CN110126365A - Honeycomb composite plate preparation method - Google Patents
Honeycomb composite plate preparation method Download PDFInfo
- Publication number
- CN110126365A CN110126365A CN201910267531.XA CN201910267531A CN110126365A CN 110126365 A CN110126365 A CN 110126365A CN 201910267531 A CN201910267531 A CN 201910267531A CN 110126365 A CN110126365 A CN 110126365A
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- China
- Prior art keywords
- honeycomb
- composite plate
- core material
- layer
- glue
- 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.)
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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 form; Layered products having particular features of form
- B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
- B32B3/12—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
-
- 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
- B32B33/00—Layered products characterised by particular properties or particular surface features, e.g. particular surface coatings; Layered products designed for particular purposes not covered by another single class
-
- 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
-
- 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
Abstract
The present invention provides a kind of honeycomb composite plate preparation method, the honeycomb composite plate includes encapsulated layer and honeycomb core material, the honeycomb composite plate preparation method includes: that chopped strand and adhesive are mixed into mixed slurry, so that the chopped strand is uniformly distributed in the adhesive;The mixed slurry described in the one surface even application of encapsulated layer, precuring glue composite layer to be formed;By both ends difference two encapsulated layers of adhesion of the honeycomb core material, the one end of at least one encapsulated layer and the honeycomb core material is attached with the precuring glue composite layer;Honeycomb composite plate described in curing molding.The present invention can rationally control the distribution of fiber and adhesive by mixing fiber with adhesive, so that the dosage of adhesive is uniform, not only retain the humidification of the tension resistance of fiber, but also be directly attached honeycomb core material, and it is convenient to form, and is suitable for automation batch jobs.
Description
Technical field
The present invention relates to kitchen and bath's decorative materials technologies, particularly relate to a kind of honeycomb composite plate preparation method.
Background technique
Background that this section is intended to provide an explanation of the embodiments of the present invention set forth in the claims or context.Herein
Description recognizes it is the prior art not because not being included in this section.
In various applications of the honeycomb composite plate for demand high intensity and light weight.For bigger intensity, this
A little plates may include light weight cellular core material and fibrous layer, because light weight cellular core material has high strength-weight ratio and antifatigue broken
Bad property, fibrous layer is for enhancing reinforcement.It is related to fibrous layer buying, coating not for fibrous layer to be applied to a cellular process
Solidify adhesive step, since the core material and adhesive layer contact area of cellular board (corrugated plating or corrugated sheet) are less and core material itself
The thin reason of structure generally requires the content of control glue, to guarantee honeycomb end bond strength, to avoid planar stretch viscous
The knotting strength problem relatively low with shearing peel strength.And uncured adhesive has certain mobility and viscosity, coating
It is uniformly a kind of perfect condition, it is extremely difficult to control, partial region appearance is excessively thin or blocked up, will affect the property of later period composite sandwich plate
Can consistency, such as the region of glue in use process may be exactly stress concentrated position less, those location points can to tie first
The combination for closing honeycomb and glue is failed, so that the intensity of composite plate is seriously destroyed and arrives and be not available.It in the prior art, is guarantor
Bond strength is demonstrate,proved, glue-line can be made to go deep into inside honeycomb cell, on the one hand increase the dosage of glue, at high cost, weight can become larger;
On the other hand, colloid penetrates into the performance that will affect keriotheca.
Summary of the invention
In view of the foregoing, it is necessary to a kind of preparation method of honeycomb composite plate is provided, by mixing fiber and adhesive
Mixed slurry is synthesized, the distribution that can rationally control fiber and adhesive both retains fiber so that the dosage of adhesive is uniform
The humidification of tension resistance, and it is directly attached honeycomb core material, it is convenient to form, and is suitable for automation batch jobs.
The embodiment of the present invention provides a kind of honeycomb composite plate preparation method, and the honeycomb composite plate includes encapsulated layer and honeycomb
Core material, the honeycomb composite plate preparation method include:
Chopped strand and adhesive are mixed into mixed slurry, so that the chopped strand uniformly divides in the adhesive
Cloth;
The mixed slurry described in the one surface even application of encapsulated layer, precuring glue composite layer to be formed;
Two encapsulated layers of adhesion, at least one encapsulated layer and the bee are distinguished into the both ends of the honeycomb core material
The one end of nest core material is attached with the precuring glue composite layer;
Honeycomb composite plate described in curing molding.
Further, in above-mentioned honeycomb composite plate preparation method provided in an embodiment of the present invention, described by chopped fibre
Before the step of dimension is mixed into mixed slurry with adhesive, the method also includes:
Continuous fiber is cut off to obtain the chopped strand by preset length, the length range of the chopped strand is
1mm-70mm。
Further, in above-mentioned honeycomb composite plate preparation method provided in an embodiment of the present invention, the fiber is enhancing
Fiber, the reinforcing fiber include one of glass fibre, carbon fiber, aramid fiber, asbestos or a variety of, the adhesive packet
Include one of epoxide-resin glue, polyurethane adhesive or a variety of combinations.
Further, described in the encapsulation in above-mentioned honeycomb composite plate preparation method provided in an embodiment of the present invention
Layer one surface even application described in mixed slurry include:
Convey the encapsulated layer;
Incude the position of the encapsulated layer;
It is uniform to the surface to be applied of the encapsulated layer when the position for sensing the encapsulated layer is consistent with predeterminated position
Apply the mixed slurry.
Further, in above-mentioned honeycomb composite plate preparation method provided in an embodiment of the present invention, described by the bee
Two contact other two encapsulated layers of adhesion of end part of nest core material, one end of at least one encapsulated layer and the honeycomb core material
Before the step of portion is attached with the precuring glue composite layer, the method also includes:
At least one in two contact ends of the honeycomb core material is carried out uneven integralization to handle to obtain surface irregularity
End is contacted, the contact end of the surface irregularity is in burr structure or broached-tooth design or other uneven structures.
Further, described by the honeycomb in above-mentioned honeycomb composite plate preparation method provided in an embodiment of the present invention
The both ends of core material respectively two encapsulated layers of adhesion the step of include:
Two contact end parts of the honeycomb core material surface that two encapsulated layers are coated with default jelly is not pressed into;
Wherein, at least a kind of in the default jelly of the two encapsulation layer surface coatings is the mixed slurry.
Further, in above-mentioned honeycomb composite plate preparation method provided in an embodiment of the present invention, the curing molding institute
Stating honeycomb composite plate includes:
Obtain the precuring treatment temperature of the precuring glue composite layer;
Based on temperature when precuring processing, the honeycomb composite plate is carried out by the way of gradient increased temperature
Curing molding processing.
Further, in above-mentioned honeycomb composite plate preparation method provided in an embodiment of the present invention, the encapsulated layer includes
One of brown paper, fibrous layer, plastic film, metal foil, ceramics, stone material, plastic plate are a variety of.
Further, in above-mentioned honeycomb composite plate preparation method provided in an embodiment of the present invention, the honeycomb core material is
One of aluminum honeycomb, paper honeycomb, plastic honeycomb or high molecular material honeycomb are a variety of.
Further, in above-mentioned honeycomb composite plate preparation method provided in an embodiment of the present invention, the honeycomb core material
The structure of cross section includes regular hexagon, rectangle, diamond shape, corrugated board shape, square, white-out is round, solid matter is round or triangle
One of shape.
The embodiment of the present invention provides a kind of honeycomb composite plate preparation method, and chopped strand and adhesive are mixed into mixing slurry
Material, so that the chopped strand is uniformly distributed in the adhesive;It is mixed described in the one surface even application of encapsulated layer
Slurry, precuring glue composite layer to be formed;Two encapsulated layers of adhesion are distinguished at the both ends of the honeycomb core material, at least one
The one end of the encapsulated layer and the honeycomb core material is attached with the precuring glue composite layer;Honeycomb described in curing molding is compound
Plate.The present invention can rationally control the distribution of fiber and adhesive by the way that fiber and adhesive are mixed into mixed slurry, so that
The dosage of adhesive is uniform, has not only retained the humidification of the tension resistance of fiber, but also be directly attached honeycomb core material, and it is convenient to form,
Suitable for automating batch jobs.
Detailed description of the invention
The present invention will be further described in detail below with reference to the accompanying drawings and specific embodiments.
Fig. 1 is the flow chart of honeycomb composite plate preparation method in a better embodiment of the invention.
Fig. 2 is the schematic diagram of honeycomb composite plate preparation facilities in a better embodiment of the invention.
Fig. 3 is the structural schematic diagram of honeycomb composite plate in a better embodiment of the invention.
Description of symbols:
Honeycomb composite plate | 100 |
Honeycomb core material | 10 |
Chopped strand | 1 |
Adhesive-layer | 30 |
Fiber gluing composite layer | 60 |
Honeycomb composite plate preparation facilities | 200 |
Mixed slurry preparation unit | 201 |
Mixed slurry coating element | 202 |
Honeycomb core material adhesion unit | 203 |
Curing molding unit | 204 |
The embodiment of the present invention that the following detailed description will be further explained with reference to the above drawings.
Specific embodiment
In order to be more clearly understood that the above objects, features, and advantages of the embodiment of the present invention, with reference to the accompanying drawing and
The present invention will be described in detail for specific embodiment.It should be noted that in the absence of conflict, the embodiment party of the application
Feature in formula can be combined with each other.
Embodiment in the following description, numerous specific details are set forth in order to facilitate a full understanding of the present invention, described reality
Applying mode is only some embodiments of the invention, rather than whole embodiments.Based on the embodiment in the present invention, originally
Field those of ordinary skill every other embodiment obtained without making creative work, belongs to this hair
The range of bright embodiment protection.
Unless otherwise defined, all technical and scientific terms used herein and the technology for belonging to the embodiment of the present invention
The normally understood meaning of the technical staff in field is identical.Term as used herein in the specification of the present invention is intended merely to
The purpose of specific embodiment is described, it is not intended that in the limitation embodiment of the present invention.
Referring to Fig. 1, Fig. 1 is the flow chart of honeycomb composite plate preparation method in a better embodiment of the invention.The bee
Honeycomb composite plate 100 includes encapsulated layer and honeycomb core material 10, which has the characteristics that light, sound insulation, can be used for
The fields such as kitchen and bath, Automobile Products, space flight and aviation.The honeycomb composite plate preparation method includes:
S101, chopped strand and adhesive are mixed into mixed slurry, so that the chopped strand is in the adhesive
It is uniformly distributed.
In the present embodiment, the fibrous material in the chopped strand 1 may include glass fibre, carbon fiber, aramid fiber
One of fiber, asbestos are a variety of, and the adhesive includes epoxide-resin glue, modified polyurethane glue or other adhesives.?
Before described the step of chopped strand 1 and adhesive are mixed into mixed slurry, the method also includes: by continuous fiber by pre-
If length is cut off to obtain the chopped strand 1, the length range of the chopped strand 1 is 1mm-70mm.
Chopped strand 1 is mixed in adhesive and is sufficiently stirred to obtain the mixed slurry, so that the chopped strand 1
It is uniformly distributed in the adhesive, wherein agitating mode includes manually stirring or being put into agitating device to be stirred.It is stirring
When mixing the mixed slurry, heat treatment can be carried out to the mixed slurry, so that the mobility of the mixed slurry increases
By force, it is easy to stirring operation.
S102, the mixed slurry described in the one surface even application of encapsulated layer, precuring glue composite layer to be formed.
In the present embodiment, the encapsulated layer include brown paper, fibrous layer, plastic film, metal foil, ceramics, stone material,
One of plastic plate is a variety of.Mixed slurry described in even application includes: the conveying envelope on one surface of encapsulated layer
Fill layer;Incude the position of the encapsulated layer;When the position for sensing the encapsulated layer is consistent with predeterminated position, to the encapsulation
Mixed slurry described in the surface even application to be applied of layer.Wherein, the predeterminated position is the pre-set position of user.
After the mixed slurry described in the one surface even application of encapsulated layer, precuring glue composite layer to be formed.Wherein,
The precuring glue composite layer is that heated at constant temperature is carried out under precuring temperature to the glue composite layer, and it is compound to obtain precuring glue
Layer.The precuring glue composite layer includes chopped strand 1 and adhesive.
S103, two encapsulated layers of adhesion, at least one encapsulated layer are distinguished into the both ends of the honeycomb core material 10
And the one end of the honeycomb core material 10 is attached with the precuring glue composite layer.
In the present embodiment, the structure of the cross section of the honeycomb core material 10 include regular hexagon, rectangle, diamond shape, watt
One of corrugated paper board shape, square, white-out circle, solid matter circle or triangle.The honeycomb core material 10 is aluminum honeycomb, paper wasp
One of nest, plastic honeycomb or high molecular material honeycomb.The other adhesion of end part is contacted by the two of the honeycomb core material described
The one end of two encapsulated layers, at least one encapsulated layer and the honeycomb core material is attached with the precuring glue composite layer
The step of before, the method also includes: at least one in the two of honeycomb core material contact ends is carried out at uneven integralization
Reason obtains the contact end of surface irregularity, and the contact end of the surface irregularity is in burr structure or broached-tooth design or other
Uneven structure.Wherein, the burr structure can be unordered, and be in orderly bending.The warp architecture designs not only
Contact area is big, while tension between the adhesive and honeycomb core material 10 after solidifying, resistance to compression and shear strength are more preferable, the two knot
It closes stronger.By carrying out uneven integralization processing to the honeycomb core material 10, contact area can be increased.
The both ends by the honeycomb core material 10 respectively two encapsulated layers of adhesion the step of include: by the bee
Two contact end parts of nest core material 10 are not pressed into two default glue agent layers;Wherein, at least one institute in the two default glue agent layers
State precuring glue composite layer.It is understood that the one end of at least one encapsulated layer and the honeycomb core material 10 is with described
The attachment of precuring glue composite layer.Other viscose glues can be passed through between the other end and the encapsulated layer of the honeycomb core material 10
Layer 30 is attached, and other adhesive-layers 30 can be epoxy glue layer or modified polyurethane glue-line.
Honeycomb composite plate 100 described in S104, curing molding.
In the present embodiment, honeycomb composite plate 100 described in the curing molding includes: that the acquisition precuring glue is compound
The precuring treatment temperature of layer;It is multiple to the honeycomb by the way of gradient increased temperature based on the precuring treatment temperature
Plywood 100 carries out curing molding processing.
The embodiment of the present invention provides a kind of honeycomb composite plate preparation method, and chopped strand 1 is mixed into adhesive and is mixed
Slurry, so that the chopped strand 1 is uniformly distributed in the adhesive;It is mixed described in the one surface even application of encapsulated layer
Close slurry, precuring glue composite layer to be formed;Two encapsulated layers of adhesion are distinguished at the both ends of the honeycomb core material 10, until
The one end of a few encapsulated layer and the honeycomb core material 10 is attached with the precuring glue composite layer;Bee described in curing molding
Honeycomb composite plate.The embodiment of the present invention can rationally control the distribution of fiber 1 Yu adhesive by mixing fiber 1 with adhesive,
So that the dosage of adhesive is uniform, not only retain the humidification of the tension resistance of fiber 1, but also be directly attached honeycomb core material 10, at
Type is convenient, is suitable for automation batch jobs.
Referring to Fig. 2, Fig. 2 is the schematic diagram of honeycomb composite plate preparation facilities in a better embodiment of the invention.Such as Fig. 2
It is shown, include: in the honeycomb composite plate preparation facilities 200 mixed slurry preparation unit 201, mixed slurry coating element 202,
Honeycomb core material adhesion unit 203 and curing molding unit 204.
Wherein, the mixed slurry preparation unit 201 is used to chopped strand 1 and adhesive being mixed into mixed slurry, directly
It is uniformly distributed in the adhesive to the chopped strand 1.The mixed slurry coating element 202 is used in the encapsulated layer
Mixed slurry described in one surface even application, precuring glue composite layer to be formed.The honeycomb core material adhesion unit 203 is used for will
Distinguish two encapsulated layers of adhesion, at least one encapsulated layer and the one of the honeycomb core material in the both ends of the honeycomb core material
End is attached with the precuring glue composite layer.The curing molding unit 204 is for honeycomb composite plate described in curing molding.
In the present embodiment, the mixed slurry coating element 202 includes transport platform, coating subelement, location sensitive
Subelement and managing main frame.Wherein, transport platform, the transport platform include opposite starting point and end.The starting point
It is equipped with a coating section between the end, the coating of the mixed slurry is carried out by applying subelement.The position sense
Answer subelement for sensing encapsulated layer in the position of the transport platform and output position information is to managing main frame.The managing main frame
It is electrically connected with the location sensitive subelement, coating subelement.The managing main frame detects position after receiving location information
Whether information is consistent with preset position information, if unanimously, issuing coating instruction to the coating subelement.
Specifically, the encapsulated layer is placed in the transport platform, the encapsulated layer needs to apply the mixing slurry
One surface of material and the coating subelement face;The transport platform is defeated from starting point to the end by the encapsulated layer
It send;The location sensitive subelement incudes the encapsulated layer in the position of the transport platform;When sensing the encapsulated layer in institute
When stating the predetermined position in transport platform, coating instruction is sent to the coating subelement by managing main frame;Apply subelement
When receiving coating instruction, the mixed slurry is applied to a surface of the encapsulated layer.
Two encapsulated layers after coating are delivered to the honeycomb core material in opposite directions and glued by the mixed slurry coating element 202
Even unit 203.The honeycomb core material adhesion unit 203 includes attachment subelement and position sensor, the position sensor sense
It answers two encapsulated layers and the honeycomb core material 10 come from other direction conveying to reach predeterminated position, and location information is sent out
It send to managing main frame, managing main frame exports two-sided attachment instruction after receiving location information, to the attachment subelement.It is described
Attachment subelement, which receives two-sided attachment instruction and is sandwiched between two encapsulated layers and applies pressure the honeycomb core material 10, to be made a reservation for
Type.In other embodiments, the institute that the position sensor can incude an encapsulated layer and come from other direction conveying
It states honeycomb core material 10 and reaches predeterminated position, the attachment subelement receives single side attachment instruction for the honeycomb core material 10 and the envelope
Layer adhesion is filled, the entirety after adhesion continues on to another predeterminated position with the encapsulated layer after another coating of adhesion.
Fig. 3 is please referred to, Fig. 3 is the structural schematic diagram of honeycomb composite plate in a better embodiment of the invention.The honeycomb
Composite plate 100 is prepared using honeycomb composite plate preparation method provided in an embodiment of the present invention.The honeycomb composite plate
100 have the characteristics that light, sound insulation, can be used for the fields such as kitchen and bath, Automobile Products, space flight and aviation.The honeycomb composite plate
100, including comb core material 10, chopped strand 1, adhesive-layer 30 and fiber gluing composite layer 60.Wherein, the fiber gluing
It is formed after the solidification of the mixed slurry of composite layer 60, the chopped strand 1 in the fiber gluing composite layer 60 is in uniform point
Cloth.The adhesive-layer 30 is the glue-line made of other adhesives other than the mixed slurry.By first will be described
Chopped strand 1 is mixed with the adhesive, obtains mixed slurry, can relatively easily control chopped strand 1 described
Distribution in fiber gluing composite layer 60, and forming step is simple, is conducive to automatic continuous production.The honeycomb core material 10 is real
Existing final application product lightness, sound insulation, heat insulation function key stratum structure.In the present embodiment, the honeycomb core material 10
For hexagon aluminum honeycomb, one end is directly attached viscose composite layer 60, and the other end is directly attached the adhesive-layer 30.
It is understood that in other embodiments, it is viscous that the both ends of the honeycomb core material 10 can directly be attached the fiber
Glue composite layer 60.For the bond strength for improving adhesive and honeycomb core material 10, can design the contact end of honeycomb core material 10
Carry out uneven integralization processing, Lai Zeng great contact area.
Embodiment of above is only to illustrate the technical solution of the embodiment of the present invention rather than limits, although referring to above preferable
The embodiment of the present invention is described in detail in embodiment, those skilled in the art should understand that, it can be to this hair
The technical solution of bright embodiment is modified or equivalent replacement should not all be detached from the embodiment of the present invention technical solution spirit and
Range.
Claims (10)
1. a kind of honeycomb composite plate preparation method, the honeycomb composite plate include encapsulated layer and honeycomb core material, which is characterized in that institute
Stating honeycomb composite plate preparation method includes:
Chopped strand and adhesive are mixed into mixed slurry, so that the chopped strand is uniformly distributed in the adhesive;
The mixed slurry described in the one surface even application of encapsulated layer, precuring glue composite layer to be formed;
Two encapsulated layers of adhesion, at least one encapsulated layer and the honeycomb core are distinguished into the both ends of the honeycomb core material
The one end of material is attached with the precuring glue composite layer;
Honeycomb composite plate described in curing molding.
2. honeycomb composite plate preparation method according to claim 1, which is characterized in that described by chopped strand and viscose glue
Agent was mixed into before the step of mixed slurry, the method also includes:
Continuous fiber is cut off to obtain the chopped strand by preset length, the length range of the chopped strand is 1mm-
70mm。
3. honeycomb composite plate preparation method according to claim 1, which is characterized in that fibrous material in the chopped strand
Including one of glass fibre, carbon fiber, aramid fiber, asbestos or a variety of, the adhesive includes epoxide-resin glue, poly- ammonia
One of ester gum or a variety of combinations.
4. honeycomb composite plate preparation method according to claim 1, which is characterized in that described on one surface of encapsulated layer
Include: the step of mixed slurry described in even application
Convey the encapsulated layer;
Incude the position of the encapsulated layer;
When the position for sensing the encapsulated layer is consistent with predeterminated position, to the surface even application to be applied of the encapsulated layer
The mixed slurry.
5. honeycomb composite plate preparation method according to claim 1, which is characterized in that described by the honeycomb core material
Two contact other two encapsulated layers of adhesion of end part, the one end of at least one encapsulated layer and the honeycomb core material is with described
Before the step of precuring glue composite layer is attached, the method also includes:
At least one in two contact ends of the honeycomb core material is carried out uneven integralization to handle to obtain the contact of surface irregularity
End.
6. honeycomb composite plate preparation method according to claim 1, which is characterized in that described by the two of the honeycomb core material
End respectively two encapsulated layers of adhesion the step of include:
Two contact end parts of the honeycomb core material two default glue agent layers are not pressed into;Wherein, in the two default glue agent layers
At least one precuring glue composite layer.
7. honeycomb composite plate preparation method according to claim 1, which is characterized in that honeycomb described in the curing molding is multiple
Plywood includes:
Obtain the precuring treatment temperature of the precuring glue composite layer;
Based on the precuring treatment temperature, curing molding is carried out to the honeycomb composite plate by the way of gradient increased temperature
Processing.
8. honeycomb composite plate preparation method according to claim 1, which is characterized in that the encapsulated layer include brown paper,
One of fibrous layer, plastic film, metal foil, ceramics, stone material, plastic plate are a variety of.
9. honeycomb composite plate preparation method according to claim 1, which is characterized in that the honeycomb core material be aluminum honeycomb,
One of paper honeycomb, plastic honeycomb or high molecular material honeycomb are a variety of.
10. honeycomb composite plate preparation method according to claim 1, which is characterized in that the cross section of the honeycomb core material
Structure include regular hexagon, rectangle, diamond shape, corrugated board shape, square, white-out is round, solid matter is round or triangle in
It is a kind of.
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CN201910267531.XA CN110126365A (en) | 2019-04-03 | 2019-04-03 | Honeycomb composite plate preparation method |
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Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0798102A2 (en) * | 1996-03-27 | 1997-10-01 | Isola AG | Self-sticking prepreg, process for its manufacture and use of it |
CN1772477A (en) * | 2005-09-15 | 2006-05-17 | 时光 | Honeycomb board compounding process |
CN2785851Y (en) * | 2005-04-07 | 2006-06-07 | 黄桂芳 | Ultra-thin stone cellular board |
JP2007008002A (en) * | 2005-06-30 | 2007-01-18 | Kyocera Chemical Corp | Flame-retardant lightweight board |
-
2019
- 2019-04-03 CN CN201910267531.XA patent/CN110126365A/en active Pending
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0798102A2 (en) * | 1996-03-27 | 1997-10-01 | Isola AG | Self-sticking prepreg, process for its manufacture and use of it |
CN2785851Y (en) * | 2005-04-07 | 2006-06-07 | 黄桂芳 | Ultra-thin stone cellular board |
JP2007008002A (en) * | 2005-06-30 | 2007-01-18 | Kyocera Chemical Corp | Flame-retardant lightweight board |
CN1772477A (en) * | 2005-09-15 | 2006-05-17 | 时光 | Honeycomb board compounding process |
Non-Patent Citations (5)
Title |
---|
刘智恩: "《材料科学基础》", 30 September 2013, 西北工业大学出版社 * |
刘祖毅: "《尼龙喷涂》", 31 December 1978, 机械工业出版社 * |
王云渤等: "《飞机装配工艺学》", 31 August 1990, 国防工业出版社 * |
王建清等: "《包装材料学》", 28 February 2017, 中国轻工业出版社 * |
陈开勋等: "《精细化工产品化学及应用》", 30 September 1995, 西北大学出版社 * |
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