CN110468355A - The formation system and material of carbon fiber reinforced aluminum matrix composite - Google Patents
The formation system and material of carbon fiber reinforced aluminum matrix composite Download PDFInfo
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- CN110468355A CN110468355A CN201910884446.8A CN201910884446A CN110468355A CN 110468355 A CN110468355 A CN 110468355A CN 201910884446 A CN201910884446 A CN 201910884446A CN 110468355 A CN110468355 A CN 110468355A
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- carbon fiber
- aluminium
- aluminium alloy
- reinforced aluminum
- composite
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- 229920000049 Carbon (fiber) Polymers 0.000 title claims abstract description 181
- 239000004917 carbon fiber Substances 0.000 title claims abstract description 181
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 title claims abstract description 179
- 239000002131 composite material Substances 0.000 title claims abstract description 133
- 229910052782 aluminium Inorganic materials 0.000 title claims abstract description 107
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 title claims abstract description 107
- 239000011159 matrix material Substances 0.000 title claims abstract description 49
- 230000015572 biosynthetic process Effects 0.000 title claims abstract description 18
- 239000000463 material Substances 0.000 title abstract description 9
- 229910000838 Al alloy Inorganic materials 0.000 claims abstract description 91
- 239000004411 aluminium Substances 0.000 claims abstract description 52
- 239000005030 aluminium foil Substances 0.000 claims abstract description 31
- 239000007788 liquid Substances 0.000 claims abstract description 25
- 239000000835 fiber Substances 0.000 claims abstract description 23
- 238000001816 cooling Methods 0.000 claims abstract description 21
- 238000000034 method Methods 0.000 claims abstract description 21
- 230000000694 effects Effects 0.000 claims abstract description 15
- 238000005096 rolling process Methods 0.000 claims abstract description 7
- 238000000137 annealing Methods 0.000 claims abstract description 4
- 230000008018 melting Effects 0.000 claims description 19
- 238000002844 melting Methods 0.000 claims description 19
- 238000004804 winding Methods 0.000 claims description 17
- 230000001502 supplementing effect Effects 0.000 claims description 16
- 239000007787 solid Substances 0.000 claims description 11
- 238000002360 preparation method Methods 0.000 claims description 8
- 229910052571 earthenware Inorganic materials 0.000 claims description 5
- 238000004781 supercooling Methods 0.000 claims description 5
- 238000005303 weighing Methods 0.000 claims description 5
- 230000008014 freezing Effects 0.000 claims description 4
- 238000007710 freezing Methods 0.000 claims description 4
- 238000010438 heat treatment Methods 0.000 claims description 4
- 238000012545 processing Methods 0.000 claims description 4
- 238000007711 solidification Methods 0.000 claims description 4
- 230000008023 solidification Effects 0.000 claims description 4
- 238000005259 measurement Methods 0.000 claims description 3
- 239000012528 membrane Substances 0.000 claims description 3
- 238000012546 transfer Methods 0.000 claims description 3
- 229910045601 alloy Inorganic materials 0.000 claims description 2
- 239000000956 alloy Substances 0.000 claims description 2
- 238000007670 refining Methods 0.000 claims description 2
- 239000002994 raw material Substances 0.000 claims 1
- 238000001125 extrusion Methods 0.000 abstract description 4
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 5
- 229910052799 carbon Inorganic materials 0.000 description 5
- 238000009833 condensation Methods 0.000 description 3
- 230000005494 condensation Effects 0.000 description 3
- 230000002708 enhancing effect Effects 0.000 description 3
- 230000001965 increasing effect Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 239000007791 liquid phase Substances 0.000 description 2
- 239000013589 supplement Substances 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 238000003723 Smelting Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 229910010293 ceramic material Inorganic materials 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 239000006052 feed supplement Substances 0.000 description 1
- 239000011888 foil Substances 0.000 description 1
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 1
- 239000010931 gold Substances 0.000 description 1
- 229910052737 gold Inorganic materials 0.000 description 1
- 238000005470 impregnation Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 238000009716 squeeze casting Methods 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C47/00—Making alloys containing metallic or non-metallic fibres or filaments
- C22C47/02—Pretreatment of the fibres or filaments
- C22C47/06—Pretreatment of the fibres or filaments by forming the fibres or filaments into a preformed structure, e.g. using a temporary binder to form a mat-like element
- C22C47/062—Pretreatment of the fibres or filaments by forming the fibres or filaments into a preformed structure, e.g. using a temporary binder to form a mat-like element from wires or filaments only
- C22C47/064—Winding wires
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C47/00—Making alloys containing metallic or non-metallic fibres or filaments
- C22C47/08—Making alloys containing metallic or non-metallic fibres or filaments by contacting the fibres or filaments with molten metal, e.g. by infiltrating the fibres or filaments placed in a mould
- C22C47/12—Infiltration or casting under mechanical pressure
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C49/00—Alloys containing metallic or non-metallic fibres or filaments
- C22C49/02—Alloys containing metallic or non-metallic fibres or filaments characterised by the matrix material
- C22C49/04—Light metals
- C22C49/06—Aluminium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C49/00—Alloys containing metallic or non-metallic fibres or filaments
- C22C49/14—Alloys containing metallic or non-metallic fibres or filaments characterised by the fibres or filaments
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Crystallography & Structural Chemistry (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
Abstract
The invention discloses a kind of formation system of carbon fiber reinforced aluminum matrix composite and materials.The system is by the way that the carbon fiber wire on carbon fiber wire wheel to be uniformly immersed in aluminium alloy melt, aluminium alloy liquid film is formed between carbon fiber wire, aluminium alloy liquid film solidifies along carbon fiber wire direction and is combined together to form carbon fiber aluminium film composite layer under cooling effect, then after being preheated to carbon fiber aluminium film composite layer with aluminium foil by primary heater through the first squeeze roll together with the rolling of the second squeeze roll, form fibre reinforced aluminum-base composite layer, it is wound into, which constantly on Filament Wound Composite roller under the extruding for squeezing smooth roll, by secondary heater annealing forms carbon fiber reinforced aluminum matrix composite, high temperature extrusion increases the bond strength of fibre reinforced aluminum-base composite layer Yu carbon fiber reinforced aluminum matrix composite interface.Therefore, the system has many advantages, such as that simple process, at low cost and the carbon fiber effect in conjunction with aluminium base are good.
Description
Technical field
The present invention relates to carbon fiber reinforced aluminum matrix composite technical field more particularly to a kind of fibre reinforced aluminium base are multiple
The formation system and material of condensation material.
Background technique
The continuous carbon fiber reinforced aluminum matrix composite of interfacial structure has specific strength, specific modulus, thermal conductivity high, thermally expands
The features such as coefficient is low, and high temperature dimensional stability is good.There is impact resistance, good toughness, thermal conductivity and electric conductivity compared with ceramic material
Good feature, therefore carbon fiber reinforced aluminum matrix composite is widely used in the fields such as space flight and aviation, in auto industry, electricity
Son, sports goods, building field are also widely used.Common preparation and forming method have solid state process and two kinds of liquid phase process, Gu
State method is mainly powder metallurgic method and diffusion bonding method;Liquid phase process mainly has infiltrated with molten metal method, squeeze casting method and vacuum pressure
Method of impregnation etc..But continuous carbon fibre reinforced aluminum matrix composites preparation process in the prior art is typically complex, the period
It is long, at high cost, low efficiency, therefore the high-performance composite materials of simple process be scientific research and continuous carbon fibre enhancing aluminium base
The emphasis of composite material industrialization.
Summary of the invention
The technical problem to be solved by the present invention is to how provide a kind of simple process and carbon fiber effect in conjunction with aluminium base
The formation system of good carbon fiber reinforced aluminum matrix composite.
In order to solve the above technical problems, the technical solution used in the present invention is: a kind of fibre reinforced aluminum-base composite material
The formation system of material, it is characterised in that: including melting kettle, the periphery of the melting kettle is provided with crucible heater, described
Crucible heater makes it be melted into aluminium alloy melt for heating to the aluminium alloy stock in the crucible;It is described molten
Right side outside refining crucible is provided with carbon fiber wire wheel, equally spaced on the carbon fiber wire wheel to be wound with carbon fiber wire;The earthenware
Directive wheel is provided with right above crucible, the directive wheel is immersed in carbon fiber wire for changing the direction of transfer of carbon fiber wire
In the aluminium alloy melt of melting kettle;It is provided with cooling device on the left of the crucible, the cooling device is used for from crucible
Aluminium alloy liquid film between the carbon fiber wire inside sent out carries out cooling treatment, so that liquid aluminium membrane orienting is solidified as solid aluminum
Film, and be freezing together to form carbon fiber aluminium film composite layer with carbon fiber wire;The is provided on the left of the cooling device
One squeeze roll is provided with the second squeeze roll on the left of first squeeze roll, sets on the upside of second squeeze roll
It is equipped with aluminium foil wheel, aluminium foil is wound on the aluminium foil wheel, is kept between first squeeze roll and second squeeze roll
There is gap, and be provided with primary heater above the gap, the primary heater is used for the aluminium for entering the gap
Foil and carbon fiber aluminium film composite layer are preheated, and Filament Wound Composite roller is provided with below the gap, the winding roller
Underface, which is provided with, squeezes smooth roll, and described squeeze is provided with the second heating around smooth roll and Filament Wound Composite roller
Device, the secondary heater are used to heat the carbon fiber reinforced aluminum matrix composite and the smooth roll of extruding;
The carbon fiber reinforced aluminum matrix composite wound on smooth roll and the winding roller that squeezes directly contacts;
The carbon fiber wire being wrapped on the carbon fiber wire wheel makes carbon fiber wire enter aluminium conjunction after changing direction by directive wheel
In golden melt, make to overwork aluminium alloy melt formation aluminium alloy liquid film, aluminium alloy between carbon fiber wire under the action of interfacial tension
Liquid film directional solidification after the cooling treatment of apparatus for supercooling is solid-state aluminium film, and is freezing together to form carbon fiber with carbon fiber wire
Aluminum film compounded layer is tieed up, carbon fiber aluminium film composite layer is transferred into the gap between the first squeeze roll and second squeeze roll
Top, then aluminium foil and carbon fiber aluminium film composite layer enter in the gap simultaneously, first by between primary heater pair
Carbon fiber aluminium film composite layer and aluminium foil below gap are heated, then squeezing by the first squeeze roll and the second squeeze roll
Pressure effect makes the two combine to form fibre reinforced aluminum-base composite layer, and last fibre reinforced aluminum-base composite layer first passes through
The heating of secondary heater is made annealing treatment, then is wound into after extruding and smooth processing by squeezing smooth roll described multiple
On condensation material winding roller, carbon fiber reinforced aluminum matrix composite is formed.
A further technical solution lies in: the system also includes the aluminium alloy feed supplement being located at right above crucible dresses
It sets, the aluminium alloy feed supplementing device is for supplementing aluminium alloy stock into the crucible.
A further technical solution lies in: the system also includes the weighing device for being located at the crucible bottom, the titles
The gross mass for measuring the crucible and the aluminium alloy in it is set in refitting, for according to the control of the weight information of measurement
Aluminium alloy stock is added into the crucible in aluminium alloy feed supplementing device.
A further technical solution lies in: carbon fiber wire placing groove, the carbon fiber are formed on the carbon fiber wire wheel
Silk is wound into the carbon fiber wire placing groove, guarantees two adjacent carbon fibers by the position-limiting action of carbon fiber wire placing groove
The distance between silk.
A further technical solution lies in: guide groove, the guide groove and the carbon fiber are formed on the directive wheel
Silk placing groove corresponds, and the carbon fiber wire is entered in aluminium alloy melt by the effect of the guide groove;Initial aluminum is closed
Golden feeding stage, directive wheel is not with solid aluminium alloy contact, and before preparation process starts, starting crucible heater closes solid aluminium
After gold is molten into aluminium alloy melt, aluminium alloy is supplemented by aluminium alloy feed supplementing device until not crossing guide groove.
A further technical solution lies in: it is described to squeeze smooth roll by squeezing smooth roller lift device setting in institute
The underface for stating Filament Wound Composite roller, as the composite material is wound on the winding roller, the extruding leveling rolling
Roller lifting device adjusts the position for squeezing smooth roll according to the value of feedback of device for measuring force so that squeeze smooth roll always with
The outermost composite material of winding roller directly contacts, and squeezes smooth roll to composite material progress by described
It squeezes, improves the combination effect between the aluminium foil and the carbon fiber aluminium film composite layer.
A further technical solution lies in: the carbon fiber wire wheel, directive wheel, the first squeeze roll and fibre reinforced aluminium
Linear velocity is equal during rotation for the bar that based composites are formed.
The invention also discloses a kind of carbon fiber reinforced aluminum matrix composites, it is characterised in that: is carried out using the system
Preparation.
The beneficial effects of adopting the technical scheme are that the system is by by the carbon fiber on carbon fiber wire wheel
Dimension silk is uniformly immersed in aluminium alloy melt, and aluminium alloy liquid film, the aluminium alloy liquid film under cooling effect are formed between carbon fiber wire
It is solidified along carbon fiber wire direction and is combined together to form carbon fiber aluminium film composite layer, then by primary heater to carbon fiber
It ties up after aluminum film compounded layer is preheated with aluminium foil through the first squeeze roll together with the rolling of the second squeeze roll, forms carbon fiber
Dimension enhancing aluminum-base composite layer, being annealed by secondary heater, it is constantly wound into composite material under the extruding for squeezing smooth roll
Carbon fiber reinforced aluminum matrix composite is formed on winding roller, high temperature extrusion increases fibre reinforced aluminum-base composite layer and carbon fiber
The bond strength of reinforced aluminum matrix composites interface.Therefore, the system has simple process, at low cost and carbon fiber and aluminium
Base junction closes the advantages that effect is good.
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 structural schematic diagram of system described in the embodiment of the present invention;
Fig. 2 is the structural schematic diagram of directive wheel in system described in the embodiment of the present invention;
Wherein: 1, aluminium foil;2, primary heater;3, the first squeeze roll, carbon fiber reinforced aluminum matrix composite;4, carbon fiber
Silk;5, carbon fiber aluminium film composite layer;5-1, aluminium alloy liquid film;6, melting kettle;7, directive wheel;7-1, guide groove;8, aluminium alloy
Melt;9, carbon fiber wire wheel;10, crucible heater;11, aluminium alloy feed supplementing device;12, device for measuring force;13, leveling rolling is squeezed
Roller;14, secondary heater;15, the second squeeze roll;16, carbon fiber reinforced aluminum matrix composite, the first squeeze roll;17, claim
Refitting is set;18, cooling device;19, Filament Wound Composite roller;20, compression roller lifting device is wound.
Specific embodiment
With reference to the attached drawing in the embodiment of the present invention, technical solution in the embodiment of the present invention carries out clear, complete
Ground description, it is clear that described embodiment is only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
In the following description, numerous specific details are set forth in order to facilitate a full understanding of the present invention, but the present invention can be with
Implemented using other than the one described here other way, those skilled in the art can be without prejudice to intension of the present invention
In the case of do similar popularization, therefore the present invention is not limited by the specific embodiments disclosed below.
As shown in Figure 1, the invention discloses a kind of formation system of carbon fiber reinforced aluminum matrix composite, including melting earthenware
Crucible 6, the periphery of the melting kettle 6 are provided with crucible heater 10, and the crucible heater 10 is used for in the crucible
Aluminium alloy stock is heated, it is made to be melted into aluminium alloy melt 8;Right side outside the melting kettle 6 is provided with carbon fiber
Silk wheel 9, it is equally spaced on the carbon fiber wire wheel 9 to be wound with carbon fiber wire 4;Directive wheel 7 is provided with right above the crucible,
The directive wheel 7 makes carbon fiber wire 4 be immersed in the aluminium alloy melt of melting kettle 6 for changing the direction of transfer of carbon fiber wire 4
It is interior;Cooling device 18 is provided on the left of the crucible, the cooling device is used for the carbon fiber sent out out of crucible
Between aluminium alloy liquid film 5-1 carry out cooling treatment so that liquid aluminium membrane orienting is solidified as solid-state aluminium film, and solidified with carbon fiber wire
Carbon fiber aluminium film composite layer 5 is formed together;The left side of the cooling device 18 is provided with the first squeeze roll 3, and described first
The left side of squeeze roll 3 is provided with the second squeeze roll 15, and the upside of second squeeze roll 15 is provided with aluminium foil wheel (in figure
Do not regard out), aluminium foil 1 is wound on the aluminium foil wheel, is kept between first squeeze roll 3 and second squeeze roll 15
There is gap, and be provided with primary heater 2 above the gap, the primary heater 2 is used for the entrance gap
Aluminium foil 1 and carbon fiber aluminium film composite layer 5 are preheated, and Filament Wound Composite roller 19 is provided with below the gap, described to twine
It is provided with immediately below roller and squeezes smooth roll 13, it is described to squeeze smooth roll 13 and the setting of 19 surrounding of Filament Wound Composite roller
There is secondary heater 14, the secondary heater 14 is used for the carbon fiber reinforced aluminum matrix composite 16 and squeezes leveling rolling
Roller 13 is heated;It is described to squeeze the carbon fiber reinforced aluminum matrix composite wound on smooth roll 13 and the winding roller
16 directly contact;
The carbon fiber wire 4 being wrapped on the carbon fiber wire wheel 9 enters carbon fiber wire 4 after changing direction by directive wheel 7
In aluminium alloy melt 8, make to overwork aluminium alloy melt formation aluminium alloy liquid film 5- between carbon fiber wire 4 under the action of interfacial tension
1, aluminium alloy liquid film the 5-1 directional solidification after the cooling treatment of apparatus for supercooling 18 are solid-state aluminium film, and are solidified with carbon fiber wire
Carbon fiber aluminium film composite layer 5 is formed together, and carbon fiber aluminium film composite layer 5 is transferred into the first squeeze roll 3 and described second
The top in the gap between squeeze roll 15, then aluminium foil 1 and carbon fiber aluminium film composite layer 5 enter in the gap simultaneously,
First by primary heater 2 to below gap carbon fiber aluminium film composite layer 5 and aluminium foil 2 heat, then pass through first
The squeezing action of squeeze roll 3 and the second squeeze roll 15 makes the two combine to form fibre reinforced aluminum-base composite layer
21, last fibre reinforced aluminum-base composite layer 21 is described multiple by being wound into after squeezing the extruding and smooth processing of smooth roll 13
On condensation material winding roller 19, carbon fiber reinforced aluminum matrix composite 16 is formed.
Further, as shown in Figure 1, the system also includes the aluminium alloy feed supplementing devices being located at right above the crucible
11, the aluminium alloy feed supplementing device 11 enables the system to complete described for supplementing aluminium alloy stock into the crucible
The continuous preparation of composite material.
Further, as shown in Figure 1, the system also includes the weighing device 17 for being located at the crucible bottom, the title
Refitting sets 17 for measuring the gross mass of the crucible and the aluminium alloy in it, for controlling institute according to the weight information of measurement
It states aluminium alloy feed supplementing device 11 and aluminium alloy stock is added into the crucible.
Further, as shown in Figure 1, being formed with carbon fiber wire placing groove, the carbon fiber wire on the carbon fiber wire wheel 9
4 are wound into the carbon fiber wire placing groove, guarantee two adjacent carbon fibers by the position-limiting action of carbon fiber wire placing groove
The distance between silk.As Figure 1-Figure 2, guide groove 7-1, the guide groove 7-1 and the carbon are formed on the directive wheel 7
Fiber filament placing groove corresponds, and the carbon fiber wire 4 is entered in aluminium alloy melt 8 by the effect of the guide groove 7-1;
Initial aluminium alloy feeding stage, directive wheel 7 with solid aluminium alloy contact, before preparation process starts, do not start crucible heater 10
So that solid aluminum alloy melting be aluminium alloy melt 8 after, by aluminium alloy feed supplementing device 11 supplement aluminium alloy until do not cross be oriented to
Slot 7-1.
Further, as shown in Figure 1, the smooth roll 13 of the extruding is arranged by squeezing smooth roller lift device 20
In the underface of the Filament Wound Composite roller 19, as the composite material is wound on the winding roller, the extruding
Smooth roller lift device 20 squeezes the position of smooth roll 13 according to the value of feedback of device for measuring force 12, so that squeezing leveling rolling
Roller 13 is directly contacted with the outermost composite material of the winding roller always, by the smooth roll 13 that squeezes to described
Composite material is squeezed and is annealed, and the combination effect between the aluminium foil 1 and the carbon fiber aluminium film composite layer 5 is improved.
Further, as shown in Figure 1, the winding roller, carbon fiber wire wheel 9, directive wheel 7, the first squeeze roll 3 and carbon fiber
Tieing up the bar that reinforced aluminum matrix composites 16 are formed, linear velocity is equal during rotation.
The embodiment of the invention also discloses a kind of forming method of carbon fiber reinforced aluminum matrix composite, the forming method
Using carbon fiber reinforced aluminum matrix composite formation system, include the following steps:
1) 4 surface of carbon fiber wire is carried out copper facing first to be modified, the aluminium of carbon fiber wire 4 or different model to a certain diameter closes
Before golden system prepares the composite material, progress 4 spacing of carbon fiber wire experiment first, by being gradually increased or reducing carbon fiber
The distance between silk 4, so that carbon fiber wire 4 can be formed after entering aluminium alloy melt 8 between adjacent carbon fiber wire 4
Then complete aluminium alloy liquid film selects to have to obtain the carbon fiber wire spacing range of the alloy system further according to needs
The directive wheel 7 of the suitable guide groove 7-1 of width, and the carbon fiber wire wheel 9 with the suitable carbon fiber wire placing groove of width, are opened
Dynamic primary heater 2 and secondary heater 14;
2) carbon fiber wire 4 is wrapped on carbon fiber wire wheel 9, the free end of each carbon fiber wire 4 first passes around on directive wheel 7
The corresponding guide groove change side 7-1 is twined back into the gap between the first squeeze roll 3 and second squeeze roll 15
On Filament Wound Composite roller 19, aluminium foil 1 is wound by the gap between the first squeeze roll 3 and the second squeeze roll 15
Onto Filament Wound Composite roller 19, it is not bonded together in initial stage aluminium foil 1 and carbon fiber wire 4 at this time.
3) aluminium alloy stock is added in melting kettle 6, directive wheel 7 starts earthenware not with solid aluminium alloy contact at this time
Crucible heater 10, smelting temperature be 700-1000 DEG C so that solid aluminum alloy melting be aluminium alloy melt 8 after, pass through aluminium alloy
Feed supplementing device 11 supplements aluminium alloy until not crossing guide groove 7-1, and start the system, squeezes the first squeeze roll 3, second
Roll 15, thermally conductive smooth roll 13, winding roller 19 and carbon fiber wire wheel 9 rotate, and rotation linear velocity is identical, wherein the first extruding is rolled
Roller 3 and the second squeeze roll 15 relatively rotate, and squeeze smooth roll 13 and relatively rotate with Filament Wound Composite roller 19, so that carbon fiber
Silk 4 is tieed up to move;
4) start cooling device 18, carbon fiber wire 4 is then made constantly to be immersed in the aluminium alloy of melting kettle 6 by directive wheel 7
In melt, after carbon fiber wire 4 leaves aluminium alloy melt, aluminium alloy liquid film 5-1 is formed between carbon fiber wire 4;
5) when aluminium alloy liquid film 5-1 is through 18 top of apparatus for supercooling, make aluminium alloy liquid film 5-1 fast under cooling device effect
Prompt drop temperature improves interfacial tension, and when being cooled to aluminum alloy solidification point or less, aluminium alloy liquid film is oriented along carbon fiber wire direction
It solidifies and is combined together to form carbon fiber aluminium film composite layer 5;Carbon fiber aluminium film composite layer 5 and aluminium foil 1 are in the first squeeze roll 3
It meeting above gap between the second squeeze roll 15, primary heater 2 is arranged along the length direction of the first squeeze roll 3,
Primary heater 2 to below carbon fiber aluminium film composite layer 5 and aluminium foil 1 preheat;
6) carbon fiber aluminium film composite layer 5 and aluminium foil 1 are formed continuously under the action of the first squeeze roll 3 and the second squeeze roll 15
Fibre reinforced aluminum-base composite layer 21, preheating enhance the combination under extrusion of aluminium foil 1 and carbon fiber aluminium film composite layer 5
Power;With the rotation for squeezing smooth roll 13 and Filament Wound Composite roller 19, increase by the carbon fiber that secondary heater 14 heats
Strong aluminum-base composite layer 21 is constantly wound on Filament Wound Composite roller 19 in the case where squeezing smooth roll 13 and squeezing forms carbon fiber increasing
Strong aluminum matrix composite 16, subsequent carbon fiber reinforced aluminum matrix composite 16 are constantly annealed by secondary heater 14, are passed through again
The extruding for squeezing smooth roll 13 is crossed, the fibre reinforced aluminium realizing fibre reinforced aluminum-base composite layer 21 and being wound
The combination of based composites 16;Secondary heater 14 is also preheated to the smooth roll 13 of extruding simultaneously, and heat is transmitted to continuous shape
At carbon fiber reinforced aluminum matrix composite 16, prevent the smooth roll 13 of extruding of supercooling from reducing enhancing carbon fiber aluminium film composite layer
5 with the temperature of 1 binding site of aluminium foil;
After preparing carbon fiber reinforced aluminum matrix composite 16 and starting, the bar of carbon fiber reinforced aluminum matrix composite 16 constantly increases
Greatly, it while adjusting so that the linear velocity of the bar of carbon fiber reinforced aluminum matrix composite 16 is stablized;
7) as the diameter of the Filament Wound Composite roller 19 of winding carbon fiber reinforced aluminum matrix composite 16 constantly increases, carbon fiber
Reinforced aluminum matrix composites 16 and the stress squeezed between smooth roll 13 are increasing, at this time should by the feedback of device for measuring force 12
Then stress value is adjusted by squeezing smooth roller lift device 20 and squeezes smooth 13 position of roll realization Filament Wound Composite
The distance between outermost carbon fiber reinforced aluminum matrix composite 16 and the smooth roll 13 of extruding are constant on roller 19;
8) along with the preparation of continuous carbon fibre reinforced aluminum matrix composites 3, the aluminium alloy melt 8 in melting kettle 6 is reduced, and is led to
Aluminium alloy feed supplementing device 11 is crossed to the constantly addition aluminium alloy stock of melting kettle 6, while according to the numerical value change of weighing system 17
Adjustment guarantees that the amount for the aluminium alloy that aluminium alloy liquid film 5-1 takes away and aluminium alloy source enter the amount of melting kettle 6, until needed for reaching
The carbon fiber reinforced aluminum matrix composite 3 of size or weight.
The system and method are by the way that the carbon fiber wire on carbon fiber wire wheel to be uniformly immersed in aluminium alloy melt, in carbon
Aluminium alloy liquid film is formed between fiber filament, aluminium alloy liquid film is solidified and is combined together along carbon fiber wire direction under cooling effect
Carbon fiber aluminium film composite layer is formed, is passed through after then being preheated by primary heater to carbon fiber aluminium film composite layer and aluminium foil
Together with first squeeze roll is rolled with the second squeeze roll, fibre reinforced aluminum-base composite layer is formed, secondary heater is passed through
Annealing, it is constantly wound into formation fibre reinforced aluminum-base composite on Filament Wound Composite roller under the extruding for squeezing smooth roll
Material, high temperature extrusion increases fibre reinforced aluminum-base composite layer and the combination of carbon fiber reinforced aluminum matrix composite interface is strong
Degree.Therefore, the system and method have many advantages, such as that simple process, at low cost and the carbon fiber effect in conjunction with aluminium base are good.
Claims (8)
1. a kind of formation system of carbon fiber reinforced aluminum matrix composite, it is characterised in that: described molten including melting kettle (6)
The periphery of refining crucible (6) is provided with crucible heater (10), and the crucible heater (10) is used to close the aluminium in the crucible
Golden raw material is heated, it is made to be melted into aluminium alloy melt (8);The right side of the melting kettle (6) outside is provided with carbon fiber
Silk takes turns (9), equally spaced on the carbon fiber wire wheel (9) to be wound with carbon fiber wire (4);It is provided with and leads right above the crucible
To wheel (7), the directive wheel (7) makes carbon fiber wire (4) be immersed in melting earthenware for changing the direction of transfer of carbon fiber wire (4)
In the aluminium alloy melt of crucible (6);It is provided on the left of the crucible cooling device (18), the cooling device is used for from crucible
Aluminium alloy liquid film (5-1) between the carbon fiber wire (4) inside sent out carries out cooling treatment, so that liquid aluminium membrane orienting is solidified as
Solid-state aluminium film, and be freezing together to form carbon fiber aluminium film composite layer (5) with carbon fiber wire;Close to the cooling device (18)
Left side is provided with the first squeeze roll (3), is provided with the second squeeze roll (15), institute on the left of first squeeze roll (3)
It states and is provided with aluminium foil wheel on the upside of the second squeeze roll (15), be wound on the aluminium foil wheel aluminium foil (1), first extruding is rolled
Gap is maintained between roller (3) and second squeeze roll (15), and is provided with primary heater above the gap
(2), the primary heater (2) is used to carry out the aluminium foil (1) and carbon fiber aluminium film composite layer (5) that enter the gap pre-
Heat is provided with Filament Wound Composite roller (19) below the gap, is provided with extruding leveling rolling immediately below the winding roller
Roller (13), described squeeze is provided with secondary heater (14) around smooth roll (13) and Filament Wound Composite roller (19), described
Secondary heater (14) is used to heat the carbon fiber reinforced aluminum matrix composite (16) and the smooth roll (13) of extruding
Processing;The carbon fiber reinforced aluminum matrix composite (16) wound on smooth roll (13) and the winding roller that squeezes directly connects
Touching;
The carbon fiber wire (4) being wrapped on the carbon fiber wire wheel (9) makes carbon fiber wire after changing direction by directive wheel (7)
(4) it enters in aluminium alloy melt (8), makes to overwork aluminium alloy melt shape under the action of interfacial tension between carbon fiber wire (4)
At aluminium alloy liquid film (5-1), aluminium alloy liquid film (5-1) directional solidification after the cooling treatment of apparatus for supercooling (18) is solid aluminum
Film, and be freezing together to form carbon fiber aluminium film composite layer (5) with carbon fiber wire, carbon fiber aluminium film composite layer (5) is transferred into
The top in the gap between the first squeeze roll (3) and second squeeze roll (15), then aluminium foil (1) and carbon fiber aluminium film
Composite layer (5) enters in the gap simultaneously, aluminum film compounded to the carbon fiber below gap by primary heater (2) first
Layer (5) and aluminium foil (2) are heated, and are then made by the first squeeze roll (3) and the squeezing action of the second squeeze roll (15)
The two combines to form fibre reinforced aluminum-base composite layer (21), and last fibre reinforced aluminum-base composite layer (21) first passes through
The heating of secondary heater is made annealing treatment, then is wound into institute after extruding and smooth processing by squeezing smooth roll (13)
It states on Filament Wound Composite roller (19), is formed carbon fiber reinforced aluminum matrix composite (16).
2. the formation system of carbon fiber reinforced aluminum matrix composite as described in claim 1, it is characterised in that: the system is also
Including being located at the aluminium alloy feed supplementing device (11) right above the crucible, the aluminium alloy feed supplementing device (11) is used for the earthenware
Aluminium alloy stock is supplemented in crucible.
3. the formation system of carbon fiber reinforced aluminum matrix composite as claimed in claim 2, it is characterised in that: the system is also
Including be located at the crucible bottom weighing device (17), the weighing device (17) for measure the crucible and its in
The gross mass of aluminium alloy adds for being controlled in aluminium alloy feed supplementing device (11) the Xiang Suoshu crucible according to the weight information of measurement
Enter aluminium alloy stock.
4. the formation system of carbon fiber reinforced aluminum matrix composite as described in claim 1, it is characterised in that: the carbon fiber
It is formed with carbon fiber wire placing groove on silk wheel (9), the carbon fiber wire (4) is wound into the carbon fiber wire placing groove, passes through
The position-limiting action of carbon fiber wire placing groove guarantees adjacent the distance between two carbon fiber wires.
5. the formation system of carbon fiber reinforced aluminum matrix composite as claimed in claim 4, it is characterised in that: the directive wheel
(7) it is formed on guide groove (7-1), the guide groove (7-1) and the carbon fiber wire placing groove correspond, the carbon fiber
Silk (4) is entered in aluminium alloy melt (8) by the effect of the guide groove (7-1);Initial aluminium alloy feeding stage, directive wheel
(7) not with solid aluminium alloy contact, before preparation process starts, starting crucible heater (10) makes solid aluminum alloy melting be aluminium
After alloy melt (8), aluminium alloy is supplemented by aluminium alloy feed supplementing device (11) until not crossing guide groove (7-1).
6. the formation system of carbon fiber reinforced aluminum matrix composite as described in claim 1, it is characterised in that: described squeeze is put down
Whole roll (13) by squeezing the setting of smooth roller lift device (20) in the underface of the Filament Wound Composite roller (19), with
The composite material be wound on the winding roller, it is described to squeeze smooth roller lift device (20) according to device for measuring force
(12) value of feedback squeezes the position of smooth roll (13) to adjust so that squeeze smooth roll (13) always with the winding roller
The outermost composite material directly contacts, and is squeezed by the smooth roll (13) of extruding the composite material,
Improve the combination effect between the aluminium foil (1) and the carbon fiber aluminium film composite layer (5).
7. the formation system of carbon fiber reinforced aluminum matrix composite as described in claim 1, it is characterised in that: the carbon fiber
The bar that silk wheel (9), directive wheel (7), the first squeeze roll (3) and carbon fiber reinforced aluminum matrix composite (16) are formed is rotating
Process centerline velocities are equal.
8. a kind of carbon fiber reinforced aluminum matrix composite, it is characterised in that: use the system system as described in claim 1-7
It is standby.
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN115044843A (en) * | 2022-06-29 | 2022-09-13 | 东北大学 | Preparation method of rolled carbon fiber reinforced aluminum alloy composite material |
KR20220165957A (en) * | 2021-06-09 | 2022-12-16 | 박희준 | Manufacturing method of material containing carbon fiber |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS58136735A (en) * | 1982-02-08 | 1983-08-13 | Nippon Soken Inc | Manufacture of carbon fiber reinforced composite aluminum material |
CN1394979A (en) * | 2002-06-28 | 2003-02-05 | 太原理工大学 | Aluminium base mixed continuous carbon fibre composite material and its preparation |
CN103911610A (en) * | 2014-04-01 | 2014-07-09 | 太原理工大学 | Preparation method of shielding aluminum-based aluminum plate |
CN105039877A (en) * | 2015-08-05 | 2015-11-11 | 同济大学 | Carbon fiber reinforced aluminum-based composite material and preparation method and application thereof |
CN108453244A (en) * | 2018-03-06 | 2018-08-28 | 王书杰 | The preparation facilities of copper clad aluminum composite bar |
-
2019
- 2019-09-19 CN CN201910884446.8A patent/CN110468355B/en active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS58136735A (en) * | 1982-02-08 | 1983-08-13 | Nippon Soken Inc | Manufacture of carbon fiber reinforced composite aluminum material |
CN1394979A (en) * | 2002-06-28 | 2003-02-05 | 太原理工大学 | Aluminium base mixed continuous carbon fibre composite material and its preparation |
CN103911610A (en) * | 2014-04-01 | 2014-07-09 | 太原理工大学 | Preparation method of shielding aluminum-based aluminum plate |
CN105039877A (en) * | 2015-08-05 | 2015-11-11 | 同济大学 | Carbon fiber reinforced aluminum-based composite material and preparation method and application thereof |
CN108453244A (en) * | 2018-03-06 | 2018-08-28 | 王书杰 | The preparation facilities of copper clad aluminum composite bar |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20220165957A (en) * | 2021-06-09 | 2022-12-16 | 박희준 | Manufacturing method of material containing carbon fiber |
KR102597746B1 (en) * | 2021-06-09 | 2023-11-02 | 박희준 | Manufacturing method of material containing carbon fiber |
CN115044843A (en) * | 2022-06-29 | 2022-09-13 | 东北大学 | Preparation method of rolled carbon fiber reinforced aluminum alloy composite material |
CN115044843B (en) * | 2022-06-29 | 2023-09-22 | 东北大学 | Preparation method of rolled carbon fiber reinforced aluminum alloy composite material |
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