CN100485067C - Method for preparing high-strength plasticity aluminum-base composite material by employing TiB2 particles - Google Patents

Method for preparing high-strength plasticity aluminum-base composite material by employing TiB2 particles Download PDF

Info

Publication number
CN100485067C
CN100485067C CNB2007100725909A CN200710072590A CN100485067C CN 100485067 C CN100485067 C CN 100485067C CN B2007100725909 A CNB2007100725909 A CN B2007100725909A CN 200710072590 A CN200710072590 A CN 200710072590A CN 100485067 C CN100485067 C CN 100485067C
Authority
CN
China
Prior art keywords
aluminum
particle
particulate
pressure
composite material
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CNB2007100725909A
Other languages
Chinese (zh)
Other versions
CN101104899A (en
Inventor
姜龙涛
武高辉
修子扬
苟华松
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Harbin Institute of Technology
Original Assignee
Harbin Institute of Technology
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Harbin Institute of Technology filed Critical Harbin Institute of Technology
Priority to CNB2007100725909A priority Critical patent/CN100485067C/en
Publication of CN101104899A publication Critical patent/CN101104899A/en
Application granted granted Critical
Publication of CN100485067C publication Critical patent/CN100485067C/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Powder Metallurgy (AREA)

Abstract

The invention provides a high-plasticity aluminum-based composite material containing TiB2 particles and a preparation method thereof, and relates to an aluminum-based composite material and a preparation method thereof. The invention solves the problems of the prior art, such as poor plasticity and toughness and difficulty in secondary processing. The composite material contains (by volume) titanium diboride reinforcement particles 10-25 percent, aluminum particles 25-35 percent, and aluminum alloy matrix in balance. The preparation method comprises: (1) weighing titanium diboride reinforcement particles, aluminum particles and aluminum alloy matrix; (2) mixing by mechanical dry method to obtain a reinforcement powder; (3) placing the reinforcement powder in a die and compression-molding; (4) heating the die; (5) melting aluminum alloy and casting in the die; (6) applying a pressure on the die with molten aluminum and maintaining the pressure for a period of time and cooling; (7) demoulding and taking the cast ingot, that is reinforced aluminum-based composite material. The inventive aluminum-based composite material has high plasticity and good wear resistance and is adapted to secondary processing and machining.

Description

Adopt TiB 2The preparation method of particulate high-strength plasticity aluminum-base composite material
Technical field
The present invention relates to the preparation method of reinforced aluminum matrix composites, especially relate to the preparation method of high-strength plasticity particle aluminum matrix composite.
Background technology
Particle enhanced metal-base composites has not only possessed some good characteristics of fiber and whisker enhanced metal-base composites, and have concurrently strengthen body low price, preparation technology easy relatively, be easy to secondary processing, performance and have isotropy and advantage such as wear-resisting, therefore use very extensive.Require in the not extra high environment at specific tenacity, specific modulus, as fields such as Aeronautics and Astronautics structural part, automobile, motorcycle component, textile manufacturing machines, particulate reinforced composite has demonstrated the incomparable superiority of traditional metal materials.Therefore, it will be expected to substitute traditional material in these field parts.Though the research to aluminum matrix composite is very extensive; but mass-producing is at present used and still is difficult to realize; mainly be because compare with traditional material; particulate reinforced composite still exists some problems to be badly in need of solving, and wherein plasticity and toughness are low is to limit the major cause that it is used as the structural part mass-producing.Therefore improve particle enhanced aluminum-based composite material plasticity in recent years and toughness has become one of research focus of this direction.A large amount of studies show that, the adding that fragility strengthens body makes the plasticity of alloy and toughness that in various degree decline all be arranged, especially the plasticity of material with do not strengthen matrix alloy accordingly and compare, low one more than the order of magnitude, this phenomenon makes that not only its security as structural part is difficult to guarantee, more be difficult to realize secondary processing, make some baroque forming parts difficulties.Studies show that, the plasticity of metal-base composites is relevant with following factor: the character, the particulate size-grade distribution that strengthen body, the interface bonding state between particle shape and the matrix alloy and the plasticity of matrix alloy, ag(e)ing behavio(u)r etc., particulate character wherein, and the consistency between the matrix, interfacial state become the principal element that influences matrix material plasticity.Research also shows TiB 2Ceramic particle not only has and is only second to adamantine hardness and modulus, and have and aluminium between good wetting property, and be difficult for and aluminium between surface reaction takes place, be that a kind of ideal aluminium alloy strengthens body.In recent years, the research of TiB2 particle enhanced aluminum-based composite material is increasing, mostly concentrate in the research to the preparation method, be mainly concerned with the preparation method and be: self propagating high temperature synthesizes preparation methods such as (SHS), mechanical alloying (MA), reaction sintering (XDTM), mixing salt reaction method (LSM), melt contact reaction method, pressure-free impregnation method, stirring casting method.TiB among present these materials and the preparation method 2The chemical reaction products of the selection of particle form, content, matrix alloy, particle and matrix etc. maybe can not be effectively controlled.TiB is disclosed among Americana US 6290748 B1 2Two kinds of preparation methods of particle enhanced aluminum-based composite material belong to combining of above-mentioned stirring casting and mixing salt reaction method.First method is earlier with TiB 2Ceramic phase is dispersed in the liquid aluminium (alloy), then with TiB 2Ceramic phase mixes with sodium aluminum fluoride that adds or other fluorochemical powder, then with mixture and aluminium (alloy) 700~1000 ℃ of fusions, be frozen into matrix material.Second method is to generate the TiB of different size by molten aluminum or alloying element (Mg/Ca) with a certain amount of fluorochemical (few than amount in the original position method of formation) reduction reaction in inert atmosphere 2Crystal, TiB 2Distribution of sizes determined by the fluorochemical that adds and the composition and the preparation temperature of aluminium alloy.The advantage of these two kinds of methods is that the optional kind of matrix is many, can generate high-volume fractional and surpass 50% TiB 2/ Al matrix material (volume fraction 0~60%, particulate size can from the micron to the nanometer); Shortcoming is atmosphere (humidity, oxygen level etc.) strict, and is higher to equipment and environment requirement, especially inevitably has the residual of reactant in the matrix material, the composition complexity, thus influence material property, especially the influence to plasticity is bigger.
Summary of the invention
The present invention is in order to solve the existing low problem of particle enhanced aluminum-based composite material toughness: make the plasticity of alloy and toughness that in various degree reduction all be arranged because fragility strengthens the adding of body, especially the plasticity of material with do not strengthen matrix alloy accordingly and compare, reduced by one more than the order of magnitude, this phenomenon makes that not only its security as structural part is difficult to guarantee, more be difficult to realize secondary processing, make some baroque forming parts difficulties; On the other hand, existing TiB 2/ Al composite material preparation process is strict to atmosphere (humidity, oxygen level etc.), and is higher to equipment and environment requirement, thereby inevitably has the residual of reactant in matrix material, the composition complexity, thus influence material property, especially toughness is low.The invention provides a kind of employing TiB 2The preparation method of particulate high-strength plasticity aluminum-base composite material, the concrete technical scheme that addresses the above problem is as follows:
Aluminum matrix composite of the present invention strengthens body particle, aluminum particulate and aluminum matrix alloy by TiB2 to be formed, the body of per-cent TiB2 enhancing by volume particle is 10~25%, aluminum particulate be 25~35% and surplus be that aluminum matrix alloy is made.
TiB 2The particle diameter that strengthens body is 0.5~5 μ m, and the particle diameter of aluminum particulate is 5~10 μ m.
Aluminum matrix alloy is Al-Cu-Mg, Al-Mg-Si or Al-Zn-Mg.
The present invention adopts TiB 2The step of the method for granules preparation high-strength plasticity reinforced aluminum matrix composites is as follows:
Step 1, by volume per-cent is got TiB2 and is strengthened that the body particle is 10~25%, aluminum particulate is 25~35%;
It is 0.5~5 μ m that TiB2 strengthens the body particle grain size, and the aluminum particulate particle diameter is 5~10 μ m;
Step 2, adopt the mechanical type dry mixed body powder that is enhanced standby the material powder of step 1;
Step 3, place mould inner pressure to make prefabricated section in the enhancing body powder of step 2;
The mold heated to 450 ℃ that strengthens the body prefabricated powder block~600 ℃ is equipped with step 4, step 3;
Step 5, the aluminum matrix alloy of surplus is heated to 750 ℃~850 ℃, aluminum melt is cast in the mould of step 4;
Step 6, the mould that step 5 is cast with aluminum melt apply the pressure of 5~30Mpa on pressing machine, base aluminum liquation body is infiltrated up to strengthen in the hole between the body powder particle, treats that aluminum melt infiltrates fully to keep-up pressure 10~20 minutes and cooling after strengthening in the hole between the body powder particle;
After step 7, the cooling, ingot casting is taken out in the demoulding, promptly prepares employing TiB of the present invention 2Granules preparation high-strength high-plasticity aluminum matrix composite.
The present invention utilizes the TiB of pressure method of impregnation preparation 2Particle enhanced aluminum-based composite material not only can effectively be controlled the generation (mainly can avoid the residual problems of reactant such as in-situ reaction or mixed salt method) of impurity in the matrix material, and utilizes matrix material that the present invention prepares because TiB 2Particle has good interface to combine with aluminium alloy, and matrix material has the advantage of high strength, high-ductility; Compare with the reinforced aluminum matrix composites of the existing method preparation that utilizes in-situ authigenic, this kind reinforced aluminum matrix composites not only has specific rigidity height, characteristic that specific tenacity is high, and plasticity can be significantly improved, and (table 1 has provided several employing TiB 2The performance of particle high strength, high-ductility reinforced aluminum matrix composites).The present invention adopts TiB 2Particulate aluminum matrix composite composition is simple, clean, and the plasticity height, wear resistance is good and be easy to the secondary processing moulding, meets requirement of massive production.The preparation method of matrix material of the present invention adopts the pressure impregnation technology, and technology is simple, and cost is low, density height, material property height and steady quality.
Description of drawings
Fig. 1 is TiB under the stereoscan photograph of matrix material of the present invention 2Uniform particles is distributed in the synoptic diagram in the alloy matrix aluminum, and Fig. 2 is the extruding synoptic diagram.1 is pressure head among Fig. 2, the 2nd, and casting chamber, the 3rd, bottom die cavity, the 4th, mould, the 5th, electric furnace.
Embodiment
Embodiment one: present embodiment strengthens body particle, aluminum particulate and aluminum matrix alloy by TiB2 to be formed, and the body of per-cent TiB2 enhancing by volume particle accounts for 10~25%, and median size is 0.5~5 μ m; Aluminum particulate accounts for 25~35%, and median size is 5~10 μ m; All the other are aluminum matrix alloy, and aluminum matrix alloy is Al-Cu-Mg, Al-Mg-Si or Al-Zn-Mg.
Embodiment two: by volume per-cent gets that TiB2 strengthens that the body particle is 10% to present embodiment, aluminum particulate is 35%, all the other make for aluminum matrix alloy.
Embodiment three: by volume per-cent gets that TiB2 strengthens that the body particle is 25% to present embodiment, aluminum particulate is 25%, all the other make for aluminum matrix alloy.
Embodiment four: by volume per-cent gets that TiB2 strengthens that the body particle is 17.5% to present embodiment, aluminum particulate is 30%, all the other make for aluminum matrix alloy.
Embodiment five: the step of present embodiment method is as follows:
Step 1, by volume per-cent is got TiB2 and is strengthened that the body particle is 10~25%, aluminum particulate is 25~35%;
It is 0.5~5 μ m that TiB2 strengthens the body particle grain size, and the aluminum particulate particle diameter is 5~10 μ m;
Step 2, adopt the mechanical type dry mixed body powder that is enhanced standby the material powder of step 1;
Step 3, place mould inner pressure to make prefabricated section in the enhancing body powder of step 2;
The mold heated to 450 ℃ that strengthens the body prefabricated powder block~600 ℃ is equipped with step 4, step 3;
Step 5, the aluminum matrix alloy of surplus is heated to 750 ℃~850 ℃, aluminum melt is cast in the mould of step 4;
Step 6, the mould that step 5 is cast with aluminum melt apply the pressure of 5~30Mpa on pressing machine, base aluminum liquation body is infiltrated up to strengthen in the hole between the body powder particle, treats that the aluminum melt body infiltrates fully to keep-up pressure 10~20 minutes and cooling after strengthening in the hole between the body powder particle;
After step 7, the cooling, ingot casting is taken out in the demoulding, promptly prepares and adopts TiB 2Granules preparation high-strength high-plasticity reinforced aluminum matrix composites.
Embodiment six: the difference of present embodiment and embodiment five is step 1, and by volume per-cent gets that TiB2 strengthens that the body particle is 10%, aluminum particulate is 35%, all the other are aluminum matrix alloy; It is 1 μ m that TiB2 strengthens the body particle grain size, and the aluminum particulate particle diameter is 5 μ m; Step 4 is with mold heated to 525 ℃; Step 5 is heated to 850 ℃ with aluminum matrix alloy; Apply the pressure of 10Mpa on the step 6 pressing machine, keep-uped pressure 20 minutes.Other step is identical with embodiment five.
Embodiment seven: the difference of present embodiment and embodiment five is step 1, and by volume mark per-cent gets that TiB2 strengthens that the body particle is 17.5%, aluminum particulate is 30%, all the other are aluminum matrix alloy; It is 3 μ m that TiB2 strengthens the body particle grain size, and the aluminum particulate particle diameter is 7 μ m; Step 4 is with mold heated to 450 ℃; Step 5 is heated to 800 ℃ with aluminum matrix alloy; Apply the pressure of 20Mpa on the step 6 pressing machine, keep-uped pressure 15 minutes.Other step is identical with embodiment five.
Embodiment eight: the difference of present embodiment and embodiment five is step 1, and by volume mark per-cent gets that TiB2 strengthens that the body particle is 25%, aluminum particulate is 25%, all the other are aluminum matrix alloy; It is 5 μ m that TiB2 strengthens the body particle grain size, and the aluminum particulate particle diameter is 9 μ m; Step 4 is with mold heated to 600 ℃; Step 5 is heated to 750 ℃ with aluminum matrix alloy; Apply the pressure of 30Mpa on the step 6 pressing machine, keep-uped pressure 10 minutes.Other step is identical with embodiment five.
Table one, employing TiB 2The performance index of granules preparation high strength, high-ductility reinforced aluminum matrix composites (T6 processing)
Title material Elastic modulus G Pa Yield strength MPa Tensile strength MPa Unit elongation (%)
(15Vol%TiB 2+30Vol%Al) P/6061Al 107.1 298.8 364.1 11.2
(20Vol%TiB 2+25Vol%Al) P/6061A1 120.3 384.9 472.6 9.8
(25Vol%TiB 2+20Vol%Al) P/6061A1 135.7 410.3 520 7.1

Claims (3)

1, adopts TiB 2The preparation method of particulate high-strength plasticity aluminum-base composite material is characterized in that the step of this method is as follows:
Step 1, by volume per-cent is got TiB2 and is strengthened that the body particle is 10~25%, aluminum particulate is 25~35%;
Step 2, adopt the mechanical type dry mixed body powder that is enhanced standby the material powder of step 1;
Step 3, place mould inner pressure to make prefabricated section in the enhancing body powder of step 2;
The mold heated to 450 ℃ that strengthens the body prefabricated powder block~600 ℃ is equipped with step 4, step 3;
Step 5, the aluminum matrix alloy of surplus is heated to 750 ℃~850 ℃, aluminum melt is cast in the mould of step 4;
Step 6, the mould that step 5 is cast with aluminum melt apply the pressure of 5~30MPa on pressing machine, base aluminum liquation body is infiltrated up to strengthen in the hole between the body powder particle, treats that the aluminum melt body infiltrates fully to keep-up pressure 10~20 minutes time after strengthening in the hole between the body powder particle;
After step 7, the cooling, ingot casting is taken out in the demoulding, promptly prepares and adopts TiB 2Granules preparation high-strength plasticity reinforced aluminum matrix composites.
2, employing TiB according to claim 1 2The preparation method of particulate high-strength plasticity aluminum-base composite material is characterized in that step 1 by volume per-cent gets that TiB2 strengthens that the body particle is 10%, aluminum particulate is 35%, all the other are aluminum matrix alloy; It is 3 μ m that TiB2 strengthens the body particle grain size, and the aluminum particulate particle diameter is 7 μ m; Step 4 is with mold heated to 525 ℃; Step 5 is heated to 850 ℃ with aluminum matrix alloy; Apply the pressure of 10MPa on the step 6 pressing machine, keep-up pressure 20 minutes time.
3, employing TiB according to claim 1 2The preparation method of particulate high-strength high-plasticity aluminum matrix composite is characterized in that step 1 by volume mark per-cent gets that TiB2 strengthens that the body particle is 17.5%, aluminum particulate is 30%, all the other are aluminum matrix alloy; It is 5 μ m that TiB2 strengthens the body particle grain size, and the aluminum particulate particle diameter is 9 μ m; Step 4 is with mold heated to 450 ℃; Step 5 is heated to 800 ℃ with aluminum matrix alloy; Apply the pressure of 20MPa on the step 6 pressing machine, keep-up pressure 15 minutes time.
CNB2007100725909A 2007-07-31 2007-07-31 Method for preparing high-strength plasticity aluminum-base composite material by employing TiB2 particles Active CN100485067C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CNB2007100725909A CN100485067C (en) 2007-07-31 2007-07-31 Method for preparing high-strength plasticity aluminum-base composite material by employing TiB2 particles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CNB2007100725909A CN100485067C (en) 2007-07-31 2007-07-31 Method for preparing high-strength plasticity aluminum-base composite material by employing TiB2 particles

Publications (2)

Publication Number Publication Date
CN101104899A CN101104899A (en) 2008-01-16
CN100485067C true CN100485067C (en) 2009-05-06

Family

ID=38998977

Family Applications (1)

Application Number Title Priority Date Filing Date
CNB2007100725909A Active CN100485067C (en) 2007-07-31 2007-07-31 Method for preparing high-strength plasticity aluminum-base composite material by employing TiB2 particles

Country Status (1)

Country Link
CN (1) CN100485067C (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109834273A (en) * 2017-11-28 2019-06-04 北京有色金属研究总院 A kind of preparation method of particle enhanced aluminum-based composite material thin plate

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102021557B (en) * 2010-12-03 2012-06-13 湖北工业大学 Preparation method of Al2O3 and TiB2 compound coating synthesized by aluminium alloy surface stirring rubbing processing and heating reaction
CN103111601B (en) * 2012-10-15 2015-02-25 柳州市双铠工业技术有限公司 Manufacturing process method for composite wear-resistant lining board
CN103710560B (en) * 2013-12-23 2016-01-20 江苏大学 A kind of method of continuous production aluminum-based in-situ composite materials
CN103882350B (en) * 2014-04-10 2016-03-02 哈尔滨工业大学 A kind of high volume fraction grain strengthens the method for metal-base composites large plastometric set
CN105349817A (en) * 2015-10-29 2016-02-24 无锡桥阳机械制造有限公司 Technology for preparing composite material
CN105734347B (en) * 2016-02-23 2018-03-30 中南大学 A kind of method that discharge plasma sintering prepares boride titanium particle reinforced aluminum matrix composites
CN106853530B (en) * 2017-01-13 2019-04-16 哈尔滨工业大学 A kind of method of powdering-hot pressed sintering preparation stratiform titanium composite material
CN107523712B (en) * 2017-07-27 2021-10-15 深圳市翠绿贵金属材料科技有限公司 Preparation process of silver copper oxide composite material
CN108034866B (en) * 2018-01-22 2019-08-23 哈尔滨工业大学 A kind of high-performance aluminium silicon nitride based composites and preparation method thereof
CN109261935B (en) * 2018-10-19 2020-10-27 华南理工大学 High-entropy alloy reinforced aluminum-based composite material and extrusion casting method thereof
CN109811173B (en) * 2019-01-29 2020-01-07 清华大学深圳研究生院 TiB2Preparation method of-Al composite material and TiB2-Al composite material
CN110938759A (en) * 2019-11-26 2020-03-31 纽维科精密制造江苏有限公司 Production process of in-situ self-generated aluminum-based composite material for aluminum profile
CN111730042A (en) * 2020-07-01 2020-10-02 吕新起 Preparation method of ceramic particle reinforced steel-based composite material based on SHS technology
CN112410642A (en) * 2020-11-20 2021-02-26 重庆理工大学 Titanium-aluminum-based composite material and preparation method thereof
CN113322401B (en) * 2021-05-28 2022-03-11 中南大学 (TiB)2Al-Cu/Al-Cu aluminum-based composite material and preparation method thereof
CN113718184A (en) * 2021-07-23 2021-11-30 西安交通大学 TiB2Preparation method of particle-synergistically-modified carbon fiber reinforced aluminum-based composite material
CN113909456B (en) * 2021-09-14 2023-04-25 昆明理工大学 Preparation method of rare earth doped particle reinforced steel-based composite material
CN115555570B (en) * 2022-09-30 2023-11-21 中国航发北京航空材料研究院 Method for controlling uniformity of distribution structure of particle reinforced titanium-based composite material reinforcement

Non-Patent Citations (4)

* Cited by examiner, † Cited by third party
Title
CR法生成TiB2/Al复合材料制备工艺研究. 张树瑜,柴跃生.山西机械,第115期. 2002
CR法生成TiB2/Al复合材料制备工艺研究. 张树瑜,柴跃生.山西机械,第115期. 2002 *
颗粒增强铝基复合材料的组织与性能. 凌兴珠,徐振民.中国有色金属学报,第8卷第2期. 1998
颗粒增强铝基复合材料的组织与性能. 凌兴珠,徐振民.中国有色金属学报,第8卷第2期. 1998 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109834273A (en) * 2017-11-28 2019-06-04 北京有色金属研究总院 A kind of preparation method of particle enhanced aluminum-based composite material thin plate

Also Published As

Publication number Publication date
CN101104899A (en) 2008-01-16

Similar Documents

Publication Publication Date Title
CN100485067C (en) Method for preparing high-strength plasticity aluminum-base composite material by employing TiB2 particles
CN104235237B (en) Brake disc made of carborundum foamed ceramics/aluminum alloy composite materials and production method of road vehicle brake disc
CN107022691B (en) A method of graphene reinforced aluminum matrix composites are prepared by raw material of multi-layer graphene microplate
CN102337423B (en) Preparation method of ceramic-powder-enhanced zinc-aluminum alloy based composite material
CN108359825B (en) A kind of preparation method of ceramics-graphene enhancing Cu-base composites
CN101775563B (en) Carbon fiber reinforced aluminum matrix piston material and preparation method thereof
CN109321767B (en) Method for preparing hybrid particle reinforced aluminum matrix composite material by composite reinforcement method
CN1318167C (en) Near clean shaping preparation method of granular reinforced metal base composite material based on region selection laser sintering
CN101423904B (en) Method for manufacturing high volume fraction particulate reinforced metal-matrix composite pipes
CN107058787A (en) A kind of method that graphene reinforced aluminum matrix composites are prepared by raw material of graphite microchip
CN106086726A (en) SiC nanowire reinforced aluminum matrix composites and preparation method thereof
CN110423915B (en) Preparation method of aluminum-based composite material
CN1045049A (en) A kind of method that between material product and foundry goods, obtains metallurgical, bond
CN110438379B (en) Preparation method of lithium-containing magnesium/aluminum-based composite material
CN104099488B (en) The method that titanium aluminum carbon granule strengthens Zn Al Alloy Matrix Composites is prepared in a kind of pressureless sintering-pressurization densification
CN100453666C (en) Pressure-free impregnation preparation method for Al2O3 particle reinforced aluminum base composite material
CN104120310A (en) Aluminum-based composite material and preparation method thereof
CN109852834A (en) A kind of preparation method of nano-ceramic particle enhancing Metal Substrate classification configuration composite material
CN103540783A (en) Titanium aluminum carbon particle-enhanced zinc-aluminum composite material and pressureless sintering preparation method thereof
CN110205536A (en) A kind of titanium/titanium carbide core-shell structure reinforced aluminum matrix composites and preparation method thereof
US20210062315A1 (en) Preparation method of a lithium-containing magnesium/aluminum matrix composite
CN1498705A (en) Casting infiltration method of heating power for preparing composite alloy material with metal base
CN102676956B (en) Method for preparing iron-based surface composite material by virtue of in-situ synthesis
CN1042502A (en) The method that contains the matrix material of controlled content of reinforcer agent with metal matrix production
CN102899517B (en) In-situ SiC-TiC particle mixing enhanced aluminum-based composite material and preparation process thereof

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant