CN113564549B - Method for depositing DLC (diamond-like carbon) thick film by high-density plasma composite carbon source - Google Patents

Method for depositing DLC (diamond-like carbon) thick film by high-density plasma composite carbon source Download PDF

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CN113564549B
CN113564549B CN202110757165.3A CN202110757165A CN113564549B CN 113564549 B CN113564549 B CN 113564549B CN 202110757165 A CN202110757165 A CN 202110757165A CN 113564549 B CN113564549 B CN 113564549B
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thick film
dlc
substrate
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CN113564549A (en
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李海涛
程东海
张体明
戎易
李文杰
刘钊泽
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Nanchang Hangkong University
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    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/22Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
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    • 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
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/06Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
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    • 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
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/06Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
    • C23C14/14Metallic material, boron or silicon
    • C23C14/16Metallic material, boron or silicon on metallic substrates or on substrates of boron or silicon
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    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/22Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
    • C23C14/34Sputtering
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    • C23C14/345Applying energy to the substrate during sputtering using substrate bias
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    • 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
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/22Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
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    • C23C14/3485Sputtering using pulsed power to the target
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    • 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
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Abstract

The invention discloses a method for depositing DLC thick film by high-density plasma composite carbon source, which comprises five steps of pretreatment of a substrate, preparation before film coating, preparation of Ti-Si transition buffer layer, preparation of DLC thick film, aging and liquid nitrogen cooling. The method is used for preparing the high-hardness corrosion-resistant DLC thick film.

Description

Method for depositing DLC (diamond-like carbon) thick film by high-density plasma composite carbon source
Technical Field
The invention relates to the technical field of surface coatings and materials, in particular to a method for depositing a DLC thick film by using a high-density plasma composite carbon source.
Background
Resource consumption is an important problem facing human sustainable development at present. The metal material has wide application in various fields such as military chemical industry, aerospace, transportation, production and construction, machining, electronic industry and the like, and can be said to cover all the fields. However, for some metal materials, a large amount of metal materials are often consumed due to factors such as abrasion, corrosion and high-temperature oxidation, so that not only are resources wasted and the cost increased, but also significant potential safety hazards exist. For example, the magnesium alloy member is worn and corroded seriously, and the iron and steel material is rusted and oxidized. The development of the surface coating technology brings good news for solving the problems, and on the premise of ensuring the performance of the matrix, the performance of the matrix can be obviously improved, and the wear rate and corrosion rate of the matrix material are greatly reduced. However, the thickness of the traditional film is limited, generally less than 10 μm, so that the improvement of the wear resistance and corrosion resistance of the matrix material is very limited. DLC thick film is a better amorphous carbon material, the lubrication and thickness guarantee of carbon element, stable structure and inertia of the DLC thick film, excellent heat conduction and heat dissipation capacity and the like of the DLC thick film, and can solve the consumption loss of abrasion, corrosion, oxidation and the like in most application occasions. Moreover, the DLC amorphous structure eliminates columnar crystals and reduces the passage of corrosive ions into the matrix through grain boundaries, which is also a great benefit for the improvement of corrosion resistance. Therefore, the invention has very important significance.
Disclosure of Invention
The invention aims to solve the problems that: the method for depositing the DLC thick film by the high-density plasma composite carbon source can solve the problems of low hardness of the metal surface, no wear resistance, easy oxidation and easy corrosion.
The technical scheme provided by the invention for solving the problems is as follows: a method for depositing a DLC thick film by using a high density plasma composite carbon source, the method comprising the steps of:
1. pretreatment of a matrix: cutting and sampling a substrate, grinding the substrate by metallographic abrasive paper with different meshes, cleaning the substrate in an aqueous solution of oxalic acid, citric acid and sodium benzenesulfonate, and then performing cleaning in NaHCO 3 Soaking the solution to neutralize residual acid, washing with deionized water twice, polishing, and ultrasonically cleaning the polished substrate in acetone, absolute ethyl alcohol and deionized water;
2. preparing before coating: putting the substrate cleaned in the step one in N 2 Drying with cold air under air flow, placing into a magnetron sputtering vacuum chamber, checking the air tightness of the vacuum chamber, vacuumizing until the vacuum degree in the vacuum chamber is lower than 1 × 10 -3 Introducing argon gas, adjusting the air pressure in the vacuum chamber, starting a pulse power supply and a bias power supply, and carrying out sputtering cleaning and etching on the substrate;
3. preparing a Ti-Si transition buffer layer: introducing argon into the vacuum chamber, adopting a Ti-Si alloy target as a cathode, and preparing a transition buffer layer by using the alloy target through plasma magnetron sputtering under the action of pulse and bias voltage;
4. preparing a DLC thick film: introducing argon and propane, volatilizing toluene, conveying the toluene into a vacuum chamber, depositing and preparing a Pd element doped DLC thick film on a Ti-Si transition buffer layer in a mixed atmosphere of argon, propane and toluene by adopting a method of pulse and bias voltage cooperated with magnetron sputtering of a palladium target (Pd), wherein the doping proportion of the Pd is controlled by pulse power;
5. aging and liquid nitrogen cooling: and according to the method of the fourth step, the prepared DLC thick film is cooled to room temperature, taken out of the vacuum chamber, aged for a period of time, put into liquid nitrogen and cooled for a moment, and taken out.
Preferably, the substrate in the first step may be any one of magnesium alloy, aluminum alloy, alloy steel or titanium alloy.
Preferably, the concentration of the oxalic acid, the citric acid, the sodium benzenesulfonate and the sodium bicarbonate in the step one is 5 to 40wt%; ultrasonic cleaning is carried out in acetone, absolute ethyl alcohol and deionized water for 10-30 min respectively, and the ultrasonic power is 100-200W.
Preferably, in the second step, the pressure of the vacuum chamber for etching and cleaning the substrate by the Ar ions is 0.5 Pa-1.5 Pa, the bias voltage of the substrate is-500V-1500V, the power of the pulse power supply is 300-500W, the duty ratio is 20-70%, the Ar flow is 15-100sccm, and the etching and cleaning of the Ar ions are carried out for 5 min-30 min to obtain the substrate with a clean surface.
Preferably, the thickness of the Ti-Si transition buffer layer in the third step is 0.05-0.6 μm, the atomic percentage of Si element in the Ti-Si target is 5-95 at%, and the deposition time is 1-10 min.
Preferably, the pulse power in the third step is 300-500W, the duty ratio is 20-70%, the bias voltage is-100-500V, the Ar flow is 15-100 sccm, and the working air pressure is 0.5-1.5 Pa.
Preferably, the pulse power in the fourth step is 300-500W, the duty ratio is 20-70%, the bias voltage is-100 to-500V, the DLC thickness is 120-220 μm, and the deposition time is 4-7 h.
Preferably, in the fourth step, the flow rate of Ar is 15-100 sccm, the flow rate of propane is 50-200 sccm, the flow rate of toluene is 50-200 sccm, the working pressure is 1.0-2.5Pa, the power of a pulse power supply for sputtering the Pd target is 50-300W, the duty ratio is 10-80%, the bias voltage is-50-200V, and the doping proportion of Pd is 10-50 wt%.
Preferably, the aging time in the fifth step is 10-90 h, the aging temperature is 15-30 ℃, and the liquid nitrogen is cooled for 5-30 s.
Compared with the prior art, the invention has the advantages that:
1. the invention adopts the magnetron sputtering technology of pulse plus bias to prepare the Pd-doped DLC thick film on the surface of the metal material, breaks through the prior periodic film and greatly simplifies the operation and the flow.
2. Propane and toluene high-density gas is used as a mixed carbon source, so that the gas ionization rate is high, the plasma density and energy are high, the thick film deposition thickness is 120-220 mu m, the phenomena of breakage, wear-through and the like do not exist, and the capability of absolutely protecting a matrix is realized. The metal Pd of the silver white with the face-centered cubic structure is adopted as a doping element, so that the plasticity and the toughness of the thick film can be greatly improved, the frictional wear performance of the thick film is greatly improved, and the Pd doping proportion is controllable;
3. the aging is beneficial to releasing the stress of the thick film, the liquid nitrogen cooling greatly improves the hardness of the thick film, and the superhard effect is achieved;
4. the method is safe, reliable, green and pollution-free, has high production efficiency, simple required equipment, convenient operation and easy realization, and is worthy of popularization.
Drawings
The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the description serve to explain the invention and do not limit the invention.
FIG. 1 is an SEM cross-sectional profile of a DLC thick film in example 1;
FIG. 2 is HRTEM and SAED electron diffraction images of the DLC thick film in example 1, with HRTEM on the left and SAED electron diffraction images on the right.
FIG. 3 is an acoustic emission curve of the bonding performance of the DLC thick film in example 1;
FIG. 4 is the electrochemical polarization curve of the DLC thick film in example 1;
FIG. 5 is a graph showing the friction coefficient of a DLC thick film in example 1.
Detailed Description
The embodiments of the present invention will be described in detail with reference to the drawings and examples, so that the implementation process of how to apply the technical means to solve the technical problems and achieve the technical effects can be fully understood and implemented.
The first embodiment is as follows: the embodiment is a method for depositing a DLC thick film by using a high-density plasma composite carbon source, which comprises the following steps:
1. pretreatment of a matrix: grinding the matrix with metallographic abrasive paper of different meshes, cleaning in mixed solution of oxalic acid, citric acid and sodium benzenesulfonate, and adding NaHCO 3 Neutralizing the solution, washing and polishing the solution by deionized water twice, and then respectively ultrasonically cleaning the solution in acetone, absolute ethyl alcohol and deionized water;
2. preparing before coating: putting the substrate cleaned in the step one in N 2 Drying with cold air under air flow, placing in a magnetron sputtering vacuum chamber, vacuumizing until the vacuum degree is lower than 1 × 10 -3 After Pa, introducing argon and adjusting the air pressure in the vacuum chamber, starting a pulse and bias power supply, and carrying out sputtering cleaning and etching on the substrate for 5-30 min;
3. preparing a Ti-Si transition buffer layer: introducing argon, and sputtering a Ti-Si alloy target by adopting a pulse and bias mixed magnetron sputtering method to prepare a Ti-Si transition buffer layer;
4. preparing a DLC thick film: introducing argon, propane and toluene, and in a composite carbon source atmosphere, adopting a pulse + bias mixed magnetron sputtering method to deposit a Pd-doped DLC thick film by sputtering a Pd target;
5. aging and liquid nitrogen cooling: and cooling the DLC thick film prepared in the fourth step, taking the DLC thick film out of the vacuum chamber, aging for a period of time, and then cooling in liquid nitrogen for a while.
The second embodiment is as follows: the first difference between the present embodiment and the specific embodiment is: the matrix in the first step comprises various metal materials such as magnesium alloy, aluminum alloy, titanium alloy, steel and the like. The mesh number of the metallographic abrasive paper for grinding is 280#, 500#, 800#, 1000#, 1500#, 2000#, 2500#, 3000#, 3500#, 4000# and 5000#. The rest is the same as the first embodiment.
The third concrete implementation mode: this embodiment is different from the first or second embodiment in that: the polishing in the first step is as follows: al with the granularity of 0.5-2.5 mu m for the polished substrate 2 O 3 And (5) polishing under the action of the polishing paste. The ultrasonic cleaning time in the step one is 10-30 min, and the ultrasonic power is 100-200W. Oxalic acid, citric acid, sodium benzenesulfonate and NaHCO 3 The concentration is 5-40%, and the cleaning time is 10-30 min. The other is the same as in one or both of the first and second embodiments.
The fourth concrete implementation mode: the difference between this embodiment mode and one of the first to third embodiment modes is: in the second step, the power of the pulse power supply is 300-500W, the duty ratio is 20-70%, and the bias voltage is-500V-1500V. The others are the same as in one of the first to third embodiments.
The fifth concrete implementation mode: the difference between this embodiment and one of the first to fourth embodiments is: in the second step, the working pressure is 0.5-1.5Pa, the Ar flow is 15-100 sccm, and the sputtering time is 5-30 min. The other is the same as one of the first to fourth embodiments.
The sixth specific implementation mode: the difference between this embodiment and one of the first to fifth embodiments is: the concrete operation of the Ti-Si transition buffer layer in the step three is as follows: firstly, fixing a cleaned substrate on a sample frame, vacuumizing to a preset value, introducing argon, opening a flow valve switch, sputtering a Ti-Si alloy target (Si atomic percent is 5-95%) under the combined action of pulse (300-500W, 20-70% duty ratio) and bias voltage (-100-500V), and depositing a Ti-Si transition buffer layer on the substrate, wherein the working pressure is 0.5-1.5 Pa. The other is the same as one of the first to fifth embodiments.
The seventh embodiment: the difference between this embodiment and one of the first to sixth embodiments is: in the third step, the thickness of the Ti-Si transition buffer layer is 0.05-0.6 mu m, the Ar flow is 15-100 sccm, the deposition time is 1-10 min, and the background is trueDimensional 1 x 10 -4 ~5×10 -3 . The other is the same as one of the first to ninth embodiments.
The specific implementation mode is eight: the difference between this embodiment and one of the first to seventh embodiments is: the purity of argon in the step four is 99.00-99.999%, the flow rate is 15-100 sccm, the purity of propane and toluene is 99.00-99.99%, and the flow rate is 50-200 sccm. The pulse power is 100-400W, the duty ratio is 10-80%, the bias voltage is-50V to-200V, and the working air pressure is 1.0-2.5 Pa. The rest is the same as one of the first to seventh embodiments.
The specific implementation method nine: the present embodiment differs from the first to eighth embodiments in that: step four, the deposition time of the DLC film is 4 to 7 hours, the thickness is 120 to 220 mu m, and the Pd doping proportion is 10 to 50 percent by weight. The rest is the same as the first to eighth embodiments.
The detailed implementation mode is ten: the difference between this embodiment and one of the first to ninth embodiments is that: and the aging time in the step five is 10-90 h, and the aging can be carried out at room temperature and the temperature can be 15-35 ℃. And cooling the film for 5 to 30 seconds by using liquid nitrogen to obtain the superhard wear-resistant DLC aperiodic thick film. The other is the same as one of the first to ninth embodiments.
The following examples are given to illustrate the present invention, and the following examples are carried out on the premise of the technical solution of the present invention, and give detailed embodiments and specific procedures, but the scope of the present invention is not limited to the following examples.
Example 1:
this example shows a method for depositing DLC thick film by high density plasma composite carbon source
The method comprises the following steps:
1. pretreatment of a matrix: grinding magnesium alloy matrix with size of 20mm × 20mm × 3mm with metallographic abrasive paper step by step, cleaning in mixed solution of oxalic acid, citric acid and sodium benzenesulfonate, and washing with NaHCO 3 Soaking in solution for neutralization, washing with deionized water twice, and adding Al 2 O 3 Polishing under the action of the polishing paste to obtain a substrate with a smooth surface. Then ultrasonic cleaning the substrate in acetone, absolute ethyl alcohol and deionized water respectively, and ultrasonic cleaningThe time of (2) is 20min, and the ultrasonic power is 120W. Wherein the element content of the matrix is as follows: al:3.0911wt.%, zn:0.7862wt.%, mn:0.2863wt.%, mg: and (4) the balance. The grinding is sequentially performed by using 280#, 500#, 800#, 1000#, 1500#, 2000#, 2500#, 3000#, 3500#, 4000#, 4500# and 5000# metallographic abrasive paper.
2. Preparation before film coating: in N 2 Blowing the mixture with cold air under air flow, and putting the mixture into a magnetron sputtering vacuum chamber. The Pd target is well installed, the cleaned substrate is fixed on a sample rack, the distance between the target material and the sample rack is adjusted to be 60mm, and then the top cover of the vacuum chamber is closed and the air tightness of the vacuum chamber is checked. Then starting a mechanical pump to pump vacuum, and starting a molecular pump to further pump vacuum when the vacuum degree is lower than 10Pa until the background vacuum degree in the vacuum chamber is less than or equal to 1 multiplied by 10 -3 Pa. Introducing argon gas and regulating the air pressure in the vacuum chamber, then starting the high-power pulse power supply and the bias power supply, sputtering and cleaning and etching the magnesium alloy substrate, thus the combination property of the film and the substrate can be improved.
3. Preparing a Ti-Si transition buffer layer: introducing argon gas with the purity of 99.99 percent and the flow rate of 60sccm, and preparing a Ti-Si transition buffer layer on the surface of the substrate cleaned by the ion etching by utilizing a pulse and bias magnetron sputtering technology to obtain the Ti-Si transition buffer layer-substrate.
4. Preparing a DLC thick film: introducing argon, propane and toluene, sputtering a high-purity Pd metal target by using a pulse and bias composite magnetron sputtering technology in a high-density carbon source atmosphere to prepare a Pd-doped DLC thick film, and obtaining the DLC thick film-Ti-Si transition buffer layer-substrate.
5. And (3) liquid nitrogen cooling: after the preparation is finished, the DLC thick film is aged for 60 hours at the room temperature of 25 ℃, and then is cooled for 10 seconds by liquid nitrogen, thus finishing the preparation of the DLC amorphous non-periodic thick film on the surface of the magnesium alloy substrate.
Step one, the concentration of the oxalic acid, the citric acid and the sodium benzenesulfonate in the mixed solution is 10 percent, and NaHCO is adopted 3 10% by mass of the solution, al 2 O 3 The particle size of the polishing paste was 1.5. Mu.m.
And step two, the power of the pulse power supply is 450W, the duty ratio is 60%, and the bias voltage is-1000V. The flow rate of Ar is 60sccm, the working pressure is 1.0Pa, and the pre-sputtering time is 20min.
And step three, the power of the pulse power supply is 450W, the duty ratio is 60%, and the bias voltage is-200V. The flow rate of Ar is 60sccm, the working pressure is 1.0Pa, the sputtering time is 5min, and the thickness of the Ti-Si transition buffer layer is 200nm.
And step four, the purity of the Ar gas is 99.99 percent, and the flow rate is 60sccm. The power of the pulse power supply is 450W, the duty ratio is 60 percent, and the bias voltage is-200V. The working pressure is 2.0Pa, and the deposition time is 5h.
And the purity of the propane and the toluene in the step four is 99.99 percent, and the flow rate is 150sccm. The purity of the Pd metal target is 99.9 percent, the Pd doping proportion is 30 percent, and the thickness of the DLC thick film is 157.2 mu m.
The liquid nitrogen cooling operation in the fifth step is as follows: and closing all gas paths, closing all power supplies, taking out the thick film after cooling, aging at room temperature for 60h, and putting the thick film into liquid nitrogen for cooling for 10s.
The method adopts the magnetron sputtering technology of high-power pulse and bias voltage, has high preparation efficiency, large film thickness, good performance, economy and practicality, and is an amorphous aperiodic wear-resistant thick film. Ti-Si is adopted as a buffer transition layer, so that the problem of poor bonding force between a substrate and a film caused by thermal physical property parameter difference is solved, and the film/substrate bonding performance is improved. The Pd element is doped in the DLC thick film, so that the toughness can be obviously improved, the friction and wear resistance of the DLC can be further improved, and a matrix can be effectively protected. The amorphous structure of DLC eliminates the columnar crystal structure in the traditional PVD method, reduces the channel of the external corrosive ions invading the matrix, and obviously improves the corrosion resistance. Moreover, the amorphous carbon has good lubricating effect, and is very helpful for improving the corrosion resistance and the wear resistance of the magnesium alloy matrix.
FIG. 1 is the SEM cross-sectional morphology of a thick film of DLC. As can be seen from FIG. 1, the thick film had a uniform thickness and a dense structure, and the thickness of the deposited film was 157.2 μm for 5 hours.
FIG. 2 is HRTEM observation of a DLC thick film. The observation of an F20 transmission electron microscope shows that the DLC film prepared by the method has an amorphous carbon structure, and the DLC thick film prepared by the embodiment is proved to be a high-quality material.
FIG. 3 is an adhesion acoustic emission curve of a DLC thick film. As can be seen from FIG. 3, the DLC thick film prepared by the method of the present invention has a film-based bonding strength of more than 45N and a bonding strength of 157.2 μm thick film.
FIG. 4 is the electrochemical polarization curve of DLC thick film tested in 3.5% NaCl solution. As can be seen from FIG. 4, the etching potential of the DLC thick film prepared by the method of the present invention is-0.565V, and the etching current density is 5.82X 10 -8 A/cm 2 It is proved that the DLC thick film has excellent corrosion resistance.
FIG. 5 is a graph showing the coefficient of friction of a DLC thick film at room temperature and 30% relative humidity. As can be seen from FIG. 5, the DLC thick film has a small coefficient of friction, less than 0.035, exhibiting good wear resistance.
The experiments prove that the method for depositing the DLC thick film by the high-density plasma composite carbon source is a method for depositing the DLC thick film.
The foregoing is merely illustrative of the preferred embodiments of the present invention and is not to be construed as limiting the claims. The present invention is not limited to the above embodiments, and the specific structure thereof is allowed to vary. All changes which come within the scope of the invention as defined by the appended claims are intended to be embraced therein.

Claims (6)

1. A method for depositing a DLC thick film by using a high-density plasma composite carbon source is characterized by comprising the following steps: the method comprises the following steps:
1. pretreatment of a matrix: cutting and sampling a substrate, grinding the substrate by metallographic abrasive paper with different meshes, cleaning the substrate in an aqueous solution of oxalic acid, citric acid and sodium benzenesulfonate, and then cleaning the substrate in NaHCO 3 Soaking the neutralized residual acid in the solution, washing with deionized water twice, polishing, and ultrasonically cleaning the polished substrate in acetone, absolute ethyl alcohol and deionized water respectively;
2. preparing before coating: putting the substrate cleaned in the step one in N 2 Drying with cold air under air flow, placing into a magnetron sputtering vacuum chamber, checking the air tightness of the vacuum chamber, vacuumizing until the vacuum degree in the vacuum chamber is lower than 1 × 10 -3 Introducing argon gas, adjusting the air pressure in the vacuum chamber, starting a pulse power supply and a bias power supply, and carrying out sputtering cleaning and etching on the substrate;
3. preparing a Ti-Si transition buffer layer: introducing argon into the vacuum chamber, adopting a Ti-Si alloy target as a cathode, and preparing a transition buffer layer by using the alloy target through plasma magnetron sputtering under the action of pulse and bias voltage;
4. preparing a DLC thick film: introducing argon and propane, volatilizing toluene, conveying the toluene into a vacuum chamber, depositing and preparing a Pd element-doped DLC thick film on a Ti-Si transition buffer layer in a mixed atmosphere of argon, propane and toluene by adopting a method of pulse and bias voltage cooperated with magnetron sputtering of a palladium target, wherein the Pd doping proportion is controlled by pulse power;
5. aging and liquid nitrogen cooling: according to the method of the fourth step, after cooling the prepared DLC thick film to room temperature, taking out the DLC thick film from the vacuum chamber, aging for a period of time, putting the DLC thick film into liquid nitrogen for cooling for a moment, and taking out the DLC thick film;
in the second step, the pressure of the vacuum chamber for etching and cleaning the substrate by the Ar ions is 0.5 Pa-1.5 Pa, the bias voltage of the substrate is-500V-1500V, the power of the pulse power supply is 300-500W, the duty ratio is 20-70%, the Ar flow is 15-100sccm, and the etching and cleaning of the Ar ions are carried out for 5 min-30 min to obtain the substrate with a clean surface;
in the fourth step, the pulse power is 300-500W, the duty ratio is 20-70%, the bias voltage is-100 to-500V, the thickness of DLC is 120-220 mu m, and the deposition time is 4-7 h;
in the fourth step, the flow rate of Ar is 15-100 sccm, the flow rate of propane is 50-200 sccm, the flow rate of toluene is 50-200 sccm, the working pressure is 1.0-2.5Pa, the power of a pulse power supply for sputtering the Pd target is 50-300W, the duty ratio is 10-80%, the bias voltage is-50-200V, and the doping proportion of Pd is 10-50 wt%.
2. The method for depositing the DLC thick film by using the high-density plasma composite carbon source as claimed in claim 1, wherein the method comprises the following steps: the substrate in the first step can be any one metal of magnesium alloy, aluminum alloy, alloy steel or titanium alloy.
3. The method of claim 1, wherein the high-density plasma composite carbon source is used for depositing DLC thick film, and the method comprises the following steps: the concentration of oxalic acid, citric acid, sodium benzene sulfonate and sodium bicarbonate in the first step is 5-40 wt%; ultrasonic cleaning is carried out in acetone, absolute ethyl alcohol and deionized water for 10-30 min respectively, and the ultrasonic power is 100-200W.
4. The method for depositing the DLC thick film by using the high-density plasma composite carbon source as claimed in claim 1, wherein the method comprises the following steps: in the third step, the thickness of the Ti-Si transition buffer layer is 0.05-0.6 μm, the atomic percentage of Si element in the Ti-Si target is 5-95 at%, and the deposition time is 1-10 min.
5. The method of claim 1, wherein the high-density plasma composite carbon source is used for depositing DLC thick film, and the method comprises the following steps: in the third step, the pulse power is 300-500W, the duty ratio is 20-70%, the bias voltage is-100-500V, the Ar flow is 15-100 sccm, and the working air pressure is 0.5-1.5 Pa.
6. The method of claim 1, wherein the high-density plasma composite carbon source is used for depositing DLC thick film, and the method comprises the following steps: in the fifth step, the aging time is 10-90 h, the aging temperature is 15-30 ℃, and the liquid nitrogen is cooled for 5-30 s.
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CN110184564A (en) * 2019-07-02 2019-08-30 南昌航空大学 The preparation method of Mg alloy surface low stress, high bond strength Si/DLC thick film
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