 is protruded towards panel 1, and each first protrusion 22 all has the first cavity, the first cavity
The first opening 26 is formed with second end face 25, and one end that each first protrusion 22 protrudes from first end face 21 is third end
Face, third end face are plane；The radius of third end face is 1.5-6 millimeters, and each first protrusion 22 protrudes from first end face 21
Height is 1.5-3 millimeters；The third end face of each first protrusion 22 is Nian Jie with panel 1；Second end face 25 is towards substrate 3
Setting, second end face 25 are equipped with multigroup second protrusion 23, and multigroup second protrusion 23 is set along the first direction uniform intervals of core plate 2
It sets；Every group of second protrusion 23 includes multiple second protrusions 23, second direction uniform intervals of multiple second protrusions 23 along core plate 2
Setting；The outer profile of each second protrusion 23 is truncated cone-shaped, and each second protrusion 23 is protruded towards substrate 3, and each second
Protrusion 23 all has the second cavity, and the second cavity forms the second opening 24 with first end face 21, and each second protrusion 23 is protruded
It is the 4th end face in one end of second end face 25, the 4th end face is plane；The radius of 4th end face is 1.5-6 millimeters, each
The height that second protrusion 23 protrudes from second end face 25 is 1.5-5 millimeters；4th end face of each second protrusion 23 is and base
Plate 3 is bonded；Along the first direction of core plate 2, the first protrusion 22 and the second protrusion 23 are arranged alternately successively, the first adjacent protrusion 22
Centre-to-centre spacing between the second protrusion 23 is 9-18 millimeters；Along the second direction of core plate 2, the first protrusion 22 and the second protrusion 23
It is arranged alternately successively, the centre-to-centre spacing between the adjacent first protrusion 22 and the second protrusion 23 is 9-18 millimeters；Basal plane and panel 1
It is made of aluminium alloy, core plate 2 is made of aluminum.
It should be noted that in the present embodiment, core plate 2 is rectangle core plate 2, and the first direction of core plate 2 is the length of core plate 2
Direction is spent, the second direction of core plate 2 is the width direction of core plate 2.It is that rectangle is compound by the composite plate that the core plate 2 is fabricated
Plate, if desired the composite plate of other shapes, can be tailored by rectangle composite plate.
Wherein, first end face 21 is equipped with multiple first protrusions 22, and each first protrusion 22 all has the first cavity,
Second end face 25 is equipped with multiple second protrusions 23, and each second protrusion 23 all has the second cavity, due to the first protrusion
22 and second protrusion 23 thickness of composite plate can be made to increase, improve composite plate intensity, and due to the first cavity and second empty
The weight of chamber, core plate 2 does not increase, and can save the raw material of manufacture core plate 2, reduces composite plate overall weight.
Wherein, the shape of the first protrusion 22 is truncated cone-shaped, and the radius of the first protrusion 22 is by third end face to first end face 21
It can gradually increase, can also be gradually reduced, it is preferable that the radius of the first protrusion 22 is gradual to first end face 21 by third end face
Increase, the radius of third end face is 1.5-6 millimeters, can ensure that third end face and the contact area of panel 1 are more closed at this time
It is suitable, and the radius of the first protrusion 22 is gradually increased by third end face to first end face 21, can improve the steady of the first protrusion 22
It is qualitative, when the first protrusion 22 receives external force, it is not easy to be deformed.The adhesive strength Increased Plasma Half-life of laboratory accelerated ageing
One times or more.
Wherein, the shape of the second protrusion 23 is truncated cone-shaped, and the radius of the second protrusion 23 is by third end face to second end face 25
It can gradually increase, can also be gradually reduced, it is preferable that the radius of the second protrusion 23 is gradual to second end face 25 by third end face
Increase, the radius of the 4th end face is 1.5-6 millimeters, can ensure that the 4th end face and the contact area of substrate 3 are more closed at this time
It is suitable, and the radius of the second protrusion 23 is gradually increased by the 4th end face to second end face 25, can improve the steady of the second protrusion 23
It is qualitative, when the second protrusion 23 receives external force, it is not easy to be deformed.The adhesive strength Increased Plasma Half-life of laboratory accelerated ageing
One times or more.
Wherein, first end face 21 is equipped with multigroup first protrusion 22, and multigroup first protrusion 22 is equal along the first direction of core plate 2
Even interval setting；Every group of first protrusion 22 includes multiple first protrusions 22, second direction of multiple first protrusions 22 along core plate 2
Uniform intervals are arranged, and due to being evenly spaced on multiple first protrusions 22 in first end face 21, can increase bond area, and
And producing balanced forces point, prevent punching shear caused by unbalanced stress.
Wherein, second end face 25 is equipped with multigroup second protrusion 23, and multigroup second protrusion 23 is equal along the first direction of core plate 2
Even interval setting；Every group of second protrusion 23 includes multiple second protrusions 23, second direction of multiple second protrusions 23 along core plate 2
Uniform intervals are arranged, and due to being evenly spaced on multiple second protrusions 23 in second end face 25, can increase bond area, and
And producing balanced forces point, prevent punching shear caused by unbalanced stress.
Also, due to the first direction along core plate 2, the first protrusion 22 and the second protrusion 23 are arranged alternately successively, adjacent
Centre-to-centre spacing between first protrusion 22 and the second protrusion 23 is 9-18 millimeters；Along the second direction of core plate 2, the first raised 22 Hes
Second protrusion 23 is arranged alternately successively, and the centre-to-centre spacing between the adjacent first protrusion 22 and the second protrusion 23 is 9-18 millimeters, energy
Enough make core plate 2 and the adhesive spots of substrate 3 and panel 1 interleaved, to staggeredly stress point, make composite plate in all directions by
Power more uniformly and balances, and composite plate is not easily broken or bending, and between adjacent the first protrusion 22 and the second protrusion 23
Centre-to-centre spacing is 9-18 millimeters, being capable of the stress of preferable balanced composite plate in all directions.
Further, since being equipped with the first protrusion 22 between the first end face 21 and panel 1 of core plate 2, make first end face 21 and face
A space interlayer is formed between plate 1, which can weaken the propagation of sound, while can also weaken the biography of heat
It broadcasts, to improve, composite plate is heat-insulated and the ability of sound insulation.Furthermore since the first protrusion 22 has the first cavity, the first cavity
The propagation with trap heat and sound can be further interfered, heat-insulated and sound insulation the ability of composite plate is enhanced.Also, first is convex
It plays the air that 22 can effectively obstruct between first end face 21 and panel 1 to flow, reduces the air flow property of the space interlayer,
It can play the role of the propagation of interference and trap heat and sound.
Similarly, since being equipped with the second protrusion 23 between the second end face 25 and substrate 3 of core plate 2, make second end face 25 and base
Also a space interlayer is formed between plate 3, which can weaken the propagation of sound, while can also weaken the biography of heat
It broadcasts, to improve, composite plate is heat-insulated and the ability of sound insulation.Furthermore since the second protrusion 23 has the second cavity, the second cavity
The propagation with trap heat and sound can be further interfered, heat-insulated and sound insulation the ability of composite plate is enhanced.Also, second is convex
It plays the air that 23 can effectively obstruct between second end face 25 and substrate 3 to flow, reduces the air flow property of the space interlayer,
It can play the role of the propagation of interference and trap heat and sound.
Also, for core plate 2 while playing connection function, core plate 2 can reduce the internal stress of composite plate, especially reduce
The internal stress of middle layer, when composite plate is by applied external force, core plate 2 can be suffered by each position of efficient balance composite plate
Active force, the active force suffered by panel 1, substrate 3 and core plate 2 can be distributed to each position of composite plate by core plate 2, made
It is more balanced in compound wrench, it is unlikely to deform, bending or fractures.Meanwhile core plate 2 will be divided into two between panel 1 and substrate 3
Space interlayer, and the interbedded air of two spaces cannot mutual convection current, reduce conduction of velocity of the air to heat,
To improve the heat-insulating property of composite plate.
Preferably, the thickness of substrate 3 is 0.3-0.6 millimeters, and the thickness of panel 1 is 0.5-1.0 millimeters, the thickness of core plate 2
Degree is 0.3-0.6 millimeters, and the thickness of composite plate is 3-10 millimeters, thick and heavy than reducing 50%-70%.
Further, the outer surface of panel 1 is equipped with decorative film, and composite plate can be made to have decorative function, and
And decorative film can not be scraped off with protection panels 1.
Further, the first protrusion 22 and the second protrusion 23 are made of calendering technology.Calendering technology can be relatively
Roll on thick core plate and the first protrusion 22 and the second protrusion 23, to thicken core plate, compound plate thickness is made to increase, and improves multiple
Plywood intensity.
Further, the third end face of each first protrusion 22 is be bonded by adhesive linkage with panel 1, each second protrusion
23 the 4th end face is be bonded by adhesive linkage with substrate 3, and adhesive linkage is made of ethylene-vinyl acetate copolymer.
The English name of ethylene-vinyl acetate copolymer is ethylene-vinylacetate copolymer, English
Referred to as EVA.Its toxicity is smaller, can reduce the toxicant of composite plate volatilization, improves environmental-protecting performance.
Further, middle layer includes multiple core plates 2；Multiple core plates 2 stack gradually, and are located at the more of 2 one end of multiple core plates
The third end face of a first protrusion 22 is Nian Jie with panel 1, is located at the 4th of multiple second protrusions 23 of 2 other end of multiple core plates
End face is Nian Jie with substrate 3.
Multiple core plates 2 stack gradually, and can be bonded using glue between multiple core plates 2, and core plate 2 can be made thick
Degree increases, to improve the intensity of composite plate.
Further, middle layer further includes the first closure member 27 and the second closure member 28；The setting of first closure member 27 is the
In two openings 24, for closing the second opening 24；The setting of second closure member 28 is in the first opening 26, for closing the first opening
26。
Wherein, the first closure member 27 can close the second opening 24, so that the second cavity forms closed cavity；Second closing
Part 28 can close the first opening 26, so that the first cavity forms closed cavity.At this point it is possible to the first cavity and the second cavity
Middle injection inert gas hollow can improve that composite plate is heat-insulated and the effect of sound insulation to make the first cavity and the second cavity be formed
Fruit.
Wherein, the first closure member 27 and the second closure member 28 can be closed plate, or closing block etc. is any to be suitble to
Structure, using the first closure member 27 and the second closure member 28 make the first opening 26 and second opening 24 closing, to make first
Cavity and the second cavity, which are formed, hollow can improve that composite plate is heat-insulated and the effect of sound insulation.
Further, the outer profile of the first closure member 27 is truncated cone-shaped, and the first closure member 27 is Nian Jie with first end face 21, and
It is the 5th end face that first closure member 27, which is protruded with one end of first end face 21, and the 5th end face is plane, and the 5th end face with it is described
Panel 1 is bonded；The outer profile of second closure member 28 is truncated cone-shaped, and the second closure member 28 is Nian Jie with second end face 25, and the second envelope
One end that closing member 28 protrudes from second end face 25 is the 6th end face, and the 6th end face is plane, and the 6th end face is Nian Jie with panel 1.
First closure member 27 and the second closure member 28 are while closing the first cavity and the second cavity, additionally it is possible to right respectively
Panel 1 and substrate 3 are supported, and further increase bond area, improve adhesive strength, and further balanced bond area,
Punching shear caused by preventing unbalanced stress.
Further, the radius of the 5th end face is less than the radius of third end face, and the radius of the 6th end face is less than the 4th end face
Radius.The arrangement of the in first end face 21 first protrusion 22 and the first closure member 27 can be made to have not regulation, that is,
It no matter says from any angle, any direction, the edge of the first protrusion 22 and the first closure member 27 that set gradually all cannot
It draws a straight line, makes the first protrusion 22 and the first closure member 27 in the upper no directionality of arrangement, therefore composite plate is in each side
Upward being more uniformly stressed and balancing, and composite plate is not easy to be bent over or fracture, and composite plate in all directions anti-
Bending ability, structural strength and bending flexibility are also more uniform and balance, and eliminate composite plate and are held in all directions to power
By the otherness of ability, bending resistance, structural strength and the bending flexibility of composite plate are further increased.
Composite plate provided in this embodiment, due to being respectively equipped with first in the first end face 21 and second end face 25 of core plate 2
Protrusion 22 and second protrusion 23, the third end face of the first protrusion 22 are plane, and the third end face of each first protrusion 22 is and face
Plate 1 is bonded, and can be expanded the bond area of the first protrusion 22 and panel 1, be improved adhesive strength；4th end face of the second protrusion 23
The 4th end face for plane, each second protrusion 23 is Nian Jie with substrate 3, and it is bonding with substrate 3 can to expand the second protrusion 23
Area improves adhesive strength；And since the first protrusion 22 and the second protrusion 23 are arranged alternately, can balanced bond area, prevent
Only punching shear caused by unbalanced stress improves Wind-Pressure Resistance deformability.
Embodiment 2
Compound board manufacturing apparatus provided in this embodiment, as shown in Figure 5 to Figure 6, the composite plate for manufacturing embodiment 1,
Including calender stack, feed component and composite component；Calender stack includes the upper roller 4 being oppositely arranged and lower roll 5；Outside upper roller 4
Surface is equipped with multigroup convex die head 41, and multigroup convex die head 41 is arranged along the circumferential uniform intervals of upper roller 4, every group of convex die head
41 include multiple convex die heads 41, and multiple convex die heads 41 are arranged along the axial uniform intervals of upper roller 4, and each convex die head 41
It is truncated cone-shaped；The outer surface of lower roll 5 is equipped with multigroup lower punch head 51, and multigroup lower punch head 51 is along the circumferential uniform of lower roll 5
Interval setting, every group of lower punch head 51 include multiple lower punch heads 51, axial uniform intervals of multiple lower punch heads 51 along lower roll 5
Setting, and each lower punch head 51 is truncated cone-shaped；When upper roller 4 and lower roll 5 rotate, along the axial direction of upper roller 4, convex die head 41
It is arranged alternately with lower punch head 51, for the first protrusion of calendering formation and the second protrusion on core plate；Component is fed to be used for face
Plate, core plate and substrate are delivered to composite component；Composite component is used to panel, core plate and core plate being complex as composite plate.By upper
Roller 4 and lower roll 5 roll core plate, make to form the first protrusion in the first end face of core plate, and the is formd in second end face
Two is raised, and punch-pin is respectively provided on upper roller 4 and lower roll 5, and cooperation need not be utilized even, reduce the abrasion of mold, improve mold
Efficiency, and can continuous production core plate, and by be fed component by panel, by calendering formation core plate and substrate convey
To composite component carry out composite molding, can continuous production composite plate, improve production efficiency.
Specifically, calender stack includes two pairs of upper rollers being oppositely arranged 4 and lower roll 5, and core plate passes through two pairs of 4 Hes of upper roller successively
The calendering formation of lower roll 5 can reduce the breakage rate of core plate, and in each pair of upper roller 4 and lower roll 5, and upper roller 4 connects with driving device
It connects to drive upper roller 4 to rotate, driving device is not provided on lower roll 5, core movement is driven using upper roller 4, to drive lower roll 5 to transport
It is dynamic,
One in front and one in back, preliminary roller is equipped with driving device to two pairs of homotype rollers, and core movement, core plate is driven to drive back roller movement, from
And reach the function of Automatic Track Finding, the smart blind copy servomechanism installation of decompressor use is eliminated, improve calendering synchronizes essence
Degree and the reliability of action greatly reduce the maintenance cost of device compared with punching press mould moulding process.
Composite component includes heating furnace and hot press, and panel, core plate and substrate carry out linear by heating furnace and hot press
Hot paste is compound, and wherein hot press can use energy-saving electromagnetic heating roller, can then be sent into cooling thermomechanical components, cooling thermomechanical components
Including cooling furnace and straightener roll, the composite plate after composite molding enters in cooling furnace after cooling, is answered into straightener roll to eliminate
Power, subsequently enters lateral deburring component and cutting component is cut to suitable size, and automatic stacking is translated finally by sucked type
Composite plate is carried out stacking by component.The compound board manufacturing apparatus can save raw material, improve the feature of environmental protection of manufacturing process, enhancing life
The reliability of production realizes serialization manufacture, improves production efficiency.
Embodiment 3
Composite board manufacture method provided in this embodiment, for manufacturing composite plate described in embodiment 1, including following step
Suddenly：
Calendering formation step：Using the calender stack of embodiment 2, calendering formation first is raised on core plate and second is convex
It rises；
It is fed step：Panel, core plate and substrate are delivered to composite component；
Composite steps：Panel, core plate and substrate are sent into heating furnace and the linear hot paste of hot press progress is compound；
Calendering formation step can continuous production core plate, and by be fed step and composite steps by panel, by calendering
Molding core plate and substrate be delivered to composite component carry out composite molding, can continuous production composite plate, improve production efficiency.
Preferably, composite board manufacture method is further comprising the steps of：
Cooling step：The composite plate of composite molding is cooled down；
Eliminate stress steps：Composite plate after cooling is fed through in straightener roll to eliminate stress；
Cut step：Composite plate is cut to suitable size by lateral deburring component and cutting component；
Palletization step：Composite plate is translated into automatic stacking component by sucked type, composite plate is subjected to stacking
The composite board manufacture method can save raw material, improve the feature of environmental protection of manufacturing process, enhance the reliability of production, real
Show serialization manufacture, improves production efficiency.
Finally it should be noted that：The above embodiments are only used to illustrate the technical solution of the present invention., rather than its limitations；To the greatest extent
Present invention has been described in detail with reference to the aforementioned embodiments for pipe, it will be understood by those of ordinary skill in the art that：Its according to
So can with technical scheme described in the above embodiments is modified, either to which part or all technical features into
Row equivalent replacement；And these modifications or replacements, various embodiments of the present invention technology that it does not separate the essence of the corresponding technical solution
The range of scheme.
Claims (10)
1. a kind of composite plate, which is characterized in that including substrate, middle layer and panel, the substrate, the middle layer and the face
Plate is bonded successively；
The middle layer includes core plate, and the core plate has the first end face and second end face being oppositely arranged；
The first end face is arranged towards the panel, and the first end face is equipped with multigroup first protrusion, multigroup first protrusion
First direction uniform intervals along core plate are arranged；Every group first protrusion includes multiple first protrusions, and multiple first protrusions are along core
The second direction uniform intervals of plate are arranged, and the first direction is vertical with the second direction；
The outer profile of each first protrusion is truncated cone-shaped, and each first protrusion is protruded towards the panel, often
A first protrusion all has the first cavity, and first cavity and the second end face form the first opening, and each the
One end that one protrusion protrudes from the first end face is third end face, and the third end face is plane；
The radius of the third end face is 1.5-6 millimeters, and the height that each first protrusion protrudes from first end face is
1.5-5 millimeter；
The third end face of each first protrusion is Nian Jie with the panel；
The second end face is arranged towards the substrate, and the second end face is equipped with multigroup second protrusion, multigroup second protrusion
First direction uniform intervals along core plate are arranged；Every group second protrusion includes multiple second protrusions, and multiple second protrusions are along core
The second direction uniform intervals of plate are arranged；
The outer profile of each second protrusion is truncated cone-shaped, and each second protrusion is protruded towards the substrate, often
A second protrusion all has the second cavity, and second cavity and the first end face form the second opening, and each the
One end that two protrusions protrude from the second end face is the 4th end face, and the 4th end face is plane；
The radius of 4th end face is 1.5-6 millimeters, and the height that each second protrusion protrudes from second end face is
1.5-5 millimeter；
4th end face of each second protrusion with the substrate bonding；
Along the first direction of the core plate, first protrusion and second protrusion are arranged alternately successively, and adjacent first is convex
It is 9-18 millimeters to play the centre-to-centre spacing between the second protrusion；Along the second direction of the core plate, first protrusion and described the
Two protrusions are arranged alternately successively, and the centre-to-centre spacing between the adjacent first protrusion and the second protrusion is 9-18 millimeters；
The basal plane and panel are made of aluminium alloy, and the core plate is made of aluminum.
2. composite plate according to claim 1, which is characterized in that the thickness of the substrate is 0.3-0.6 millimeters, described
The thickness of panel is 0.5-1.0 millimeters, and the thickness of the core plate is 0.3-0.6 millimeters, and the thickness of the composite plate is 3-10
Millimeter.
3. composite plate according to claim 1, which is characterized in that first protrusion and second protrusion are by calendering
Technique is made.
4. composite plate according to claim 1, which is characterized in that it is each first protrusion third end face with the panel
It is bonded by adhesive linkage, the 4th end face of each second protrusion is be bonded by adhesive linkage with the substrate, the bonding
Layer is made of ethylene-vinyl acetate copolymer.
5. according to the composite plate described in any one of claim 1-4, which is characterized in that the middle layer includes multiple core plates；
Multiple core plates stack gradually, be located at multiple core plate one end it is multiple first protrusion third end faces with the panel
Bonding, be located at multiple core plate other ends it is multiple second protrusion the 4th end faces with the substrate bonding.
6. according to the composite plate described in any one of claim 1-4, which is characterized in that the middle layer further includes the first envelope
Closing member and the second closure member；
The first closure member setting is in second opening, for closing second opening；
The second closure member setting is in first opening, for closing first opening.
7. composite plate according to claim 6, which is characterized in that the outer profile of first closure member is truncated cone-shaped, institute
State that the first closure member is Nian Jie with the first end face, and one end of first closure member protrusion and the first end face is the 5th
End face, the 5th end face is plane, and the 5th end face is Nian Jie with the panel；
The outer profile of second closure member is truncated cone-shaped, and second closure member is Nian Jie with the second end face, and described the
One end that two closure members protrude from the second end face is the 6th end face, and the 6th end face is plane, and the 6th end face
It is Nian Jie with the panel.
8. composite plate according to claim 7, which is characterized in that the radius of the 5th end face is less than the third end face
Radius, the radius of the 6th end face is less than the radius of the 4th end face.
9. a kind of compound board manufacturing apparatus, for the composite plate described in any one of manufacturing claims 1-8, which is characterized in that
Including calender stack, feed component and composite component；
The calender stack includes the upper roller being oppositely arranged and lower roll；
The outer surface of the upper roller is equipped with multigroup convex die head, and multigroup convex die head is between the circumferential direction of the upper roller is uniform
Every setting, convex die head described in every group includes multiple convex die heads, and multiple convex die heads are along the axial uniform of the upper roller
Interval setting, and each convex die head is truncated cone-shaped；
The outer surface of the lower roll is equipped with multigroup lower punch head, and multigroup lower punch head is between the circumferential direction of the lower roll is uniform
Every setting, lower punch head described in every group includes multiple lower punch heads, and multiple lower punch heads are along the axial uniform of the lower roll
Interval setting, and each lower punch head is truncated cone-shaped；
When the upper roller and lower roll rotate, along the axial direction of the upper roller, the convex die head and the lower punch head are alternately set
It sets, for the first protrusion of calendering formation and the second protrusion on core plate；
The feed component is used to the panel, the core plate and the substrate being delivered to the composite component；
The composite component is used to the panel, the core plate and the substrate being complex as composite plate.
10. a kind of composite board manufacture method, for the composite plate described in any one of manufacturing claims 1-8, feature exists
In including the following steps：
Calendering formation step：Using the calender stack described in claim 9, calendering formation first is raised on core plate and second is convex
It rises；
It is fed step：The panel, the core plate and the substrate are delivered to the composite component；
Composite steps：The panel, the core plate and the substrate are complex as composite plate.
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110202847A (en) * | 2019-06-12 | 2019-09-06 | 中国航空制造技术研究院 | A kind of internal novel light sandwich and preparation method thereof being connected to |
| CN112078218A (en) * | 2020-09-04 | 2020-12-15 | 武汉美术新型建材有限公司 | Three-dimensional aluminum core composite board production line and three-dimensional aluminum core composite board produced by same |
Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20040096628A1 (en) * | 2000-12-14 | 2004-05-20 | Werner Saathoff | Composite panel, preferably of plastic, and method for its production |
| CN1697732A (en) * | 2003-02-28 | 2005-11-16 | 哈尼赛尔复合株式会社 | Composite panel, manufacturing method thereof and manufacturing apparatus thereof |
| CN201484042U (en) * | 2009-07-31 | 2010-05-26 | 陈猛 | Metal compound decorative panel with intermediate layer provided with buckle plate |
| CN101842228A (en) * | 2007-11-02 | 2010-09-22 | 特耐克斯股份公司 | Composite for geotechnics, building and the like, with impermeable layer |
| CN102398387A (en) * | 2011-08-06 | 2012-04-04 | 张玉梅 | Metal lightweight multilayer composite plate |
| CN102774051A (en) * | 2011-05-12 | 2012-11-14 | 都江堰金祥装饰工程有限公司 | Composite plate having improved structure |
| CN203141935U (en) * | 2013-03-20 | 2013-08-21 | 湖北上大模具材料科技有限公司 | Aluminum-plastic composite plate |
| CN203185748U (en) * | 2013-03-12 | 2013-09-11 | 苏州良才物流科技股份有限公司 | Composite board |
| WO2015089307A1 (en) * | 2013-12-13 | 2015-06-18 | Celltech Metals, Inc. | Sandwich structure |
| CN208760102U (en) * | 2018-04-18 | 2019-04-19 | 陈猛 | Composite plate and composite plate curtain wall |
-
2018
- 2018-04-18 CN CN201810350304.9A patent/CN108327356B/en active Active
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20040096628A1 (en) * | 2000-12-14 | 2004-05-20 | Werner Saathoff | Composite panel, preferably of plastic, and method for its production |
| CN1697732A (en) * | 2003-02-28 | 2005-11-16 | 哈尼赛尔复合株式会社 | Composite panel, manufacturing method thereof and manufacturing apparatus thereof |
| CN101842228A (en) * | 2007-11-02 | 2010-09-22 | 特耐克斯股份公司 | Composite for geotechnics, building and the like, with impermeable layer |
| CN201484042U (en) * | 2009-07-31 | 2010-05-26 | 陈猛 | Metal compound decorative panel with intermediate layer provided with buckle plate |
| CN102774051A (en) * | 2011-05-12 | 2012-11-14 | 都江堰金祥装饰工程有限公司 | Composite plate having improved structure |
| CN102398387A (en) * | 2011-08-06 | 2012-04-04 | 张玉梅 | Metal lightweight multilayer composite plate |
| CN203185748U (en) * | 2013-03-12 | 2013-09-11 | 苏州良才物流科技股份有限公司 | Composite board |
| CN203141935U (en) * | 2013-03-20 | 2013-08-21 | 湖北上大模具材料科技有限公司 | Aluminum-plastic composite plate |
| WO2015089307A1 (en) * | 2013-12-13 | 2015-06-18 | Celltech Metals, Inc. | Sandwich structure |
| CN208760102U (en) * | 2018-04-18 | 2019-04-19 | 陈猛 | Composite plate and composite plate curtain wall |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110202847A (en) * | 2019-06-12 | 2019-09-06 | 中国航空制造技术研究院 | A kind of internal novel light sandwich and preparation method thereof being connected to |
| CN112078218A (en) * | 2020-09-04 | 2020-12-15 | 武汉美术新型建材有限公司 | Three-dimensional aluminum core composite board production line and three-dimensional aluminum core composite board produced by same |
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|---|---|
| CN108327356B (en) | 2023-11-10 |
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