CN106216672A - A kind of Metal toughened ceramic matric composite part increases material preparation method - Google Patents

A kind of Metal toughened ceramic matric composite part increases material preparation method Download PDF

Info

Publication number
CN106216672A
CN106216672A CN201610533508.7A CN201610533508A CN106216672A CN 106216672 A CN106216672 A CN 106216672A CN 201610533508 A CN201610533508 A CN 201610533508A CN 106216672 A CN106216672 A CN 106216672A
Authority
CN
China
Prior art keywords
ceramic
drip molding
preparation
liquid
powder
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
CN201610533508.7A
Other languages
Chinese (zh)
Other versions
CN106216672B (en
Inventor
顾德阳
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.)
Sichuan Tian Yuan Additive Manufacturing Materials Co Ltd
Original Assignee
Sichuan Tian Yuan Additive Manufacturing Materials Co Ltd
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 Sichuan Tian Yuan Additive Manufacturing Materials Co Ltd filed Critical Sichuan Tian Yuan Additive Manufacturing Materials Co Ltd
Priority to CN201610533508.7A priority Critical patent/CN106216672B/en
Publication of CN106216672A publication Critical patent/CN106216672A/en
Application granted granted Critical
Publication of CN106216672B publication Critical patent/CN106216672B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/20Direct sintering or melting
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B33ADDITIVE MANUFACTURING TECHNOLOGY
    • B33YADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
    • B33Y10/00Processes of additive manufacturing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/30Process control
    • B22F10/36Process control of energy beam parameters
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/60Treatment of workpieces or articles after build-up
    • B22F10/66Treatment of workpieces or articles after build-up by mechanical means
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F12/00Apparatus or devices specially adapted for additive manufacturing; Auxiliary means for additive manufacturing; Combinations of additive manufacturing apparatus or devices with other processing apparatus or devices
    • B22F12/40Radiation means
    • B22F12/41Radiation means characterised by the type, e.g. laser or electron beam
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P10/00Technologies related to metal processing
    • Y02P10/25Process efficiency

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Materials Engineering (AREA)
  • Powder Metallurgy (AREA)
  • Laser Beam Processing (AREA)

Abstract

The present invention relates to a kind of Metal toughened ceramic matric composite part and increase material preparation method.Its step includes: Bi Sn granule strengthens ceramic matric composite design, the determination of ceramic base material and the preparation of granule, the preparation of Bi Sn alloying pellet and preservation, drip molding digital-to-analogue slicing delamination processes, the laser gain material manufacture of drip molding, the Non-Destructive Testing of drip molding, and the post processing final drip molding of acquisition.It has, and formation of parts internal stress is minimum, combination property strong, and integrated cost is low, drip molding is lightweight, smooth surface, it is possible to meets use and requires, improves the advantages such as its service life.

Description

A kind of Metal toughened ceramic matric composite part increases material preparation method
Technical field
The present invention relates to composite and increase material manufacture shaping technical field, particularly relate to a kind of Metal toughened ceramic base and be combined Material parts increases material preparation method.
Background technology
Ceramic material the most all has the highest hardness, is very suitable for being manufactured into machine components.But, they have again A great defect, i.e. they suffer from the highest fragility, and this makes them seldom be manufactured into machine components.If it is sharp As the second phase, material is obtained with addition metal toughness reinforcing, then problem can achieve a solution.Coaxial powder-feeding laser melting coating (LCD) it is a kind of increasing material manufacturing technology that can manufacture bigger machine components.When carrying out laser coaxial powder feeding cladding, laser beam, Powder conveying, protective gas supply synchronization are carried out, and can be effectively improved quality and the powder using efficiency of cladding layer.But, for Ceramic material, owing to its fragility is higher, and relevant research is still few, can overcome drawbacks described above it is therefore proposed that a kind of Preparation method has important Research Significance.
Summary of the invention
The deficiency existed for the preparation method in prior art, metal combined with ceramic material, the purpose of the present invention It is: providing a kind of Metal toughened ceramic matric composite part to increase material preparation method, the method has formation of parts internal stress Minimum, combination property is strong, and integrated cost is low, drip molding is lightweight, smooth surface, it is possible to meets to use and requires, improves it and use The advantages such as life-span.
In order to achieve the above object, the present invention adopts the following technical scheme that realization:
A kind of Metal toughened ceramic matric composite part increases material preparation method, it is characterised in that this preparation method includes Following steps:
1) first carry out the design of material of Bi-Sn pacticle toughening ceramic base composite, determine ceramic main material, wherein pottery Main material includes in SiO2, Al2O3, Si3N4, TiC, TiN, TiC+TiN, h-NB, WC, Anhydrite, quartz any one or a combination thereof;
2) determine the kind of ceramic base material and the preparation of granule, according to the performance requirement of drip molding, determine and which kind of uses Ceramic material is as major ingredient, and wherein the particle diameter of ceramic particle is 30-300 μm, is positioned over by its granule and is arranged on increasing material manufacture machine In the powder feeder of bed, and carrying out drying isothermal holding, temperature during insulation is 800-1000 DEG C, gives over to standby;
3) using granule prepared by atomization Bi-Sn alloy, the particle diameter of this alloying pellet is 30-300 μm, is heated molten Changing to liquid, fusion temperature is 139-232 DEG C, is positioned over by the Bi-Sn alloying pellet of liquid and is arranged on what increasing material produced lathes Being incubated in liquid alloy shower nozzle near laser instrument shower nozzle, give over to standby, temperature during insulation is 80-100 DEG C;
4) utilize CAD 3D graphics software that the STL threedimensional model of metalwork is carried out slicing delamination process on computers, Increasing manufacture process parameter to input to computer, thickness is 0.3-3mm;Computer control system controls the shower nozzle of 3D printer Moving on axle at X, Y, Z tri-, movement locus is consistent with each slicing delamination figure;
5) computer control system controls 3D printer powder feeder powder feeding, starts laser instrument and inert gas shielding gas supplies Device of air, is layered the step section in this step and forms, it is thus achieved that drip molding, and material conveying includes that industrial computer controls pottery The powder sending quantity of material powder and the liquor charging amount of liquid Bi-Sn alloy, both couplings, to reach the component requirements of design of material, open Dynamic laser instrument carries out selective melting or the cladding of ceramic material, during use inert gas shielding, successively process, will Liquid Bi-Sn alloy is ejected into the near focal point of laser instrument so that it is mix with melted ceramic material;Wherein, the tool of laser instrument Body parameter is: power P=400-10000W, spot diameter D=2-8mm, scan velocity V=2-3m/min, and overlapping rate is 30- 40%, the pressurized jet speed of liquid alloy is 50-200m/s, and the liquid-drop diameter scope of injection is 10-30 μm, liquid alloy with The mass percent of ceramic powders is 10-30%;
6) to above-mentioned steps 5) in drip molding carry out Non-Destructive Testing, wherein the method for this Non-Destructive Testing includes: scanning road Under footpath, physical behavior when moulding material fusing and solidification is observed;Temperature field and the three dimensional analysis of residual stress field in scanning process With display;Ceramic powders fusing and Simulation of Solidification Process, and the mechanical performance of prediction drip molding;Form part mechanical performance Comprehensive detection, contrasts with simulation result simultaneously;
7) above-mentioned steps 6 is completed) after, stamped metal part is carried out post processing and obtains final stamped metal part, post processing bag Include blasting treatment and/or polishing, make the precision of drip molding and surface roughness reach to design requirement.
As the further optimization of such scheme, above-mentioned steps 5) described in the automatic powder feeding system of ceramic powders use coaxial the most just To automatic powder feeding system or use non-coaxial lateral automatic powder feeding system to carry out powder feeding.
As the further optimization of such scheme, above-mentioned steps 5) in laser instrument be carbon dioxide laser or optical fiber Laser instrument;Noble gas uses nitrogen or argon.
As the further optimization of such scheme, above-mentioned steps 1) described in the toughness reinforcing metal material of employing also include Co, Al, Mn, Zn or Cr.
Above-mentioned steps 1) in, the drip molding of simple ceramic material manufacture is difficult to the most greatly practicality because of fragility, proposes to use gold Belong to material granule toughness reinforcing, its plasticity and tensile strength can also be increased simultaneously, toughness reinforcing for example with Bi-Sn alloying pellet, below Narration is all as a example by it.Can serve as toughness reinforcing metal material and also include Co, Al, Mn, Zn, Cr or their alloy etc..Gold Belong to (alloy) and the most on the one hand play the effect of binding agent, on the other hand can increase the toughness etc. that material is overall, thus obtain Obtain excellent comprehensive mechanical performance.They ratios shared in the composite are that design of material needs to consider, usual quality Percentage ratio is about 10-30%.It addition, use Bi-Sn alloy, (eutectic composition is Sn42Bi58, select the composition near eutectic point) Another reason be that it has the cold characteristic risen of pyrocondensation, be combined with each other with the ceramic material expanded with heat and contract with cold, can significantly subtract Internal stress in few composite;
Accompanying drawing explanation
Accompanying drawing 1 is the schematic flow sheet that a kind of Metal toughened ceramic matric composite part increases material preparation method.
Detailed description of the invention
1 pair of one Metal toughened ceramic matric composite part of the present invention increases material preparation method work specifically below in conjunction with the accompanying drawings Explanation.
A kind of Metal toughened ceramic matric composite part increases material preparation method, it is characterised in that this preparation method includes Following steps:
1) first carry out the design of material of Bi-Sn pacticle toughening ceramic base composite, determine ceramic main material, wherein pottery Main material includes in SiO2, Al2O3, Si3N4, TiC, TiN, TiC+TiN, h-NB, WC, Anhydrite, quartz any one or a combination thereof;
2) determine the kind of ceramic base material and the preparation of granule, according to the performance requirement of drip molding, determine and which kind of uses Ceramic material is as major ingredient, and wherein the particle diameter of ceramic particle is 30-300 μm, is positioned over by its granule and is arranged on increasing material manufacture machine In the powder feeder of bed, and carrying out drying isothermal holding, temperature during insulation is 800-1000 DEG C, gives over to standby;
3) using granule prepared by atomization Bi-Sn alloy, the particle diameter of this alloying pellet is 30-300 μm, is heated molten Changing to liquid, fusion temperature is 139-232 DEG C, is positioned over by the Bi-Sn alloying pellet of liquid and is arranged on what increasing material produced lathes Being incubated in liquid alloy shower nozzle near laser instrument shower nozzle, give over to standby, temperature during insulation is 80-100 DEG C;
4) utilize CAD 3D graphics software that the STL threedimensional model of metalwork is carried out slicing delamination process on computers, Increasing manufacture process parameter to input to computer, thickness is 0.3-3mm;Computer control system controls the shower nozzle of 3D printer Moving on axle at X, Y, Z tri-, movement locus is consistent with each slicing delamination figure;
5) computer control system controls 3D printer powder feeder powder feeding, starts laser instrument and inert gas shielding gas supplies Device of air, is layered the step section in this step and forms, it is thus achieved that drip molding, and material conveying includes that industrial computer controls pottery The powder sending quantity of material powder and the liquor charging amount of liquid Bi-Sn alloy, both couplings, to reach the component requirements of design of material, open Dynamic laser instrument carries out selective melting or the cladding of ceramic material, during use inert gas shielding, successively process, will Liquid Bi-Sn alloy is ejected into the near focal point of laser instrument so that it is mix with melted ceramic material;Wherein, the tool of laser instrument Body parameter is: power P=400-10000W, spot diameter D=2-8mm, scan velocity V=2-3m/min, and overlapping rate is 30- 40%, the pressurized jet speed of liquid alloy is 50-200m/s, and the liquid-drop diameter scope of injection is 10-30 μm, liquid alloy with The mass percent of ceramic powders is 10-30%;
6) to above-mentioned steps 5) in drip molding carry out Non-Destructive Testing, wherein the method for this Non-Destructive Testing includes: scanning road Under footpath, physical behavior when moulding material fusing and solidification is observed;Temperature field and the three dimensional analysis of residual stress field in scanning process With display;Ceramic powders fusing and Simulation of Solidification Process, and the mechanical performance of prediction drip molding;Form part mechanical performance Comprehensive detection, contrasts with simulation result simultaneously;
7) above-mentioned steps 6 is completed) after, stamped metal part is carried out post processing and obtains final stamped metal part, post processing bag Include blasting treatment and/or polishing, make the precision of drip molding and surface roughness reach to design requirement.
Above-mentioned steps 5) described in the automatic powder feeding system of ceramic powders use coaxial forward automatic powder feeding system or use non-coaxial Lateral automatic powder feeding system carries out powder feeding.Above-mentioned steps 5) in laser instrument be carbon dioxide laser or optical fiber laser;Inertia Gas uses nitrogen or argon.Above-mentioned steps 1) described in the toughness reinforcing metal material of employing also include Co, Al, Mn, Zn or Cr。
The above-mentioned description to embodiment is to be understood that for ease of those skilled in the art and apply this Bright.These embodiments obviously easily can be made various amendment by person skilled in the art, and described herein General Principle is applied in other embodiments without through performing creative labour.Therefore, the invention is not restricted to enforcement here Example, those skilled in the art are according to the announcement of the present invention, and the improvement made without departing from scope and amendment all should be Within protection scope of the present invention.

Claims (4)

1. a Metal toughened ceramic matric composite part increases material preparation method, it is characterised in that this preparation method include as Lower step:
1) first carry out the design of material of Bi-Sn pacticle toughening ceramic base composite, determine ceramic main material, the most ceramic main material Including any one or a combination thereof in SiO2, Al2O3, Si3N4, TiC, TiN, TiC+TiN, h-NB, WC, Anhydrite, quartz;
2) determine the kind of ceramic base material and the preparation of granule, according to the performance requirement of drip molding, determine which kind of pottery of employing Material is as major ingredient, and wherein the particle diameter of ceramic particle is 30-300 μm, is positioned over by its granule and is arranged on what increasing material produced lathes In powder feeder, and carrying out drying isothermal holding, temperature during insulation is 800-1000 DEG C, gives over to standby;
3) using granule prepared by atomization Bi-Sn alloy, the particle diameter of this alloying pellet is 30-300 μm, is heated and is melted to Liquid, fusion temperature is 139-232 DEG C, is positioned over by the Bi-Sn alloying pellet of liquid and is arranged on the laser that increasing material produces lathes Being incubated in liquid alloy shower nozzle near device shower nozzle, give over to standby, temperature during insulation is 80-100 DEG C;
4) utilize CAD 3D graphics software that the STL threedimensional model of metalwork carries out slicing delamination process on computers, increase material Fabrication process parameters inputs to computer, and thickness is 0.3-3mm;Computer control system control 3D printer shower nozzle X, Y, Z tri-moves on axle, and movement locus is consistent with each slicing delamination figure;
5) computer control system controls 3D printer powder feeder powder feeding, starts laser instrument and inert gas shielding gas supply dress Putting, be layered the step section in this step and form, it is thus achieved that drip molding, material conveying includes that industrial computer controls ceramic material The powder sending quantity of powder and the liquor charging amount of liquid Bi-Sn alloy, both couplings, to reach the component requirements of design of material, start and swash Light device carries out selective melting or the cladding of ceramic material, during use inert gas shielding, successively process, by liquid Bi-Sn alloy is ejected into the near focal point of laser instrument so that it is mix with melted ceramic material;Wherein, the concrete ginseng of laser instrument Number is: power P=400-10000W, spot diameter D=2-8mm, scan velocity V=2-3m/min, and overlapping rate is 30-40%, The pressurized jet speed of liquid alloy is 50-200m/s, and the liquid-drop diameter scope of injection is 10-30 μm, liquid alloy and pottery The mass percent of powder is 10-30%;
6) to above-mentioned steps 5) in drip molding carry out Non-Destructive Testing, wherein the method for this Non-Destructive Testing includes: under scanning pattern Physical behavior when moulding material fusing and solidification is observed;In scanning process, the three dimensional analysis of temperature field and residual stress field is with aobvious Show;Ceramic powders fusing and Simulation of Solidification Process, and the mechanical performance of prediction drip molding;Form part mechanical performance comprehensive Detection, contrasts with simulation result simultaneously;
7) above-mentioned steps 6 is completed) after, stamped metal part being carried out post processing and obtains final stamped metal part, post processing includes spray Sand processes and/or polishing, makes the precision of drip molding and surface roughness reach to design requirement.
A kind of Metal toughened ceramic matric composite part the most according to claim 1 increases material preparation method, and its feature exists In above-mentioned steps 5) described in the automatic powder feeding system of ceramic powders use coaxial forward automatic powder feeding system or use non-coaxial laterally to give Powder mode carries out powder feeding.
A kind of Metal toughened ceramic matric composite part the most according to claim 1 increases material preparation method, and its feature exists In above-mentioned steps 5) in laser instrument be carbon dioxide laser or optical fiber laser;Noble gas uses nitrogen or argon Gas.
A kind of Metal toughened ceramic matric composite part the most according to claim 1 increases material preparation method, and its feature exists In above-mentioned steps 1) described in employing toughness reinforcing metal material also include Co, Al, Mn, Zn or Cr.
CN201610533508.7A 2016-07-07 2016-07-07 A kind of Metal toughened ceramic matric composite part increases material preparation method Active CN106216672B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610533508.7A CN106216672B (en) 2016-07-07 2016-07-07 A kind of Metal toughened ceramic matric composite part increases material preparation method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610533508.7A CN106216672B (en) 2016-07-07 2016-07-07 A kind of Metal toughened ceramic matric composite part increases material preparation method

Publications (2)

Publication Number Publication Date
CN106216672A true CN106216672A (en) 2016-12-14
CN106216672B CN106216672B (en) 2017-12-26

Family

ID=57519312

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610533508.7A Active CN106216672B (en) 2016-07-07 2016-07-07 A kind of Metal toughened ceramic matric composite part increases material preparation method

Country Status (1)

Country Link
CN (1) CN106216672B (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106777822A (en) * 2017-01-22 2017-05-31 河海大学 Two-dimentional high-content particle strengthens composite three-phase meso-mechanical model and method for building up
CN107689278A (en) * 2017-08-25 2018-02-13 华南理工大学 A kind of La Fe Si base magnetic refrigeration composite materials and preparation method thereof
CN108858660A (en) * 2018-06-19 2018-11-23 南京理工大学 Continuous fiber toughening ceramic based composites increasing material manufacturing device and its manufacturing method

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1693016A (en) * 2005-03-14 2005-11-09 深圳大学 Quick mfg. method for powder metallurgy formation
JP2007217727A (en) * 2006-02-14 2007-08-30 National Institute For Materials Science Functional composite material having ceramics-containing closed cell metal, and manufacturing method
CN102179517A (en) * 2011-04-15 2011-09-14 华中科技大学 Laser-induction hybrid melting direct forming method and device
CN103113112A (en) * 2013-02-04 2013-05-22 西安交通大学 Preparation method of metal toughened ceramic-based composite material turbine blade
CN105478777A (en) * 2015-12-14 2016-04-13 中国航空工业集团公司北京航空制造工程研究所 Metal/ceramic gradient material and preparation method thereof
CN105566860A (en) * 2015-12-11 2016-05-11 上海联泰科技股份有限公司 Ceramic material for 3D (three-dimensional) light curing forming printing and preparation method thereof

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1693016A (en) * 2005-03-14 2005-11-09 深圳大学 Quick mfg. method for powder metallurgy formation
JP2007217727A (en) * 2006-02-14 2007-08-30 National Institute For Materials Science Functional composite material having ceramics-containing closed cell metal, and manufacturing method
CN102179517A (en) * 2011-04-15 2011-09-14 华中科技大学 Laser-induction hybrid melting direct forming method and device
CN103113112A (en) * 2013-02-04 2013-05-22 西安交通大学 Preparation method of metal toughened ceramic-based composite material turbine blade
CN105566860A (en) * 2015-12-11 2016-05-11 上海联泰科技股份有限公司 Ceramic material for 3D (three-dimensional) light curing forming printing and preparation method thereof
CN105478777A (en) * 2015-12-14 2016-04-13 中国航空工业集团公司北京航空制造工程研究所 Metal/ceramic gradient material and preparation method thereof

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106777822A (en) * 2017-01-22 2017-05-31 河海大学 Two-dimentional high-content particle strengthens composite three-phase meso-mechanical model and method for building up
CN106777822B (en) * 2017-01-22 2019-02-12 河海大学 Two-dimentional high-content particle enhancing composite material three-phase meso-mechanical model and method for building up
CN107689278A (en) * 2017-08-25 2018-02-13 华南理工大学 A kind of La Fe Si base magnetic refrigeration composite materials and preparation method thereof
CN108858660A (en) * 2018-06-19 2018-11-23 南京理工大学 Continuous fiber toughening ceramic based composites increasing material manufacturing device and its manufacturing method

Also Published As

Publication number Publication date
CN106216672B (en) 2017-12-26

Similar Documents

Publication Publication Date Title
CN106001571B (en) Metal part selective laser alloying additive manufacturing method
US11833615B2 (en) Method for preparing multiple-material variable-rigidity component by efficient collaborative additive manufacturing
CN106735967B (en) A kind of method of ultrasonic vibration assistant electric arc increasing material manufacturing control shape control
CN103521769B (en) A kind of increasing material manufacture method be shaped based on many material particles high velocity jet
Khan et al. Selective Laser Melting (SLM) of pure gold
CN105935771B (en) A kind of metal die 3D printing laser microcell processing method
CN107217253B (en) Light-powder-gas coaxial conveying laser cladding impact forging forming composite manufacturing method
CN101054667B (en) Material for repairing high-hardness engine member abandonment die by laser and application thereof
CN105695981B (en) A kind of titanium alloy surface high tenacity high rigidity resistance to compression coating and preparation method thereof
CN106694872A (en) Compound additional material manufacturing method applicable to parts and dies
He et al. Experimental study on the fabrication profile and mechanical properties by substrate-inclined angle using laser melting deposition (LMD) integrating with the substrate of stainless steel
CN102179517A (en) Laser-induction hybrid melting direct forming method and device
Lestan et al. Laser deposition of Metco 15E, Colmony 88 and VIM CRU 20 powders on cast iron and low carbon steel
CN106216672A (en) A kind of Metal toughened ceramic matric composite part increases material preparation method
Paul et al. Metal additive manufacturing using lasers
JP2002510361A (en) Surface abrasion resistant sintered machine parts and method of manufacturing the same
CN109396434A (en) A method of titanium alloy component is prepared based on selective laser melting process
JP2003532539A (en) Method for producing a net near shape mold
CN211199407U (en) Metal matrix surface coating structure and forming device
CN106903394A (en) A kind of almag structural member increasing material manufacturing method
CN104647474B (en) A kind of die of rotating die cutting equipment and its forming method of blade
Zhang et al. Influences of processing parameters on dilution ratio of laser cladding layer during laser metal deposition shaping
CN105386035A (en) Manufacturing process for hard facing aluminum injection molds
CN111570793A (en) Selective laser melting preparation method of variable-density gradient metal material with porous structure
CN111733414A (en) Method for preparing WC particle reinforced metal matrix composite coating by cladding and melt-injection step by step through double welding guns

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant