CN1092004A - Metal ceramic surface composite material and production process thereof - Google Patents
Metal ceramic surface composite material and production process thereof Download PDFInfo
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- CN1092004A CN1092004A CN 93111991 CN93111991A CN1092004A CN 1092004 A CN1092004 A CN 1092004A CN 93111991 CN93111991 CN 93111991 CN 93111991 A CN93111991 A CN 93111991A CN 1092004 A CN1092004 A CN 1092004A
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- ceramic
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- preheating
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- 229910052751 metal Inorganic materials 0.000 title claims abstract description 45
- 239000002184 metal Substances 0.000 title claims abstract description 45
- 239000000919 ceramic Substances 0.000 title claims abstract description 44
- 239000002131 composite material Substances 0.000 title claims abstract description 39
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 17
- 239000000463 material Substances 0.000 claims abstract description 22
- 238000005266 casting Methods 0.000 claims abstract description 18
- 239000004576 sand Substances 0.000 claims abstract description 17
- 239000011159 matrix material Substances 0.000 claims abstract description 15
- 239000002245 particle Substances 0.000 claims abstract description 11
- 229910010293 ceramic material Inorganic materials 0.000 claims abstract description 10
- 238000002156 mixing Methods 0.000 claims abstract description 9
- 238000005187 foaming Methods 0.000 claims abstract description 6
- 238000000465 moulding Methods 0.000 claims abstract description 5
- 239000011268 mixed slurry Substances 0.000 claims abstract 2
- 239000000843 powder Substances 0.000 claims description 14
- 238000005516 engineering process Methods 0.000 claims description 10
- 150000001875 compounds Chemical class 0.000 claims description 9
- -1 Sodium alkyl sulfonate Chemical class 0.000 claims description 8
- 229910004298 SiO 2 Inorganic materials 0.000 claims description 7
- 229910052708 sodium Inorganic materials 0.000 claims description 7
- 239000011734 sodium Substances 0.000 claims description 7
- 239000006188 syrup Substances 0.000 claims description 7
- 235000020357 syrup Nutrition 0.000 claims description 7
- 229910000881 Cu alloy Inorganic materials 0.000 claims description 6
- KGBXLFKZBHKPEV-UHFFFAOYSA-N boric acid Chemical compound OB(O)O KGBXLFKZBHKPEV-UHFFFAOYSA-N 0.000 claims description 6
- 239000004327 boric acid Substances 0.000 claims description 6
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 6
- 230000015572 biosynthetic process Effects 0.000 claims description 5
- 239000007921 spray Substances 0.000 claims description 4
- JOYRKODLDBILNP-UHFFFAOYSA-N Ethyl urethane Chemical compound CCOC(N)=O JOYRKODLDBILNP-UHFFFAOYSA-N 0.000 claims description 3
- 229910001060 Gray iron Inorganic materials 0.000 claims description 3
- ZLMJMSJWJFRBEC-UHFFFAOYSA-N Potassium Chemical compound [K] ZLMJMSJWJFRBEC-UHFFFAOYSA-N 0.000 claims description 3
- 229910052700 potassium Inorganic materials 0.000 claims description 3
- 239000011591 potassium Substances 0.000 claims description 3
- 239000003822 epoxy resin Substances 0.000 claims description 2
- 239000000835 fiber Substances 0.000 claims description 2
- 125000002496 methyl group Chemical group [H]C([H])([H])* 0.000 claims description 2
- 229920001568 phenolic resin Polymers 0.000 claims description 2
- 229920000647 polyepoxide Polymers 0.000 claims description 2
- 239000011347 resin Substances 0.000 claims description 2
- 229920005989 resin Polymers 0.000 claims description 2
- 238000005755 formation reaction Methods 0.000 claims 3
- 239000005007 epoxy-phenolic resin Substances 0.000 claims 1
- 239000006260 foam Substances 0.000 claims 1
- 238000000034 method Methods 0.000 abstract description 22
- CWYNVVGOOAEACU-UHFFFAOYSA-N Fe2+ Chemical compound [Fe+2] CWYNVVGOOAEACU-UHFFFAOYSA-N 0.000 abstract description 3
- 239000012467 final product Substances 0.000 abstract 1
- 238000002844 melting Methods 0.000 abstract 1
- 230000008018 melting Effects 0.000 abstract 1
- 239000011156 metal matrix composite Substances 0.000 abstract 1
- 239000000047 product Substances 0.000 abstract 1
- 238000005507 spraying Methods 0.000 abstract 1
- 239000004604 Blowing Agent Substances 0.000 description 4
- 239000011230 binding agent Substances 0.000 description 4
- 229910001018 Cast iron Inorganic materials 0.000 description 3
- 239000012744 reinforcing agent Substances 0.000 description 3
- LSNNMFCWUKXFEE-UHFFFAOYSA-M Bisulfite Chemical compound OS([O-])=O LSNNMFCWUKXFEE-UHFFFAOYSA-M 0.000 description 2
- 239000000853 adhesive Substances 0.000 description 2
- 230000001070 adhesive effect Effects 0.000 description 2
- 125000000217 alkyl group Chemical group 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 239000007769 metal material Substances 0.000 description 2
- 238000002360 preparation method Methods 0.000 description 2
- 239000002994 raw material Substances 0.000 description 2
- 239000002002 slurry Substances 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 229910001208 Crucible steel Inorganic materials 0.000 description 1
- 238000003723 Smelting Methods 0.000 description 1
- 239000007864 aqueous solution Substances 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000013467 fragmentation Methods 0.000 description 1
- 238000006062 fragmentation reaction Methods 0.000 description 1
- 230000008595 infiltration Effects 0.000 description 1
- 238000001764 infiltration Methods 0.000 description 1
- 239000002905 metal composite material Substances 0.000 description 1
- 150000002736 metal compounds Chemical class 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- XZWYZXLIPXDOLR-UHFFFAOYSA-N metformin Chemical compound CN(C)C(=N)NC(N)=N XZWYZXLIPXDOLR-UHFFFAOYSA-N 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 239000005011 phenolic resin Substances 0.000 description 1
- 238000001556 precipitation Methods 0.000 description 1
- 238000005215 recombination Methods 0.000 description 1
- 230000006798 recombination Effects 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 238000003756 stirring Methods 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
- 238000005406 washing Methods 0.000 description 1
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- Manufacture Of Alloys Or Alloy Compounds (AREA)
Abstract
A metal ceramic surface composite material and a production process thereof belong to a metal matrix composite material and a production process thereof. The invention solves the problem that the surface of a metal matrix is compounded with ceramic by using a common casting method and is formed into a product in one step. The production process of the invention comprises the following steps: crushing the ceramic material into particles, proportionally and sequentially adding and mixing the components, preheating a sand mold, spraying the mixed slurry to the surface of the sand mold for foaming, closing the mold and standing, and melting and casting the metal matrix for molding. The invention simplifies the production process, can obtain a final product by one-step molding, can improve the performances of wear resistance, heat resistance and the like of the metal surface, and saves materials. The invention is used for producing ferrous and nonferrous metal surfaces and composite materials.
Description
The invention belongs to metal-base composites and production technology thereof.Closely-related with it at present technology is to adopt casting die (Songyuan City is great beautiful, " manufacture method of the dispersion-strengthened type composite of particle ", Japan Patent JP59-145742) to produce the aluminum matrix composite that ceramic particle strengthens.The technical process of this method is at first ceramic powders to be made the formed body of porous, puts into the casting mold casting metals equably, makes metal liquid immerse the formed body of porous by the atmospheric pressure of 500-1000 subsequently.Be rolled again after solidifying or push, make porous, shaped fragmentation body be graininess and be dispersed among the metal, thereby obtain the aluminum matrix composite that whole compound ceramic particle strengthens.This method needs pressurization in recombination process, also need rolling or extruding after compound, and raw material need be reprocessed just can become final products, so complex technical process.
The objective of the invention is at above-mentioned the deficiencies in the prior art, a kind of metal ceramic surface composite and production technology thereof are proposed, compound and products thereof being molded in the casting process of setting of metal and pottery once finished, pressurization and following process process have been saved, directly obtaining inside is metallic matrix, the top layer is the product of metal ceramic composite bed, can improve the metal surface wear-resistingly, anti-wash away, heat resistance, saving metal material.
In order to realize the foregoing invention purpose, technical scheme of the present invention is: batch mixing at first, simultaneously with the sand mold preheating, then with the slurry spary that mixes to the sand mold surface blister, mould assembling was left standstill after foaming was handled, and simultaneously with metal molten, used the cast molding of normal pressure conventional cast method then.
The used raw material of the present invention are made up of intermixture, inorganic adhesive, organic adhesive, blowing agent, reinforcing agent, metal matrix material.Wherein adopt water as intermixture, ratio is 10-60%wt, in boric acid, the Boratex any is as inorganic binder, ratio is 1-10%wt, adopt in industrial syrup, phenolic resins, epoxy resin, the methyl fibre resin any as organic binder bond, ratio is 1-10%wt: adopt sodium alkyl sulfonate or alkyl sulfonic acid potassium or urethane fat as blowing agent, ratio is 1-10%wt; Select industrial SiO for use
2, Al
2O
3, MgO, SiC, Si
3N
4, AlN and ZrO
2In any ceramic powders do reinforcing agent, ratio is 30-80%wt.Metal matrix material adopts cast iron or cast steel or Birmasil or cast copper alloy.
In material therefor, above-mentioned every kind of ceramic material all is ground into the powder of granularity 0.01~1mm, and sodium alkyl sulfonate or alkyl sulfonic acid potassium or urethane fat are the aqueous solution of commercially available 20-80%wt; The industry syrup is industry proportion 2-4g/cm
2Liquid.Other various material purity are 90%-99.99%.
Batch mixing is undertaken by the agitator that motor is bought with 500-2000 rev/min speed drive in agitator.Charging sequence is followed successively by intermixture, inorganic binder, organic binder bond, blowing agent and reinforcing agent, every kind of material adds the back stirring and was added into down a kind of material in 5~10 minutes again, is suspended state (the agitator bottom does not have precipitation) until last ceramic powders in mixed liquor.
The sand mold preheating was carried out 6~14 hours at 80 ℃~200 ℃.
Surperficial spary foaming to the casting sand type after the preheating.The spary foaming is by the nozzle on the agitator, is (1~10) kilogram/mm with pressure
2Compressed air, with (1~5) kilogram/minute flow with the slurry spary that the mixes casting sand type surface after the preheating, by the effect of organic burning volatilization and blowing agent, form the thick porous ceramic layer of 2-8mm on the surface, loam core.Hole in the porous ceramic layer should evenly distribute, and mutual UNICOM, and the bore hole size size should be controlled between the 0.5-2mm.
The surface of final products of the present invention is a ceramic-metal composite, and matrix is a metal, and this metal is non-ferrous metal or its alloy, ferrous metal or its alloy.Do not have separating interface between composite bed and the matrix, metal by matrix to surperficial continuous transition.Ceramic particle evenly distributes in the composite bed, and content is 10%~70%wt.
The present invention compares with background technology and has the following advantages:
(1), the surface infiltration combination process that proposes of the present invention makes metal compound in the metal surface with pottery, and is rather than whole compound.At metal surface (as Fig. 2), because the invigoration effect of ceramic particle, wear-resisting, anti-the washing away with performance such as heat-resisting that makes the metal surface improved.Therefore, for the occasion of only requiring the material surface performance, can save metal material greatly.
(2), the present invention adopts normal pressure conventional cast method to realize the compound of metal and pottery, avoided the pressurization in other method to wait other complex techniques process, simplified production process.
(3), metal and compound and moulding product of pottery are once finished, directly obtain to have the final products of the various sizes of metal ceramic composite bed, and no longer carry out following process and directly use by the conventional cast method.And adopt other method, after metal and the Ceramic Composite, often need following process to use.
Fig. 1 is a process chart of the present invention.
Fig. 2 is hypoeutectic grey cast-iron and SiO
2The tissue morphology of composite surface material.
Illustrated below:
Embodiment 1:
Hypoeutectic grey cast-iron-SiO
2The producing of composite surface material (reinforced by weight percentage)
Adopting granularity according to above-mentioned technological process furnish component is 0.5mmSiO
2Ceramic powders 68%, boric acid 2%, industrial syrup 6%, sodium alkyl sulfonate 6%, water 18%, reinforced by aforementioned charging sequence, batch mixing [1], the technological parameter of production process all mixed 5 minutes with 1000 rev/mins after adopting every kind of material to add, sand mold preheating [2] is that sand mold was 150 ℃ of preheatings 10 hours, with mixed slip spary foaming [3], during spary, 5 kilograms/mm of compressed air pressure
2, 3 kilograms/minute of material spray flows are with the casting sand type surface of composite material slip spary after the preheating, formation thickness is 2-5mm, and bore hole size is 0.5-2mm, evenly distributes, and the porous ceramics that is interconnected is laminated, and mould assembling was left standstill [4] 20 minutes, 1250 ℃ of casting [6] temperature behind the cast iron smelting [5].
By obtaining the thick metal ceramic composite bed of 2-5mm in Cast Iron Surface after this technological parameter casting.The contained SiO of this composite bed
2The percentage by weight of ceramic particle is 30-60%, and the microhardness of metal is HV260 in the composite bed, is higher than the microhardness of parent metal, and composite bed is 2 times of matrix at 850 ℃ thermal fatigue property.
Embodiment 2:
At Birmasil ZL101(Al-7%Si) surface preparation Al
2O
3The metal ceramic composite bed that ceramic particle strengthens.
According to the technological process that proposes, its furnish component adopts, and granularity is the Al of 0.5mm
2O
3Pottery powder 60%, boric acid 4%, industrial syrup 9%, sodium alkyl sulfonate 8%, water 19%.After the technological parameter of production process adopts each material to add, all with 1000 rev/mins of mixing speeds.Mixed 5 minutes, sand mold was 150 ℃ of preheatings 12 hours, during spary, 4 kilograms/mm of compressed air pressure, 2.5 kilograms of branches of material spray flow are sprayed onto casting sand type surface after the preheating with the composite material slip, and formation thickness is 2-5mm, bore hole size is that 0.5-2mm evenly distributes, and the porous ceramic layer that is interconnected.Left standstill 720 ℃ of cast temperatures after the mould assembling 20 minutes.
Can obtain thickness in the Al-7%Si aluminum alloy surface by this technological parameter is the composite bed of 4mm, and its wearability is 3 times of parent metal.
Embodiment 3:
At cast copper alloy (ZQSn6-6-3) surface preparation Al
2O
3The metal ceramic composite bed that strengthens.
Remove cast temperature and adopt 1100 ℃, all the other batching compositions are identical with embodiment 2 with technological parameter, can obtain the thick metal ceramic composite bed of 4mm at copper alloy surface after the casting.
Claims (6)
1, a kind of production technology of metal ceramic surface composite, comprise required ceramic material is ground into granular, batch mixing and to the casting sand type preheating in proportion, mould assembling is left standstill and metal molten, cast molding is characterized in that:
(1), every kind of ceramic material is ground into the powder that granularity is 0.01-1mm;
(2), by following component, percentage by weight, order is reinforced successively:
Water 10-60%,
Boric acid or Boratex 1--10%,
Industry syrup or epoxy resin or
Phenolic resins or methyl fibre resin 1--10%,
Sodium alkyl sulfonate or alkyl sulfonic acid
Potassium or urethane fat 1--10%,
SiO
2Or Al
2O
3Or MgO or SiC
Or Si
3N
4Or AlN or ZrO
2Ceramic powders 30--80%,
After above-mentioned every kind of material adds, all with the mixing speed be 500-2000 rev/min, stirred 5-10 minute, add a kind of material down again, in mixed liquor, be suspended state until ceramic powders;
(3), to the surperficial spary foaming of the casting sand type after the preheating, spary foam by the nozzle on the agitator, usefulness (1-10) kilogram/mm
2Compressed air, with (1-5) kilogram/minute flow with the casting sand type surface of mixed slurry spary after the preheating, formations thickness is 2-8mm, bore hole size is 0.5-2mm, evenly distributes, and the porous ceramic layer of mutual UNICOM.
2, implement the described metal ceramic surface composite of claim 1, comprise metal matrix material, it is characterized in that the weight percentage of contained ceramic particle in metal matrix material and the ceramic material composite bed after compound is 10-70%.
3, the production technology of metal ceramic surface composite according to claim 1 is characterized in that hypoeutectic grey cast-iron-SiO
2The production technology of composite surface material is:
(1) SiO
2Ceramic material is ground into the powder that granularity is 0.5mm;
(2) by following component, percentage by weight, order is reinforced successively:
Water 18%,
Boric acid 2%,
Industry syrup 6%,
Sodium alkyl sulfonate 6%,
SiO
2Ceramic powders 68%,
After above-mentioned every kind of material adds, all, stirred 5 minutes, add a kind of material down again, until SiO with 1000 rev/mins mixing speed
2Ceramic particle is suspended state in mixed liquor;
(3), with 5 kilograms/mm
2Compressed air, with 3 kilograms/minute material spray flow, with the casting sand type surface of composite material slip spary after the preheating, formation thickness is 2-5mm, bore hole size is 0.5-2mm, evenly distributes, and the porous ceramic layer that is interconnected.
4, implement the described metal ceramic surface composite of claim 3 and comprise matrix material hypoeutectic grey cast-iron, it is characterized in that hypoeutectic grey cast-iron and SiO
2The contained SiO of composite bed after ceramic material is compound
2The percetage by weight of ceramic particle is 30-60%.
5, the production technology of metal ceramic surface composite according to claim 1 is characterized in that Birmasil ZL101(AL-7%Si) or cast copper alloy (ZQSn6-6-3) is equal and Al
2O
3The production technology of ceramic surface composite is:
(1), Al
2O
3It is the 0.5mm powder that ceramic material is ground into granularity;
(2), by following component, percentage by weight, order is reinforced successively:
Water 19%,
Boric acid 4%,
Industry syrup 9%,
Sodium alkyl sulfonate 8%,
Al
2O
3Ceramic powders 60%,
After above-mentioned every kind of material adds, all, stirred 5 minutes, add a kind of material down again, until Al with 1000 rev/mins mixing speed
2O
3Ceramic powders is suspended state in mixed liquor;
(3) with 4 kilograms/mm
2Compressed air, with the casting sand type surface of composite material slip spary after the preheating, formation thickness is 2-5mm with 2.5 kilograms of/minute material spray flows, bore hole size is 0.5-2mm, evenly distributes, and the porous ceramic layer that is interconnected.
6, implement the described metal ceramic surface composite of claim 5, comprise matrix material Birmasil ZL101(Al-7%Si) or cast copper alloy (ZQSn6-6-3), it is characterized in that Birmasil ZL101(Al-7%Si) or cast copper alloy (ZQSn6-6-3) is equal and Al
2O
3The contained Al of composite bed after ceramic material is compound
2O
3The percetage by weight of ceramic material is 30-60%.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 93111991 CN1036180C (en) | 1993-10-12 | 1993-10-12 | Cast metal ceramic surface composite material and production process thereof |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 93111991 CN1036180C (en) | 1993-10-12 | 1993-10-12 | Cast metal ceramic surface composite material and production process thereof |
Publications (2)
Publication Number | Publication Date |
---|---|
CN1092004A true CN1092004A (en) | 1994-09-14 |
CN1036180C CN1036180C (en) | 1997-10-22 |
Family
ID=4989737
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN 93111991 Expired - Fee Related CN1036180C (en) | 1993-10-12 | 1993-10-12 | Cast metal ceramic surface composite material and production process thereof |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN1036180C (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1313229C (en) * | 2005-02-01 | 2007-05-02 | 济南大学 | Method and apapratus for preparing network ceramic skeleton reinforced metal-base composite material |
CN101698230B (en) * | 2009-10-24 | 2011-12-14 | 内蒙古科技大学 | Method for preparing surface composite sinterer grate bars |
CN102700192A (en) * | 2012-06-21 | 2012-10-03 | 北京理工大学 | Metal and ceramic composite material and preparation method of metal and ceramic composite material |
CN102787253A (en) * | 2012-07-26 | 2012-11-21 | 西安理工大学 | Preparation method for SiC and graphite hybrid reinforced copper-based surface composite material |
CN103357853A (en) * | 2013-08-06 | 2013-10-23 | 宁国市华丰耐磨材料有限公司 | Strengthened abrasion proof steel ball made of nano materials |
CN107824765A (en) * | 2017-10-19 | 2018-03-23 | 驻马店恒久机械制造有限公司 | A kind of impeller flange form steel pricker closes brake drum and preparation method thereof |
-
1993
- 1993-10-12 CN CN 93111991 patent/CN1036180C/en not_active Expired - Fee Related
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1313229C (en) * | 2005-02-01 | 2007-05-02 | 济南大学 | Method and apapratus for preparing network ceramic skeleton reinforced metal-base composite material |
CN101698230B (en) * | 2009-10-24 | 2011-12-14 | 内蒙古科技大学 | Method for preparing surface composite sinterer grate bars |
CN102700192A (en) * | 2012-06-21 | 2012-10-03 | 北京理工大学 | Metal and ceramic composite material and preparation method of metal and ceramic composite material |
CN102700192B (en) * | 2012-06-21 | 2014-12-17 | 北京理工大学 | Preparation method of metal and ceramic composite material |
CN102787253A (en) * | 2012-07-26 | 2012-11-21 | 西安理工大学 | Preparation method for SiC and graphite hybrid reinforced copper-based surface composite material |
CN102787253B (en) * | 2012-07-26 | 2014-07-02 | 西安理工大学 | Preparation method for SiC and graphite hybrid reinforced copper-based surface composite material |
CN103357853A (en) * | 2013-08-06 | 2013-10-23 | 宁国市华丰耐磨材料有限公司 | Strengthened abrasion proof steel ball made of nano materials |
CN107824765A (en) * | 2017-10-19 | 2018-03-23 | 驻马店恒久机械制造有限公司 | A kind of impeller flange form steel pricker closes brake drum and preparation method thereof |
Also Published As
Publication number | Publication date |
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CN1036180C (en) | 1997-10-22 |
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