CN108340640A - A kind of composite material heating plate and preparation method thereof - Google Patents
A kind of composite material heating plate and preparation method thereof Download PDFInfo
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- CN108340640A CN108340640A CN201810149251.4A CN201810149251A CN108340640A CN 108340640 A CN108340640 A CN 108340640A CN 201810149251 A CN201810149251 A CN 201810149251A CN 108340640 A CN108340640 A CN 108340640A
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- heating plate
- heating
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- carbon fibre
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- 238000010438 heat treatment Methods 0.000 title claims abstract description 173
- 239000002131 composite material Substances 0.000 title claims abstract description 52
- 238000002360 preparation method Methods 0.000 title abstract description 5
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 32
- 239000011162 core material Substances 0.000 claims abstract description 32
- 239000000835 fiber Substances 0.000 claims abstract description 31
- 229910052799 carbon Inorganic materials 0.000 claims abstract description 26
- 239000010410 layer Substances 0.000 claims abstract description 24
- 239000002344 surface layer Substances 0.000 claims abstract description 20
- 239000004745 nonwoven fabric Substances 0.000 claims abstract description 14
- 229920000049 Carbon (fiber) Polymers 0.000 claims abstract description 13
- 239000004917 carbon fiber Substances 0.000 claims abstract description 13
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims abstract description 13
- 229920001169 thermoplastic Polymers 0.000 claims abstract description 13
- 239000004416 thermosoftening plastic Substances 0.000 claims abstract description 13
- 239000002184 metal Substances 0.000 claims abstract description 8
- 229910052751 metal Inorganic materials 0.000 claims abstract description 8
- 239000000463 material Substances 0.000 claims abstract description 7
- 230000006798 recombination Effects 0.000 claims abstract description 7
- 238000005215 recombination Methods 0.000 claims abstract description 7
- 238000004519 manufacturing process Methods 0.000 claims abstract description 6
- 150000001875 compounds Chemical class 0.000 claims description 13
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 12
- 229910052802 copper Inorganic materials 0.000 claims description 12
- 239000010949 copper Substances 0.000 claims description 12
- 239000004814 polyurethane Substances 0.000 claims description 10
- 239000003292 glue Substances 0.000 claims description 7
- 239000010439 graphite Substances 0.000 claims description 6
- 229910002804 graphite Inorganic materials 0.000 claims description 6
- 230000001413 cellular effect Effects 0.000 claims description 5
- 239000000945 filler Substances 0.000 claims description 5
- 238000013461 design Methods 0.000 claims description 4
- 238000000034 method Methods 0.000 claims description 4
- 229920002635 polyurethane Polymers 0.000 claims description 4
- 238000003825 pressing Methods 0.000 claims description 4
- 238000004513 sizing Methods 0.000 claims description 4
- 238000005187 foaming Methods 0.000 claims description 3
- 238000000465 moulding Methods 0.000 claims description 3
- 239000004593 Epoxy Substances 0.000 claims description 2
- 238000000748 compression moulding Methods 0.000 claims description 2
- 238000001816 cooling Methods 0.000 claims description 2
- 238000003801 milling Methods 0.000 claims description 2
- 239000004033 plastic Substances 0.000 claims description 2
- 229920003023 plastic Polymers 0.000 claims description 2
- 230000005494 condensation Effects 0.000 claims 1
- 238000009833 condensation Methods 0.000 claims 1
- 230000000694 effects Effects 0.000 description 6
- 238000009413 insulation Methods 0.000 description 6
- 238000012546 transfer Methods 0.000 description 5
- 239000000853 adhesive Substances 0.000 description 3
- 230000001070 adhesive effect Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 239000007788 liquid Substances 0.000 description 3
- 230000005855 radiation Effects 0.000 description 3
- 239000004831 Hot glue Substances 0.000 description 2
- 239000013078 crystal Substances 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 229920006332 epoxy adhesive Polymers 0.000 description 2
- 238000007731 hot pressing Methods 0.000 description 2
- 230000001788 irregular Effects 0.000 description 2
- 238000002156 mixing Methods 0.000 description 2
- 229910052755 nonmetal Inorganic materials 0.000 description 2
- 239000005413 snowmelt Substances 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 241000132536 Cirsium Species 0.000 description 1
- 206010037660 Pyrexia Diseases 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- -1 compound metals Chemical class 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 238000005485 electric heating Methods 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 229920006335 epoxy glue Polymers 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012856 packing Methods 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 229920005989 resin Polymers 0.000 description 1
- 239000011347 resin Substances 0.000 description 1
- 229920005992 thermoplastic resin Polymers 0.000 description 1
- 239000002759 woven fabric Substances 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
-
- 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
- B32B3/02—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 features of form at particular places, e.g. in edge regions
- B32B3/08—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 features of form at particular places, e.g. in edge regions characterised by added members at particular parts
-
- 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
- B32B3/10—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 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 shape; Layered products comprising a layer 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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- 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
- B32B3/30—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 formed with recesses or projections, e.g. hollows, grooves, protuberances, ribs
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/06—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the heating method
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/10—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the pressing technique, e.g. using action of vacuum or fluid pressure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/04—Interconnection of layers
- B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
- B32B9/04—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B9/047—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material made of fibres or filaments
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/106—Carbon fibres, e.g. graphite fibres
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/30—Properties of the layers or laminate having particular thermal 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
- B32B2307/00—Properties of the layers or laminate
- B32B2307/30—Properties of the layers or laminate having particular thermal properties
- B32B2307/304—Insulating
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/70—Other properties
- B32B2307/718—Weight, e.g. weight per square meter
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Surface Heating Bodies (AREA)
- Resistance Heating (AREA)
Abstract
The invention discloses a kind of composite material heating plate and preparation method thereof, wherein composite material heating plate, including multiple heating plate units, each plate unit that heats includes core material and is covered in the heating surface layer of core material upper surface or/and lower surface;Heating surface layer includes carbon fibre heating plate, and carbon fiber heating on piece is fixedly installed two conductiving metal strips as electricity-linkingup point, and the upper and lower surface recombination of carbon fibre heating plate is stained with non-woven fabrics, and the outer surface of non-woven fabrics is provided with thermoplastic composite layer;The core materials lateral surface is provided at least one temperature sensor, contact and the heating face layer contacts of temperature sensor.Temperature sensor, which is arranged, can accurately measure the temperature of heating surface layer, convenient for accurately controlling.The problem of non-woven fabrics, thermoplastic composite layer are nonmetallic materials, and there is no electric leakages, has a safety feature.Plate unit, modularized production, and easy to disassemble, repair are heated by setting, it is at low cost.
Description
Technical field
The present invention relates to a kind of composite material heating plates and preparation method thereof.
Background technology
Heating, the floor heating heating device of the carriage body of heat insulation function, building and deicing device for melting snow etc. are needed, is required for
Use heating device.In these fields, existing common heating device includes following several:
1), internal liquid circulation heats:Using liquid such as water, oil as circulating-heating medium (as shown in Figure 1), will send out
Heat pipeline is embedded in heated die plate, is made to be reached predetermined temperature by warm object by heat transfer etc. and is kept controllable temperature range (temperature
Control device control), so that it is met actual operation requirements, such mode of heating heating source and be integrated, such as hot pressing by warm object
The oil heating of airborne equipment, the water circulating-heating etc. inside composite material mould.
2), internal resistance silk heats:Using the metal wires such as resistance wire, net as heating source, made by temperature by heat transfer etc.
Object reaches predetermined temperature and keeps controllable temperature range (temperature controller control), it is made to meet actual operation requirements, such as electric heating
Blanket, disappear ice snow melt panel etc..
3), separate type heats:(as shown in Figure 2) is heated as heating source or compressor using resistance wire, it is right by heat
Stream, heat radiation etc. make to be reached predetermined temperature by warm object and keep controllable temperature range (temperature controller control), so that it is met practical
Requirement, such mode of heating heating source and be separate type by warm object, such as the heater that military, civilian carriage body uses,
The floor heating of building, insulated building of equipment etc..
But existing above-mentioned mode of heating has the following disadvantages:
Internal circulating-heating:
1), the older easy failure of heating line influences heating effect, or even influences to use;
2), heating rate is slower;
3), fever pipeline occupies certain space, keeps heating module volume bigger than normal inside heating module, lays particular stress on.
Internal resistance silk heats:
1), there are security risk, maintenance is bad to be easy to happen leaky, serious initiation fire;
2) occasion of high-power heating, is needed, heating module occupied space is larger, such as the ice snow melt that disappears;
3) it influences to use after, breaking down.
Separate type heats:
1), heating source occupied space is big, improper for the limited occasion in space;
2) it, for the big occasion of heating space, can only be heated by thermal convection current and heat radiation, spacial temperature elevation speed
Slowly;
3), compressor heating is easy to be out of order.
For above-mentioned heating device there are the problem of, need in a hurry it is a kind of it is simple in structure, small, heating is fast, safety
Heating device.
Invention content
The purpose of the present invention is to provide a kind of composite material heating plate and preparation method thereof, solve to add in the prior art
The technical issues of thermal is complicated, volume is big, heating is slow, poor safety performance.
In order to solve the above-mentioned technical problem, the present invention adopts the following technical scheme that:
A kind of composite material heating plate, including multiple heating plate units, each heating plate cell edges are fixedly installed company
Fitting, adjacent heating plate unit are combined into heating plate by connector cooperation;
Each heating plate unit includes core material and is covered in the heating surface layer of core material upper surface or/and lower surface;It is described to add
Hot-face layer includes carbon fibre heating plate, and carbon fiber heating on piece is fixedly installed at least two conductiving metal strips as electricity-linkingup point,
The upper and lower surface recombination of carbon fibre heating plate is stained with non-woven fabrics, and the outer surface of non-woven fabrics is provided with thermoplastic composite layer;Institute
It states core materials lateral surface and is provided at least one temperature sensor, contact and the heating face layer contacts of temperature sensor.
Carbon fibre heating plate is made of carbon fiber, organic fiber and graphite packing, organic fiber as heating plate inside
Skeleton among carbon fiber is scattered in skeleton so that conductive unit is unordered, constitutes current path.After powering on, in external micro-current
Under the action of, carbon crystal molecule does unordered Brownian movement, between molecule irregular movement generate friction, convert electrical energy into heat
Energy.Heat is transmitted to heated object nonmetallic composite cover in such a way that thermal convection current, heat radiation or heat are transmitted, while compound
There is the heat insulation core material of intralamellar part certain heat insulation effect, thermoplastic composite layer to have certain mechanical strength so that compound
Plate has multifunctionality.
Temperature sensor, which is arranged, can accurately measure the temperature of heating surface layer, convenient for accurately controlling.
The problem of non-woven fabrics, thermoplastic composite layer are nonmetallic materials, and there is no electric leakages, security performance
It is good.
Plate unit, modularized production, and easy to disassemble, repair are heated by setting, it is at low cost.
It is further improved, the carbon fibre heating plate is using organic fiber as skeleton, by carbon fiber and electrically conductive graphite filler
Mixing is evenly distributed with into skeleton, pressing and forming.After powering on, under the action of external micro-current, carbon crystal molecule makees unordered cloth
Bright movement, between molecule irregular movement generate friction, convert electrical energy into thermal energy.
It is further improved, the thickness of the heating surface layer is 0.6mm -3mm, and thickness is thin, small, takes up space small, together
When heat transfer it is fast.
It is further improved, the heating surface layer further includes being arranged in the overlay film of thermoplastic composite layer outer surface or multiple
Conjunction face layer.Overlay film or composite cover, including metal and non-metal surfaces layer are set according to actual demand, plays anti-corrosion, improve intensity
The effects that.
It is further improved, the core material is cystosepiment, foaming cellular core plate or normal cellular core plate.Convenient material drawing, cost
It is low, it is light-weight, and heat insulation effect is good.
It is further improved, the side of the core material opens up fluted, and depth of groove is 5mm -10mm, and temperature sensor is set
It sets in a groove.Prevent temperature sensor exposed outside, influence measurement accuracy, at the same protect temperature sensor avoid and other
Object collides and damages.
It is further improved, direct current or alternating current may be used to composite material heater plate;Be applicable in voltage be 7V~
220V;Maximum heating temperature is 120 DEG C;Maximum heating rate is 11~13 DEG C/min;Average heating rate be 3~4 DEG C/
min.Pressure-resistant range is wide, highly practical, and quick heating is efficient.
A kind of production method of composite material heating plate, includes the following steps:
1), using machine fiber as skeleton, the fillers such as carbon fiber and electrically conductive graphite is mixed and are evenly distributed with into skeleton, are pressed into
Carbon fibre heating plate is made in type;
2) two copper bars, are arranged in parallel as electricity-linkingup point, copper bar and carbon fiber heating in one side surface of carbon fibre heating plate
Piece passes to carbon fibre heating plate by PU glue stickings, by electric energy by copper bar;
3) the upper and lower surface of carbon fibre heating plate, protection copper bar and good bonding circle of offer, are arrived by non-woven fabric compounded;Nothing
Woven fabric is that the thermoplastic resins such as felt and PP are combined, and the PP resins in non-woven fabrics can melt under the high temperature conditions, with carbon fiber
Dimension heating plate directly merges molding, does not need adhesive, composite instant.By one layer of the coating that PU glue is very thin at the copper bar back side, face
When connect with carbon fibre heating plate, by by it is non-woven fabric compounded reach to carbon fibre heating plate copper bar is further fixed, it is thin
Thin PU glue coats have no effect on the electric conductivity between copper bar and carbon fibre heating plate.
4), thermoplastic composite is overlayed on to the upper and lower surface of step 3) institute forming face layer, carry out compression molding, molding
Temperature is 200~240 DEG C, and heating time is 2~5min, and heating finishes, and during cooling, mold continues to keep closing
State 1min~3min;
5), by numerical control CNC according to design requirement in one side surface milling groove of core material, depth of groove is in 5mm~10mm
Between, multiple temperature sensors are provided in groove;
6), heating surface layer is laid on to the upper surface or/and lower surface of core material by design size, by heat it is compound or
Be that sizing is compound is complex as heating plate unit by the two;
7), adjacent heating plate unit is connected by connector multiple heating plate units being combined into heating plate;It will be more
Temperature sensor in a heating plate unit realizes that parallel connection is connect with controller by master-slave socket.
In step 4) and 5) it is further improved, further includes the following steps between being arranged:Outside thermoplastic composite layer
The overlay film or composite cover on surface.
It is further improved, in the step 6), if compound using heating, specially:Heat combined temp be 200~
220 DEG C, 1~2min of heating time, 1~2min of dwell time;
If compound using being glued, specially:If compound using epoxy systems glue, combined temp is 35~80 DEG C, multiple
The conjunction time is 1~10h, such as EPLY-1 epoxy adhesives, EPLY-2 epoxy adhesives.
If using polyurethane system, sizing temperature be 140~160 DEG C of temperature, room temperature roll recombination time be 5~
15min, such as PUR hot melt adhesive, a kind of polyurethane adhesive capable of rapid positioning, Henkel, Fuller, ten thousand Li Deng producers all produce at present.
Epoxy glue:Hot pressing is compound, needs to heat, and the time is longer, generally uses this technique at present;Polyurethane adhesive:It refers in particular to
PUR hot melt adhesive, sizing, the time is short, and positioning is fast, this glue-applying technique patent applied for, and only we make on a large scale at present
With.
The present invention has the advantages that compared with prior art:
1, occupied space is low:For nonmetallic composite cover as heating source, thickness is very thin, is integrally formed with composite plate.
2, mode of heating is various:Heat transfer can be selected to be directly heated to object or thermal convection current and hot spoke according to occasion
Penetrate indirectly heat.
3, heat insulation effect is good:Heating speed is fast, after being combined into composite plate with heat insulation core material, passes through the temperature control of inside setting
Sensor can keep composite plate continually and steadily in certain temperature, and low energy consumption.
4, safety coefficient is high:The problem of heating surface layer is nonmetallic composite, and there is no electric leakages;When a certain region goes out
When existing problem, the heating of other regions is not influenced;It is simple in structure, long lifespan.
5, modular board:Composite heating plate be modular sheet material be laid with, by controller realize each module board independence and
Associated working, under conditions of not influencing heating work, aspect repair and replacement.
6, mechanical property is good:Heating plate enhances face layer and nonmetal heating plastic material, recoverable is used to be fabricated to multiple
Have good mechanical property after closing heating plate, is a kind of multifunction board.
7, thistle board:Core material and composite heating face are nonmetallic materials, and whole plate surface density is low.
8, overlay film type is more:Can according to actual demand on the outside of heating surface layer overlay film or other compound metals or nonmetallic
Face layer.
Description of the drawings
Fig. 1 is the schematic diagram of internal liquid circulation heating in the prior art.
Fig. 2 is the schematic diagram of separate type heating in the prior art.
Fig. 3 is that heating surface layer removes schematic diagram in the present invention.
Fig. 4 is composite material heating plate side schematic view of the present invention.
Fig. 5 is the connection figure between multiple heating plate units.
Fig. 6 is the relational graph of the heating time-current-temperature in embodiment.
Specific implementation mode
To keep the purpose of the present invention and technical solution clearer, below in conjunction with the embodiment of the present invention to the present invention's
Technical solution is clearly and completely described.
Such as Fig. 3-6, a kind of composite material heating plate, including three heating plate units, each heating plate cell edges are fixed
It is provided with connector, by the cooperation of two neighboring heating plate unit connector, multiple heating plate units are combined into heating
Plate;The width a of each heating plate unit is 0.166m, and length b is 2.5m, and adjacent copper bar spacing c is 0.83m.In the present embodiment
Middle connector is slot, plug construction.
Each heating plate unit includes core material and is covered in the heating surface layer 1 of 2 upper and lower surface of core material;It is described to add
Hot-face layer 1 includes carbon fibre heating plate 11, and there are three parallel conductiving metal strips 12 to make for fixed setting on carbon fibre heating plate 11
For electricity-linkingup point, 11 upper and lower surface recombination of carbon fibre heating plate is stained with non-woven fabrics 13, and the outer surface of non-woven fabrics 13 is provided with thermoplastic
Property composite layer 14, as shown in Figure 3.The core materials lateral surface is provided at least one temperature sensor 3, temperature sensor 3
Contact is contacted with heating surface layer 1.
In the present embodiment, the carbon fibre heating plate 11 is using organic fiber as skeleton, by carbon fiber and electrically conductive graphite
Filler mixing is evenly distributed with into skeleton, pressing and forming.In the present embodiment, the thickness of the heating surface layer is 2mm, and thickness is thin, body
Product is small, takes up space small, while heat transfer is fast.
In the present embodiment, the heating surface layer 1 further includes that covering in 14 outer surface of thermoplastic composite layer is arranged
Film.In other embodiments, composite cover can be metal or nonmetallic thin plate.
In the present embodiment, the core material 2 is cystosepiment.In other embodiments, core material is foaming cellular core plate or general
Logical honeycomb core plate.
In the present embodiment, the side of the core material 2 opens up fluted, depth of groove 8mm, temperature sensor setting
In a groove, as shown in Figure 4.
Three heating each plates of plate unit are connected into heating plate, each heating plate unit medium temperature degree sensor 3 passes through male and female
Plug realization is connected in parallel peripheral control unit, as shown in Figure 5.It is wet with 24 DEG C of environment temperature using the composite material heating plate
60% (RH) is spent, alternating voltage 220V, 25.8 Ω of heating plate resistance are heated to for 80 DEG C, heating time-current-temperature
Relationship such as Fig. 6, shown in table 1.
The data of 1 heating time of table-current-temperature
As can be seen from the above table, the composite material heating plate, heating 1min temperature are just raised to 35 DEG C, and 12min reaches 70
DEG C, 0.5h reaches 80 DEG C, and the efficiency of heating surface is high, and heating is steady, and electric current is constant.
Do not done in the present invention illustrate be the prior art or can be realized by the prior art, and this hair
The preferable case study on implementation that case is only the present invention, implementation model not for the purpose of limiting the invention are embodied described in bright
It encloses.That is equivalent changes and modifications made by all contents according to scope of the present invention patent all should be used as the technology model of the present invention
Farmland.
Claims (10)
1. a kind of composite material heating plate, which is characterized in that including multiple heating plate units, each heating plate cell edges are fixed
It is provided with connector, adjacent heating plate unit is combined into heating plate by connector cooperation;
Each heating plate unit includes core material and is covered in the heating surface layer of core material upper surface or/and lower surface;The heating surface
Layer includes carbon fibre heating plate, and carbon fiber heating on piece is fixedly installed at least two conductiving metal strips as electricity-linkingup point, carbon fiber
The dimension upper and lower surface recombination of heating plate is stained with non-woven fabrics, and the outer surface of non-woven fabrics is provided with thermoplastic composite layer;The core material
Side is provided at least one temperature sensor, contact and the heating face layer contacts of temperature sensor.
2. composite material heating plate according to claim 1, which is characterized in that the carbon fibre heating plate is with organic fiber
As skeleton, carbon fiber and electrically conductive graphite filler are mixed and are evenly distributed with into skeleton, pressing and forming.
3. composite material heating plate according to claim 1 or 2, which is characterized in that the thickness of the heating surface layer is
0.6mm—3mm。
4. composite material heating plate according to claim 3, which is characterized in that the heating surface layer further includes being arranged in heat
The overlay film or composite cover of plastic composites layer outer surface.
5. composite material heating plate according to claim 4, which is characterized in that the core material is cystosepiment, foaming cellular
Core plate or normal cellular core plate.
6. composite material heating plate according to claim 5, which is characterized in that the side of the core material open up it is fluted,
Depth of groove is 5mm -10mm, and temperature sensor is arranged in a groove.
7. composite material heating plate according to claim 6, which is characterized in that direct current or alternating current may be used to multiple
Condensation material heater plate;It is 7V~220V to be applicable in voltage;Maximum heating temperature is 120 DEG C;Maximum heating rate is 11~13
℃/min;Average heating rate is 3~4 DEG C/min.
8. the production method of the composite material heating plate described in any one of claim 1-7, which is characterized in that including walking as follows
Suddenly:
1), using organic fiber as skeleton, carbon fiber and electrically conductive graphite filler is mixed and are evenly distributed with into skeleton, pressing and forming, system
At carbon fibre heating plate;
2) two copper bars, are arranged in parallel as electricity-linkingup point in one side surface of carbon fibre heating plate, copper bar is logical with carbon fibre heating plate
PU glue stickings are crossed, electric energy is passed into carbon fibre heating plate by copper bar;
3) the upper and lower surface of carbon fibre heating plate, protection copper bar and good bonding circle of offer, are arrived by non-woven fabric compounded;
4), by thermoplastic composite overlay on step 3) at face layer upper and lower surface, carry out compression molding, molding temperature is
200~240 DEG C, heating time is 2~5min, and after heating, during cooling, mold continues the state for keeping closing
1min~3min;
5), by numerical control CNC according to design requirement in one side surface milling groove of core material, depth of groove between 5mm~10mm,
Multiple temperature sensors are provided in groove;
6), heating surface layer is laid on to the upper surface or/and lower surface of core material by design size, it is multiple by heating compound or sizing
It closes and the two is complex as heating plate unit;
7) it, is connected by the connector between adjacent heating plate unit, multiple heating plate units is combined into heating plate;It will
Temperature sensor in multiple heating plate units realizes that parallel connection is connect with controller by master-slave socket.
9. the production method of composite material heating plate according to claim 8, which is characterized in that further include being arranged in step
And 5) 4) following steps between:In thermoplastic composite layer outer surface overlay film or composite cover.
10. the production method of composite material heating plate according to claim 8 or claim 9, which is characterized in that the step 6)
In, use heat compound method for:It is 200~220 DEG C, 1~2min of heating time to heat combined temp, the dwell time 1~
2min;
Use be glued compound method for:If compound using epoxy systems glue, combined temp is 35~80 DEG C, and recombination time is
1~10h;If compound using polyurethane system glue, combined temp is 140~160 DEG C of temperature, and recombination time is 5~15min.
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US20150252175A1 (en) * | 2014-03-04 | 2015-09-10 | Frx Polymers, Inc. | Epoxy compositions |
CN106488593A (en) * | 2015-11-04 | 2017-03-08 | 石家庄邦迪高分子材料有限公司 | A kind of Far infrared carbon fiber composite heating film |
CN206418724U (en) * | 2016-12-09 | 2017-08-18 | 久盛地板有限公司 | Built-in carbon fiber electrothermal layer consolidated floor |
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CN201203194Y (en) * | 2008-04-01 | 2009-03-04 | 陆上驰 | Electrothermic composite ground warming floor |
CN102046864A (en) * | 2008-05-28 | 2011-05-04 | 瑟尔瑞株式会社 | Electrically conductive pad and a production method thereof |
US20150252175A1 (en) * | 2014-03-04 | 2015-09-10 | Frx Polymers, Inc. | Epoxy compositions |
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Application publication date: 20180731 |