CN116926484A - Processing technology of zirconium yttrium chromium alloy sputtering target material - Google Patents

Processing technology of zirconium yttrium chromium alloy sputtering target material Download PDF

Info

Publication number
CN116926484A
CN116926484A CN202310979383.0A CN202310979383A CN116926484A CN 116926484 A CN116926484 A CN 116926484A CN 202310979383 A CN202310979383 A CN 202310979383A CN 116926484 A CN116926484 A CN 116926484A
Authority
CN
China
Prior art keywords
sputtering target
yttrium
zirconium
alloy sputtering
chromium alloy
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
CN202310979383.0A
Other languages
Chinese (zh)
Other versions
CN116926484B (en
Inventor
张凤戈
张学华
魏铁峰
张欠男
岳万祥
施政
孟晓亭
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.)
At&m Six Nine Materials Co ltd
Zhuozhou Antai Liujiu New Material Technology Co ltd
Suzhou Liujiu New Material Technology Co ltd
Original Assignee
At&m Six Nine Materials Co ltd
Zhuozhou Antai Liujiu New Material Technology Co ltd
Suzhou Liujiu New Material Technology Co ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by At&m Six Nine Materials Co ltd, Zhuozhou Antai Liujiu New Material Technology Co ltd, Suzhou Liujiu New Material Technology Co ltd filed Critical At&m Six Nine Materials Co ltd
Priority to CN202310979383.0A priority Critical patent/CN116926484B/en
Publication of CN116926484A publication Critical patent/CN116926484A/en
Application granted granted Critical
Publication of CN116926484B publication Critical patent/CN116926484B/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
    • 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
    • C23C14/3407Cathode assembly for sputtering apparatus, e.g. Target
    • C23C14/3414Metallurgical or chemical aspects of target preparation, e.g. casting, powder metallurgy
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D7/00Casting ingots, e.g. from ferrous metals
    • B22D7/005Casting ingots, e.g. from ferrous metals from non-ferrous metals
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/02Making non-ferrous alloys by melting
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C16/00Alloys based on zirconium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/16Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of other metals or alloys based thereon
    • C22F1/18High-melting or refractory metals or alloys based thereon
    • C22F1/186High-melting or refractory metals or alloys based thereon of zirconium or alloys based thereon
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E30/00Energy generation of nuclear origin
    • Y02E30/30Nuclear fission reactors

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Physical Vapour Deposition (AREA)

Abstract

The application relates to the technical field of sputtering target material processing, and particularly discloses a processing technology of a zirconium yttrium chromium alloy sputtering target material. The processing technology comprises the following steps: mixing 72.5-79 parts by weight of zirconium blocks, 16-22 parts by weight of yttrium blocks and 2.5-7.5 parts by weight of chromium blocks to obtain a mixture; under the protection of inert gas and electromagnetic stirring, heating and melting the mixture to obtain a metal mixed solution; pouring the metal mixed solution in an ingot mould, removing the ingot mould, and cooling to room temperature to obtain an alloy ingot; and carrying out heat treatment on the alloy ingot to obtain the zirconium yttrium chromium alloy sputtering target material. The zirconium yttrium chromium alloy sputtering target material obtained by the processing technology has the advantages of average grain size less than 50 mu m and yttrium processing loss rate less than 5%, ensures the yttrium content in the zirconium yttrium chromium alloy sputtering target material, reduces yttrium resource waste, has the advantages of high compactness, no air hole, no segregation, no crack, uniform structure and easy processing, and meets the market demand.

Description

Processing technology of zirconium yttrium chromium alloy sputtering target material
Technical Field
The application relates to the technical field of sputtering target material processing, in particular to a processing technology of a zirconium yttrium chromium alloy sputtering target material.
Background
The engine is used as a power machine and is widely applied to the fields of aviation, power generation, transportation and the like. Turbine blades of an engine often handle high temperature environments during operation, where the turbine blades are subjected not only to significant mechanical loads, but also to high temperature oxidation and hot corrosion. In order to increase the service life of the turbine blade and ensure the normal operation of the engine, a thermal insulation coating is often coated on the surface of the turbine blade. The yttria-stabilized zirconia thermal insulation coating has the characteristics of good stability, low heat conductivity coefficient, good oxidation resistance and excellent wear resistance at high temperature, and has been applied to turbine blades. The heat-insulating coating is generally processed by adopting a zirconium yttrium alloy sputtering target material, and the heat-insulating coating is sprayed on the surface of the turbine blade in a sputtering mode, so that the quality of the zirconium yttrium alloy sputtering target material is the basis for ensuring the heat-insulating coating.
Zirconium and yttrium alloy sputtering target materials are generally obtained by mixing zirconium blocks and yttrium blocks, melting and casting. However, the applicant finds that in practical processing, the melting temperature of the zirconium block and the yttrium block is high, and at high temperature, metal yttrium is easy to volatilize, so that yttrium resource is wasted, and the content of yttrium in the zirconium yttrium alloy sputtering target material is influenced.
Disclosure of Invention
In order to reduce volatilization of yttrium in the zirconium yttrium alloy sputtering target processing process, the application provides a processing technology of a zirconium yttrium chromium alloy sputtering target, which adopts the following technical scheme:
a processing technology of a zirconium yttrium chromium alloy sputtering target material comprises the following steps:
s1, mixing 72.5-79 parts by weight of zirconium blocks, 16-22 parts by weight of yttrium blocks and 2.5-7.5 parts by weight of chromium blocks to obtain a mixture;
s2, under the protection of inert gas and electromagnetic stirring, heating and melting the mixture to obtain a metal mixed solution;
s3, pouring the metal mixed solution in an ingot mould, removing the ingot mould, and cooling to room temperature to obtain an alloy ingot;
and S4, performing heat treatment on the alloy ingot to obtain the zirconium yttrium chromium alloy sputtering target material.
By adopting the technical scheme, the obtained zirconium yttrium chromium alloy sputtering target material has the average grain size smaller than 50 mu m, and has the advantages of high density, no air hole, no segregation, no crack, uniform structure and easy processing, and meets the market demand.
In the zirconium yttrium chromium alloy sputtering target material processing, chromium blocks are added into zirconium blocks and yttrium blocks to obtain a mixture, and further a metal mixed solution is obtained. Chromium in the metal mixed solution can play a role in stabilizing yttrium, reduce the oxidation and volatilization of yttrium, and reduce the volatilization of yttrium by being matched with the inert gas protection in the step S2. According to the processing technology, through mutual matching of the steps, the yttrium processing loss rate is reduced and is less than 5%, so that the yttrium content in the zirconium yttrium chromium alloy sputtering target material is ensured, the yttrium resource waste is reduced, and the processing stability of the zirconium yttrium chromium alloy sputtering target material is improved.
Meanwhile, the application also limits the addition amount of the chromium blocks, thereby realizing the limit of the chromium element content in the zirconium yttrium chromium alloy sputtering target material, reducing the influence of the chromium element content on the stabilization of yttrium, and reducing the influence of the chromium element content on the performance of the thermal insulation coating. And when the addition amount of the chromium blocks is 2.5-7.5 parts by weight, the yttrium can play a good role in stabilizing yttrium, the performance of the thermal insulation coating cannot be influenced, and the market demand is met.
Optionally, in step S2, the temperature is raised to 1750-1900 ℃ and the temperature is raised to melt for 45-60min.
By adopting the technical scheme, the temperature rise and melting temperature and the temperature rise and melting time are optimized, so that the zirconium block, the yttrium block and the chromium block can form a metal mixed solution conveniently.
Optionally, the inert gas is argon, and the pressure of the argon is 0.03-0.09MPa.
By adopting the technical scheme, the pressure of argon is optimized, volatilization of yttrium in the metal mixed solution is reduced, yttrium content in the zirconium yttrium chromium alloy sputtering target material is ensured, and processing stability of the zirconium yttrium chromium alloy sputtering target material is improved.
In various embodiments, the pressure of the argon gas is 0.06MPa, which may also be set to 0.03MPa, 0.04MPa, 0.05MPa, 0.07MPa, 0.08MPa, 0.09MPa, etc., as desired.
Optionally, in step S2, the frequency of the electromagnetic stirring is 8-12Hz.
By adopting the technical scheme, the zirconium block, the yttrium block and the chromium block can increase the uniformity of raw material mixing and improve the uniformity of yttrium in the zirconium yttrium chromium alloy sputtering target material through electromagnetic stirring.
In various embodiments, the frequency of the electromagnetic stirring is 10Hz, which may also be set to 8Hz, 9Hz, 11Hz, 12Hz, etc., as desired.
Optionally, the temperature of the ingot mould is 890-910 ℃.
By adopting the technical scheme, the ingot mould is preheated to 890-910 ℃, so that the moisture and volatile matters in the ingot mould can be effectively removed, and the influence of sundries is reduced. And when the metal mixed solution is poured and cooled, the temperature of the ingot mould is firstly reduced and then reduced to the room temperature, so that the cooling gradient of the metal mixed solution is effectively reduced, the metal mixed solution can be fed better, the utilization rate is increased, the situation that an alloy ingot is cracked due to the fact that the metal mixed solution is rapidly cooled to the room temperature is reduced, and the performance of the zirconium-yttrium-chromium alloy sputtering target is also improved.
In various embodiments, the temperature of the ingot mold is 900 ℃, which may also be set to 890 ℃, 895 ℃, 905 ℃, 910 ℃, etc., as desired.
In step S3, the metal mixed solution is poured into an ingot mould, and then is subjected to heat preservation treatment for 10-30min, and then the ingot mould is removed. In various embodiments, the incubation time is 20 minutes, which may also be set to 10 minutes, 15 minutes, 25 minutes, 30 minutes, etc., as desired.
Optionally, the ingot mould is a graphite crucible, and an antioxidation layer is arranged on the surface of the graphite crucible.
Optionally, the antioxidation layer is a yttrium oxide layer.
When the metal mixture is poured in the graphite crucible, if the metal mixture is in direct contact with the graphite crucible, a reaction may occur, thereby corroding the graphite crucible and forming metal carbide. Therefore, an oxidation-resistant layer is provided on the surface of the graphite crucible. The oxidation resistant layer is arranged as an yttrium oxide layer, so that the corrosion of the metal mixed liquid to the graphite crucible can be reduced, the temperature of the metal mixed liquid can be adapted, and the casting of the metal mixed liquid is facilitated.
Optionally, in step S4, the heat treatment of the alloy ingot specifically includes: and heating the alloy ingot to 840-850 ℃, carrying out heat preservation treatment for 2-4h, quickly cooling to 290-310 ℃, and then cooling to room temperature, thereby obtaining the zirconium yttrium chromium alloy sputtering target.
By adopting the technical scheme, the alloy ingot is heated to 840-850 ℃ so that the crystal grains of the alloy ingot are enlarged, and the uniformity of yttrium in the alloy ingot can be effectively improved. And the grains become larger, the performance of the zirconium yttrium chromium alloy sputtering target is reduced, and the preparation of the thermal insulation coating is not facilitated. Therefore, the alloy ingot is further cooled rapidly from 840-850 ℃ to 290-310 ℃ by rapid cooling, the quenching effect is achieved, the grains are effectively refined, the grains are reduced, the performance of the zirconium yttrium chromium alloy sputtering target is improved, and the preparation of the thermal insulation coating is facilitated.
Optionally, in step S4, the cooling rate of the cooling is 550-560 ℃/min.
When the cooling rate is too slow, the effect of refining the crystal grains of the alloy ingot is affected, and even the effect of refining the crystal grains cannot be achieved; when the cooling rate is too fast, the alloy ingot may have larger internal stress, causing cracking of the alloy ingot. And when the cooling rate is 550-560 ℃/min, the zirconium yttrium chromium alloy sputtering target material can be cooled rapidly, grains can be effectively refined, the average grain size is less than 15 mu m, and the performance of the zirconium yttrium chromium alloy sputtering target material is improved.
In various embodiments, the cooling rate is 555 ℃/min, which may also be set to 550 ℃/min, 560 ℃/min, etc., as desired.
Optionally, in step S4, the temperature rising rate of the temperature rising is 8-12 ℃/min.
By adopting the technical scheme, the heating rate is optimized, the equipment investment cost is reduced because the heating rate is too fast, and the processing efficiency is also reduced because the heating rate is too slow.
In various embodiments, the heating rate is 10deg.C/min, which may also be set to 8deg.C/min, 9deg.C/min, 11deg.C/min, 12deg.C/min, etc., as desired.
In summary, the application has the following beneficial effects:
the zirconium yttrium chromium alloy sputtering target material obtained by the processing technology has the average grain size of less than 50 mu m, has the advantages of high compactness, no air holes, no segregation, no cracks, uniform structure and easy processing, ensures the yttrium content in the zirconium yttrium chromium alloy sputtering target material, reduces the yttrium resource waste, and improves the processing stability of the zirconium yttrium chromium alloy sputtering target material in the processing process, wherein the yttrium processing loss rate is less than 5%.
Detailed Description
In order that the application may be more readily understood, the application will be further described in detail with reference to the following examples, which are given by way of illustration only and are not limiting in scope of application. The starting materials or components used in the present application may be prepared by commercial or conventional methods unless specifically indicated.
Examples
Table 1 content of each raw material of the mixture (unit: 10 g)
Examples Example 1 Example 2 Example 3 Example 4 Example 5 Example 6
Zirconium block 75 79 77 73 77.5 72.5
Yttrium block 20 16 18 22 20 20
Chromium block 5 5 5 5 2.5 7.5
Totals to 100 100 100 100 100 100
Example 1
A processing technology of a zirconium yttrium chromium alloy sputtering target material comprises the following steps:
s1, adding yttrium blocks and chromium blocks into zirconium blocks, and stirring for 10min to obtain a mixture.
The proportions of the raw materials of the zirconium block, the yttrium block and the chromium block are shown in table 1.
S2, adding the mixture into a vacuum induction melting furnace, starting electromagnetic stirring, wherein the frequency of the electromagnetic stirring is 10Hz, vacuumizing and introducing argon to ensure that the pressure of the argon is 0.06MPa, and then heating to 1800 ℃ for melting treatment for 45min to obtain a metal mixed solution.
And S3, pouring the metal mixed solution in an ingot mould with the temperature of 900 ℃, carrying out heat preservation treatment for 20min, removing the ingot mould, and cooling to 25 ℃ to obtain an alloy ingot which is a cylinder with the diameter of 165mm.
The ingot mould is a graphite crucible, an antioxidation layer is arranged on the surface of the graphite crucible, and the antioxidation layer is an yttrium oxide layer.
S4, heating the alloy ingot to 845 ℃ at a heating rate of 10 ℃/min, and carrying out heat preservation treatment for 3 hours. Then rapidly cooling to 300 ℃ at a cooling rate of 555 ℃/min. And then cooling to 25 ℃ to obtain the zirconium yttrium chromium alloy sputtering target.
Examples 2 to 6
The difference between the processing technology of the zirconium yttrium chromium alloy sputtering target material and the embodiment 1 is that in the step S1, the raw material proportions of the zirconium block, the yttrium block and the chromium block are different, and the raw material proportions of the zirconium block, the yttrium block and the chromium block are shown in the table 1.
Example 7
The processing technology of the zirconium yttrium chromium alloy sputtering target material is different from that of the embodiment 1 in that in the step S2, the temperature rise and melting temperature are 1750 ℃.
Example 8
The processing technology of the zirconium yttrium chromium alloy sputtering target material is different from that of the embodiment 1 in that in the step S2, the temperature rise and melting temperature is 1900 ℃.
Example 9
The processing technology of the zirconium yttrium chromium alloy sputtering target material is different from that of the embodiment 1 in that in the step S2, the temperature rising and melting time is 60min.
Example 10
The processing technology of the zirconium yttrium chromium alloy sputtering target material is different from that of the embodiment 1 in that in the step S3, the temperature of the ingot mould is 800 ℃.
Example 11
The processing technology of the zirconium yttrium chromium alloy sputtering target material is different from that of the embodiment 1 in that in the step S4, the temperature of heating is 800 ℃.
Example 12
The processing technology of the zirconium yttrium chromium alloy sputtering target material is different from that of the embodiment 1 in that in the step S4, the cooling rate of cooling is 400 ℃/min.
Example 13
The processing technology of the zirconium yttrium chromium alloy sputtering target material is different from that of the embodiment 1 in that in the step S4, the cooling rate of cooling is 300 ℃/min.
Comparative example
Comparative example 1
The processing technology of the zirconium yttrium chromium alloy sputtering target material is different from that of the embodiment 1 in that in the step S1, the raw material proportions of the zirconium block, the yttrium block and the chromium block are different, and the weight proportions of the zirconium block, the yttrium block and the chromium block are 80:20:0, namely, the chromium block is not added.
Performance detection
(1) Zirconium yttrium chromium alloy sputtering targets obtained in examples 1 to 9 and comparative example 1 were taken as test samples, and yttrium content in the test samples was detected, and the detection results are shown in table 2.
Wherein the yttrium addition amount is the yttrium addition amount in the mixture; the yttrium content is the yttrium content in the zirconium yttrium chromium alloy sputtering target material; the yttrium processing loss rate is the loss rate in the process of processing yttrium blocks into zirconium yttrium chromium alloy sputtering targets, and the yttrium processing loss rate=yttrium addition amount-yttrium content.
(1) The zirconium yttrium chromium alloy sputtering targets obtained in examples 1 to 13 and comparative example 1 were each taken as a sample, and the average grain size of the samples was examined, and the examination results are shown in table 2.
TABLE 2 detection results
Note that: "/" indicates undetected.
As can be seen from Table 2, the zirconium yttrium chromium alloy sputtering target material obtained by the processing technology has lower yttrium processing loss rate in the processing process, and the yttrium processing loss rate is 4.28-4.56%, so that the yttrium content in the zirconium yttrium chromium alloy sputtering target material is ensured, the yttrium resource waste is reduced, and the processing stability of the zirconium yttrium chromium alloy sputtering target material is improved. Meanwhile, the zirconium yttrium chromium alloy sputtering target material also has good average grain size which is 13.24-47.49 mu m, especially in examples 1-9, and the average grain size is 13.24-13.52 mu m, so that the zirconium yttrium chromium alloy sputtering target material has the advantages of high compactness, no air holes, no segregation and uniform structure, and meets the market demand.
Comparing example 1 with example 10, it can be seen that the temperature of the ingot mold in step S3 has a certain effect on the average grain size of the zirconium yttrium chromium alloy sputtering target, and the average grain size is smaller when the temperature of the ingot mold is 890-910 ℃. By combining with example 11, it can be seen that the temperature of the alloy ingot in step S4 also has a certain effect on the average grain size of the zirconium yttrium chromium alloy sputtering target, and the temperature of the alloy ingot is 840-850 ℃, so that the zirconium yttrium chromium alloy sputtering target exhibits better performance.
Comparing example 1 with examples 12-13, it can be seen that the average grain size of the zirconium yttrium chromium alloy sputtering target increases with decreasing cooling rate, and the average grain size is less than 15 μm at a cooling rate of 550-560 ℃/min, which shows better performance.
It should be noted that the above-described embodiments are only for explaining the present application and do not constitute any limitation of the present application. The application has been described with reference to exemplary embodiments, but it is understood that the words which have been used are words of description and illustration, rather than words of limitation. Modifications may be made to the application as defined in the appended claims, and the application may be modified without departing from the scope and spirit of the application. Although the application is described herein with reference to particular means, materials and embodiments, the application is not intended to be limited to the particulars disclosed herein, as the application extends to all other means and applications which perform the same function.

Claims (10)

1. A processing technology of a zirconium yttrium chromium alloy sputtering target material is characterized in that: the method comprises the following steps:
s1, mixing 72.5-79 parts by weight of zirconium blocks, 16-22 parts by weight of yttrium blocks and 2.5-7.5 parts by weight of chromium blocks to obtain a mixture;
s2, under the protection of inert gas and electromagnetic stirring, heating and melting the mixture to obtain a metal mixed solution;
s3, pouring the metal mixed solution in an ingot mould, removing the ingot mould, and cooling to room temperature to obtain an alloy ingot;
and S4, performing heat treatment on the alloy ingot to obtain the zirconium yttrium chromium alloy sputtering target material.
2. The process for manufacturing a zirconium yttrium chromium alloy sputtering target according to claim 1, wherein the process comprises the following steps: in the step S2, the temperature is raised to be between 1750 and 1900 ℃ and the temperature is raised to be between 45 and 60 minutes.
3. The process for manufacturing a zirconium yttrium chromium alloy sputtering target according to claim 1, wherein the process comprises the following steps: the inert gas is argon, and the pressure of the argon is 0.03-0.09MPa.
4. The process for manufacturing a zirconium yttrium chromium alloy sputtering target according to claim 1, wherein the process comprises the following steps: in step S2, the frequency of electromagnetic stirring is 8-12Hz.
5. The process for manufacturing a zirconium yttrium chromium alloy sputtering target according to claim 1, wherein the process comprises the following steps: the temperature of the ingot mould is 890-910 ℃.
6. The process for manufacturing a zirconium yttrium chromium alloy sputtering target according to claim 1, wherein the process comprises the following steps: the ingot mould is a graphite crucible, and an antioxidation layer is arranged on the surface of the graphite crucible.
7. The process for manufacturing a zirconium yttrium chromium alloy sputtering target according to claim 6, wherein the process comprises the following steps: the antioxidation layer is a yttrium oxide layer.
8. The process for manufacturing a zirconium yttrium chromium alloy sputtering target according to claim 1, wherein the process comprises the following steps: in step S4, the heat treatment of the alloy ingot specifically includes: and heating the alloy ingot to 840-850 ℃, carrying out heat preservation treatment for 2-4h, quickly cooling to 290-310 ℃, and then cooling to room temperature, thereby obtaining the zirconium yttrium chromium alloy sputtering target.
9. The process for manufacturing a zirconium yttrium chromium alloy sputtering target according to claim 8, wherein the process comprises the following steps: in the step S4, the cooling rate of cooling is 550-560 ℃/min.
10. The process for manufacturing a zirconium yttrium chromium alloy sputtering target according to claim 8, wherein the process comprises the following steps: in the step S4, the temperature rising rate of the temperature rising is 8-12 ℃/min.
CN202310979383.0A 2023-08-05 2023-08-05 Processing technology of zirconium yttrium chromium alloy sputtering target material Active CN116926484B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202310979383.0A CN116926484B (en) 2023-08-05 2023-08-05 Processing technology of zirconium yttrium chromium alloy sputtering target material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202310979383.0A CN116926484B (en) 2023-08-05 2023-08-05 Processing technology of zirconium yttrium chromium alloy sputtering target material

Publications (2)

Publication Number Publication Date
CN116926484A true CN116926484A (en) 2023-10-24
CN116926484B CN116926484B (en) 2024-01-30

Family

ID=88380679

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202310979383.0A Active CN116926484B (en) 2023-08-05 2023-08-05 Processing technology of zirconium yttrium chromium alloy sputtering target material

Country Status (1)

Country Link
CN (1) CN116926484B (en)

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5335717A (en) * 1992-01-30 1994-08-09 Howmet Corporation Oxidation resistant superalloy castings
CN1153446A (en) * 1995-12-29 1997-07-02 黄安荣 Electrothermal lanthanum chromate body and its mfg. method
JP2003301262A (en) * 2002-04-10 2003-10-24 Sumitomo Metal Mining Co Ltd Ferroelectric thin film, and sputtering target material for forming ferroelectric thin film
KR20070082401A (en) * 2006-02-16 2007-08-21 학교법인 포항공과대학교 Ferritic type stainless steel containing yttrium
CN101629276A (en) * 2009-08-05 2010-01-20 中国核动力研究设计院 Zirconium-yttrium alloy target preparation method
US20120114975A1 (en) * 2010-11-05 2012-05-10 Solar Applied Materials Technology Corp. Sputtering Targets And Recording Materials Of Hard Disk Formed From The Sputtering Target
CN103270190A (en) * 2010-12-22 2013-08-28 吉坤日矿日石金属株式会社 Sintered body sputtering target
JP2016031933A (en) * 2014-07-25 2016-03-07 国立研究開発法人産業技術総合研究所 Proton-conducting laminate structure
RU2591932C1 (en) * 2015-06-10 2016-07-20 Федеральное государственное унитарное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" (ФГУП "ВИАМ") Method of wear-resistant coating producing
CN107099700A (en) * 2017-05-15 2017-08-29 深圳市万泽航空科技有限责任公司 A kind of method for preparing CoCrAlY alloy target materials
CN115181869A (en) * 2022-08-01 2022-10-14 江苏美特林科特殊合金股份有限公司 Method for producing nickel-based high-temperature alloy containing Y, ce, la and Nd

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5335717A (en) * 1992-01-30 1994-08-09 Howmet Corporation Oxidation resistant superalloy castings
CN1153446A (en) * 1995-12-29 1997-07-02 黄安荣 Electrothermal lanthanum chromate body and its mfg. method
JP2003301262A (en) * 2002-04-10 2003-10-24 Sumitomo Metal Mining Co Ltd Ferroelectric thin film, and sputtering target material for forming ferroelectric thin film
KR20070082401A (en) * 2006-02-16 2007-08-21 학교법인 포항공과대학교 Ferritic type stainless steel containing yttrium
CN101629276A (en) * 2009-08-05 2010-01-20 中国核动力研究设计院 Zirconium-yttrium alloy target preparation method
US20120114975A1 (en) * 2010-11-05 2012-05-10 Solar Applied Materials Technology Corp. Sputtering Targets And Recording Materials Of Hard Disk Formed From The Sputtering Target
CN103270190A (en) * 2010-12-22 2013-08-28 吉坤日矿日石金属株式会社 Sintered body sputtering target
JP2016031933A (en) * 2014-07-25 2016-03-07 国立研究開発法人産業技術総合研究所 Proton-conducting laminate structure
RU2591932C1 (en) * 2015-06-10 2016-07-20 Федеральное государственное унитарное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" (ФГУП "ВИАМ") Method of wear-resistant coating producing
CN107099700A (en) * 2017-05-15 2017-08-29 深圳市万泽航空科技有限责任公司 A kind of method for preparing CoCrAlY alloy target materials
CN115181869A (en) * 2022-08-01 2022-10-14 江苏美特林科特殊合金股份有限公司 Method for producing nickel-based high-temperature alloy containing Y, ce, la and Nd

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
潘钱付;刘超红;蒋明忠;尹昌耕;: "锆钇合金靶件性能对镀膜工艺影响研究", 核动力工程, no. 02, pages 25 - 29 *

Also Published As

Publication number Publication date
CN116926484B (en) 2024-01-30

Similar Documents

Publication Publication Date Title
CN114134385B (en) Refractory medium-entropy alloy and preparation method thereof
CN109207755B (en) Production process of 1-series aluminum alloy plate
CN102994920A (en) High and low temperature compound resistance reduction treatment method for copper and copper alloy
CN109355632A (en) A method of improving molybdenum and its alloy sputtering target grain uniformity
CN104480445A (en) Aluminum alloy target and preparation method thereof
CN106893947A (en) It is a kind of to be resistant to 400 degree of preparation methods of the bearing steel of high temperature
KR101288592B1 (en) Method of manufacturing an oxide dispersion strengthened platinum-rhodium alloy
CN114293158B (en) Preparation method of tungsten-silicon alloy target
CN116926484B (en) Processing technology of zirconium yttrium chromium alloy sputtering target material
CN115044794B (en) Cu- (Y) with excellent performance 2 O 3 -HfO 2 ) Alloy and preparation method thereof
CN111719127A (en) Preparation method of nickel-chromium-aluminum-yttrium-silicon alloy target material
CN100500907C (en) Heat treatment process for large size as-cast high-Nb TiAl-base alloy to obtain complete lamellar structure
CN109628777B (en) Method for improving corrosion resistance of high-entropy alloy
CN113718190A (en) Method for improving boiling nitric acid corrosion resistance and wear resistance of zirconium alloy
CN106244988A (en) A kind of high resistant target manufacture method
WO2021103843A1 (en) Laser cladding and welding high-entropy alloy alcocrfeni/27simn steel composite layer and preparation method therefor
CN113604762A (en) Vacuum solid solution and aging treatment process for improving high-temperature plasticity of GH4738 alloy ring piece
CN112981265A (en) Carbon-free high-speed steel and preparation method thereof
CN113046586A (en) Cu-Cr alloy and ultrasonic-assisted smelting method thereof
CN109396380B (en) Method for preparing high-heat-conductivity baking tray through semi-solid die-casting
He et al. Effect of deformation temperature on dynamic recrystallization and CSL grain boundary distribution of Fe-36% Ni invar alloy
CN114183448A (en) High-strength corrosion-resistant bolt and production process thereof
CN113059160B (en) Composite preparation method of complex low-gap phase titanium alloy component
CN110629123A (en) Method for improving thermal fatigue resistance of alloy steel casting
CN112795825A (en) Titanium-based Mxene-enhanced aluminum alloy and preparation process thereof

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