CN101016591A - Method of preparing SiCp/Al composite material with complicated shape and high volume percent ratio - Google Patents

Method of preparing SiCp/Al composite material with complicated shape and high volume percent ratio Download PDF

Info

Publication number
CN101016591A
CN101016591A CN 200710064281 CN200710064281A CN101016591A CN 101016591 A CN101016591 A CN 101016591A CN 200710064281 CN200710064281 CN 200710064281 CN 200710064281 A CN200710064281 A CN 200710064281A CN 101016591 A CN101016591 A CN 101016591A
Authority
CN
China
Prior art keywords
sic
matrix material
skeleton
monomer
getting
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.)
Granted
Application number
CN 200710064281
Other languages
Chinese (zh)
Other versions
CN100449012C (en
Inventor
何新波
曲选辉
马强
任淑彬
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.)
University of Science and Technology Beijing USTB
Original Assignee
University of Science and Technology Beijing USTB
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 University of Science and Technology Beijing USTB filed Critical University of Science and Technology Beijing USTB
Priority to CNB2007100642817A priority Critical patent/CN100449012C/en
Publication of CN101016591A publication Critical patent/CN101016591A/en
Application granted granted Critical
Publication of CN100449012C publication Critical patent/CN100449012C/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Ceramic Products (AREA)

Abstract

The invention discloses a preparing method of SiCp/Al composite with complete shape and high analytic in metal base composite material researching domain, which comprises the following steps: allocating pre-mixing liquid with monomer, cross linker and disperser; adding into SiC powder; balling; getting stable suspension with SiC volume content at 50-70%; adding into trigger and activator; stirring evenly; injecting into unapertured mold; solidifying and shaping in incubator with temperature at 50-70 deg.c; getting green compact; drying; discharging glue; presintering; getting SiC bone; placing Al alloy of 4-8% Mg, 6-12% Si on the adaptive position of bone; putting into heater; heating-up at 900-1200 deg.c under the protection of inert gas; inflating high pure nitrogen; keeping the temperature at 1-6 h; cooling; getting the product. This invention possesses the merit of cheap cost.

Description

The high volume fraction ratio SiC of a kind of complicated shape pThe preparation method of/Al matrix material
Technical field
The invention belongs to field of research of metal, provide a kind of complicated shape high volume fraction ratio SiC especially pThe preparation method of/Al matrix material.
Background technology
High-volume fractional (50~70%) SiC p/ Al matrix material combines the premium properties of metallic aluminium and SiC, have excellent physics and mechanical property, as higher modulus of elasticity, high specific tenacity, characteristics such as good heat-conducting, in Electronic Packaging, fields such as aerospace are with a wide range of applications, no matter still be that the practical application direction always is one of problem of field of research of metal hottest point theoretically, emerged a large amount of preparation methods, as casting, jet deposition, powder metallurgic method etc., but because that these methods generally have a cost is too high, the not enough homogeneous of material structure, shortcomings such as poor performance, and only be applicable to the situation of low volume fraction.In addition, because SiC pThe extremely difficult mechanical workout of carrying out of/Al matrix material has also limited its further development to a great extent.Therefore, the advanced near-net-shape technology of preparing of development remains one of main direction of its research.
At present, can prepare high-volume fractional SiC pThe method of/Al matrix material has only method of impregnation.Whether rely on the effect of external force according to infiltration process, method of impregnation is divided into pressure infiltration and two research directions of pressure-free impregnation substantially.The pressure method of impregnation need apply extra pressure or vacuum condition in infiltration process, therefore to the requirement harshness of equipment, complicated operation, cost are very high.Advantages such as and pressure-free impregnation need not complex apparatus, and it is simple to have technology, with low cost have the better development prospect.The liquid metal Infiltration Technics is divided into two steps of skeleton preparation-infiltration, and the preparation of skeleton is the precondition of all technologies.At present, the preparation method of SiC skeleton mainly contains powder compression, injection molding etc.The SiC preform of pressing preparation exists density unevenness even, is subjected to mould to limit the simple shape that can only be shaped.And injection molding technology can only be applied to make small-sized component.Advantages such as the gel casting forming technology is a kind of new ceramic material colloidal shaping method, has plastic complicated shape large-scale component, and the molding blank quality is good, precision is high, equipment is simple, cost of investment is low all have the potential using value in a lot of fields.The gel injection volume content and the high volume fraction ratio SiC of solid particulate in the slurry pThe volume fraction of SiC is more identical in the/Al matrix material.Based on above reason, the present invention at first utilizes the gel casting forming technology to prepare porous SiC skeleton, combines with pressure-free impregnation technology cheaply then, has successfully prepared the high volume fraction ratio SiC of complicated shape p/ Al matrix material has solved the technical barrier of its low-cost preparation effectively.
Summary of the invention
The object of the present invention is to provide the high volume fraction ratio SiC of a kind of complicated shape pThe preparation method of/Al matrix material has solved high volume fraction ratio complicated shape SiC pThe low-cost near-net-shape technology of preparing difficult problem of/Al matrix material.
The present invention utilizes gel casting forming and pressure-free impregnation two step process to prepare complicated shape high-volume fractional silicon-carbide particle reinforced aluminium-base (SiC p/ Al) matrix material.The specific implementation method is:
(1) slurry preparation: at first preparation contains the aqueous solution (premixed liquid) of monomer, linking agent, and wherein monomeric massfraction is 10~20%, and the mass ratio of monomer and linking agent is (30: 1)~(120: 1); (for guaranteeing high dimension precision, solid content is 50~70%, and this volume content is final SiC to pre-determined volume content to add SiC powder and dispersion agent in above-mentioned premixed liquid pThe volume fraction of SiC in the/Al matrix material), obtain original slurry.Adopt means such as vibration, ball milling to make SiC homodisperse in slurry then, obtain the stable suspension of high solid loading.
(2) curing molding: add the initiator and the catalyzer of cumulative volume 0.5~1.O% and 0.05~0.1% in above-mentioned suspensoid, be injected into after stirring in the no punch die, the insulation can that moves into 50~70 ℃ is realized curing molding, obtains the SiC green compact, drying.
(3) skeleton is prepared: the above-mentioned dried of heating below 600 ℃, and the whole organic phases of burn off, and continue to be warming up to 800~1100 ℃, and be incubated 1~4 hour, skeleton is carried out presintering, but possessed the porous SiC prefabrication type skeleton of manipulation strength.
(4) pressure-free impregnation: will contain massfraction and be 4~8% Mg and the Al alloy of 6~12%Si and place SiC skeleton correct position to put into holding furnace together; be warming up to 900~1200 ℃ under the inert atmosphere protection; conversion atmosphere is incubated and naturally cools to room temperature after 1~6 hour to high pure nitrogen, obtains SiC p/ Al matrix material.
Solvent in the premixed liquid of the present invention is not limited only to water, can be other organic medium such as ethanol etc., and monomer needs to have bigger solubleness in selected solvent.As water base acrylamide system, water-based acrylic hydroxyl ethyl ester system, ethanol based acrylamide system etc.
The particle diameter of SiC raw material powder of the present invention can be chosen in relative broad range, different proportionings has determined that the volume fraction of SiC can be controlled between 50~70% in the matrix material, can guarantee that like this green compact have very little shrinkage in drying process, formed precision is higher.
Major advantage of the present invention is:
1, the moulding process of SiC skeleton is simple, and its shape and size are unrestricted, and moulding process is very low to the requirement of mold material.
2, can prepare the complicated shape high volume fraction SiC p/ Al matrix material, with low cost, functional.
The SiC that 3, can directly prepare nearly end form p/ Al matrix material need not machining, the dimensional precision height.
Description of drawings
Fig. 1 is a process flow sheet of the present invention.
Embodiment
Embodiment 1: the preparation volume fraction is 50% SiC p/ Al composite material parts
With the deionized water is solvent, and acrylamide (AM) is a monomer, and methylene-bisacrylamide (MBAM) is for linking agent preparation monomer mass mark is 10%, MBAM and AM mass ratio are 1: 30 premixed liquid.The powder that with particle diameter is 2.5 μ m and 28 μ m is that 1: 4 ratio joins in the above-mentioned premixed solution with mass ratio, tetramethyl-oxyammonia 10% (TMAH) aqueous solution that adds powder quality mark 1.5% simultaneously makes SiC account for 50% of total volume fraction as dispersion agent.With the aluminum oxide is ball-milling medium, is mixed in the ball milling bucket 2 hours, obtains homogeneous dispersive SiC slurry.In above-mentioned slurry, add cumulative volume O.8% Ammonium Persulfate 98.5 5% aqueous solution (ASP) and 0.08% Tetramethyl Ethylene Diamine (TEMED) as catalyzer, back injection nonporous plastic mould stirs, the thermostat container of putting into 70 ℃ is incubated 40 minutes, continues insulation 6 hours after the demoulding under the atmosphere of high humidity.Improve temperature and accelerate rate of drying, till no longer changing to quality.Put into process furnace and be warming up to 400 ℃, be incubated 1 hour, continue to be warming up to 600, insulation post-heating to 1000 half an hour insulation carrying out in 2 hours presintering processing places SiC skeleton top with the aluminium alloy that accounts for SiC skeleton cumulative volume 50% required quality, feeds argon gas and is warming up to 1000 ℃, conversion atmosphere is to high pure nitrogen, be incubated 1 hour, furnace cooling obtains 50% SiC p/ Al matrix material.
Embodiment 2: the preparation volume fraction is 60% SiC p/ Al composite material parts
With water is solvent, acrylamide (AM) is a monomer, methylene-bisacrylamide (MBAM) is 15% for linking agent preparation monomer mass mark, MBAM and AM mass ratio are 1: 70 premixed liquid, the powder that with particle diameter is 7 μ m and 63 μ m is that 1: 2 ratio joins in the above-mentioned premixed solution with mass ratio, tetramethyl-oxyammonia 10% (TMAH) aqueous solution that adds powder quality mark 2.0% simultaneously is as dispersion agent, ball milling 4 hours, stir and obtain homogeneous dispersive SiC slurry, stir and in above-mentioned suspensoid, add Ammonium Persulfate 98.5 5% aqueous solution (ASP) of slurry volume mark 0.6% and 0.06% ‰ Tetramethyl Ethylene Diamine (TEMED) as catalyzer, back injection nonporous plastic mould stirs, the thermostat container of putting into 60 ℃ of high humidity is incubated 40 minutes, the follow-up continuation of insurance temperature of the demoulding 5 hours.Accelerate rate of drying, till no longer changing to quality.Put into process furnace and be warming up to 400 ℃, be incubated 2 hours, continue to be warming up to 600 ℃, insulation post-heating to 900 ℃ presintering half an hour 2 hours places SiC skeleton correct position with the aluminium that accounts for SiC skeleton cumulative volume 40% required aluminium alloy quality, feeds high pure nitrogen, be warming up to 1100 ℃, be incubated 3 hours, furnace cooling obtains 60% SiC p/ Al matrix material.
Embodiment 3: the preparation volume fraction is 70% SiC p/ Al composite material parts
With the deionized water is solvent, acrylamide (AM) is a monomer, methylene-bisacrylamide (MBAM) is 20% for linking agent preparation monomer mass mark, MBAM and AM mass ratio are 1: 120 premixed liquid, with particle diameter is 0.8 μ m, the powder of 7 μ m and 63 μ m is that 1: 2: 4 ratio joins in the above-mentioned premixed solution with mass ratio, make the volume of SiC account for 70% of cumulative volume, tetramethyl-oxyammonia 10% (TMAH) aqueous solution that adds powder quality mark 2.8% simultaneously is as dispersion agent, ball milling 6 hours, stir and obtain homogeneous dispersive SiC suspensoid, in above-mentioned suspensoid, add Ammonium Persulfate 98.5 5% aqueous solution (ASP) of slurry volume mark 0.4% and 0.04% Tetramethyl Ethylene Diamine (TEMED) as catalyzer, the no punch die of back injection stirs, the thermostat container of putting into 50 ℃ is incubated 40 minutes, the follow-up continuation of insurance temperature of the demoulding 5 hours, improve temperature and accelerate rate of drying, till no longer changing to quality.Put into process furnace and be warming up to 400 ℃, be incubated 1 hour, continue to be warming up to 600 ℃, insulation post-heating half an hour is to pre-sintering temperature insulation 2 hours, naturally cooling.Calculating accounts for the quality of above-mentioned SiC skeleton cumulative volume 30% required aluminium alloy, is placed on SiC skeleton top and puts into the controlled process furnace of atmosphere together, feeds high pure nitrogen, is warming up to 1200 ℃, is incubated 4 hours, and furnace cooling obtains 70% SiC p/ Al matrix material.

Claims (3)

1, the high volume fraction ratio SiC of a kind of complicated shape pThe preparation method of/Al matrix material, gel injection-pressure-free impregnation prepared SiC p/ Al matrix material is characterized in that, processing step is:
(1) slurry preparation: preparation contains the premixed liquid of monomer, linking agent and dispersion agent, and wherein monomeric massfraction is 10~20%, and the mass ratio of monomer and linking agent is (30: 1)~(120: 1); In premixed liquid, add the SiC powder and make it account for 50~70% of premixed liquid volume content, obtain original slurry; Adopt vibration, ball milling means to make SiC homodisperse in slurry then, obtain the stable suspension of high solid loading;
(2) curing molding: the initiator and the catalyzer that in above-mentioned suspensoid, add cumulative volume 0.5~1.0% and 0.05~0.1% respectively, be injected into after stirring in the no punch die, the insulation can that moves into 50~70 ℃ is realized curing molding, obtains the SiC green compact, and it is carried out drying;
(3) skeleton is prepared: the whole organic phases of burn off below 600 ℃, and continue to be warming up to 800~1100 ℃, and be incubated 1~4 hour, skeleton is carried out presintering, but possessed the porous SiC prefabrication type skeleton of manipulation strength;
(4) pressure-free impregnation: will contain massfraction and be 4~8% Mg and the Al alloy of 6~12%Si and place SiC skeleton correct position to put into process furnace together; be warming up to 900~1200 ℃ under the inert atmosphere protection; conversion atmosphere is incubated and naturally cools to room temperature after 1~6 hour to high pure nitrogen, obtains SiC p/ Al matrix material.
2, according to claims 1 described method, it is characterized in that: the solvent in the described premixed liquid is water or ethanol, and monomer is acrylamide system, Hydroxyethyl acrylate system or ethanol based acrylamide system.
3, according to claims 1 described method, it is characterized in that: the volume fraction of SiC is controlled between 50~70% in the matrix material.
CNB2007100642817A 2007-03-08 2007-03-08 Method of preparing SiCp/Al composite material with complicated shape and high volume percent ratio Expired - Fee Related CN100449012C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CNB2007100642817A CN100449012C (en) 2007-03-08 2007-03-08 Method of preparing SiCp/Al composite material with complicated shape and high volume percent ratio

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CNB2007100642817A CN100449012C (en) 2007-03-08 2007-03-08 Method of preparing SiCp/Al composite material with complicated shape and high volume percent ratio

Publications (2)

Publication Number Publication Date
CN101016591A true CN101016591A (en) 2007-08-15
CN100449012C CN100449012C (en) 2009-01-07

Family

ID=38725816

Family Applications (1)

Application Number Title Priority Date Filing Date
CNB2007100642817A Expired - Fee Related CN100449012C (en) 2007-03-08 2007-03-08 Method of preparing SiCp/Al composite material with complicated shape and high volume percent ratio

Country Status (1)

Country Link
CN (1) CN100449012C (en)

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101244936B (en) * 2008-03-24 2010-06-02 北京科技大学 Injection mold SiC ceramic preliminary shaping blank method for reinforcing metallic infiltration
CN101898240A (en) * 2010-08-09 2010-12-01 西安科技大学 Preparation method of SiC/Al composite material for electronic packaging
CN101941231A (en) * 2010-09-09 2011-01-12 中国科学院长春光学精密机械与物理研究所 Gel injection molding technology of large-sized and complicated-shape silicon carbide ceramic biscuit
CN102229693A (en) * 2010-09-29 2011-11-02 蒙特集团(香港)有限公司 Method for making abrasion-resistant copolymerized resin by using waste silicon carbide micro powder produced after solar silicon chip wire cutting
CN102229499A (en) * 2010-09-29 2011-11-02 蒙特集团(香港)有限公司 Method for preparing composite anti-static and wear resistant ceramic by using depleted carborundum/silicon powder generated through solar silicon wafer linear cutting
CN101604635B (en) * 2009-07-03 2011-11-23 重庆大学 Method for preparing SiCp/A1 electronic packing part by using vibrating acceleration sedimentation technology
CN101736215B (en) * 2008-11-25 2012-03-28 北京有色金属研究总院 Preparation method of Mg/SiCp composite material
CN102806335A (en) * 2011-05-31 2012-12-05 比亚迪股份有限公司 Silicon carbide particle reinforced aluminum matrix composite and preparation method thereof
CN104496480A (en) * 2014-12-08 2015-04-08 中国建筑材料科学研究总院 Silicon carbide ceramic preform, aluminum-based silicon carbide ceramic material, and preparation method of silicon carbide ceramic preform
CN104841944A (en) * 2014-12-01 2015-08-19 沈阳理工大学 Gel method preparation process for SiC/Al composite powder
CN109055798A (en) * 2018-08-03 2018-12-21 北京汽车股份有限公司 Preparation method, brake disc and the vehicle of brake disc for vehicle
CN111850339A (en) * 2020-06-24 2020-10-30 南昌航空大学 Composite material with high thermal conductivity and incomplete cladding of interface phase, and preparation method and test method thereof
CN111995425A (en) * 2020-08-05 2020-11-27 湖南航天诚远精密机械有限公司 Gel casting material composition of aluminum silicon carbide composite material, prefabricated part and preparation method of structural part
CN112570690A (en) * 2020-10-19 2021-03-30 广州城建职业学院 Preparation method of three-dimensional reticular silicon carbide ceramic reinforced aluminum matrix composite
CN112981281A (en) * 2021-02-07 2021-06-18 哈尔滨工业大学 Method for improving interlaminar shear strength of Cf/Al composite material complex component

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1991016801A1 (en) * 1990-04-20 1991-10-31 Martin Marietta Energy Systems, Inc. A method of nitriding refractory metal articles
CN1187292C (en) * 2003-05-30 2005-02-02 武汉理工大学 Process for preparing porous ceramic by water-based gel injection moulding method
CN1297363C (en) * 2005-01-05 2007-01-31 北京科技大学 Method for producing high-volume fractional silicon-carbide particle reinforced aluminium-base composite material member
CN1325431C (en) * 2005-10-18 2007-07-11 中国海洋大学 Gel molding-injection base from high-strength ceramic composite materials and shaping method thereof

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101244936B (en) * 2008-03-24 2010-06-02 北京科技大学 Injection mold SiC ceramic preliminary shaping blank method for reinforcing metallic infiltration
CN101736215B (en) * 2008-11-25 2012-03-28 北京有色金属研究总院 Preparation method of Mg/SiCp composite material
CN101604635B (en) * 2009-07-03 2011-11-23 重庆大学 Method for preparing SiCp/A1 electronic packing part by using vibrating acceleration sedimentation technology
CN101898240A (en) * 2010-08-09 2010-12-01 西安科技大学 Preparation method of SiC/Al composite material for electronic packaging
CN101941231A (en) * 2010-09-09 2011-01-12 中国科学院长春光学精密机械与物理研究所 Gel injection molding technology of large-sized and complicated-shape silicon carbide ceramic biscuit
CN102229693A (en) * 2010-09-29 2011-11-02 蒙特集团(香港)有限公司 Method for making abrasion-resistant copolymerized resin by using waste silicon carbide micro powder produced after solar silicon chip wire cutting
CN102229499A (en) * 2010-09-29 2011-11-02 蒙特集团(香港)有限公司 Method for preparing composite anti-static and wear resistant ceramic by using depleted carborundum/silicon powder generated through solar silicon wafer linear cutting
CN102229693B (en) * 2010-09-29 2012-12-26 蒙特集团(香港)有限公司 Method for making abrasion-resistant copolymerized resin by using waste silicon carbide micro powder produced after solar silicon chip wire cutting
CN102229499B (en) * 2010-09-29 2014-04-30 蒙特集团(香港)有限公司 Method for preparing composite anti-static and wear resistant ceramic by using depleted carborundum/silicon powder generated through solar silicon wafer linear cutting
CN102806335A (en) * 2011-05-31 2012-12-05 比亚迪股份有限公司 Silicon carbide particle reinforced aluminum matrix composite and preparation method thereof
CN102806335B (en) * 2011-05-31 2015-07-22 比亚迪股份有限公司 Silicon carbide particle reinforced aluminum matrix composite and preparation method thereof
CN104841944A (en) * 2014-12-01 2015-08-19 沈阳理工大学 Gel method preparation process for SiC/Al composite powder
CN104496480A (en) * 2014-12-08 2015-04-08 中国建筑材料科学研究总院 Silicon carbide ceramic preform, aluminum-based silicon carbide ceramic material, and preparation method of silicon carbide ceramic preform
CN109055798A (en) * 2018-08-03 2018-12-21 北京汽车股份有限公司 Preparation method, brake disc and the vehicle of brake disc for vehicle
CN109055798B (en) * 2018-08-03 2020-08-21 北京汽车股份有限公司 Preparation method of brake disc for vehicle, brake disc and vehicle
CN111850339A (en) * 2020-06-24 2020-10-30 南昌航空大学 Composite material with high thermal conductivity and incomplete cladding of interface phase, and preparation method and test method thereof
CN111995425A (en) * 2020-08-05 2020-11-27 湖南航天诚远精密机械有限公司 Gel casting material composition of aluminum silicon carbide composite material, prefabricated part and preparation method of structural part
CN112570690A (en) * 2020-10-19 2021-03-30 广州城建职业学院 Preparation method of three-dimensional reticular silicon carbide ceramic reinforced aluminum matrix composite
CN112981281A (en) * 2021-02-07 2021-06-18 哈尔滨工业大学 Method for improving interlaminar shear strength of Cf/Al composite material complex component
CN112981281B (en) * 2021-02-07 2021-11-09 哈尔滨工业大学 Method for improving interlaminar shear strength of Cf/Al composite material complex component

Also Published As

Publication number Publication date
CN100449012C (en) 2009-01-07

Similar Documents

Publication Publication Date Title
CN100449012C (en) Method of preparing SiCp/Al composite material with complicated shape and high volume percent ratio
CN104907567B (en) A kind of method for preparing high-density complicated shape cemented carbide parts and cutter
CN101397210B (en) Gel-casting moulding technique for preparing silicon nitride ceramics heating element
CN100554456C (en) A kind of method for preparing high volume-fraction carborundum granule-reinforced copper-based composite material
CN1325431C (en) Gel molding-injection base from high-strength ceramic composite materials and shaping method thereof
CN104496480B (en) Silicon carbide ceramics precast body, aluminum-base silicon carbide ceramic material and preparation method thereof
CN101440440B (en) Aluminum based composite material and method and apparatus for forming aluminum based composite material part
CN102500748A (en) Method for preparing aluminum silicon carbide composite material
CN101747054A (en) Gel-casting method of silicon nitride ceramic material containing silicon metal powders
CN106435241B (en) A kind of porous Si3N4/ SiC complex phase ceramics strengthen the preparation method of metal-base composites
CN101260488A (en) Silicon nitride ceramic particles enhancement aluminum-base composite material and preparing method thereof
CN104446487A (en) Slurry and method for gelcasting pressureless sintered silicon carbide ceramics
CN1686642A (en) Method of preparing high size precision profiled molybdenum parts
CN107500772A (en) A kind of silicon carbide ceramics precast body, aluminum-base silicon carbide ceramic material and preparation method thereof
CN105543526A (en) Method for preparing high-compactness titanium or titanium alloy by using gel casting formation
CN102554228B (en) Method for forming ultrathin-wall porous metal pipe fitting
CN103586468B (en) TiAl alloy powder near-net-shaping method
CN111995425A (en) Gel casting material composition of aluminum silicon carbide composite material, prefabricated part and preparation method of structural part
CN1187289C (en) Method for preparing gelatin mold made from functional gradient material in static magnetic field
CN1944482B (en) Gel polymer for gel injection molding and its preparing method
CN100519009C (en) Process for preparing orienting-reinforced aluminum -based composite material
CN1491761A (en) Method for preparing Kovar alloy electronic package box
CN101972852A (en) Method for preparing complex molybdenum part
CN109108288B (en) Method for preparing hollow sphere metal matrix light composite material by powder injection molding
CN111020264A (en) Three-dimensional accumulation body reinforced titanium-based composite material and preparation method 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
C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20090107

Termination date: 20120308