WO2002083286A1 - Recipient a vide en alliage au titane et element a vide - Google Patents
Recipient a vide en alliage au titane et element a vide Download PDFInfo
- Publication number
- WO2002083286A1 WO2002083286A1 PCT/JP2002/002566 JP0202566W WO02083286A1 WO 2002083286 A1 WO2002083286 A1 WO 2002083286A1 JP 0202566 W JP0202566 W JP 0202566W WO 02083286 A1 WO02083286 A1 WO 02083286A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- vacuum
- titanium alloy
- titanium
- surface roughness
- ultra
- Prior art date
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C23—COATING 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
- C23C—COATING 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
- C23C8/00—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
- C23C8/06—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases
- C23C8/08—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases only one element being applied
- C23C8/10—Oxidising
- C23C8/16—Oxidising using oxygen-containing compounds, e.g. water, carbon dioxide
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C14/00—Alloys based on titanium
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/922—Static electricity metal bleed-off metallic stock
- Y10S428/923—Physical dimension
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12993—Surface feature [e.g., rough, mirror]
Definitions
- the present invention relates to a titanium alloy vacuum container and a vacuum component capable of easily achieving an ultra-high vacuum in a short time after evacuation.
- vacuum equipment is widely used in all industries, including equipment for manufacturing various electronic devices in the semiconductor industry, and is also used in advanced science and technology fields such as high energy physics and solid surface science. It is indispensable.
- semiconductor electronic vacuum device for parts and LSI manufacture already 10-5 ultrahigh vacuum of 10 one 7 Pa from Pa, but also high-quality semiconductor thin and ultra high for Seisuru create the superstructure film in vacuum deposition apparatus, Ru required der the following ultimate pressure 10- 8 Pa.
- it is necessary to control the stacking on the order of one atomic layer under extremely clean ultra-high vacuum.
- it is absolutely necessary to develop a vacuum equipment that can easily reach 10 to 18 Pa or less.
- ultra-high vacuum containers and ultra-high vacuum parts are made of stearyl emissions less steel or Aluminum Niumu alloy
- a general vacuum apparatus reaches the following ultra-high vacuum region 10_ 5 Pa
- vacuum baking vacuum baking
- 10 to 8 Pa or less In equipment that requires ultra-high vacuum, such as vacuum deposition equipment in which semiconductors with a thickness of several nanometers are stacked in multiple layers, such as sputtering pumps and titanium pumps, etc. It is necessary to combine multiple ultra-high vacuum pumps, and furthermore, it is necessary to provide a shroud (refrigerant pool) cooled with liquid nitrogen in the equipment.
- titanium or a titanium alloy is more expensive than stainless steel or the like, it has a high specific strength, is lightweight, has excellent corrosion resistance, and is manufactured in a high vacuum. Extremely small amount of gas mixed into metal structure It is a material that can be suitably used for ultra-high vacuum containers and the like. For example, it has been studied by the inventors (T. Chi jiraatsu, et. Al, J. Vac. Soc. Jpn. Vol 42,
- a vacuum device in which the surface roughness is reduced to 100 nm or less by puff polishing or electrolytic polishing of a metal (preferably titanium) that has been subjected to high vacuum refining is used. No. 3030458).
- titanium has the disadvantage that surface smoothing is difficult. That is, according to the study of the present inventors shown in the above-mentioned literature, the surface roughness of titanium subjected to general puff polishing and electrolytic polishing is about the same as that of stainless steel subjected to the same polishing treatment.
- the vacuum material surface is a mirror surface required to provide an ultra-high vacuum vessel with a small amount of gas emission that can achieve ultra-high vacuum of 10 to 8 Pa or less in a short period of time, about 15 nm, which is four times as large. There is a problem that it is difficult to perform such a smoothing process.
- the metal gasket flange for vacuum sealing made of titanium can be used approximately 10 times when a metal gasket made of oxygen-free copper, which is commonly used, is used. And there is a problem that a vacuum leak occurs.
- titanium alloys general industrial titanium alloys have high strength and are difficult to machine or have surface treatment properties required for materials for vacuum equipment. Materials are being developed. For example, an ultra-high vacuum titanium alloy (JP-A-06-065661) that emits a small amount of gas containing platinum-based metal, transition metal, rare earth element, etc. A high vacuum container (Japanese Patent Application Laid-Open No. 06-064600) is disclosed, and it is shown that the amount of outgassing is 1 Z10 or less as compared with stainless steel.
- Japanese Patent Application Laid-Open No. 06-064600 Japanese Patent Application Laid-Open No. 06-064600
- the ultra-high vacuum that can achieve ultra-high vacuum in a short time, which is the goal of the present invention,
- the surface treatment properties of the materials required to provide the containers have not been clarified. Further, in the disclosed technology, since a relatively expensive alloy element is used, there is a problem that the apparatus becomes expensive.
- titanium alloys have been developed in a wide variety of materials in addition to those for vacuum equipment.For example, they are excellent in decorativeness, robustness, workability, biocompatibility, and cost.
- a technology using iron and oxygen as alloy elements Japanese Patent Laid-Open No. 10-017962
- a technology using iron, oxygen and silicon as alloy elements Japanese Patent Application Laid-Open No. Hei 10-017961 discloses that application to a wide range of products such as sports applications is expected in addition to accessories.
- this disclosed technology does not clarify the suitability of a material for a vacuum device, such as gas release characteristics and surface treatment characteristics.
- An object of the present invention is to provide a titanium alloy vacuum container and a vacuum component that can easily achieve an ultra-high vacuum in a short time after evacuation in view of the situation related to such a vacuum device. I do. Disclosure of the invention
- a titanium alloy vacuum container and a vacuum part are a vacuum container and a vacuum part whose main parts are made of a titanium alloy. It is a titanium alloy vacuum vessel and a vacuum component which are finely divided into fine particles of not more than m and have a surface roughness of at least 50 nm or less which can be exposed to vacuum at least.
- the surface roughness means the center line average roughness (Ra) measured in the range of 10 ⁇ 10 / m by an atomic force microscope.
- the surface roughness is the surface roughness of the titanium alloy.
- These are titanium alloy vacuum vessels and vacuum components with a thickness of 10 nm or less.
- the titanium alloy is preferably a titanium alloy having a Vickers hardness of 230 Hv or more and a hardness of 310 Hv or less.
- the above titanium alloy can be a titanium alloy having a passivation film formed by a thin titanium oxide layer or a nitride layer on a surface exposed to at least a vacuum. It is desirable to have a film thickness of 10 nm or less.
- the titanium alloy used for the titanium alloy vacuum vessel and the vacuum component of the present invention includes iron (F e) 0.3 w to 0.5 wt%, and oxygen (0) 0.3 wt% to 0.5 wt%. %, And the balance is preferably a titanium alloy composed of titanium (Ti) and unavoidable impurities.
- FIG. 1 is a diagram showing an example of the relationship between the surface roughness and the gas release rate of a titanium alloy desired as a material for a titanium alloy vacuum vessel and a vacuum component of the present invention.
- FIG. 2 is an external view of a vacuum container prototyped as an embodiment of the titanium alloy vacuum container of the present invention, in which (a) is a top view, and (b) is a top view of the vacuum container.
- FIG. 3 is a diagram showing the evacuation characteristics of the prototype vacuum vessel of FIG. 2, and is a pressure evacuation curve showing an example of evacuation after vacuum evacuation.
- FIG. 4 is a graph showing the evacuation characteristics of the prototype vacuum vessel of FIG. 2, and is a pressure evacuation curve showing an example without vacuum vacuuming.
- the vacuum vessel according to the present invention is not limited to a so-called vessel-shaped vessel, but is a means for surrounding a space evacuated to a vacuum state, including a pipe-shaped or duct-shaped vessel. It is a thing.
- the evacuation process of a vacuum vessel exposed to the atmosphere is (1) a process in which the pressure decreases exponentially depending on the volume, and (2) a gas species adsorbed on the inner surface of the vessel is desorbed and the pressure is determined. It is said that there are four processes: (3) the process in which the gas diffused from inside the container material and released into the vacuum determines the pressure, and (4) the process in which the gas permeating from the atmosphere finally determines the pressure.
- Quantity of gas released from the vacuum material is typically represent a gas release rate (Pa m / sec), in order to obtain the ultra-high vacuum of about 1 xlO- 8 Pa is, 10_ 9 ⁇ 10- 1 D Pa outgassing rate of m / sec is will require an, 1 xlO- 9 Pa to obtain the following extremely high vacuum is required 10_ 1 Q Pa m / sec table below outgassing rate.
- the present inventor studied the factors of gas release of the vacuum material from various angles and selected a material in order to reduce the amount of gas released from the vacuum vessel and the vacuum components. That is, (1) a material that is dense and has appropriate hardness so that a mirror-like surface that reduces the amount of adsorbed gas can be obtained relatively easily; ) In order to reduce the diffusion and emission of gas from the inside of the material, it is necessary to judge that the material is a dense material that contains a small amount of gas and prevents the diffusion of gas. As a vacuum material that is likely to satisfy the conditions, the gas is contained in the material because it has a fine-grained structure, is dense, has appropriate hardness, is easy to be mirror-finished, and is manufactured with high vacuum precision. A titanium alloy with the characteristic of a small amount was selected as the vacuum material.
- the next step is to consider the development of a new titanium alloy when examining which titanium alloy is most suitable for ultra-high vacuum materials.
- the present inventors have already developed a wide variety of titanium alloys in addition to the titanium alloys developed as vacuum materials, and among them, If a titanium alloy suitable as a material for vacuum could be found, it would be extremely advantageous in terms of cost, and it was decided that ultra-high vacuum materials would be used for titanium alloys already developed.
- the present invention has been completed by conducting a study on the suitability of all of them.
- the first condition is that the fineness should be reduced to approximately l0 ⁇ m or less for the denseness, and that the surface smoothing treatment should be 1 X set the surface roughness outgassing rate 10- 1 m / sec stand Ru can handle sufficiently to extremely high vacuum device following 10- 9 Pa is obtained as the second condition, further, a predetermined surface roughness
- the desired condition is that the surface smoothing treatment to obtain the desired degree of hardness can be performed relatively easily, and the material hardness that has suitable workability and durability is also a desirable condition. This is the result of extensive research on titanium alloys that meet these conditions, targeting already developed titanium alloys.
- the crystal grain size is finer and denser is one of the factors that enable the mirror-finish treatment, and at the same time, reduces the diffusion and release of gas from the inside of the material. As shown in 10-017962, it is also a factor that improves flaw resistance, and is suitable as a material for ultra-high vacuum equipment that extremely dislikes leakage from the atmosphere.
- the conditions to be set are conditions that can be supplied industrially easily and inexpensively, and the present invention has characteristics as an extremely suitable material for vacuum, which will be described in detail later. It is set to about 10 mm or less, assuming that titanium alloy can be almost achieved.
- the surface roughness that achieves a gas release rate of 10—HPa m / sec is described in detail in the examples below, but as a result of measuring and examining the relationship between the surface roughness and the gas release rate, it was found to be 50 nm or less. It is set.
- the titanium alloy vacuum container and the vacuum component of the present invention are a vacuum container and a vacuum component whose main part is made of a titanium alloy. m or less, and the surface roughness of the surface exposed to vacuum is at least 50 nm or less, whereby the amount of desorbed gas from the inner surface of the container, and Since the amount of gas diffused and released from the inside of the container material can be greatly reduced, it is possible to easily achieve an extremely high vacuum in a short time after evacuation.
- the amount of desorbed gas from the material surface can be reduced to near the limit, that is, the amount of diffusion gas from inside the material or the amount of permeated gas from the atmosphere.
- the amount can be reduced to a level that does not cause a problem in comparison, and the present invention can be carried out more preferably.
- the titanium alloy described below can achieve a surface roughness of about 5 nm even by a relatively simple polishing method, and can suitably carry out the present invention.
- the vacuum flange of an ultra-high vacuum device is provided with a knife edge and a metal gasket is used to seal the vacuum.
- a material which is hard to cause cracks and has a suitable hardness which does not cause a problem in workability As described above, a titanium alloy with a hardness of 110 to 160 Hv generates a vacuum leak after opening and closing about ten times, while a titanium alloy (Ti-6A1-4V) with a hardness of 350 Hv is difficult to machine. It costs money.
- the hardness of the titanium alloy is important not only in the vacuum flange portion, but for example, the present inventors have made a prototype of a vacuum container using Ti-6A 4V, There were problems such as rapid wear of the tool and the problem of vacuum leakage from the weld site due to the difficulty of welding due to the inclusion of a large amount of alloying elements. Another problem is that titanium alloys with a large amount of added alloy are expensive.
- the titanium alloy described below is used. As a result of examining the performance of using the vacuum sealing part many times, it was confirmed that vacuum leakage did not occur even when opening and closing more than 30 times, and the suitable titanium alloy hardness was 230 Hv or more. And set to 310Hv or less.
- a uniform thin passivation film such as a thin oxide film or a nitrided film is formed on the surface by thermal oxidation treatment or nitridation treatment, thereby preventing gas diffusion and transmission inside the material. It is known that this can be achieved (for example, Ito and Minato: Vacuum, 40 (1997) ⁇ 248-250).
- a titanium layer having a thin titanium oxide layer or nitride layer formed on its surface is also provided. It can be an alloy.
- the thickness of the passivation film is preferably 1 Onm or less in order to avoid an increase in the gas adsorption surface and effectively cope with an extremely high vacuum.
- a desirable titanium alloy for the above-described vacuum vessel and vacuum parts is the titanium alloy KS100 disclosed in the above-mentioned Japanese Patent Application Laid-Open No. H10-017962. Further, the suitability for use in a vacuum device is examined in detail. As a result, it contains 0.3 w-0.5 wt% of iron and 0.3 wt% -0.5 wt% of oxygen, disclosed as a preferred embodiment in JP-A-10-017962, with the balance being Ti and inevitable. It is a titanium alloy composed of impurities.
- a detailed embodiment including the method for producing a titanium alloy is disclosed in Japanese Patent Application Laid-Open No. 10-017962, but the reason for limiting the range of the chemical component composition of the titanium alloy in the present invention is as follows. If the oxygen content is less than 0.3 wt%, the hardness is insufficient, and if the oxygen content exceeds 0.5 wt%, the workability (formability) deteriorates, and if the iron content is less than 0.3 wt%, the surface roughness deteriorates, When the content exceeds 0.5wt%, processability
- the sample used was the above-mentioned titanium alloy KS100 (a titanium alloy containing 0.35 wt% of oxygen and 0.35 wt% of iron, with the balance being Ti and unavoidable impurities).
- Samples TP1 to TP3 that had been subjected to polishing and a stainless steel sample SP that had been polished were prepared for comparison, and the gas release rate was examined using the orifice method. 180 samples of 20 mm x 20 mm x 1 mm t were used for each sample. The measurement of the gas release rate by the orifice method was performed using a prototype titanium alloy vacuum vessel described later as the second embodiment.
- the pretreatment of the sample was only to perform a heat treatment at 90 ° C for 24 hours in air after alcohol washing.
- the measurement conditions were as follows: as an initial condition, after 30 minutes of opening the device to the atmosphere, the exhaust system was started up and evacuated for 3 hours, and then the chamber was vacuum-baked at 180 ° C and the sample section at 220 ° C. Was performed for 48 hours, and the gas release rate was determined from the ultimate pressure after cooling for 48 hours.
- the heating temperature is set to a relatively low temperature in consideration of the use of a real vacuum device.
- the surface roughness is a center line average roughness (Ra) measured in a range of 10 ⁇ 10 // m using an atomic force microscope (AFM).
- Example Comparative Example polished titanium emissions alloy TN was polished stearate Despite being roughly 50 times coarser than the gas SP, its outgassing rate is 1.8xlO- 1 D Pam / sec, which is about the same. This is because the titanium alloy has undergone a vacuum melting process in the manufacturing process, and the crystal grains of the titanium alloy have become finer and denser.
- the surface roughness should be 50 nm or less.
- the reason why the gas release rate decreases linearly with the surface roughness in the range of surface roughness 10 to 100 nm is that the gas released from the surface is the dominant gas release amount.
- the fact that the surface roughness shows a saturation tendency at a surface roughness of 10 nm or less means that the amount of gas released from other factors, such as diffusion and emission from the inside of the material, has become dominant.
- the gas emission characteristics indicate such a tendency, and the surface roughness is preferably set to a point indicating a saturation tendency.
- the surface roughness showing a saturation tendency can be smaller than about 10nm.
- the surface roughness of 10 nm which can achieve less than about one-tenth of the gas release rate ( 1 ⁇ 10-1 Q Pani / sec) required for ultra-high vacuum, is usually These are sufficient setting conditions.
- the experiment was performed by measuring the temperature dependence of the gas release rate using the titanium alloy sample TP1 with a roughness of 7 lnm after the measurement of the gas release rate performed in the first embodiment.
- Table 2 shows the results.
- the activation energy for outgassing was calculated to be approximately 20 kJ / mo1, which is the value of hydrogen diffusion in stainless steel. The value is much smaller than that of activated energy 45 kJ / mo1.
- the present titanium alloy has a very low gas release rate UxlO-H Pam / sec in the chamber as shown in the first embodiment, and has a small gas release activation energy according to the present embodiment. This confirms that the amount of gas released by diffusion is smaller than that of existing stainless steel.
- FIG. 2 is an external view of a vacuum vessel prototyped as an embodiment of the titanium alloy vacuum vessel of the present invention, in which (a) is a top view, and (b) is a top view.
- Titanium emissions alloy used was Ri Oh with KS100 was subjected to surface polishing of the surface roughness 3.8 nm, the vacuum vessel, the volume 6.7x10- 3 m 3, an inner surface area 375 xlO- 3 m 2, an intermediate diameter 5.4 is separated by an orifice with a small It is divided into Check (volume 4.2x10- 3 m 3, the inner surface area 210x10- 3 m 2) and the upstream vacuum chamber (volume 2.5x10- 3 m 3, the inner surface area 165xl0_ 3 m 2).
- the main exhaust pump 55 ( ⁇ 10-3 111 3/36 (; to connect the 150x10- 3 m 3 / sec turbomolecular pump (TMP) in series, the crude Technology of and evacuation device is connected to the downstream vacuum chamber using a 150x10 one 3 m 3 / min of oil rotary pump (RP) to the pump, j over de type downstream vacuum chamber and the upstream vacuum chamber ionization A vacuum gauge (EG) is installed.
- the heating temperature for vacuum baking of a vacuum vessel is often set to 200 ° C or higher, but here, a relatively low temperature of 160 ° C is used for 48 hours. Vacuum baking was performed, and then the pressure of the vacuum vessel was measured for 48 hours.
- Figure 3 shows the pressure evacuation curves of the upstream vacuum chamber (shown by the solid line) and the downstream vacuum chamber (shown by the dashed line) with the end time of the vacuum base being set to 0. despite the vacuum base one King at low temperatures, in 2 hours and very short evacuation time that would have, upstream vacuum chamber 8.0xl0- 8 Pa, to reach the ultra high vacuum region of the downstream vacuum chamber 1.4x10 one 8 Pa, after 48 hours, the upstream vacuum chamber 1.6x10- 8 Pa, the downstream vacuum chamber reached extremely high vacuum region called 6.5x10 one 9 Pa.
- the pressure in the upstream vacuum chamber is higher Ri by the pressure in the downstream vacuum chamber, Ri by the O Li off office provided in the middle of the vacuum vessel, evacuation speed of the upstream vacuum chamber (2.6x10- 3 m 3 / sec) is about two orders of magnitude lower than the evacuation speed of the downstream vacuum chamber.
- Figure 4 shows the results, and is a pressure evacuation curve without vacuum baking based on the start time of the main exhaust pump TMP.
- the pressure of the downstream vacuum chamber (indicated by the dashed line), which has the form of a normal vacuum apparatus (a form in which a vacuum is evacuated directly without using an orifice, etc.) after 3 hours 6.2x10- 7 Pa, 30 hours after 5.7xlO_ 8 Pa, after between 48 o'clock reached 3.9xlO_ 8 Pa. That is, titanium emission alloy vacuum container of the present invention, the also rather subjected to vacuum base one King, 10_ 7 Pa stand ultra-high vacuum can be obtained in a short time of evacuation, also easily 10 one 8 This indicates that a pressure on the order of Pa can be obtained.
- the upstream vacuum chamber (indicated by the solid line) is a 3 hours after 7. OxlO_ 6 Pa, 30 hours after 6. 3x10- 7 Pa, 48 hours after 4.6x10- 7 Pa, approximately an order of magnitude even Ri by the downstream vacuum chamber
- the value is high because, as described above, the evacuation speed of the upstream vacuum chamber is significantly reduced due to the resistance of the orifice.
- the structure of the titanium alloy KS100 is finely divided into approximately 10 ⁇ m or less and contains a dense titanium alloy KS100 (containing 0.35w of oxygen and 0.35wt% of iron, and the rest is Ti and inevitable It has been demonstrated that the use of a titanium alloy consisting of impurities) can reduce the gas emission rate by reducing the surface roughness, and the gas emission rate required for ultra-high vacuum. (1x10-11 Q Pam / sec or less) was demonstrated to achieve a surface roughness of 50 nm or less, and it is more preferable that the surface roughness be 10 nm or less. I showed you something. We have also demonstrated that the amount of outgassing due to diffusion from inside the material is smaller than that of existing stainless steel.
- a titanium vacuum container using such a titanium alloy KS100 was prototyped, and the evacuation experiments showed that even a relatively simple evacuation device could be used to achieve a short evacuation. be reached by Ri ultra-high vacuum, and further, was the real testimony that you ultra-high vacuum of this and Do rather than 10- 8 Pa subjected to base one King Ru can be easily realized.
- the sample is a vacuum flange made of the above-mentioned titanium alloy KS100 (hardness 280 HV).
- Two kinds of pure titanium (JIS-2 type: hardness 145Hv) flanges were prepared in the same manner.
- an oxygen-free copper gasket which is a general ultra-high vacuum seal, is sandwiched between two sample flanges, and the vacuum leak at the vacuum-sealed part is checked using a vacuum leak tester Technician).
- the number of tests was 30.
- Table 3 shows the test results. Here, the presence or absence of vacuum leakage was judged to be 1 ⁇ 10-10 Pa m 3 / sec or more as a result of vacuum leakage. , was visually determined.
- a thin titanium oxide layer was formed on the surface of the titanium alloy. An example in which is formed will be described.
- the sample is the above titanium alloy KS100 set to a surface roughness of 0.7 nm.
- the reason why the surface roughness was set to 0.7 nm was that it was thought that separation or cracking of microstructure due to oxidation could be observed with an atomic force microscope. This delamination or cracking of the structure is a factor that increases the outgassing rate, and the passivation film that reduces the outgassing rate has a uniform structure with less separation and cracking of the tissue in a micro area. It must be a film.
- the oxidation of the titanium alloy was performed by thermal oxidation. That is, the titanium alloy was placed in a vacuum chamber, the pressure was evacuated to 4 xl O- 4 Pa, and then the sample was heated at a temperature 20 ° C higher than the oxidation treatment temperature for 2 hours. After performing the king, the sample temperature was set to the oxidation treatment temperature, oxygen (purity 99.7%) was introduced at 1 atm, and the oxidation treatment was performed for 2 hours. There are four oxidation treatment temperatures: 150, 200, 300 and 400 ° C.
- the thickness of the titanium alloy oxide film was obtained by physically etching a part of the oxide film by an ion beam sputter method and measuring by a stylus type surface roughness meter. Table 4 shows the results of the peeling test and the results of surface roughness and film thickness.
- the surface of the untreated sample, 200 ° C treated sample and 30 (each surface of the TC treated sample was observed with an atomic force microscope in the area of 10 ⁇ 10 m. As in the case of the surface, there was no micro-separation roughness, and as shown in Table 4, the surface roughness of the sample treated at 200 ° C was almost the same as that of the untreated sample. That is, the oxidation treatment at 200 ° C. is a preferable condition for forming an extremely uniform oxide film.
- the thickness of the titanium oxide layer of the sample treated at 200 ° C. is about 8 nra. .
- the surface of the sample treated at 300 ° C was observed to have a separation roughness of about 1 xlm, reflecting this, and the surface roughness (1.9 nm) was roughly three times that of the untreated sample. ing.
- the oxide film thickness of this sample is about 1 Onm. That is, in the oxidation treatment at 300 ° C, the oxidation does not proceed in the depth direction of the titanium alloy and the oxidation of the surface layer progresses as compared with the oxidation treatment at 200 ° C, resulting in a rough surface. It turned out that it only formed a surface.
- the surface oxidation treatment conditions of the titanium alloy used in the present example are preferably set to an oxidation treatment temperature of 200 ° C. and an oxidation treatment time of about 2 hours. Reflecting the fact that the degree is as small as 0.7 nm, it was clarified that an extremely uniform thin oxide layer of about 8 nm can be formed.
- this titanium oxide film is a passivation film for reducing the gas release rate, and is one of the important elemental technologies for making an ultra-high vacuum device effective. .
- the surface roughness was set to 0.7 nm, observation by an atomic force microscope was possible, and the surface state of the oxide film was evaluated microscopically. One of the characteristics is that the optimum oxide film formation conditions are determined.
- the passivation film of the titanium nitride film can be similarly formed by the surface nitriding treatment of the titanium alloy. And can be.
- a titanium alloy plate (2 mm t) having the composition shown in Table 5 was manufactured, its surface was polished, and its surface roughness and hardness were measured.
- the plates of each composition were cold-formed into a bend and joined by TIG welding to form a welded tube with a diameter of 100 mm and a length of 300 mm, and compared the workability.
- Table 5 shows the results of each evaluation.
- No. 1 is a comparative example with too low oxygen content and lacks hardness
- No. 2 is a comparative example with too much iron content and a minute crack was generated at the welded part
- No. 3 was a comparative example in which the iron content was too low, and a surface roughness of 1 Onm or less could not be achieved by polishing
- No. 4 was a comparative example in which the oxygen content was too high. Interforming was difficult.
- No. 5 to No. 9 are examples satisfying the composition specified as a desirable component composition of the titanium alloy in the present invention, and the surface roughness and the hardness are within appropriate ranges. There was no problem with workability.
- the titanium alloy of the sixth embodiment has desirable characteristics as a material of a titanium alloy vacuum container and a vacuum component, which is the aim of the present invention, and is disclosed in -As shown in JP-A No. 0-962, it is excellent in robustness, biocompatibility, or cost, and is suitable as a material for the titanium alloy vacuum container and vacuum components of the present invention.
- a method of forming a thin titanium oxide layer on the surface of a titanium alloy was described in detail.However, a passivation film that reduces the gas release rate by using titanium oxide was described. Any method can be used as long as it can be formed, and there is no particular limitation on the present invention, such as the oxidation treatment temperature, the oxidation treatment time, or the thickness of the titanium oxide film to be formed.
- Industrial applicability The vacuum vessel and the vacuum part made of a titanium alloy of the present invention are a vacuum vessel and a vacuum part in which desorption gas from the inner surface and diffusion / release gas from the inside of the material are greatly reduced. This has the effect that an ultra-high vacuum can be easily achieved in a short time.
- the evacuation speed of the evacuation pump is small, or a plurality of evacuation pumps are not required in an ultra-high vacuum, and thus there is an effect that an energy-saving vacuum apparatus can be realized.
- the titanium alloy vacuum vessel and vacuum component of the present invention having such an effect require a vacuum apparatus for producing semiconductor thin films and electronic components that require high throughput, and the need to achieve an ultra-high vacuum. It can be implemented more effectively as a surface analysis device and an atomic operation device to be used, or as a vacuum container and a vacuum component of a high energy accelerator facility.
Landscapes
- Chemical & Material Sciences (AREA)
- Organic Chemistry (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Physical Vapour Deposition (AREA)
- Manufacture And Refinement Of Metals (AREA)
- Chemical Vapour Deposition (AREA)
- Solid-Phase Diffusion Into Metallic Material Surfaces (AREA)
- Thermally Insulated Containers For Foods (AREA)
- Packages (AREA)
- Sampling And Sample Adjustment (AREA)
Description
Claims
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP02761963A EP1374984B1 (en) | 2001-03-26 | 2002-03-18 | Titanium alloy vacuum container and vacuum part |
DE60209130T DE60209130T2 (de) | 2001-03-26 | 2002-03-18 | Vakuumbehälter und vakuumteil aus titanlegierung |
US10/312,701 US6841265B2 (en) | 2001-03-26 | 2002-03-18 | Titanium alloy vacuum and vacuum part |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2001088100A JP3694465B2 (ja) | 2001-03-26 | 2001-03-26 | チタン合金製真空容器及び真空部品 |
JP2001-88100 | 2001-03-26 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2002083286A1 true WO2002083286A1 (fr) | 2002-10-24 |
Family
ID=18943241
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/JP2002/002566 WO2002083286A1 (fr) | 2001-03-26 | 2002-03-18 | Recipient a vide en alliage au titane et element a vide |
Country Status (6)
Country | Link |
---|---|
US (1) | US6841265B2 (ja) |
EP (1) | EP1374984B1 (ja) |
JP (1) | JP3694465B2 (ja) |
AT (1) | ATE317293T1 (ja) |
DE (1) | DE60209130T2 (ja) |
WO (1) | WO2002083286A1 (ja) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP3930420B2 (ja) * | 2002-11-20 | 2007-06-13 | 愛三工業株式会社 | チタン部材の表面処理方法 |
DE102004045883A1 (de) * | 2004-09-22 | 2006-04-06 | Diehl Bgt Defence Gmbh & Co. Kg | Verfahren zur Herstellung eines Spiegels aus einem Werkstoff auf Titanbasis, sowie Spiegel aus einem solchem Werkstoff |
JP6266727B1 (ja) * | 2016-10-24 | 2018-01-24 | トクセン工業株式会社 | 医療機器用金属線 |
JP6729628B2 (ja) * | 2018-04-25 | 2020-07-22 | 東横化学株式会社 | 貯蔵容器 |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH04249674A (ja) * | 1990-12-28 | 1992-09-04 | Kurein:Kk | 真空容器 |
JPH0953163A (ja) * | 1995-08-11 | 1997-02-25 | Mitsubishi Heavy Ind Ltd | チタン製真空容器の熱処理方法 |
JPH10265935A (ja) * | 1997-03-27 | 1998-10-06 | Vacuum Metallurgical Co Ltd | 超高真空容器及び超高真空部品 |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS60188608A (ja) * | 1984-03-07 | 1985-09-26 | 株式会社東芝 | ネジ部材 |
JPH065661A (ja) | 1992-06-17 | 1994-01-14 | Shindo Denshi Kogyo Kk | Tab用フィルムキャリア |
JPH064600A (ja) | 1992-06-24 | 1994-01-14 | Matsushita Electric Ind Co Ltd | イメージ検索方法およびイメージ検索装置 |
JPH0634775A (ja) * | 1992-07-14 | 1994-02-10 | Mitsubishi Atom Power Ind Inc | 核融合装置の真空容器 |
JP2943520B2 (ja) * | 1992-08-24 | 1999-08-30 | 日産自動車株式会社 | 超高真空容器 |
US5478524A (en) * | 1992-08-24 | 1995-12-26 | Nissan Motor Co., Ltd. | Super high vacuum vessel |
JP3376240B2 (ja) | 1996-03-29 | 2003-02-10 | 株式会社神戸製鋼所 | 高強度チタン合金およびその製品並びに該製品の製造方法 |
JPH1017962A (ja) | 1996-03-29 | 1998-01-20 | Kobe Steel Ltd | 高強度チタン合金およびその製品並びに該製品の製造方法 |
JPH11164784A (ja) * | 1997-12-03 | 1999-06-22 | Nippon Sanso Kk | 金属製真空二重容器 |
JPH11221667A (ja) * | 1997-12-03 | 1999-08-17 | Nippon Sanso Kk | 金属製真空二重容器の製造方法 |
-
2001
- 2001-03-26 JP JP2001088100A patent/JP3694465B2/ja not_active Expired - Lifetime
-
2002
- 2002-03-18 EP EP02761963A patent/EP1374984B1/en not_active Expired - Lifetime
- 2002-03-18 AT AT02761963T patent/ATE317293T1/de not_active IP Right Cessation
- 2002-03-18 US US10/312,701 patent/US6841265B2/en not_active Expired - Lifetime
- 2002-03-18 DE DE60209130T patent/DE60209130T2/de not_active Expired - Lifetime
- 2002-03-18 WO PCT/JP2002/002566 patent/WO2002083286A1/ja active IP Right Grant
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH04249674A (ja) * | 1990-12-28 | 1992-09-04 | Kurein:Kk | 真空容器 |
JPH0953163A (ja) * | 1995-08-11 | 1997-02-25 | Mitsubishi Heavy Ind Ltd | チタン製真空容器の熱処理方法 |
JPH10265935A (ja) * | 1997-03-27 | 1998-10-06 | Vacuum Metallurgical Co Ltd | 超高真空容器及び超高真空部品 |
Also Published As
Publication number | Publication date |
---|---|
EP1374984A4 (en) | 2004-10-27 |
ATE317293T1 (de) | 2006-02-15 |
US6841265B2 (en) | 2005-01-11 |
DE60209130T2 (de) | 2006-08-03 |
EP1374984B1 (en) | 2006-02-08 |
JP3694465B2 (ja) | 2005-09-14 |
DE60209130D1 (de) | 2006-04-20 |
EP1374984A1 (en) | 2004-01-02 |
JP2002282673A (ja) | 2002-10-02 |
US20030162042A1 (en) | 2003-08-28 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US6107199A (en) | Method for improving the morphology of refractory metal thin films | |
JP5210498B2 (ja) | 接合型スパッタリングターゲット及びその作製方法 | |
Sun et al. | Low temperature plasma nitriding characteristics of precipitation hardening stainless steel | |
JP2009542918A (ja) | コーティング装置および方法 | |
JP2010132974A (ja) | Ni−Mo系合金スパッタリングターゲット板 | |
JP6847356B2 (ja) | 水素分離膜の製造方法及び水素分離膜 | |
EP3827922B1 (en) | Method of diffusion bonding a nickel-based superalloy. | |
Kao et al. | Structure, mechanical properties and thermal stability of nitrogen-doped TaNbSiZrCr high entropy alloy coatings and their application to glass moulding and micro-drills | |
CN113235051B (zh) | 一种纳米双相高熵合金薄膜及其制备方法 | |
WO2002083286A1 (fr) | Recipient a vide en alliage au titane et element a vide | |
US20080017278A1 (en) | High Melting Point Metal Based Alloy Material Lexhibiting High Strength and High Recrystallization Temperature and Method for Production Thereof | |
WO2016111288A1 (ja) | ダイヤモンドライクカーボン層積層体およびその製造方法 | |
CN107614719B (zh) | 硬质合金和被覆硬质合金 | |
Latushkina et al. | Formation of wear-resistant nanostructured TiN/Cu coatings | |
JP2014214336A (ja) | クロム含有金属材料及びクロム含有金属材料の製造方法 | |
Chu et al. | Ion nitriding of titanium aluminides with 25–53 at.% Al I: nitriding parameters and microstructure characterization | |
JP3281173B2 (ja) | 高硬度薄膜及びその製造方法 | |
JP6934691B2 (ja) | 水素分離膜の製造方法及び水素分離膜 | |
Spitz et al. | Phase formation and microstructure evolution of reactively rf magnetron sputtered Cr–Zr oxynitride thin films | |
JP2011012336A (ja) | 多層皮膜被覆部材およびその製造方法 | |
KIM et al. | Isothermal age-hardening behaviour in a Au-1.6 wt% Ti alloy | |
Zou et al. | Hard and tough nitrogen doped tungsten coatings deposited by HIPAC: Microstructure and mechanical properties | |
Wu et al. | Transforming microstructures and mechanical properties of (CoCrNi) 93-xAl7Ndx medium entropy alloy films by annealing | |
Makishi et al. | Feature of M Phase Formed by Plasma Nitriding of Ni-base Alloys–Surface Engineering of Ni-base Alloys by Means of Plasma Nitriding | |
JPH05339702A (ja) | 傾斜機能薄膜 |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
AK | Designated states |
Kind code of ref document: A1 Designated state(s): CN DE GB KR US |
|
AL | Designated countries for regional patents |
Kind code of ref document: A1 Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LU MC NL PT SE TR |
|
DFPE | Request for preliminary examination filed prior to expiration of 19th month from priority date (pct application filed before 20040101) |
Free format text: (EXCEPT CN, DE, GB, KR, EP (AT, BE, CH, CY, DE, DK, ES, FI, FR, GB, GR, IE, IT, LU, MC, NL, PT, SE,TR)) |
|
121 | Ep: the epo has been informed by wipo that ep was designated in this application | ||
WWE | Wipo information: entry into national phase |
Ref document number: 10312701 Country of ref document: US |
|
WWE | Wipo information: entry into national phase |
Ref document number: 2002761963 Country of ref document: EP |
|
WWP | Wipo information: published in national office |
Ref document number: 2002761963 Country of ref document: EP |
|
REG | Reference to national code |
Ref country code: DE Ref legal event code: 8642 |
|
WWG | Wipo information: grant in national office |
Ref document number: 2002761963 Country of ref document: EP |