CN108796493A - A kind of sealing of hole method of modifying of light metal surface cold spraying coating - Google Patents

A kind of sealing of hole method of modifying of light metal surface cold spraying coating Download PDF

Info

Publication number
CN108796493A
CN108796493A CN201810563205.9A CN201810563205A CN108796493A CN 108796493 A CN108796493 A CN 108796493A CN 201810563205 A CN201810563205 A CN 201810563205A CN 108796493 A CN108796493 A CN 108796493A
Authority
CN
China
Prior art keywords
cold spraying
coating
sealing
light metal
metal surface
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
CN201810563205.9A
Other languages
Chinese (zh)
Other versions
CN108796493B (en
Inventor
徐一
师鹏飞
徐伟
陈嘉源
刘万辉
周雪峰
袁婷
张黎伟
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.)
Changshu Institute of Technology
Original Assignee
Changshu 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 Changshu Institute of Technology filed Critical Changshu Institute of Technology
Priority to CN201810563205.9A priority Critical patent/CN108796493B/en
Publication of CN108796493A publication Critical patent/CN108796493A/en
Application granted granted Critical
Publication of CN108796493B publication Critical patent/CN108796493B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • C23C24/02Coating starting from inorganic powder by application of pressure only
    • C23C24/04Impact or kinetic deposition of particles
    • 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
    • C23C10/00Solid state diffusion of only metal elements or silicon into metallic material surfaces
    • C23C10/06Solid state diffusion of only metal elements or silicon into metallic material surfaces using gases
    • C23C10/08Solid state diffusion of only metal elements or silicon into metallic material surfaces using gases only one element being diffused

Abstract

The present invention relates to light metal surface protection technology fields, and in particular to the sealing of hole of light metal surface protective coating and the technical method of modification.The invention discloses a kind of based on double-deck glow plasma permeating technology to the plasma deposition heat-treatment technology method of light metal surface cold spraying coating progress sealing of hole, diffusion;The light metal workpieces of cold spraying coating treatment are put into double brightness stoves, the target of workpiece and coating same material is heated using double Hollow cathode discharge effects, target is placed on source electrode frame, under the plasma bombardment caused by glow discharge, it is thermally formed evaporation and sputtering, it is deposited in workpiece surface, it is spread because workpiece is heated, sealing of hole and DIFFUSION TREATMENT are carried out to the cold spraying of workpiece, to eliminate coating surface and internal hole, and diffusion layer is formed between coating and substrate work-piece, reaching improves cold spraying coating and the not high disadvantage of substrate work-piece bond strength.

Description

A kind of sealing of hole method of modifying of light metal surface cold spraying coating
Technical field
The present invention relates to the shells of aircraft, ship and automobile etc. and piece surface protection technology field, and in particular to a kind of The sealing of hole of light metal surface protective coating and the technical method of modification.
Background technology
Cold spraying is that compressed air accelerates metallic to critical speed(Supersonic speed), metallic direct attack to matrix surface A kind of coat preparing technology of coating is accumulated and formed to generation physical deformation afterwards.Metallic hits flat in matrix surface and securely attached It, whole process metallic is not melted.Substantially without working condition requirement, noise is less than 60 decibels for cold spraying.Cold spraying is without height Temperature, no flame, no hazardous gas, radiationless and chemical waste, can hand operation, it is safe, and directionality and good, it is operable Property it is strong, aircraft, ship and automotive coatings prepare and repair in terms of have wide utilization.
To improve the corrosion resistance of aircraft skin and parts, generally use cold spray technique carries out coating guarantor to it Shield, repair.However, protective coating prepared by cold spraying usually occurs, hole is more, disadvantage of bond strength deficiency.These defects are led Coating is caused to lose protective value rapidly under service condition.
Double-deck glow plasma permeating technology(Hereinafter referred to as:Double brightness)It is using plasma and to use solid-state metallic material As the supply source of infiltration element, the alloy-layer with specific physical chemical property is formed in electrically conductive material surface.At one In vacuum chamber, two cathodes, one anode is set.One of cathode is made of desire co-diffusioning alloy element, referred to as source electrode, in sun Pole and cathode (workpiece) connect a controllable direct current power supply respectively between source electrode.When vacuum chamber reaches certain vacuum degree and is filled with After argon gas reaches certain operating air pressure, two DC power supplies are connected, make to generate respectively between anode and workpiece, anode and source electrode Two groups of glow discharges, i.e. " double skin facade system phenomenon ".Under the argon ion bombardment effect caused by glow discharge, source electrode and work The alloying element on part surface can be sputtered out, since source potential is set at less than workpiece current potential or makes source power density Higher than workpiece power density, the supply amount of the particle sputtered out from source electrode far more than cathode reverse sputtering amount, to make these The atom high speed for the infiltration element for being sputtered out flies to workpiece surface, is adsorbed and inwardly spread by workpiece surface, make workpiece Surface forms designed alloy-layer.Temperature can be accurately controlled by adjusting parameters such as operating air pressure, source potential, cathode potentials Degree, can realize the control of the alloying element content and alloying layer thickness in alloy-layer, and in coating and base under certain soaking time Diffusion layer is formed between body workpiece(The current situation and development China engineering science 2002 of Xu Chong plasma surface metallurgical technologies;2:36-41.).
Based on this principle, the hole of cold spraying coating is eliminated using two-lime piles, and improves the knot of coating and workpiece Close intensity.Shell and piece surface guard technology of the process for cold spray technique in aircraft, ship and automobile etc. are led Further research and development and the application in domain are of great significance.
Invention content
The object of the invention overcome in the prior art light metal surface cold spraying protective coating usually occur hole it is more, combine The deficiency of the disadvantage of intensity deficiency provides a kind of light metal surface cold spraying coating sealing of hole and the surface protection technique of modification.This Invention uses double-deck glow plasma permeating technology, is carried out at sealing of hole modification to workpiece prepared by light metal surface cold spraying coating Reason substantially reduces the voidage of coating, and forms one layer of diffusion layer between coating and substrate work-piece, significantly improves cold spraying painting The bond strength of layer and substrate work-piece, to reach the barrier propterty for promoting coating.
Double-deck glow plasma permeating technical principle of the present invention is as follows:In a vacuum chamber, two cathodes and one are set A anode;One of cathode is light metal surface cold spraying coating same material target, is placed on conductive material(Such as graphite, difficulty Molten metal or high temperature alloy)In manufactured crucible, also referred to as source electrode;Another cathode is substrate work-piece;Anode is earthing pole, That is furnace body;Connect a controllable direct current power supply respectively between anode and cathode-workpiece and source electrode target;When vacuum chamber reaches certain Vacuum degree and after being filled with the operating air pressure that argon gas reaches certain, connect two DC power supplies, make anode and cathode-workpiece, anode Generate two groups of glow discharges respectively between source electrode target;Under the argon ion bombardment effect caused by glow discharge, source electrode quilt Heating melts and generates evaporation, meanwhile, the bombardment of argon ion also sputters a large amount of coating same material atom and atomic group.It splashes Atom and the atomic group high speed penetrate, being evaporated fly to workpiece surface, are adsorbed and deposited by workpiece surface.It is applied to workpiece Electric field also generates glow discharge, and workpiece is made to be heated, and will make the coating same material for being deposited on its surface after reaching suitable temperature Atom is inwardly spread, and makes that surface coating is more fine and close, porosity is substantially reduced, and formed between substrate work-piece and coating Certain thickness diffusion layer.It can by adjusting parameters such as operating air pressure, source potential, cathode potential and source electrode-workpiece spacing Temperature is accurately controlled, the control of coating compactness and thickness of diffusion layer can be realized under certain soaking time.
The present invention is achieved through the following technical solutions above-mentioned purpose:A kind of sealing of hole of light metal surface cold spraying coating Method of modifying carries out plating, in light gold using double-deck glow plasma permeating stove to workpiece prepared by light metal cold spraying coating Belong to and forms one layer of diffusion layer between matrix and cold spraying coating.
Preferably, the sealing of hole method of modifying of the light metal surface cold spraying coating, specific method are:By light metal table Cold spraying coating same material target in face is put into vacuum chamber and is placed on source electrode, and light metal surface cold spraying coated workpieces are placed under source electrode Side adjust certain interpolar away from;After adjustment vacuum chamber reaches certain vacuum degree and is filled with argon gas to operating air pressure, to source electrode plus directly Stream negative voltage makes in source electrode target micro- molten and keeps electric discharge sputtering state, then adds to light metal surface cold spraying coated workpieces negative Voltage makes workpiece be warming up to technological temperature, and it is certain that adjustment light metal surface cold spraying coated workpieces negative electricity is depressed into 200 ~ 750V heat preservations Time;Cool down later, come out of the stove to obtain the light metal surface cold spraying coated workpieces of sealing of hole modification.
Preferably, the interpolar is away from for 10 ~ 50mm;
Preferably, the pressure of the operating air pressure is 10 ~ 80Pa;
Preferably, described to add the voltage of negative DC voltage to be 200 ~ 1000V source electrode;
Preferably, the light metal surface cold spraying coated workpieces add the negative voltage of negative voltage to be 200 ~ 1000V;
Preferably, the technological temperature is 200 ~ 900 DEG C;
Preferably, the held for some time refers to 0.5 ~ 10h of heat preservation.
Preferably, the cold spraying coating is the pure titanium coating of cold spraying or cold spraying cu coating;
The present invention has the advantages that:
1)Using the coating compactness of the light metal surface cold spraying coated workpieces after double-deck glow plasma permeating technical finesse It greatly promotes, and forms one layer of diffusion layer between coating and substrate work-piece, substantially improve substrate work-piece and cold spraying Bond strength between coating;
2)Due to the typicalness of research object, achievement in research will be generalized to other fields, and engineering value is also very prominent;
3)Previous research focus mostly in two-lime piles compared with (700 °C or more) under elevated operating temperature to high-melting-point huge sum of money metal surface The work in terms of plating processing is carried out, the present invention has filled up two-lime piles and carried out table to light-alloy in low-temperature zone (600 °C or less) The technology application blank of surface treatment.
Description of the drawings
Fig. 1 is two-lime piles cold spraying coating sealing of hole modification schematic diagram.
Specific implementation mode
In order to make the objectives, technical solutions and advantages of the present invention clearer, With reference to embodiment, to this Invention is further described.It should be understood that these descriptions are merely illustrative, and it is not intended to limit the scope of the present invention.
Embodiment 1
The sealing of hole modification of the 2024 pure titanium coatings of aluminum alloy surface cold spraying
(1)Sample pre-treatment.By the pure titanium coating specimen surface alcohol washes of 2024 aluminum alloy surface cold sprayings and drying.
(2)It is fitted into double brightness plating stoves.It places pure titanium and oozes source, the pure titanium coating workpiece of 2024 aluminum alloy surface cold sprayings, adjust Whole good interpolar is away from for 40mm.
(3)It vacuumizes.Air admission hole is closed, vacuum pump is opened, air pressure in stove is extracted into 10-1Pa is hereinafter, then pass to argon gas To the operating air pressure of 40Pa.
(4)Plasma cleaning sample.Cooling water is opened, startup power supply first applies the pure titanium of 2024 aluminum alloy surface cold sprayings Layer workpiece power supply opening, applies 500V voltages, utilizes the cold spray of 2024 aluminum alloy surface of beam-plasma pair caused by glow discharge Apply pure titanium coating workpiece and carry out 30min or so bombardments, on the one hand sample is further cleaned, another aspect activating surface with Convenient for the absorption of active atomic.
(5)Plating.After pre- bombardment, voltage 600V is applied to the source electrode of double brightness plating stoves, until micro- melt of pure titanium target material adjusts again It is kept to 350 ~ 400V.The pure titanium coating workpiece voltage of 2024 aluminum alloy surface cold sprayings is then added to 700V, makes the temperature of sample Then degree is adjusted to 600 ~ 650V up to 350 DEG C to keep temperature.
(6)Cooling.After keeping the temperature 3.5h, pure titanium target material source electrode power supply is cut off, the pure titanium of 2024 aluminum alloy surface cold sprayings is applied Layer workpiece pole tension is turned down to 200V or so, and 2024 aluminum alloy surface cold spraying pure titanium coating workpiece pole is made to be put in faint glow Electricity gradually cools down.
(7)It comes out of the stove.After specimen temperature is down to 200 DEG C or less, the pure titanium coating workpiece of 2024 aluminum alloy surface cold sprayings is cut off Pole power supply closes Ar air valves, cuts off vacuum-pump power supply and cooling water.It opens vent valve and is filled with air, chamber pressure is restored to Bonnet is opened after air pressure and takes out sample.
After above-mentioned two-lime piles sealing of hole modification, the pure titanium coating porosity of 2024 aluminum alloy surface cold sprayings by 8.43% is down to 0.98%, and ~ 2 μm of diffusion layer, pure titanium coating and 2024 aluminium alloys are formd between pure titanium coating and 2024 aluminium alloys Binding force is promoted to 77.9N by 43.5N between matrix.
Embodiment 2
The sealing of hole modification of 2024 aluminum alloy surface cold spraying cu coatings
(1)Sample pre-treatment.By specimen surface alcohol washes and drying, it can first polish clean again when necessary.
(2)It is fitted into double brightness plating stoves.It places fine copper target and oozes source, 2024 aluminum alloy surface cold spraying cu coating works Part adjusts interpolar away to 30mm.
(3)It vacuumizes.Air admission hole is closed, vacuum pump is opened, air pressure in stove is extracted into 10-1Pa is hereinafter, then pass to argon gas To the operating air pressure of 30Pa.
(4)Plasma cleaning sample.Cooling water is opened, startup power supply first applies 2024 aluminum alloy surface cold spraying fine copper Layer workpiece power supply opening, applies 400V voltages, utilizes the cold spray of 2024 aluminum alloy surface of beam-plasma pair caused by glow discharge Apply cu coating workpiece and carry out 30min or so bombardment, on the one hand sample is further cleaned, another aspect activating surface with Convenient for the absorption of active atomic.
(5)Plating.After pre- bombardment, fine copper target source voltage 650V will be applied, until target it is micro- it is molten adjusted again to 400 ~ 450V is kept.2024 aluminum alloy surface cold spraying cu coating workpiece voltages are then added to 700V, make the temperature of sample up to 400 DEG C, it then adjusts to 550 ~ 650V to keep temperature.
(6)Cooling.After keeping the temperature 7h, source electrode power supply is cut off, 2024 aluminum alloy surface cold spraying cu coating workpiece are extremely electric Pressure is turned down to 250V or so, so that workpiece pole be in faint glow and is discharged, gradually cools down.
(7)It comes out of the stove.After specimen temperature is down to 200 DEG C or less, 2024 aluminum alloy surface cold spraying cu coating workpiece are cut off Pole power supply closes Ar air valves, cuts off vacuum-pump power supply and cooling water.It opens vent valve and is filled with air, chamber pressure is restored to Bonnet is opened after air pressure and takes out sample.
Porosity is down to 0.53% by 6.71% after the sealing of hole modification of 2024 aluminum alloy surface cold spraying cu coatings, pure ~ 3 μm of diffusion layer is formd between copper coating and 2024 aluminium alloys, between cu coating and 2024 alloy matrix aluminums binding force by 31.3N being promoted to 65.1N.
Although embodiments of the present invention are described in detail, it should be understood that, without departing from the present invention's In the case of spirit and scope, can embodiments of the present invention be made with various changes, replacement and change.

Claims (9)

1. a kind of sealing of hole method of modifying of light metal surface cold spraying coating, it is characterised in that:It is oozed using double-deck glow plasma Plating stove carries out plating to workpiece prepared by light metal cold spraying coating, and one layer is formed between light metal matrix and cold spraying coating Diffusion layer.
2. sealing of hole method of modifying according to claim 1, it is characterised in that:The specific steps are:By the cold spray of light metal surface Coating layer same material target is put into vacuum chamber and is placed on source electrode, and light metal surface cold spraying coated workpieces are placed in adjustment below source electrode Certain interpolar away from;After adjustment vacuum chamber reaches certain vacuum degree and is filled with argon gas to operating air pressure, to source electrode plus direct current negative electricity Pressure makes in source electrode target micro- molten and keeps electric discharge sputtering state, then adds negative voltage to make to light metal surface cold spraying coated workpieces Workpiece is warming up to technological temperature, and adjustment light metal surface cold spraying coated workpieces negative electricity is depressed into 200 ~ 750V held for some time; Cool down later, come out of the stove to obtain the light metal surface cold spraying coated workpieces of sealing of hole modification.
3. sealing of hole method of modifying according to claim 2, it is characterised in that:The interpolar is away from for 10 ~ 50mm.
4. sealing of hole method of modifying according to claim 2, it is characterised in that:The pressure of the operating air pressure is 10 ~ 80Pa.
5. sealing of hole method of modifying according to claim 2, it is characterised in that:The voltage for adding negative DC voltage to source electrode For 200 ~ 1000V.
6. sealing of hole method of modifying according to claim 2, it is characterised in that:The light metal surface cold spraying coated workpieces It is 200 ~ 1000V to add the negative voltage of negative voltage.
7. sealing of hole method of modifying according to claim 2, it is characterised in that:The technological temperature is 200 ~ 900 DEG C.
8. sealing of hole method of modifying according to claim 2, it is characterised in that:The held for some time refer to heat preservation 0.5 ~ 10h。
9. according to claim 1-8 any one of them sealing of hole method of modifying, it is characterised in that:The cold spraying coating is cold spray Apply pure titanium coating or cold spraying cu coating.
CN201810563205.9A 2018-06-04 2018-06-04 Hole sealing modification method for cold spraying coating on surface of light metal Active CN108796493B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810563205.9A CN108796493B (en) 2018-06-04 2018-06-04 Hole sealing modification method for cold spraying coating on surface of light metal

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810563205.9A CN108796493B (en) 2018-06-04 2018-06-04 Hole sealing modification method for cold spraying coating on surface of light metal

Publications (2)

Publication Number Publication Date
CN108796493A true CN108796493A (en) 2018-11-13
CN108796493B CN108796493B (en) 2020-11-06

Family

ID=64090353

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201810563205.9A Active CN108796493B (en) 2018-06-04 2018-06-04 Hole sealing modification method for cold spraying coating on surface of light metal

Country Status (1)

Country Link
CN (1) CN108796493B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20210178527A1 (en) * 2019-12-13 2021-06-17 Vast Glory Electronic & Hardware & Plastic (Hui Zhaou) Ltd Welding method for manufacturing a heat sink structure
CN113293350A (en) * 2021-05-26 2021-08-24 南京信息工程大学 Titanium alloy surface modification method

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102154639A (en) * 2011-03-10 2011-08-17 上海交通大学 Aluminum-particle-based method for preparing coating by cold spray deposition
CN103255410A (en) * 2013-04-24 2013-08-21 中国航空工业集团公司北京航空材料研究院 Preparation method of magnesium alloy corrosion resistant prevention coating
CN103882426A (en) * 2014-03-14 2014-06-25 四川理工学院 Preparation method of light metal and alloy surface composite coating thereof
CN106399914A (en) * 2016-10-19 2017-02-15 昆明理工大学 Method for eliminating porosity of sprayed coating
CN107761035A (en) * 2017-11-07 2018-03-06 西安交通大学 A kind of corrosion resistant fine and close thermal spray metal alloy coat and preparation method thereof completely

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102154639A (en) * 2011-03-10 2011-08-17 上海交通大学 Aluminum-particle-based method for preparing coating by cold spray deposition
CN103255410A (en) * 2013-04-24 2013-08-21 中国航空工业集团公司北京航空材料研究院 Preparation method of magnesium alloy corrosion resistant prevention coating
CN103882426A (en) * 2014-03-14 2014-06-25 四川理工学院 Preparation method of light metal and alloy surface composite coating thereof
CN106399914A (en) * 2016-10-19 2017-02-15 昆明理工大学 Method for eliminating porosity of sprayed coating
CN107761035A (en) * 2017-11-07 2018-03-06 西安交通大学 A kind of corrosion resistant fine and close thermal spray metal alloy coat and preparation method thereof completely

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20210178527A1 (en) * 2019-12-13 2021-06-17 Vast Glory Electronic & Hardware & Plastic (Hui Zhaou) Ltd Welding method for manufacturing a heat sink structure
CN113293350A (en) * 2021-05-26 2021-08-24 南京信息工程大学 Titanium alloy surface modification method

Also Published As

Publication number Publication date
CN108796493B (en) 2020-11-06

Similar Documents

Publication Publication Date Title
CN101698362B (en) Self-lubricating hard nanocomposite laminated coating and preparation method thereof
CN103590008B (en) One is coated with interlayer in TiAl alloy and MCrAlY and prepares Al 2o 3the method of diffusion barrier
CN105603424B (en) β (Ni, Pt) Al coatings that a kind of Si is modified and preparation method thereof
CN108796493A (en) A kind of sealing of hole method of modifying of light metal surface cold spraying coating
CN108060398A (en) A kind of fuel cell composite Nano coating and its plating method
CN108707868A (en) A kind of vacuum ion plating Ag nano-composite coatings fastener and preparation method
CN106435430B (en) A method of improving thermal spraying MCrAlY coating antioxygenic property
CN103590002A (en) Preparation method for Al-Cr coating on nickel-based superalloy
CN101310972B (en) Codeposition gradient Ni-base superalloy coating preparation technique
US20040126492A1 (en) Method and apparatus for using ion plasma deposition to produce coating
CN107164731A (en) A kind of preparation method of Mg alloy surface aluminium composite armor
CN103658790A (en) Novel high-speed steel milling cutter plated with ultrahard coating layer
CN101074476A (en) Method for producing Fe-Al intermetallic compound layer on surface of iron or steel materials
CN102676991B (en) Process for preparing superhard nanocomposite laminated coating by PVD (plating vacuum deposition) technology
CN112501569A (en) Surface gradient high-entropy alloy layer and preparation method thereof
CN110306148B (en) Method for preparing aluminum-based amorphous layer by combining thermal spraying and electron beam remelting technologies
CN102936716A (en) Method for preparing cobalt-based alloy layer on surface of TC4 titanium alloy
CN104388900B (en) A kind of method of γ TiAl alloys surface plating LaTaAlY alloy-layers
US20200199734A1 (en) Magnesium alloy surface coating method and corrosion-resistant magnesium alloy prepared thereby
WO2021072623A1 (en) Coated cutting tool for machining titanium alloy and high-temperature alloy and preparation method therefor
CN104070725B (en) Fe-Al-Nb alloy coat and preparation method thereof
CN110923636B (en) Electron beam composite plasma alloying treatment method for surface of gamma-TiAl alloy
RU2005136792A (en) METHOD FOR PRODUCING SUPERHARD COATINGS
CN105887084A (en) Method for preparing magnesium alloy composite coating with self-repair function
CN115287596B (en) Preparation method of chromium alloy layer on stainless steel

Legal Events

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