[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

CN108359976A - A method of for reducing laser melting coating alumina base composite coating crackle - Google Patents

A method of for reducing laser melting coating alumina base composite coating crackle Download PDF

Info

Publication number
CN108359976A
CN108359976A CN201810314074.0A CN201810314074A CN108359976A CN 108359976 A CN108359976 A CN 108359976A CN 201810314074 A CN201810314074 A CN 201810314074A CN 108359976 A CN108359976 A CN 108359976A
Authority
CN
China
Prior art keywords
coating
laser melting
base composite
alumina base
melting coating
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.)
Pending
Application number
CN201810314074.0A
Other languages
Chinese (zh)
Inventor
孙帅
李崇桂
李帅
张群森
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.)
Shanghai University of Engineering Science
Original Assignee
Shanghai University of Engineering Science
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 Shanghai University of Engineering Science filed Critical Shanghai University of Engineering Science
Priority to CN201810314074.0A priority Critical patent/CN108359976A/en
Publication of CN108359976A publication Critical patent/CN108359976A/en
Pending legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C24/00Coating starting from inorganic powder
    • C23C24/08Coating starting from inorganic powder by application of heat or pressure and heat
    • C23C24/10Coating starting from inorganic powder by application of heat or pressure and heat with intermediate formation of a liquid phase in the layer
    • C23C24/103Coating with metallic material, i.e. metals or metal alloys, optionally comprising hard particles, e.g. oxides, carbides or nitrides

Landscapes

  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Powder Metallurgy (AREA)

Abstract

The invention discloses a kind of methods for reducing laser melting coating alumina base composite coating crackle, and laser melting coating powder is preset in matrix surface, laser melting coating is carried out under argon atmosphere, obtain the alumina base composite coating that thickness is 0.3 0.6mm;Including:Substrate pretreated, configuration laser melting coating powder, fore-put powder and laser melting coating process;Laser melting coating powder is by mass percentage:Al2O356 72%, TiO214 18%, WC10 30%, wherein Al2O3Granularity is 20 50 μm, and laser melting coating power is 1000 2000W;The present invention forms good metallurgical binding by the way that appropriate WC, obtained alumina base composite coating dense structure, uniform and flawless is added with metal base;And process control easy to automate, it is efficient, pollution-free and at low cost, there is ideal engineering application value.

Description

A method of for reducing laser melting coating alumina base composite coating crackle
Technical field
The invention belongs to laser melting and coating technique fields, are related to one kind and are split for reducing laser melting coating alumina base composite coating The method of line.
Background technology
Laser melting and coating technique is widely used in the table of metal and alloy because of its processing time is short, flexibility and performance accuracy height Face is modified and the directly manufacture and reparation of complex parts.But though the local heating of laser beam can preferably keep base material Property, but many defects such as crackle, stomata and coarse columnar grain etc. are easy tod produce during laser cladding forming, and due to Laser melting coating is the process of a rapid heating and cooling, and cooling velocity is too fast will to cause coating to generate larger residual stress, processed These residual stress and defect seriously affect the mechanical property of drip molding in journey, even result in the macroscopic view cracking of drip molding.
In the prior art, the Chinese patent of publication number 106048599A discloses the crackle of laser cladding forming metal parts Control method improves cladding forming tissue, reduction and the technique for eliminating crackle by introducing ultrasonic vibration, and cladding layer material is Co-based alloy powder Ni60, basis material are 45 steel, using 3KW crossing currents CO2Laser carries out laser melting coating, draws in forming process Enter ultrasonic vibration installation, vibration frequency 25KHz;Ni base composite coating prepared by this method is needed without apparent crackle to molten Pond temperature carries out closed-loop control and introduces ultrasonic vibration, is affected by extraneous factor in cladding process.Publication number The Chinese patent of 105506615A discloses a kind of incident angle control laser cladding coating microstructure by changing laser And the method for fire check sensibility.In laser cladding process, rotating laser head, changing laser incident angle makes Pool and temperature Degree field changes, and microstructure, the orientation of growth and the anti-crack splitting resistance of cladding coating is caused to change, this method behaviour Make simple but higher to the required precision of laser incident angle.
Invention content
It is a kind of for reducing laser melting coating alumina base present invention aims in view of the above shortcomings of the prior art, providing The method of composite coating crackle.
To realize the above-mentioned technical purpose, the present invention adopts the following technical scheme that:
A method of for reducing laser melting coating alumina base composite coating crackle, laser melting coating powder being preset in base Body surface face carries out laser melting coating under argon atmosphere, obtains alumina base composite coating;Including:Substrate pretreated, configuration swash Light cladding powder, fore-put powder and laser melting coating process;The laser melting coating powder is by mass percentage:Al2O356- 72%, TiO214-18%, WC10-30%, wherein Al2O3Granularity is 20-50 μm;And the laser melting coating power is 1000- The thickness of 2000W, the alumina base composite coating are 0.3-0.6mm.
In some preferred embodiments, the thickness of above-mentioned alumina base composite coating is 0.4-0.6mm;More preferably , the thickness of the alumina base composite coating is 0.5mm.
Further, described matrix is Ti-6Al-4V (TC4) alloy sheets.
Further, the laser melting coating powder passes through ball milling Style of mixing powder;Wherein, ratio of grinding media to material 10:1, Ball-milling Time For 3h, rotating speed 300rpm.
Further, the fore-put powder process is:Laser melting coating powder after ball milling is pressed into quality volume with binder Than for (9-14):3-7 (g/mL) is mixed, and described matrix surface, smooth compacting and vacuum are evenly applied to after stirring evenly Drying;The coating layer thickness is 0.8-1mm.In some preferred embodiments, bonding agent is cellulose acetate and dipropyl Keto-alcohol is 1 by mass volume ratio:The mixture of 25 (g/mL), and the diacetone alcohol is to analyze pure AR.
Further, the laser melting and coating process is:Using IPG-YLS-5000 type optical fiber lasers, laser melting coating power Conveying speed for 1500-2000W, sweep speed 600mm/min, defocusing amount 60mm, the argon gas is 5L/min, purity It is 99.99%.
Compared with prior art, the beneficial effects of the present invention are:
One, it is nano level ball milling mixing powder using granularity, by the way that appropriate WC is added, obtained alumina base is compound Coating structure densification, uniform and flawless, good metallurgical binding is formed with metal base.
Two, compared with prior art, the method for the present invention can effectively improve the hardness of coating, and can effectively reduce coating and split Line, whole process control easy to automate is efficient, pollution-free and at low cost, has ideal engineer application valence Value.
Description of the drawings
Fig. 1 is the SEM photograph of laser melting coating alumina base composite coating cross section in embodiment 6.
Specific implementation mode
With reference to specific embodiment, the present invention is further explained.
Comparative example
Laser melting coating side is used on Ti-6Al-4V (TC4) the titanium alloy sheets surface of 60 (length) × 60 (width) × 10 (thickness) mm Method prepares alumina base composite coating, is as follows:
1, titanium alloy sheet surface activation process
Polishing roughening treatment is carried out with 100# coarse sandpapers to the titanium alloy sheet surface that thickness is 10mm or uses sand-blasting machine Surface sand-blasting process removes surface oxide layer and spot, to enhance the combination of titanium alloy surface and alumina base composite cladding layer, Then it is cleaned with alcohol and acetone, is dried in drying box.
2, laser melting coating powder is prepared
Laser melting coating powder is prepared by following mass percents:80%Al2O3, 20%TiO2, mixed-powder is in the ball mill Ball milling 3 hours.
3, fore-put powder
Above-mentioned mixed-powder is preset to using fore-put powder method on substrate, the technique of fore-put powder method is as follows:It will mixing Powder is mixed into paste with bonding agent, after being mixed evenly, is coated uniformly on the surface for waiting for cladding workpiece, carries out compacting and table Face physics is smooth, and coating thickness 0.8-1mm is finally dried in vacuum drying chamber.
4, laser melting coating prepares alumina base composite coating
The titanium alloy handled well is placed on Laser platform, starts robot and controls laser melting coating, wherein laser melting coating Technological parameter is:Fibre laser power is 1000W, sweep speed 600mm/min, defocusing amount 60mm, argon gas conveying speed For 5L/min, alumina base composite coating is obtained.
By test, above-mentioned alumina base composite coating macroscopically has more fine cracks, coating layer thickness 0.2- 0.4mm, coating structure is coarse, has increased number of stomata and crackle, average hardness 684.5HV0.3, the hardness with titanium alloy substrate 380HV0.3Compared to higher.
Embodiment 1
The present embodiment is essentially identical with comparative example, except that laser melting coating powder is by mass percentage in the present embodiment It is calculated as:Al2O372%, TiO218%, WC10%, wherein Al2O3Granularity is 20-50 μm.Compared with comparative example, in embodiment 1 The WC of addition 10%, for the alumina base composite coating of preparation macroscopically without apparent crackle, coating structure is uniform, withe crystalline substance group occurs It knits, stomata and crackle significantly reduce, and coating average hardness is 1099.6HV0.3
Embodiment 2
The present embodiment is substantially the same manner as Example 1, except that laser melting coating powder presses quality percentage in the present embodiment Than being calculated as:Al2O364%, TiO216%, WC20%, wherein Al2O3Granularity is 30 μm.Compared with comparative example, add in embodiment 2 20% WC, the alumina base composite coating of preparation is added macroscopically to be molded preferably, coating structure refinement, isometric crystalline tissue density Increase, pore-free, almost eliminate crackle, coating average hardness is 1132.8HV0.3, compared with matrix, hardness improves about 2 Times.
Embodiment 3
The present embodiment is substantially the same manner as Example 1, except that laser melting coating powder presses quality percentage in the present embodiment Than being calculated as:Al2O356%, TiO214%, WC30%, wherein Al2O3Granularity is 50 μm.Compared with comparative example, add in embodiment 3 30% WC, the alumina base composite coating of preparation is added macroscopically to be molded preferably, coating structure more refines, but a little gas occurs Hole, without apparent crackle, coating average hardness is 1203.8HV0.3
Embodiment 4
The present embodiment is essentially identical with comparative example, except that laser power is 1500W in the present embodiment, other experiments Condition is identical.Compared with comparative example, laser power is 1500W in embodiment 4, and the alumina base composite coating of preparation macroscopically has More tiny crackle, coating layer thickness 0.3-0.5mm, coating structure refinement have a little stomata and crackle, coating average hardness For 818.1HV0.3, compared with matrix, hardness improves about 1 times.
Embodiment 5
The present embodiment is substantially the same manner as Example 1, except that laser power is 1500W, other realities in the present embodiment It is identical to test condition.Compared with comparative example, laser power is 1500W in embodiment 5, and the alumina base composite coating of preparation is macroscopically Crackle significantly reduces, and withe crystalline substance occurs in coating, and tissue more refines, and has a little stomata and a small amount of crackle, coating average hardness to be 1163.7HV0.3
Embodiment 6
The present embodiment is substantially the same manner as Example 2, except that laser power is 1500W, other realities in the present embodiment It is identical to test condition.Compared with comparative example, laser power is 1500W in embodiment 6, and the alumina base composite coating of preparation is macroscopically Flawless, the isometric crystalline tissue density of coating increase, and structure refinement, pore-free and crackle, coating average hardness are 1205.1HV0.3
Embodiment 7
The present embodiment is substantially the same manner as Example 3, except that laser power is 1500W, other realities in the present embodiment It is identical to test condition.Compared with comparative example, laser power is 1500W in embodiment 7, and the alumina base composite coating of preparation is macroscopically Without apparent crackle, coating structure more refines, and eliminates stomata and crackle, and coating average hardness is 1277.9HV0.3
Embodiment 8
The present embodiment is essentially identical with comparative example, except that laser power is 2000W in the present embodiment, other experiments Condition is identical.Compared with comparative example, laser power is 2000W in the present embodiment, and the alumina base composite coating of preparation is macroscopically There is a small amount of tiny crackle, coating layer thickness 0.4-0.6mm occurs that a small amount of withe is brilliant, and tissue more refines in coating, has a little Crackle and stomata, coating average hardness are 1048.1HV0.3
Embodiment 9
The present embodiment is substantially the same manner as Example 1, except that laser power is 2000W, other realities in the present embodiment It is identical to test condition.Compared with comparative example, laser power is 2000W, the alumina base composite coating macroscopic view of preparation in the present embodiment The morning apparent crackle, coating withe is crystalline, and tissue density increases, and structure refinement has a little crackle and stomata, coating average hardness For 1213.5HV0.3, compared with matrix, hardness improves more than 2 times.
Embodiment 10
The present embodiment is substantially the same manner as Example 2, except that laser power is 2000W, other realities in the present embodiment It is identical to test condition.Compared with comparative example, laser power is 2000W, the alumina base composite coating macroscopic view of preparation in the present embodiment Upper flawless, Forming Quality is preferable, and the isometric crystalline tissue density of coating increases, structure refinement, eliminates crackle, and coating is average hard Degree is 1298.5HV0.3, compared with matrix, hardness improves more than 2 times.
Embodiment 11
The present embodiment is substantially the same manner as Example 3, except that laser power is 2000W, other realities in the present embodiment It is identical to test condition.Compared with comparative example, laser power is 2000W, the alumina base composite coating macroscopic view of preparation in the present embodiment Upper flawless, coating structure more refine, and eliminate crackle, and coating average hardness is 1344.0HV0.3, compared with matrix, hardness It improves more than 2 times.
Technical scheme of the present invention and advantageous effect is described in detail in embodiment described above, it should be understood that Above is only a specific embodiment of the present invention, it is not intended to restrict the invention, it is all to be done in the spirit of the present invention Any modification and improvement etc., should all be included in the protection scope of the present invention.

Claims (10)

1. a kind of method for reducing laser melting coating alumina base composite coating crackle, which is characterized in that by laser cladding powder Body is preset in matrix surface, and laser melting coating is carried out under argon atmosphere, obtains alumina base composite coating;Including:Matrix is pre- Processing, configuration laser melting coating powder, fore-put powder and laser melting coating process;The laser melting coating powder is by mass percentage For:Al2O356-72%, TiO214-18%, WC10-30%, wherein the Al2O3Granularity is 20-50 μm;And the laser Cladding power is 1000-2000W, and the thickness of the alumina base composite coating is 0.3-0.6mm.
2. a kind of method for reducing laser melting coating alumina base composite coating crackle, feature as described in claim 1 exist In the thickness of the alumina base composite coating is 0.4-0.6mm.
3. a kind of method for reducing laser melting coating alumina base composite coating crackle, feature as claimed in claim 2 exist In the thickness of the alumina base composite coating is 0.5mm.
4. a kind of method for reducing laser melting coating alumina base composite coating crackle, feature as described in claim 1 exist In described matrix is Ti-6Al-4V (TC4) alloy sheets.
5. a kind of method for reducing laser melting coating alumina base composite coating crackle, feature as described in claim 1 exist In the laser melting coating powder passes through ball milling Style of mixing powder;Wherein, ratio of grinding media to material 10:1, Ball-milling Time 3h, rotating speed are 300rpm。
6. a kind of method for reducing laser melting coating alumina base composite coating crackle, feature as described in claim 1 exist In the fore-put powder process is:It is evenly applied to after laser melting coating powder after ball milling is mixed evenly with binder Described matrix surface, smooth compacting and vacuum drying.
7. a kind of method for reducing laser melting coating alumina base composite coating crackle, feature as claimed in claim 6 exist In the mass volume ratio of the laser melting coating powder and binder is (9-14):3-7.
8. a kind of method for being used to reduce laser melting coating alumina base composite coating crackle as claimed in claims 6 or 7, feature It is, the bonding agent is that mass volume ratio is 1:25 cellulose acetate and the mixture of diacetone alcohol, and two acetone Alcohol is to analyze pure AR.
9. a kind of method for reducing laser melting coating alumina base composite coating crackle, feature as described in claim 1 exist In the coating layer thickness is 0.8-1mm.
10. a kind of method for reducing laser melting coating alumina base composite coating crackle, feature as described in claim 1 exist In the laser melting and coating process is:Using IPG-YLS-5000 type optical fiber lasers, laser melting coating power is 1500-2000W, Sweep speed is 600mm/min, defocusing amount 60mm, and the conveying speed of the argon gas is 5L/min, purity 99.99%.
CN201810314074.0A 2018-04-10 2018-04-10 A method of for reducing laser melting coating alumina base composite coating crackle Pending CN108359976A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810314074.0A CN108359976A (en) 2018-04-10 2018-04-10 A method of for reducing laser melting coating alumina base composite coating crackle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810314074.0A CN108359976A (en) 2018-04-10 2018-04-10 A method of for reducing laser melting coating alumina base composite coating crackle

Publications (1)

Publication Number Publication Date
CN108359976A true CN108359976A (en) 2018-08-03

Family

ID=63008096

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201810314074.0A Pending CN108359976A (en) 2018-04-10 2018-04-10 A method of for reducing laser melting coating alumina base composite coating crackle

Country Status (1)

Country Link
CN (1) CN108359976A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110405407A (en) * 2019-08-13 2019-11-05 黄山学院 A kind of novel restorative procedure of mold and device
CN112979348A (en) * 2021-02-26 2021-06-18 深圳陶陶科技有限公司 Structural color ceramic and preparation method and application thereof

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62246885A (en) * 1986-04-17 1987-10-28 三菱マテリアル株式会社 Ceramic coating method
CN1542166A (en) * 2003-11-07 2004-11-03 上海工程技术大学 Method for crack resistant treatment of laser cladded nano-ceramic coating
CN103305835A (en) * 2013-06-18 2013-09-18 江苏和昊激光科技有限公司 Special cobalt-based ceramic alloy powder for laser cladding on surface of gear

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62246885A (en) * 1986-04-17 1987-10-28 三菱マテリアル株式会社 Ceramic coating method
CN1542166A (en) * 2003-11-07 2004-11-03 上海工程技术大学 Method for crack resistant treatment of laser cladded nano-ceramic coating
CN103305835A (en) * 2013-06-18 2013-09-18 江苏和昊激光科技有限公司 Special cobalt-based ceramic alloy powder for laser cladding on surface of gear

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
潘斌等: "激光熔覆法制备Al2O3-TiO2涂层的显微组织与性能研究", 《材料导报B:研究篇》 *

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110405407A (en) * 2019-08-13 2019-11-05 黄山学院 A kind of novel restorative procedure of mold and device
CN112979348A (en) * 2021-02-26 2021-06-18 深圳陶陶科技有限公司 Structural color ceramic and preparation method and application thereof
CN112979348B (en) * 2021-02-26 2022-08-16 深圳陶陶科技有限公司 Structural color ceramic and preparation method and application thereof

Similar Documents

Publication Publication Date Title
CN110315075B (en) Synchronous laser heat treatment method for manufacturing nickel-based high-temperature alloy through laser additive
US20240123502A1 (en) Titanium alloy powder for selective laser melting 3d printing, selective laser melted titanium alloy and preparation thereof
CN112935252A (en) Method for preparing high-toughness eutectic high-entropy alloy based on selective laser melting technology
CN111850543A (en) Laser cladding seven-element high-entropy alloy coating and preparation method thereof
CN110983106B (en) Method for inhibiting formation of needle-like martensite phase in 3D printing forming TC4 alloy structure
CN114682800B (en) Method for manufacturing eutectic high-entropy alloy plate by ultrasonic rolling surface strengthening laser additive
CN112063951A (en) Magnesium-aluminum alloy surface laser cladding self-lubricating coating and construction method thereof
CN114481125B (en) 5-series aluminum alloy laser repair process and preparation method of used Al-Mg-Sc-Zr powder
CN111618301A (en) Process for preparing medium carbon steel by selective laser melting
CN108359976A (en) A method of for reducing laser melting coating alumina base composite coating crackle
CN114411035A (en) Precipitation strengthening type medium-entropy alloy suitable for laser additive manufacturing and preparation method thereof
CN109097620B (en) Laser additive manufacturing La2O3Method for preparing (Cu, Ni) gradient functional composite material
CN114657554A (en) Laser cladding high-entropy alloy coating for die repair and preparation method thereof
CN112779533B (en) Method for preparing metal-based composite coating on surface of stainless steel
CN108796498B (en) Method for generating ceramic phase by laser cladding aluminum alloy surface self-reaction
CN106319512A (en) Double-phase metal-based composite coating resistant to corrosion and high-temperature oxidization and preparation method thereof
CN106141507B (en) A kind of preparation method of the ceramic granule reinforced composite material film of low content of organics
CN113385856A (en) Ternary boride Mo2NiB2Alloy welding material and production process thereof
CN116021035B (en) Method for preparing high-strength and high-hardness stainless steel-based composite material by selective laser melting
CN114875291B (en) High-entropy alloy powder and preparation method thereof, and high-entropy alloy laser cladding layer and preparation method thereof
CN110408924A (en) It is a kind of for the titanium-based mixed-powder and manufacturing method of laser cladding coating and application
CN116219433A (en) Connecting layer reinforced titanium alloy wear-resistant coating and preparation method thereof
CN117660824B (en) NiCrLaCdZrC powder-based laser alloy, composite coating and preparation method of composite coating
CN116275102B (en) Rapid forming method of aircraft catapulting seat rocker arm
CN111394720A (en) Titanium-aluminum-based laser cladding powder and laser cladding method

Legal Events

Date Code Title Description
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication

Application publication date: 20180803

RJ01 Rejection of invention patent application after publication