CN110126365A - Honeycomb composite plate preparation method - Google Patents

Honeycomb composite plate preparation method Download PDF

Info

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
Authority
CN
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.)
Pending
Application number
CN201910267531.XA
Other languages
Chinese (zh)
Inventor
丁友张
朱拥军
刘国华
曹洋
陈亚楠
王翌龙
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Jiangsu Jilun Housing Technology Co Ltd
Original Assignee
Jiangsu Jilun Housing Technology Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Jiangsu Jilun Housing Technology Co Ltd filed Critical Jiangsu Jilun Housing Technology Co Ltd
Priority to CN201910267531.XA priority Critical patent/CN110126365A/en
Publication of CN110126365A publication Critical patent/CN110126365A/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00Layered 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
    • B32B3/10Layered 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
    • B32B3/12Layered 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B33/00Layered 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/12Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by using adhesives
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B7/00Layered 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
    • B32B7/04Interconnection of layers
    • B32B7/12Interconnection 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

Honeycomb composite plate preparation method
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.
CN201910267531.XA 2019-04-03 2019-04-03 Honeycomb composite plate preparation method Pending CN110126365A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201910267531.XA CN110126365A (en) 2019-04-03 2019-04-03 Honeycomb composite plate preparation method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201910267531.XA CN110126365A (en) 2019-04-03 2019-04-03 Honeycomb composite plate preparation method

Publications (1)

Publication Number Publication Date
CN110126365A true CN110126365A (en) 2019-08-16

Family

ID=67569232

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201910267531.XA Pending CN110126365A (en) 2019-04-03 2019-04-03 Honeycomb composite plate preparation method

Country Status (1)

Country Link
CN (1) CN110126365A (en)

Citations (4)

* Cited by examiner, † Cited by third party
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

Patent Citations (4)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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 *

Similar Documents

Publication Publication Date Title
CN105848860B (en) Wind turbine blade
US7179517B2 (en) Sheet moulding compound (SMC) with ventilating structure for entrapped gases
CN104797668A (en) Adherable flexible composite systems
WO2009016552A3 (en) A method of manufacturing a curved element made of composite material
AU2001293967A1 (en) Sheet moulding compound (SMC) with ventilating structure for entrapped gases
CN105291490B (en) It is a kind of to be used to form thin plate layer, honeycomb of honeycomb and preparation method thereof
EP3134257B1 (en) Panel made of laminates and method of manufacturing the same
JPH10503720A (en) Adhesives with synthetic fiber reinforcement-components for laminated wood structures
CN110126363A (en) Honeycomb composite plate preparation method
CN110126365A (en) Honeycomb composite plate preparation method
JP5324788B2 (en) Fiber reinforced plastic, method for producing the same, and kit for producing the same
CN110130571A (en) Composite sandwich plate, combined wall board and chassis
CN108016106A (en) A kind of thermoplasticity prepreg and preparation method
CN210134581U (en) Composite sandwich plate, composite wall plate and chassis
CN203793465U (en) Tensile framework layer board strip and manufacturing device and rubber belt track thereof
EP3587477B1 (en) Ultra-thin pre-preg sheets and composite materials thereof
CN215590169U (en) PVC foaming board
EP0598591A2 (en) Fibre-reinforced sheet for reinforcement
JPH09141610A (en) Decorative veneer laminated plywood and manufacture thereof
CN110126364A (en) The preparation method of honeycomb composite plate
CN210652195U (en) Be applied to trinity of circuit board production from type membrane
JPH09117902A (en) Wooden composite curved surface formed plate and manufacture thereof
JP2016216947A (en) Reinforcement sheet for concrete structure and manufacturing method thereof, and reinforcement structure for concrete structure
CN206046373U (en) Acrylic adhesive tape coating machine
JPH0423602B2 (en)

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication

Application publication date: 20190816

RJ01 Rejection of invention patent application after publication