CN110551979B - Silicon carbide surface modification method - Google Patents

Silicon carbide surface modification method Download PDF

Info

Publication number
CN110551979B
CN110551979B CN201910896598.XA CN201910896598A CN110551979B CN 110551979 B CN110551979 B CN 110551979B CN 201910896598 A CN201910896598 A CN 201910896598A CN 110551979 B CN110551979 B CN 110551979B
Authority
CN
China
Prior art keywords
modification
silicon
film
plated
nickel
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.)
Active
Application number
CN201910896598.XA
Other languages
Chinese (zh)
Other versions
CN110551979A (en
Inventor
白云立
王利
王刚
张继友
周于鸣
王永刚
孟晓辉
郭文
徐领娣
于建海
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.)
Beijing Institute of Space Research Mechanical and Electricity
Original Assignee
Beijing Institute of Space Research Mechanical and Electricity
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 Beijing Institute of Space Research Mechanical and Electricity filed Critical Beijing Institute of Space Research Mechanical and Electricity
Priority to CN201910896598.XA priority Critical patent/CN110551979B/en
Publication of CN110551979A publication Critical patent/CN110551979A/en
Application granted granted Critical
Publication of CN110551979B publication Critical patent/CN110551979B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

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
    • 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
    • C23C14/18Metallic material, boron or silicon on other inorganic substrates
    • 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
    • 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
    • C23C14/24Vacuum evaporation
    • 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
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/58After-treatment
    • C23C14/5826Treatment with charged particles
    • C23C14/5833Ion beam bombardment

Abstract

The invention relates to a silicon carbide surface modification method, which adopts PVD (physical vapor deposition) modification, and comprises the steps of cleaning a substrate, detecting the roughness before modification, putting the substrate into a clean coating machine, and putting coating materials of nickel (Ni) and silicon (Si) at corresponding positions of the coating machine; and (3) improving the vacuum degree in the vacuum chamber of the film coating machine, plating film material nickel (Ni) and film material silicon (Si) after the vacuum degree reaches the modification standard, and detecting the roughness after the modification is finished. Compared with the traditional PVD (physical vapor deposition) modification method, the method can directly reduce the surface roughness of the substrate, save the optical polishing process after modification, save the manpower, material resources and financial resources consumed in the optical polishing process, and avoid corresponding risks.

Description

Silicon carbide surface modification method
Technical Field
The invention relates to a SiC surface modification method, belongs to the technical field of optical equipment, and can be applied to the technical field of film optical preparation.
Background
SiC materials have gained widespread use in recent years in the aerospace field due to their good physical, mechanical and thermal properties. Due to many factors such as production process, material characteristics, component composition and the like, many micropores exist on the surface of SiC, and the surface compactness degree is far less than that of a glass material.
And (3) carrying out surface polishing on the SiC mirror blank with the defects of residual micropores and the like, wherein the limit range of the surface roughness after polishing is 3-4 nm, and at the moment, the optical polishing cannot further improve the surface precision and cannot meet the technical requirement of the surface roughness required by the reflector of the high-precision space camera. The surface scattering and the surface roughness are in positive correlation, if the SiC reflector is directly applied, a large amount of scattering can cause light energy loss of the space optical system, and meanwhile, the generated stray light can influence the imaging quality of the space optical system. In addition, since SiC has high hardness and chemical stability, it is difficult to directly machine it into a high-precision optical surface (mirror surface having a small RMS value).
In order to further improve the surface precision of the SiC reflector and obtain a high-precision SiC mirror blank, the SiC mirror blank needs to be subjected to surface modification treatment, and when the SiC mirror blank is modified by adopting a Physical Vapor Deposition (PVD) method, a dense modification layer Si with a certain thickness is essentially plated on the surface of the SiC mirror blank, and the thickness of the modification layer Si is generally more than 10 mu m, so that the surface defect is improved and the surface precision is improved. After the coating process of the modified layer is finished, the surface roughness of the SiC mirror blank is still high, even higher than the roughness before modification, and the modified layer on the surface of the SiC mirror blank needs to be subjected to optical cold processing, namely the surface of the mirror blank is subjected to optical precision grinding and polishing, so that a smooth surface with the roughness of about 1nm is finally obtained, and the requirement of a corresponding surface shape is met.
The traditional modification method has the following risks from the step of plating a modified layer to the step of polishing the modified layer:
sputtering points are easy to appear in the PVD modified coating process, and the sputtering points can be easy to become modified layer falling points in the polishing process, so that modification failure is caused;
the modified layer is thick, so that the time for plating the modified layer is long, the equipment and personnel are tested, and certain risks exist;
there is a risk of over-processing the modified layer during the optical polishing process and wearing through the modified layer. After the modified layer is worn, the modified layer needs to be plated again, and optical polishing is carried out again, so that the time and the labor are consumed, and the processing period is prolonged.
Disclosure of Invention
The technical problem solved by the invention is as follows: the defect that the surface roughness is unchanged or increased after the traditional silicon carbide surface modification is overcome, and the silicon carbide surface modification method is provided, so that the problems that after the traditional modification method is finished, the roughness needs to be reduced by continuous polishing, and time and labor are consumed are solved.
The technical scheme of the invention is as follows: a silicon carbide surface modification method comprises the following steps:
1) selecting coating materials of nickel and silicon, and respectively placing the coating materials in a coating machine evaporation-resistant boat and a crucible;
2) vacuumizing, and starting heating when the vacuum degree reaches high vacuum;
3) when the temperature T is reached, nickel is plated;
4) keeping the temperature T, and continuously plating silicon;
5) after the two coatings are plated, the coating is bombarded by an ion source.
The high vacuum degree is less than or equal to 3x10-3Pa。
The T is 290-310 ℃.
The T is 300 DEG C
The thickness of the nickel plated in the step 3) is 25nm-30 nm.
The thickness of the plated silicon in the step 4) is 700nm-900 nm.
The bombardment time is 4-6 minutes.
The ion source bombardment time was 5 minutes.
The ion source working parameters are 120V and 150 mA.
The distance d between each evaporation source of the film plating machine and the plated piece is less than 1 m.
Compared with the prior art, the invention has the advantages that:
(1) according to the invention, two coating materials are selected, and proper coating process parameters are applied, so that the roughness of the surface of the silicon carbide is reduced, the surface scattering is inhibited, the surface precision is improved, the optical grinding and polishing processing of the substrate is not required, and the time and the labor are saved;
(2) the traditional modification technology needs to plate a thicker modified layer on a substrate to cover the surface defects. In the existing method, two modification layers are selected, so that the surface roughness of SiC meets the precision requirement of directly plating a reflective film, and meanwhile, the thickness of a plated film material is much thinner than that required by conventional modification, so that some risks of conventional modification, such as abrasion of elements of a film plating machine, occurrence of splash points and the like, are avoided, and the success rate of modification is greatly increased;
(3) the traditional method for modifying the silicon carbide surface relates to a subsequent optical polishing process, and the method skips the optical polishing process after SiC modification, thereby saving a large amount of related resources such as manpower, material resources, financial resources and the like to a great extent and avoiding related risks of the optical polishing.
Drawings
FIG. 1 is a schematic view of a film structure;
FIG. 2 is a schematic view of a coating process;
FIG. 3 is a schematic diagram of roughness before coating;
FIG. 4 is a schematic diagram of roughness after plating.
Detailed Description
The invention avoids the risk in the process of plating the modified layer, skips the subsequent polishing optical processing process, and provides a novel method for plating the modified silicon carbide surface by utilizing a film material growth and refinement interaction mechanism, thereby finally obtaining the high-precision optical mirror surface of the SiC mirror blank. Nickel (Ni) and silicon (Si) are deposited on the surface of the unmodified silicon carbide by using a thermal evaporation process, and the structural design of the film layer is shown in fig. 1. The essence is that the growth of the silicon carbide surface in the holes is completed by utilizing the growth characteristics of the material, so that the purpose of filling the holes is achieved, meanwhile, the interaction of the film materials has a refining mechanism, so that the surface roughness is reduced, the surface scattering after film coating is inhibited, the surface modification of the SiC mirror blank is completed, and the surface precision of the SiC reflector is improved.
The invention utilizes a film material growth mechanism, selects film materials of nickel (Ni) and silicon (Si), designs a related film system, adjusts film coating parameters including film thickness, ion source parameters and other data, and a film coating process schematic diagram of each working element placing machine in a film coating machine is shown in figure 2, wherein the specific design method comprises the following steps:
(1) cleaning the substrate, and testing the substrate before roughness coating, wherein the test result is shown in figure 3;
(2) selecting film material nickel (Ni) and film material silicon (Si);
(3) placing film material nickel (Ni) on a steaming-resistant boat;
(4) placing film material silicon (Si) in an electron gun 1;
(5) vacuumizing, and when the vacuum degree reaches 3x10 according to the actual state of the film coating machine-3Heating is started when the pressure is Pa;
(6) when the temperature reaches 300 ℃, firstly plating nickel (Ni) with the thickness of 30 nm;
(7) keeping the temperature at 300 ℃, and continuously plating silicon (Si) with the thickness of 800 nm;
(8) after the two coatings are plated, bombarding for 5 minutes by an ion source with working parameters of 120V and 150 mA.
(9) And after the coating is finished, carrying out roughness detection on the substrate, wherein the test result is shown in figure 4.
The basic principle of the vacuum degree required by PVD coating is that the mean free path of gas molecules is larger than the distance between an evaporation source and a piece to be coated. According to the gas molecule motion theory, the gas molecule mean free path:
Figure BDA0002210421930000041
where σ is the gas molecule diameter, n is the density of the gas molecules, p is the gas pressure corresponding to n, and if the distance d from the evaporation source to the article to be plated is 1m, the degree of vacuum required for determining PVD should be such that
Figure BDA0002210421930000042
The distance d between each evaporation source of the film plating machine and the plated piece is less than 1m, and the vacuum degree is 3x10-3And (3) coating a film layer when the pressure is Pa, so that the theoretical design requirement is met.
The high temperature is as follows:
1) removing residual gas adsorbed on the surface of the substrate to increase the binding force between the substrate and deposited molecules;
2) the physical adsorption of the film layer is promoted to be converted into chemical adsorption, the action among molecules is enhanced, the film layer is compact, the adhesive force is increased, and the mechanical capacity is improved;
3) the difference between the crystallization temperature of vapor molecules and the temperature of the substrate is reduced, the film layer concentration is improved, the film layer hardness is increased, and the internal stress is eliminated.
The film structure change or the film material decomposition can be caused by overhigh temperature, the good interaction between the film materials is reduced, and the final temperature is selected to be 300 ℃ through experimental verification.
The SiC substrate adopting the new modification method is subjected to roughness test at the same position of the substrate before and after modification, and the test result shows that the distance between the highest point and the lowest point of the surface of the substrate before modification is 62.69+ 89.45-152.14 nm, the distance between the highest point and the lowest point of the surface after modification is 47.30+ 45.39-92.69 nm, the PV value of the surface of the substrate is reduced, which shows that the surface of the substrate tends to be smoother and the roughness is reduced. Test results show that the new modification method is adopted, namely after the surface of the SiC substrate is plated with film materials of nickel (Ni) and silicon (Si), the surface roughness of the SiC substrate is reduced, and the roughness reaches the precision requirement of plating a reflector; the scattering is suppressed; various resources required by the optical polishing process are saved.
The method overcomes the defect that the surface roughness is unchanged or increased after the traditional silicon carbide surface is modified, and solves the problems that the traditional modification method needs to continuously grind and polish to reduce the roughness and is time-consuming and labor-consuming.
The invention is not described in detail and is within the knowledge of a person skilled in the art.

Claims (1)

1. A silicon carbide surface modification method is characterized by comprising the following steps:
1) selecting film materials of nickel and silicon, and respectively placing the film materials in a film plating machine evaporation-resistant boat and an electronic crucible;
2) vacuumizing, and starting heating when the vacuum degree reaches high vacuum;
3) when the temperature T is reached, nickel is plated;
4) keeping the temperature T, and continuously plating silicon;
5) after the two kinds of film materials are plated, bombarding by an ion source;
the high vacuum degree is less than or equal to 3x10-3Pa;
The T is 290-310 ℃;
the thickness of the nickel plated in the step 3) is 25nm-30 nm;
the thickness of the plated silicon in the step 4) is 700nm-900 nm;
the bombardment time of the ion source is 4-6 minutes;
the working parameters of the ion source are 120V and 150 mA;
the distance d between each evaporation source of the film plating machine and the plated piece is less than 1 m.
CN201910896598.XA 2019-09-23 2019-09-23 Silicon carbide surface modification method Active CN110551979B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201910896598.XA CN110551979B (en) 2019-09-23 2019-09-23 Silicon carbide surface modification method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201910896598.XA CN110551979B (en) 2019-09-23 2019-09-23 Silicon carbide surface modification method

Publications (2)

Publication Number Publication Date
CN110551979A CN110551979A (en) 2019-12-10
CN110551979B true CN110551979B (en) 2021-04-13

Family

ID=68741240

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201910896598.XA Active CN110551979B (en) 2019-09-23 2019-09-23 Silicon carbide surface modification method

Country Status (1)

Country Link
CN (1) CN110551979B (en)

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0868897A (en) * 1994-08-29 1996-03-12 Nikon Corp Reflection mirror and its production method
CN101315435A (en) * 2007-06-01 2008-12-03 哈尔滨工业大学 High reflection film of silicon carbide reflection mirror within visible light wave range, and its production method
CN101470223A (en) * 2007-12-26 2009-07-01 中国科学院大连化学物理研究所 Method for fabricating RB-SiC ultra-smooth surface reflection mirror through surface modification technology
CN102094179A (en) * 2010-12-30 2011-06-15 中国科学院长春光学精密机械与物理研究所 RB-SiC base reflector surface modified layer structure and preparation method thereof
CN105970169A (en) * 2016-06-01 2016-09-28 南京施密特光学仪器有限公司 Low temperature preparation method for space silicon carbide reflector module modified layer
CN107400868A (en) * 2017-07-18 2017-11-28 中国科学院长春光学精密机械与物理研究所 Improve the method for heavy caliber silicon carbide mirror Si modification layer surface microdefect
CN107813191A (en) * 2017-10-27 2018-03-20 中国科学院国家天文台南京天文光学技术研究所 The processing method of polyether-ether-ketone optical mirror
JP2018171914A (en) * 2017-03-30 2018-11-08 日東電工株式会社 Heat-shielding and heat-insulating film

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0868897A (en) * 1994-08-29 1996-03-12 Nikon Corp Reflection mirror and its production method
CN101315435A (en) * 2007-06-01 2008-12-03 哈尔滨工业大学 High reflection film of silicon carbide reflection mirror within visible light wave range, and its production method
CN101470223A (en) * 2007-12-26 2009-07-01 中国科学院大连化学物理研究所 Method for fabricating RB-SiC ultra-smooth surface reflection mirror through surface modification technology
CN102094179A (en) * 2010-12-30 2011-06-15 中国科学院长春光学精密机械与物理研究所 RB-SiC base reflector surface modified layer structure and preparation method thereof
CN105970169A (en) * 2016-06-01 2016-09-28 南京施密特光学仪器有限公司 Low temperature preparation method for space silicon carbide reflector module modified layer
JP2018171914A (en) * 2017-03-30 2018-11-08 日東電工株式会社 Heat-shielding and heat-insulating film
CN107400868A (en) * 2017-07-18 2017-11-28 中国科学院长春光学精密机械与物理研究所 Improve the method for heavy caliber silicon carbide mirror Si modification layer surface microdefect
CN107813191A (en) * 2017-10-27 2018-03-20 中国科学院国家天文台南京天文光学技术研究所 The processing method of polyether-ether-ketone optical mirror

Also Published As

Publication number Publication date
CN110551979A (en) 2019-12-10

Similar Documents

Publication Publication Date Title
US11339468B2 (en) Magnetron sputtering scanning method for modifying silicon carbide optical reflector surface and improving surface profile
JP7426386B2 (en) Thick, low stress tetrahedral amorphous carbon coating
CN109402564B (en) AlCrSiN and AlCrSiON double-layer nano composite coating and preparation method thereof
CN111304602B (en) Super-hydrophobic diamond-like composite layer structure and preparation method thereof
CN112281125B (en) Composite metal film and preparation method and application thereof
JP6364685B2 (en) Piston ring and manufacturing method thereof
US11339100B2 (en) Graded coating of element diffusion inhibition and adhesion resistance on mold for glass molding
CN106011752B (en) A kind of preparation method of metal hard films
WO2015068776A1 (en) Method for forming intermediate layer formed between substrate and dlc film, method for forming dlc film, and intermediate layer formed between substrate and dlc film
CN110551979B (en) Silicon carbide surface modification method
TW201339331A (en) Coated article and method for making same
US20180267476A1 (en) Timepiece part, and timepiece
CN111139431A (en) Middle frame of electronic equipment, manufacturing method of middle frame and electronic equipment
CN110735107A (en) Ion surface etching method before preparation of diamond-like coating
CN107400868A (en) Improve the method for heavy caliber silicon carbide mirror Si modification layer surface microdefect
CN105755429A (en) Method for preparing cellphone screen scratch-resistant aluminum oxide coating by ion beam dual-filtering deposition technique
US7722788B2 (en) Mold inserts
CN110106470B (en) Preparation method of low-stress diamond-like carbon film
Wang et al. Deposition and application of CVD diamond films on the interior-hole surface of silicon carbide compacting dies
TW201118050A (en) A high temperature pretreatment method on surface of glass substrate for anti-reflection film
JP5082114B2 (en) Manufacturing method of carrier for holding object to be polished
CN110760798A (en) Electronic product shell and preparation method thereof
CN113549887B (en) Infrared reflection composite coating and preparation method and application thereof
JPS6137230B2 (en)
JP2003089548A (en) Method for manufacturing windshield for timepiece

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