WO2007114218A1 - チタン合金及びエンジン排気管 - Google Patents
チタン合金及びエンジン排気管 Download PDFInfo
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- WO2007114218A1 WO2007114218A1 PCT/JP2007/056799 JP2007056799W WO2007114218A1 WO 2007114218 A1 WO2007114218 A1 WO 2007114218A1 JP 2007056799 W JP2007056799 W JP 2007056799W WO 2007114218 A1 WO2007114218 A1 WO 2007114218A1
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- titanium
- titanium alloy
- mass
- temperature
- temperature oxidation
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- 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
- C23C24/00—Coating starting from inorganic powder
- C23C24/02—Coating starting from inorganic powder by application of pressure only
- C23C24/04—Impact or kinetic deposition of particles
-
- 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
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/16—Changing 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
- C22F1/18—High-melting or refractory metals or alloys based thereon
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/16—Changing 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
- C22F1/18—High-melting or refractory metals or alloys based thereon
- C22F1/183—High-melting or refractory metals or alloys based thereon of titanium or alloys based thereon
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N13/00—Exhaust or silencing apparatus characterised by constructional features ; Exhaust or silencing apparatus, or parts thereof, having pertinent characteristics not provided for in, or of interest apart from, groups F01N1/00 - F01N5/00, F01N9/00, F01N11/00
- F01N13/08—Other arrangements or adaptations of exhaust conduits
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N13/00—Exhaust or silencing apparatus characterised by constructional features ; Exhaust or silencing apparatus, or parts thereof, having pertinent characteristics not provided for in, or of interest apart from, groups F01N1/00 - F01N5/00, F01N9/00, F01N11/00
- F01N13/16—Selection of particular materials
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N2530/00—Selection of materials for tubes, chambers or housings
- F01N2530/02—Corrosion resistive metals
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- 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
- Y10T428/12292—Workpiece with longitudinal passageway or stopweld material [e.g., for tubular stock, etc.]
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- 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
- Y10T428/12458—All metal or with adjacent metals having composition, density, or hardness gradient
-
- 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
- Y10T428/31504—Composite [nonstructural laminate]
- Y10T428/31678—Of metal
Definitions
- the present invention relates to a titanium alloy excellent in high-temperature oxidation resistance, pure titanium, surface-treated titanium alloy, pure titanium, and an engine exhaust pipe that requires high-temperature acid resistance.
- the titanium alloy and pure titanium referred to in the present invention refer to titanium alloy materials and pure titanium that are formed into various shapes such as plates, strips, wires, and pipes by plastic working such as rolling or forming. Further, the titanium alloy material and pure titanium are collectively referred to as a titanium material.
- the surface-treated titanium material referred to in the present invention refers to a titanium material that has been shot blasted with aluminate fine particles.
- Titanium alloys and pure titanium are being applied in the field of transportation equipment, especially automobiles, which have a high specific strength and light weight.
- exhaust pipe materials for the exhaust system around the engine are currently the mainstream of stainless steel.
- the temperature of the exhaust pipe may be as high as 500 ° C or higher depending on the location, so high-temperature oxidation resistance is required to improve durability because oxidation proceeds quickly.
- the exhaust pipe of the exhaust system around the engine refers to an exhaust stoma hold, an exhaust pipe, a catalyst muffler, a pre-muffler, a silencer (main muffler), etc. in an automobile or motorcycle muffler
- the muffler parts are included.
- the fatigue characteristics are improved by suppressing crystal grain growth, the deterioration of corrosion resistance caused by the A1 additive is suppressed to a minimum, high-temperature oxidation resistance, scale loss resistance, and oxygen resistance Diffusion phase formation It is described to enhance.
- Patent Document 3 a material in which a titanium alloy surface is clad with A shielding has been proposed.
- Patent Document 4 a method has been proposed in which A1-Ti-based vapor deposition is applied to the titanium alloy surface.
- Patent Document 5 a method of forming a TiCrAIN film on the surface of a titanium alloy by the PVD method has been proposed.
- the clad method is expensive.
- the vapor deposition method and the PVD method have problems such as high processing costs and difficulty in forming an acid-resistant coating on the inner surface of the tube when the titanium material has a tube shape such as the exhaust pipe. Have.
- an inorganic binder and A1 powder are adhered to the surface of the titanium alloy and fired to form an oxygen barrier film (oxidation resistant film) that prevents diffusion of oxygen into the material.
- an oxygen barrier film oxygen resistant film
- a treatment method in which sealing is performed with a sealing material based on chromic acid in order to fill the voids formed between the A1 powders after the firing see Patent Document 6).
- a surface-treated titanium material that has been improved to make the surface treatment itself inexpensive and safe has been proposed.
- a surface-treated titanium material in which an oxidation-resistant fired coating layer of 5 m or more is formed on a substrate made of pure titanium or a titanium-based alloy, and the fired coating layer includes 10 at% or less of Si A1
- a metal element M where M is one or more of Ti, Zr, Cr, Si, and Al
- a compound that also has Z or zero force are filled between the alloy or pure particles. It has also been proposed (see Patent Document 7).
- an A1 containing layer is formed on the surface of the titanium alloy by fusion bonding of A1, and blasting with hard particles such as alumina, glass and metal balls (air pressure) It has also been proposed that the voids generated in the A1-containing layer are filled and eliminated by projecting hard particles with (see Patent Document 8). Furthermore, the surface of the titanium alloy member containing A1 may be shot blasted with fine particles containing elements such as molybdenum, niobium, silicon, tantalum, tungsten, and chromium to form a protective film in which these fine particles are dispersed. It has been proposed (see Patent Document 9).
- Patent Document 1 Japanese Patent Application Laid-Open No. 2001-234266 (Claims)
- Patent Document 2 JP-A-2005-290548 (Claims)
- Patent Document 3 Japanese Patent Laid-Open No. 10-99976 (Claims)
- Patent Document 4 JP-A-6-88208 (Claims)
- Patent Document 5 Japanese Patent Laid-Open No. 9-256138 (Claims)
- Patent Document 6 Japanese Patent No. 3151713 (Claims)
- Patent Document 7 Japanese Unexamined Patent Application Publication No. 2006-9115 (Claims)
- Patent Document 8 Japanese Patent Laid-Open No. 2005-36311 (full text)
- Patent Document 9 Japanese Unexamined Patent Publication No. 2000-34581 (full text)
- the exhaust pipe material of the exhaust system around the engine may generate high-temperature oxidation at a high temperature such as 8 oo ° C as the temperature of the exhaust gas increases. Therefore, as an exhaust pipe material for the exhaust system around the engine, titanium materials are required to have excellent high-temperature oxidation resistance at higher temperatures. In other words, as an exhaust pipe material for the exhaust system, titanium materials are required to have excellent high-temperature acid resistance even at temperatures as high as 850 to 870 ° C, which is higher than 800 ° C depending on the model. There is.
- the high-temperature acid resistance is limited to a performance of about 800 ° C.
- the surface-treated titanium material in which fine particles are shot blasted on the surface of a titanium alloy member containing A1 of Patent Document 9 is tested by raising the oxidation conditions to a high temperature of 950 ° C, and is superior in high-temperature oxidation!
- the present invention has been made in view of such circumstances, and an object of the present invention is to provide a titanium alloy, pure titanium, or surface treatment with improved high-temperature oxidation resistance exceeding 800 ° C.
- An object is to provide a titanium material, and an engine exhaust pipe composed of the titanium alloy, pure titanium, and surface-treated titanium material at low cost and efficiently.
- a first aspect of the present invention is a titanium alloy and an engine exhaust pipe.
- the titanium alloy excellent in high-temperature oxidation resistance according to the present invention contains 0.12 to 2% by mass of Si.
- the content of A1 is regulated to less than 0.30% by mass, and the average crystal grain size of the equiaxed grain structure of the titanium alloy is 15 m or more.
- the titanium alloy excellent in high temperature oxidation resistance of the present invention contains 0.1 to 2% by mass of Si, and the content of A1 is regulated to less than 0.30% by mass. Has a needle-like structure.
- A1 is not restricted to less than 0.30% by mass
- another titanium alloy having excellent high-temperature oxidation resistance according to the present invention contains 0.12 to 2% by mass of Si.
- A1 is the total content of Si and 2
- the titanium alloy has an equiaxed grain structure, and the average grain size is
- another titanium alloy excellent in high-temperature acid resistance of the present invention contains 0.12 to 2% by mass of Si, and A1 is Si. And the titanium alloy has a needle-like structure.
- the titanium alloy of the above-mentioned gist is further combined with the Si, at least one of which Nb, Mo, Cr internal forces are also selected.
- the content or the total content of Si and A1 is preferably 2% by mass or less.
- the above-described titanium alloy further has an average Si concentration of 0.5 at% or more on the outermost surface of the titanium alloy.
- the titanium alloy according to the above gist is further provided with an average coating thickness after drying on the surface of 10 to LOO / zm, It is preferable to have an organometallic compound coating film in which the A1 content in the coating film after drying is 30 to 90% by mass
- the titanium alloy according to the gist or the preferred embodiment described later is preferably applied to an engine exhaust pipe (for engine exhaust pipe use).
- the engine exhaust pipe excellent in high-temperature acidity resistance of the present invention is composed of a titanium alloy having a preferable aspect described later or later.
- a second aspect of the present invention is pure titanium and an engine exhaust pipe.
- the pure titanium excellent in high-temperature oxidation resistance of the present invention has a needle-like structure formed by heating pure titanium to the ⁇ transformation point or higher and then cooling.
- the pure titanium has, on its surface, an average coating thickness after drying of 10 to LOOm, and an A1 content in the coating after drying of 30 to 90% by mass. It is preferable to have a compound coating film.
- the pure titanium of the above-described gist or a preferable aspect described later is applied to an engine exhaust pipe (for engine exhaust pipe use).
- the engine exhaust pipe excellent in acid resistance of the present invention is made of pure titanium as described above. It is configured.
- a third aspect of the present invention is pure titanium and an engine exhaust pipe.
- the surface-treated titanium material excellent in high-temperature oxidation resistance of the present invention is formed on the surface of pure titanium or a titanium alloy by using aluminum oxide particles widely used as shot blast particles. It has a shot blast treatment layer, and the treatment layer has an aluminum average concentration force of at% or more.
- the average crystal grain size of the equiaxed grain structure is 15 m or more is preferable.
- an aspect in which the titanium alloy has a needle-like structure is preferable in order to increase the high temperature oxidation resistance of the titanium alloy as a base material.
- the engine exhaust pipe excellent in high-temperature acid resistance of the present invention is that the exhaust pipe is made of the surface-treated titanium material.
- a fourth aspect of the present invention is a method for producing a surface-treated titanium material.
- the surface of pure titanium or a titanium alloy is shot blasted with aluminate particles, and the aluminate particles used for the shot blasting are used.
- the aggregate as a whole contains 80% by mass or more of aluminate.
- Another method for producing the surface-treated titanium material of the present invention is a method in which the surface of pure titanium or a titanium alloy is shot blasted with aluminate particles, and the aluminate particles subjected to the shot blasting process. Contains 80% by mass or more of aluminate in a single particle.
- the titanium alloy of the present invention includes a specific amount of Si, and by actively regulating A1, it has a resistance to a higher temperature of about 850 ° C, which is higher than 800 ° C. High temperature acidity can be improved.
- the structure of pure titanium is changed to the acicular grain structure of the conventional equiaxed grain force to improve the high temperature acid resistance.
- Patent Documents 1 to 5 it is also known in Patent Documents 1 to 5 that various surface treatments of the A1 series are performed in order to increase the high temperature acid resistance of the titanium material.
- the various A1 surface treatments of these titanium materials have an effect on high-temperature acidity resistance of about 800 ° C.
- the strength exceeds 800 ° C and the higher temperature resistance of 850 ° C.
- the present invention has a surface treatment layer in which aluminate particles are embedded in a titanium material by shot blasting to form a titanium matrix and an aluminate body.
- This surface treatment layer improves the oxidation resistance at a higher temperature of 850 ° C exceeding 800 ° C.
- FIG. 1 is a drawing-substituting photograph showing the fine equiaxed grain structure of the titanium alloy of the present invention.
- FIG. 2 is a drawing-substituting photograph showing the coarse equiaxed grain structure of the titanium alloy of the present invention.
- FIG. 3 is a drawing-substituting photograph showing the acicular structure of the titanium alloy of the present invention.
- FIG. 4 is a drawing-substituting photograph showing an acicular structure of pure titanium of the present invention.
- FIG. 5 is a drawing-substituting photograph showing the equiaxed grain structure of conventional pure titanium.
- the titanium alloy according to the first embodiment of the present invention contains 0.1 to 2% by mass of Si, the content of A 1 is regulated to less than 0.30% by mass, and the titanium alloy has equiaxed crystal grains.
- the average grain size of yarn and weave is 15 m or more.
- the titanium alloy of the present invention contains 0.12 to 2% by mass of Si in order to improve high-temperature acid resistance (hereinafter also simply referred to as high-temperature oxidation resistance) exceeding 800 ° C.
- A1 is regulated to less than 0.30% by mass, and the remainder is composed of titanium and inevitable impurities.
- Si is an element essential for improving high-temperature acid resistance. Si also improves high temperature strength. For this purpose, it is necessary to contain 0.15% by mass or more of Si. On the other hand, if the Si content exceeds 2% by mass, it becomes difficult to form a calorie on the exhaust pipe of titanium alloy, which causes a significant deterioration in formability.
- A1 like Si, Nb, Mo, and Cr, is an element that improves high temperature acid resistance.
- A1 when the operating temperature of the titanium alloy exceeds 800 ° C, the action of causing the exfoliation of the oxide scale appears, and this exfoliation does not suppress the diffusion and entry of oxygen into the substrate. As a result, the acid resistance is deteriorated. Accordingly, in the present invention, A1 is positively regulated to less than 0.30% by mass, which is a range that does not cause the above-described adverse effects.
- the high temperature oxidation resistance due to A1 is remarkably reduced, and it is necessary to positively regulate A1 to less than 0.30% by mass.
- the titanium alloy has a fine equiaxed grain structure with an average grain size of less than 15 m (corresponding to claim 1).
- the structure of the titanium alloy is a relatively coarse equiaxed grain structure with an average crystal grain size of 15 m or more, or when the titanium alloy is a needle-like structure
- A1 is 0.30 mass It is not necessary to regulate to less than% (corresponding to claims 4 and 5). This is because the decrease in the high temperature acidity resistance due to A1 is suppressed by the improvement in the high temperature acidity resistance due to these relatively coarse equiaxed crystal grain structures or needle-like structures. Therefore, when the titanium alloy has these relatively coarse equiaxed grain structures or needle-like structures, it is allowed to contain A1 in a total content of 2% by mass or less with Si.
- Nb, Mo, and Cr are effective in improving the high-temperature oxidation resistance of 800 ° C and higher temperatures of about 850 ° C. Synergistic effects can be expected by adding (coexisting) with Si. Therefore, the present invention titanium alloy is further, Nb, Mo, 1 kind or 2 or more internal forces Cr is also selected, 2 mass 0/0 or less in a total amount of the S Fireflys is Si and A1 May be included. If the total amount of these elements with Si, or if A1 is included in a substantial amount (0.30% by mass or more), if the total amount of Si and A1 exceeds force% by mass, the formability deteriorates. It becomes difficult to form the exhaust pipe. Therefore, if the total amount of these elements with Si, or the substantial amount of A1 (0.30 mass% or more) is included, the total amount of Si and A1 should be 2 mass% or less.
- a titanium alloy contains oxygen and iron as main impurity elements in a melting raw material and a melting process. These oxygen and iron deteriorate the formability of the titanium alloy into the shape of the exhaust pipe. Therefore, even if it is included, the total content of oxygen and iron is preferably 0.20% by mass or less! /.
- Cu deteriorates the high-temperature oxidation resistance.
- Cu is effective in enhancing the high-temperature strength characteristics as an exhaust pipe. Therefore, Cu may be contained in an amount of 2% by mass or less in terms of the total content of S, Si, A, Si, A1, Nb, Mo, and Cr.
- the Cu content is preferably 0.5% by mass or less, more preferably 0.3% by mass or less.
- the titanium alloy set of the present invention Weaving is a preferred embodiment described below. That is, the average concentration of Si on the outermost surface of the titanium alloy To increase the average grain size of the titanium alloy structure, and to have a needle-like structure
- the titanium alloy structure is selected from one or more. A synergistic effect can also be expected by using these tissues in appropriate combination with the above component composition.
- the average concentration of Si on the outermost surface of the titanium alloy is preferably 0.5 at% or more in order to further improve the high temperature oxidation resistance.
- the Si concentrated on the outermost surface may be Si dissolved in titanium. Ti such as Ti Si and Si
- the Si concentration on the outermost surface basically increases with the Si content of the titanium alloy (base material). If manufactured, the average concentration of Si on the outermost surface of the titanium alloy may be increased to 0.5 at% or more. However, on the other hand, depending on the manufacturing method, a surface contamination layer such as oxygen or carbon may exist up to a depth of several meters. In such a case, the average concentration of Si present on the outermost surface Is less than 0.5 at%, and it is highly possible that an excellent effect of improving high-temperature acid resistance is not expected. Therefore, the Si concentration on the outermost surface of the titanium alloy is not uniformly determined by the Si content of the titanium alloy. For this reason, when the average concentration of Si on the outermost surface of the titanium alloy is 0.5 at% or more, it is preferable to select manufacturing conditions that do not form a surface contamination layer such as oxygen or carbon.
- the Si concentration on the outermost surface of the titanium alloy was determined by surface quantitative analysis using a wavelength dispersion method (Wave Dispersive Spectroscopy, abbreviated as WDS) in X-ray microanalysis analysis (Electron Probe Micro Analysis, abbreviated as EPMA). It can be measured. More specifically, the analysis part on the outermost surface is expanded to X500 to X1000, first the existing elements are examined by qualitative analysis, and then each concentration is quantitatively determined by semi-quantitative analysis using the ZAF method. I can do it. The concentration of the outermost surface varies depending on the penetration depth of the electron beam at the time of analysis.
- WDS wavelength dispersion method
- EPMA Electro Probe Micro Analysis
- the Si concentration on the outermost surface in the present invention means the average concentration of Si from the surface to a depth of about 1 to 2.5 ⁇ m.
- the Si concentration on the outermost surface means the concentration defined in this way.
- the titanium alloy structure of the present invention When manufactured by a conventional method, the titanium alloy structure of the present invention becomes equiaxed grains as usual. This equiaxed grain structure ensures properties such as formability and mechanical properties (strength) of the titanium alloy.
- the average crystal grain size greatly contributes to the high temperature acidity of the titanium alloy. That is, high temperature oxidation resistance is improved when the average crystal grain size is somewhat large. Specifically, this effect appears when the average crystal grain size is 15 m or more, preferably 20 ⁇ m or more, more preferably 30 ⁇ m or more.
- the average crystal grain size becomes excessively large, problems such as rough skin during molding and a decrease in fatigue strength occur.
- the upper limit of the average crystal grain size is It is about 100 / zm.
- Ti-Si series titanium alloy of the present invention is manufactured by a conventional method, Ti such as Ti Si and Si and Si
- Intermetallic compounds and j8 phases are dispersed and formed in the matrix titanium, which suppresses the growth of crystal grains.
- This effect of suppressing crystal grain growth of Si is also described in Patent Document 2. For this reason, it is difficult to increase the average crystal grain size to 15 m or more, which is effective in suppressing high-temperature oxidation by a conventional method, particularly in a titanium alloy containing Si.
- the rolling reduction of cold rolling which can be said to be a conventional method for producing a titanium alloy, is approximately 20 to 70% although it differs depending on the material.
- the temperature of annealing performed thereafter is 600 to 800 ° C
- the temperature on the low temperature side is about 600 to 700 ° C for annealing such as vacuum annealing that takes a long time of several hours to tens of hours.
- the conditions are adopted, and in the short time treatment such as continuous annealing pickling, the temperature condition on the high temperature side of 700-800 ° C is adopted.
- the average grain size of Ti-S titanium alloy of the present invention is cold-rolled and annealed, the average grain size is increased to 15 m or more. Difficult to do. In other words, when the average grain size of Ti-S titanium alloy is 15 / zm or less, it is manufactured within the range of this ordinary method.
- the reduction ratio of the cold rolling is reduced to 20% or less, and the annealing temperature is decreased.
- the preferred rolling reduction is 15% or less, more preferably 10% or less.
- the preferable annealing temperature is 850 ° C. or higher and ⁇ transformation point or lower. When this annealing temperature exceeds 8) the transformation temperature, a needle-like structure described later is formed. Therefore, when it is important to make the crystal grains of the member equiaxed grains and to obtain good formability and mechanical properties stably industrially, the upper limit of the annealing temperature is set to the ⁇ transformation point temperature or lower.
- the structure of the titanium alloy is a relatively coarse equiaxed grain structure with an average grain size of 15 / zm or more, as described above, A1 is not restricted to less than 0.30% by mass. It's okay. In other words, the action of these relatively coarse equiaxed grain structures improves the high-temperature oxidation resistance, and thus suppresses the high-temperature acidity reduction effect by A1. This effect becomes greater as the average grain size of the titanium alloy is larger.
- the crystal grain size referred to in the present invention is an average crystal grain size in a cross section in the rolling (L) direction of a titanium alloy.
- This crystal grain size was measured by using a 100x optical microscope to observe the surface of the sample (test piece) taken from the titanium alloy plate after mirror-polishing after 0.05-0.1 mm cross-section and mirror polishing.
- the line intercept method is used to measure in the above direction.
- the measurement line length is 0.95 mm
- the total measurement line length is 0.95 x 15 mm by observing a total of 5 fields with 3 lines per field. In this way, the average grain size measured at any 10 locations in the center of the titanium alloy plate excluding the front and rear ends of the plate was further averaged to obtain the average grain size of the titanium alloy.
- the diameter is an average crystal grain size in a cross section in the rolling (L) direction of a titanium alloy.
- the oxidation resistance is higher than 800 ° C.
- the titanium alloy may be made into a needle-like structure.
- the structure of the titanium alloy is a needle-like structure, as described above, A1 may not be regulated to less than 0.30% by mass.
- These needle-like structures suppress the decrease in high-temperature oxidation resistance due to A1 because the high-temperature oxidation resistance is improved. Note that when the annealing temperature of the titanium alloy of the present invention becomes higher than the ⁇ transformation point, the entire structure of the titanium alloy becomes the needle-like structure.
- the structure of a titanium alloy exhibits an equiaxed structure because it is finally annealed at the ⁇ transformation point or less after cold rolling.
- an acicular structure is preferred rather than an equiaxed grain.
- the method for forming the needle-like structure is not particularly limited, but the titanium alloy can be formed by, for example, cold rolling, and finally heating and cooling after the j8 transformation point.
- this needle-like structure is not related to the rolling reduction of cold rolling (even if the rolling reduction is not controlled), but only
- FIGS. 1 and 2 The cross-sectional microstructure of the equiaxed grains of the present invention is shown in FIGS. 1 and 2 (drawing substitute photos), and the cross-sectional microstructure of the needle-like structure of the present invention is shown in FIG. 3 (drawing substitute photos).
- Figs. 1 and 2 show the cross-sectional microstructure of the titanium alloy with a 100x optical microscope, and Fig. 3 with a 200x optical microscope.
- the structure in the case of Fig. 1, it exhibits an equiaxed structure and the average grain size is 15 m or less. Yes.
- the structure in the case of Fig. 2, the structure is equiaxed as in Fig. 1, but the average crystal grain size is increased to about 30 m by the combination of the low pressure reduction rate and high temperature annealing described later.
- the structure in the case of Fig. 3, the structure is a needle-like structure because the force is cooled by heating above the ⁇ transformation point described later.
- the titanium alloy in FIG. 1 is a Ti-0.5Si-0.1AH) .2Nb alloy of the present invention (both numbers are mass%), and after cold rolling at a rolling reduction of 40%, it is 6 ° C at 800 ° C. It has been subjected to minute atmospheric annealing.
- the titanium alloy shown in Fig. 2 is obtained by cold rolling the above alloy at a reduction rate of 10% and then annealing at 850 ° C for 6 minutes.
- the titanium alloy in Fig. 3 is obtained by cold rolling the above alloy at a rolling reduction of 40%, heating to 950 ° C exceeding j8 transformation point of about 900 ° C for 6 minutes, and then cooling.
- this acicular structure is clearly defined by a manufacturing method that is a history. That is, this acicular structure is defined as an acicular structure generated by a heat treatment in which the titanium alloy is heated to the
- the production method of the titanium alloy of the present invention has preferable aspects of the above production method and conditions for creating a structure
- the process itself is ingot melting, hot forging, hot rolling, annealing, cold rolling, It can be manufactured by a conventional method that also has annealing or heat treatment.
- the preferable structure for improving the high temperature oxidation resistance is changed by changing the cold rolling, annealing or heat treatment conditions.
- the titanium alloy of the present invention obtained as described above is excellent in high-temperature oxidation resistance of about 850 ° C. and can be used without surface treatment. However, it is not limited to bare without surface treatment in this way, but it can be used with various surface treatments!
- the surface treatment film itself has excellent high-temperature oxidation resistance at a higher temperature of about 850 ° C.
- the average film thickness after drying is 10 to: LOO m, and A1 content in the film after drying
- An organometallic compound coating film whose amount is 30 to 90% by mass is preferred.
- This organometallic compound coating film is stable and handles, such as nursem titanium, nursem zirconium, chromium acetate, silicone, silica sol, alumina sol and aluminum isopropoxide containing A1 pieces or A1 powder.
- This is a coating film of organometallic compounds that is easy to use and has low toxicity.
- a well-known method such as application or dipping of a coating solution such as an aqueous solution or solvent of an organometallic compound containing a predetermined amount of A1 or a dispersion liquid onto the surface of the titanium alloy of the present invention. Paint at a temperature of 200 ° C or less. If the coating film is dried at 200 ° C or less after coating, higher resistance to high-temperature oxidation can be expected.
- a coating solution such as an aqueous solution or solvent of an organometallic compound containing a predetermined amount of A1 or a dispersion liquid onto the surface of the titanium alloy of the present invention. Paint at a temperature of 200 ° C or less. If the coating film is dried at 200 ° C or less after coating, higher resistance to high-temperature oxidation can be expected.
- An organic metal compound coating film having an average coating film thickness after drying of 10 to LOO m and an average A1 content of 30 to 90% by mass in the coating film after drying. To do. If the average film thickness (film thickness) after drying is less than 10 ⁇ m, the underlying titanium is exposed to the corrosive atmosphere through defects such as pinholes, and the thickness of the coating itself is too small. The protective property of the groundwork cannot be obtained, and there is no meaning as a paint film.
- the average coating thickness (film thickness) after drying exceeds 100 m, the coating film is easily peeled off due to the influence of film stress and the like. Therefore, the average film thickness after drying should be in the range of 10 to: LOO / zm.
- the average coating thickness after drying can be measured by observing, measuring, and averaging the coating film cross-section, for example, at any 10 locations with an optical microscope.
- the average A1 content in the coating film after drying is less than 30% by mass, the effect of improving the high-temperature acidity resistance at higher temperatures is insufficient, and conversely if it exceeds 90% by mass Insufficient coating strength leads to premature destruction of the coating due to external forces or shrinkage of the substrate. Therefore, the average A1 content in the coating after drying is in the range of 30 to 90% by mass. A1 content in this coating The amount can be measured by analyzing the coating film surface or coating film cross section, for example, at any 10 locations by EPMA and averaging.
- the shape of A1 (added) in the coating film is scale-like that has the best resistance to high-temperature oxidation, even in a powdery form or a mixture of scale-like and powdery form. It is possible to obtain high temperature oxidation characteristics.
- the reason why the coating film (coating) improves the high-temperature oxidation resistance of about 850 ° C is that the coating film containing A1 itself has resistance to high-temperature oxidation. This is probably because when A1 is exposed to high temperature, A1 in the coating film reacts with titanium of the base material to form a layer having resistance to high temperature oxidation.
- the titanium cold-rolled sheets having the component compositions shown in Tables 1 and 2 were evaluated for high-temperature oxidation resistance at high temperatures at 850 ° C. Specifically, about 120 g of soot having the composition shown in Tables 1 and 2 was melted in a button arc furnace. To add titanium, the surface was cleaned cleanly and JIS Class 1 pure titanium scrap material was used. Each ingot was hot-forged, hot-rolled, and annealed by conventional methods, and then cold-rolled at a predetermined reduction rate. Thereafter, the cold-rolled sheet was degreased and annealed at a predetermined temperature and condition, and a cold-rolled sheet having a thickness of 2 mm was produced in common. And harvested the specimen 2mmt X 25mm w X 25mm 1 from the cold-rolled plate.
- examples in which the average crystal grain size of the test piece is 10 m or less indicate the rolling reduction ratio of the titanium alloy, About 40% within the range of ordinary methods. Thereafter, vacuum annealing was performed at 800 ° C for 6 minutes.
- the average crystal grain size of the test piece exceeds 15 m is different from the above-mentioned conventional method.
- the cold rolling of the titanium alloy is performed.
- the rolling force was reduced by selecting a range force of 20% or less, and a vacuum annealing was selected at a temperature range of 825 ° C or more and a ⁇ transformation point or less, and the soaking time was 6 minutes.
- the rolling reduction of the cold rolling was approximately 40% within the range of the ordinary method, and this cold rolled sheet was soaked at 950 ° C exceeding the / 3 transformation point of the titanium alloy. Vacuum heating for 6 minutes.
- the structure of the whole specimen collected from the specimen thus obtained was a needle-like structure.
- the average concentration of Si on the outermost surface of the titanium alloy is 0.5 at% or more.
- the example of enrichment of the outermost surface Si is that after cold rolling with a rolling reduction of about 40%, instead of vacuum annealing, After atmospheric annealing for 5 minutes, a 600 ° C molten salt (NaNO 55% by mass, NaOH 35% by mass, remaining so as not to have a surface contamination layer such as oxygen or carbon on the outermost surface of the titanium alloy to a depth of several meters) KC1, NaCl
- the average crystal grain size of the test piece under this production condition is 10 ⁇ m or less, and an example in which the average crystal grain size of the test piece exceeds 15 m is that the reduction ratio in cold rolling is 20% or less.
- the range force was also selected, and the reduction rate was made smaller to obtain a larger average grain size.
- the concentration of the outermost surface Si in the example in which the structure was a needle-like structure was performed by replacing only the above-mentioned atmospheric annealing process with a condition of 950 ° C exceeding the ⁇ transformation point of the titanium alloy for 6 minutes. The same process and conditions for the concentration of the uppermost surface Si were performed.
- the amount of Si on the outermost surface of each test piece was analyzed by the following method. In other words, the number of samples before analysis After ultrasonic cleaning with acetone for 5 minutes to remove contaminants such as oil adhering to the surface, analysis was performed using an EPMA analyzer JXA-8900RL manufactured by JEOL. The analysis magnification was X500, the acceleration voltage was 15 kv, the elements present on the surface were examined by qualitative analysis, and the abundance of the existing elements was determined by semi-quantitative analysis using the ZAF method.
- High temperature oxidation resistance was evaluated by a high temperature oxidation test. That is, when these specimens were exposed to a high-temperature atmosphere at a higher temperature of 850 ° C, higher than 800 ° C for 100 hours, the weight increase of the specimens before and after the high-temperature oxidation test (oxidation increase: mgZcm 2 ) was measured. And the smaller the increase in weight, the better the high-temperature oxidation resistance. For samples in which exfoliation of the oxide scale was observed, the weight of the exfoliated oxide scale was taken into account for this weight measurement. Tables 1 and 2 show these results.
- Inventive Examples 1 to 11 satisfy the component composition requirements within the range on the assumption that the structure is a fine equiaxed grain having an average crystal grain size of less than 10 m.
- Invention Example 3 containing Si alone, close to its lower limit of 0.15% by mass, is 850 ° C. in comparison with the other Invention Examples 4 and 5 having a higher Si content.
- High temperature resistance to acidity at Therefore, the effect of improving the high-temperature acid resistance at 850 ° C of Si alone is supported.
- Inventive Example 5 had a Vickers hardness of 230 points when the Si content was close to the upper limit of 2% by mass, which was about 50 to 80 points higher than the other inventive examples. For this reason, it is expected that the forming force of the titanium alloy on the exhaust pipe is difficult.
- Inventive example 2 which has a relatively high A1 content, has the same Si content and a relatively low A1 content, compared to Inventive example 1, each of which has a high temperature resistance to high temperatures at 850 ° C. However, it is relatively inferior because the scale peeling easily occurs.
- the significance of regulating the A1 content to less than 0.30% by mass in order to improve the high-temperature acid resistance at higher temperatures is supported. It is done.
- Nb, Mo, and Cr Si is added in combination with Si, and the Si content is the same. High temperature and high temperature resistance is relatively excellent. Therefore, the higher temperature resistance to high temperature resistance of titanium alloys of Nb, Mo and Cr is supported.
- Inventive Examples 12 to 26 assume the average crystal grain size and the average concentration of the outermost surface Si on the assumption that the structure is equiaxed grains.
- the average crystal grain size is 15 m or more, and the average crystal grain size is The larger the example, the better the high-temperature acidity resistance at 850 ° C. Therefore, the effect of improving the high-temperature resistance to high-temperature acidity due to the coarsening of the crystal grain size is supported.
- Inventive examples 27 to 35 in Table 2 have an average concentration of Si on the outermost surface, assuming a needle-like structure.
- Inventive Examples 28, 30, and 31 are compared with Inventive Examples 27 and 29 in which the A1 content is suppressed to 0.30 mass% or less even though the A1 content exceeds 0.30 mass%. Although they are slightly inferior, they each have excellent high-temperature acid resistance at 850 ° C. This confirms the effect of improving the high-temperature oxidation resistance at higher temperatures while suppressing the adverse effects of A1 content due to the needle-like structure.
- Inventive Example 35 in which the outermost surface Si concentration is enriched is superior in high temperature acid resistance at 850 ° C to Inventive Example 27 in which no enrichment is performed. Therefore, the combined effect of acicular organization and concentration of the outermost surface Si concentration supports the effect of improving the high-temperature high-temperature acid resistance.
- Inventive Examples 32 and 33, Nb, Mo and Cr are added in combination with Si, and the Si content is the same. High temperature oxidation resistance is relatively excellent. Therefore, the combination of the needle-like structure and the addition of Nb, Mo, and Cr supports the higher temperature resistance to high temperature resistance of titanium alloys.
- Comparative Examples 36 to 40 although the A1 content is suppressed to 0.30 mass% or less, the Si content is too small.
- Comparative Examples 37 to 40 include the use of Nb, Mo, Cr combined addition, crystal grain coarsening, acicular organization, etc. for improving high temperature acid resistance. Regardless, the high-temperature acid resistance at 850 ° C is remarkably inferior. Therefore, the improvement effect of high-temperature acid resistance at 850 ° C of Si compared to these other means is supported.
- Comparative Examples 41 and 42 have too much Si content. For this reason, the Vickers hardness was 280 to 300 points, which was about 50 to 70 points higher than that of Invention Example 5 having an upper Si content. For this reason, it is expected that molding of the titanium alloy into the exhaust pipe cannot be performed. These support the significance of the upper limit of Si content.
- Comparative Examples 43 and 44 are fine equiaxed grains with an average crystal grain size of less than 10 ⁇ m, and there is no thickening of the outermost surface Si concentration. In addition, the A1 content exceeds the upper limit. Pass. As a result, Comparative Examples 43 and 44 are significantly inferior in high-temperature acid resistance at 850 ° C. Combined with the results of the invention examples having a high A1 content, the significance of regulating the A1 content to less than 0.30% by mass in order to improve high temperature acid resistance at 850 ° C is supported. .
- the high temperature acidity test of the titanium alloy test piece of the present invention provided with the coating film is performed under the same conditions as described above, and each oxidation increase is measured.
- Each of these oxidation increases (A) and the titanium alloy of the present invention shown in Tables 1 and 2 corresponding to the titanium alloy of the present invention provided with this coating film (without the coating film) were used in the high-temperature oxidation test.
- the ratio (AZB) to the increase in amount (B) was determined, and the high temperature oxidation resistance of the coating film was evaluated. It can be said that the smaller the acid increase ratio AZB, the higher the contribution to the high temperature acid resistance on the coating film side, and the higher the high temperature acid resistance of the coating film.
- the evaluation of high-temperature oxidation resistance is ⁇ when the acid-to-acid increase ratio AZB is 0.45 or less, ⁇ exceeding 0.45 to 0.65, and X exceeding 0.65. evaluated.
- test piece For the coating, use the same test piece as in the above example, and have a film thickness (film thickness after drying) as shown in Table 3 and an A1 content in the coating film (A1 content after drying).
- the test piece was dip-coated in a solution containing a non-modified silicone resin containing scaly A1 and an organic solvent.
- Drying after painting is as follows: (1) Temporary drying at 120 ° CX for 15 minutes, followed by main drying at 190 ° CX for 30 minutes (shown in Table 3 as a drying temperature of 190 ° C), (2) Preliminary drying was performed at 120 ° CX for 15 minutes, followed by main drying at 210 ° CX for 30 minutes (described in Table 3 as a drying temperature of 210 ° C).
- the average film thickness after drying which is the above-mentioned preferable condition range, is 10 to: LOO / zm, and the A1 content in the coating film after drying is 30 to 90.
- Examples 48 and 55 to 57 of the organic metal compound coating film having a mass% are excellent in high temperature oxidation property of the coating film.
- the difference in the oxidation increase in the high-temperature oxidation test is small, and the difference in the oxidation increase is relatively large. Excellent in properties.
- Examples 47 and 49 in which the average film thickness after drying is the lower limit and upper limit of the preferred range, Examples 50, A1 content in the coating film after drying is the lower limit and upper limit of the preferred range 50 51, or drying temperature is preferred, and out of range is too high.Example 52 is preferred and out of range.
- the high temperature oxidation property of the coating film is superior.
- the high-temperature acidity of the coating film is inferior to Examples 48 and 55 to 57 in which the coating film condition is the above-described preferable condition range.
- the pure titanium is heated above the transformation point. It has the needle-like structure
- pure titanium itself of the present invention
- ordinary pure titanium having the purity of 99.5% by mass or more and from the fourth type to the first type as defined in the JIS standard can be used.
- the purity of JIS standard type 1 pure titanium is 99.8 mass% or more
- the purity of type 2 pure titanium is 99.7 mass% or more.
- the crystal grain of pure titanium has a needle-like structure that is not equiaxed grains.
- the method for forming this needle-like structure is not particularly limited, and it can be made into a needle-like structure by heating pure titanium above the j8 transformation point.
- a needle-like structure can be obtained by heating after cooling above the 8 transformation point and cooling.
- the cooling may be air cooling, water cooling or furnace cooling.
- Fig. 4 shows the cross-sectional microstructure of the needle-like structure of Type 2 pure titanium of the present invention
- Fig. 5 drawing substitute shows the cross-sectional microstructure of the equiaxed grain structure of Type 2 pure titanium for comparison.
- Photo shows each.
- the pure titanium in Fig. 4 is Invention Example 2 in Table 4 to be described later, and after the second type pure titanium is cold-rolled at a rolling reduction of 40%, it exceeds the ⁇ transformation point at 950 ° C for 6 minutes. It is air-heated and then cooled (cooled).
- the pure titanium in Fig. 4 is Comparative Example 5 in Table 4 described later, and is obtained by subjecting Type 2 pure titanium to atmospheric annealing at 800 ° C for 6 minutes after cold rolling at a rolling reduction of 40%. is there.
- the acicular structure of Fig. 4 is clearly defined by the manufacturing method that is the history of the acicular structure. That is, this needle-like structure is a needle-like structure generated by a heat treatment in which pure titanium is heated to the
- the formation of the needle-like structure or the equiaxed grain structure is the temperature of the final annealing as described above. After cold rolling, the needle-like structure is heated to more than 8 transformation points to cool the force, so that it is necessarily pure titanium and pure titanium material regardless of the previous cold rolling reduction ratio. Can be obtained over the entire surface.
- an equiaxed grain structure is inevitably obtained by annealing at a temperature below the ⁇ transformation point after cold rolling in the case of pure titanium. In this regard, even if heating at a temperature lower than the j8 transformation point is not performed immediately after the cold rolling, and heating is performed at a low temperature during this time, if it is finally heated above the j8 transformation point (the final heating temperature is ⁇ transformation). If it is above the point, a needle-like structure is obtained.
- This needle-like structure (used in the present invention) may be made into a needle-like structure using pure titanium itself having a commercially available equiaxed structure.
- pure titanium until it becomes a needle-like structure is ingot-melted, hot forged, hot rolled, annealed, cold It can be manufactured by conventional methods (commercially pure titanium manufacturing method), which are hot-rolled and annealed or heat-treated as necessary.
- the pure titanium of the present invention obtained as described above is excellent in high-temperature oxidation resistance of about 800 ° C. and can be used without surface treatment. However, it may be used after being subjected to various surface treatments as well as naked without surface treatment.
- the surface treatment film itself is excellent in high-temperature acid resistance at about 800 ° C.
- the average film thickness after drying is 10 to: LOO ⁇ m, and the A1 content in the dried film is 30 to 90% by mass.
- a metal compound coating film is preferred.
- This organometallic compound coating film contains A1 scale or A1 powder, nursem titan, nursem zirconium, chromium acetate, silicone, silica sol, alumina sol, and alumina sol. It is a coating film of organometallic compounds, such as lumi-mu isopropoxide, which is stable, easy to handle, and has low toxicity.
- Such an organic metal compound solution containing a predetermined amount of A1 or a solution using a solvent, or a coating material having a dispersion force is applied to the pure titanium surface of the present invention by a known method such as coating or dipping.
- a known method such as coating or dipping.
- the coating film is dried at 200 ° C or lower after coating, the coating film can be expected to have high-temperature acid resistance.
- the coating film is dried at a high temperature exceeding 200 ° C after coating, the drying and curing reaction of the coating film occurs rapidly, depending on the type of the coating film.
- the powder is fixed in a state where a lot of space is formed in the coating film, and this space allows oxygen to enter, and as a result, it may be difficult to obtain excellent high-temperature acid resistance.
- the coating film is dried at 200 ° C or less, it takes time to dry, so the A1 scales and A1 powder move to the position to fill the space and harden, so the space in the coating film is reduced. As a result, excellent high-temperature oxidation resistance can be obtained.
- An organic metal compound coating film having an average coating film thickness after drying of 10 to: LOO m and an average A1 content of 30 to 90% by mass in the coating film after drying. To do. If the average film thickness (film thickness) after drying is less than 10 ⁇ m, the underlying titanium is exposed to the corrosive atmosphere through defects such as pinholes, and the thickness of the coating itself is too small. The protective property of the groundwork cannot be obtained, and there is no meaning as a paint film.
- the average coating thickness (film thickness) after drying exceeds 100 m, the coating film is easily peeled off due to the influence of film stress and the like. Therefore, the average film thickness after drying should be in the range of 10 to: LOO / zm.
- the average coating film thickness after drying can be measured by observing, measuring, and averaging the coating film cross section, for example, at any 10 locations with an optical microscope.
- the average A1 content in the coating after drying is less than 30% by mass, the effect of improving high-temperature acid resistance is insufficient. Conversely, if the content exceeds 90% by mass, Insufficient strength leads to premature destruction of the coating film due to external forces and shrinkage of the substrate. Therefore, the average A1 content in the dried film is in the range of 30 to 90% by mass.
- the A1 content in the coating film can be measured by analyzing the coating film surface or coating film cross-section, for example, at any 10 locations by EPMA and averaging.
- the shape of A1 (added) in the coating film is the scale having the highest resistance to oxidation resistance at high temperatures. Even in powder form, or in a mixture of scale form and powder form, it is resistant to higher temperatures.
- High temperature oxidation resistance was evaluated by a high temperature oxidation test. That is, when these test pieces were exposed to a high-temperature atmosphere at 800 ° C. for 100 hours, the weight gain of the test pieces before and after the high-temperature oxidation test was measured (acid salt increase: mgZcm 2 ). And it was evaluated that the pure titanium example with a small weight increase was excellent in high temperature oxidation resistance. Table 4 shows these results.
- Invention Examples 1 to 4 have a needle-like structure defined in the present invention. As a result, it has excellent high-temperature oxidation resistance and excellent high-temperature oxidation resistance, as well as first-class power and fourth-class pure titanium.
- Comparative Examples 5 to 8 are conventional equiaxed grain yarns and weaves, compared with Invention Examples 1 to 4, 1 type power Even to the 4th type pure titanium, the high temperature acid resistance is remarkably inferior.
- the high-temperature acidity test of the pure titanium test piece of the present invention provided with the coating film is performed under the same conditions as described above, and each oxidation increase is measured.
- (A) corresponding to the pure titanium of the present invention provided with this coating film, the pure titanium of the present invention shown in Table 4 (without the coating film).
- the ratio (AZB) to the amount of increase in acid (B) was determined, and the high temperature oxidation resistance of the coating film was evaluated.
- the smaller the oxidation increase ratio AZB is, The contribution ratio to the high temperature acidity is high, and it can be said that the high temperature acid resistance of the coating film is high.
- Table 5 in the high temperature oxidation resistance evaluation, the oxidation increase ratio AZB was evaluated as ⁇ when the AZB ratio was 0.5 or less, ⁇ exceeding 0.5 and 0.7, and X exceeding 0.7.
- test piece For coating, use the same test piece as in the above example, and have a film thickness (film thickness after drying) as shown in Table 5 and an A1 content in the coating film (A1 content after drying).
- the test piece was dip-coated in a solution containing a non-modified silicone resin containing scaly A1 and an organic solvent.
- Drying after painting is as follows: (1) Temporary drying at 120 ° CX for 15 minutes, followed by main drying at 190 ° CX for 30 minutes (shown in Table 5 as a drying temperature of 190 ° C), (2) Preliminary drying was performed at 120 ° CX for 15 minutes, followed by main drying at 210 ° CX for 30 minutes (indicated in Table 5 as a drying temperature of 210 ° C).
- the average film thickness after drying which is the above-mentioned preferable condition range, is 10 to: LOO / zm, and the A1 content in the coating film after drying is 30 to 90.
- Examples 10 and 17 to 19 of the organic metal compound coating film having a mass% are excellent in high-temperature oxidation property of the coating film. That is, the increase in the amount of acid in the high-temperature acid test is less than the corresponding pure titanium of the present invention shown in Table 4 where no coating film is provided, and the high-temperature acidity of the coating film is excellent. .
- Examples 9 and 11 in which the average coating thickness after drying is the lower limit and upper limit of the preferred range, Examples where the A1 content in the coating after drying is the lower limit and upper limit of the preferred range Examples 12, 13 or 14 where drying temperature is preferred and range power is too high are higher than Example 14, and examples 15 and 16 where range power is also out of favor are superior in high-temperature oxidation properties of the coating film.
- the high-temperature oxidizability of the coating film is inferior to Examples 10 and 17 to 19, which are the preferable condition ranges described above.
- the surface-treated titanium material according to the third embodiment of the present invention has a shot blast treatment layer made of aluminate particles on the surface of pure titanium or a titanium alloy, and the aluminum average concentration force of this treatment layer. It is at% or more.
- the aluminate particles are used as a shot. By blasting, it is jetted and projected onto the titanium material surface at high speed. Then, aluminum oxide particles are embedded in the surface of pure titanium or titanium alloy, which is a titanium material, and a treatment layer integrated with the base material titanium mainly composed of aluminum oxide is formed. As described above, this aluminum oxide is the main component.
- the treatment layer integrated with the base material titanium improves the high-temperature oxidation resistance at higher temperatures such as 850 ° C exceeding 800 ° C.
- the aluminum oxide content (aluminum oxide concentration) of the buried layer of aluminum oxide particles (shot blasting layer) is 4 at% or more as the aluminum concentration.
- the average aluminum concentration (content: at%) in the shot blast treatment layer is the wavelength dispersion method (Wave Dispersive Spectroscopy, abbreviated WDS) in X-ray microanalysis (Electron Probe Micro Analysis, abbreviated EPMA).
- WDS Wide Dispersive Spectroscopy
- EPMA Electro Probe Micro Analysis
- the concentration of the outermost surface varies depending on the penetration depth of the electron beam at the time of analysis. By making the acceleration voltage at the time of analysis constant at 15 kv, the penetration depth of the electron beam is about 1 to 2.5 m. Therefore, the average aluminum concentration in the present invention means the average aluminum concentration from the surface of the shot blasting layer to a depth of about 1 to 2.5 ⁇ m.
- the average aluminum concentration in the shot blasted layer is the concentration defined in this way. means.
- the shot blasted layer tends to be a film or layer having a discontinuous thickness greatly different from a film or layer having a continuous thickness on the titanium surface. For this reason, it is very difficult to measure the actual thickness of the shot blasted layer, average it, quantify it, or numerically define it as a preferred thickness. Even if the film or layer has a continuous thickness, it is very difficult to determine the same amount because the thickness varies greatly.
- the cross-sectional observation ability of an optical microscope at a magnification of about 100 times at an arbitrary number of locations on the surface of the titanium can be described as an average thickness measured and discontinuous, even if it is a continuous layer with a continuous thickness.
- the shot blasted layer preferably has an average thickness of 1 / zm or more.
- the shot blasted layer is too thick, there is a risk of excessive shot blasting causing deformation of the titanium base material, and it is not necessary to increase the thickness beyond 20 m on average.
- a treatment layer integrated with titanium oxide base material titanium by embedding aluminate particles in the surface of pure titanium or titanium alloy, which is a titanium material, it is necessary to use a shot. Select blasting. According to the shot blasting process, the aluminate particles can be jetted and projected at a high speed on the surface of the titanium material, and can be embedded in the aluminum oxide substrate. As a result, a treatment layer integrated with the base material titanium mainly composed of aluminum oxide can be formed.
- the shot blasting projection pressure is preferably 3 to 7 atm. This projection pressure is too low In such a case, the embedding power of the aluminate in the base material is insufficient. As a result, the formation of the treatment layer on the surface is not sufficient, and it is difficult to make the average aluminum concentration of the treatment layer 4 at% or more. On the other hand, if the projection pressure is too high, an increase in the thickness of the treatment layer that saturates the titanium material itself (base material) is saturated, which is not suitable.
- the aluminate particles that can be used for shot blasting in the present invention may be any particle aggregate (powder, powder) in which aluminum oxide acts effectively.
- the aggregate of particles may not contain 100% aluminate particles, but may contain other oxide particles or compound particles.
- the single particle strength of aluminum oxide may not contain 100% aluminate composition, but other single oxides or compounds may be contained in single particles of aluminate.
- the aggregate strength of the aluminum oxide particles (powder, powder) to be shot blasted as a whole It is preferable to contain 80% by mass or more of aluminum oxide (A10).
- the oxide particle aggregate contains other oxide particles or compounds other than aluminum oxide, the aluminum oxide particles containing a large amount of the aluminate in a single particle may be separated from the aggregate.
- the aggregate should contain 80% by mass or more of aluminum oxide as a whole.
- the ratio of the aluminum oxide as the whole particle aggregate can be secured.
- the power of using commercially available aluminate particles to be shot blasted The particle size of aluminate particles that can be used for shot blasting in the present invention is 90% or more.
- the particle size of the product particles is preferably in the range of 180 to 425 ⁇ m.
- the particle size of the aluminum oxide particles of 90% or more becomes smaller or coarser than this, the aluminate is embedded in the titanium surface by shot blasting.
- aluminate particles are generally used for direct powdering of molten metal, atomizing method, molten metal stirring method, rotating disk dropping method, mechanical powdering, stamp mill method, ball mill method, vibration milling. It is manufactured by a known method such as a method or an attritor method.
- the titanium material referred to in the present invention refers to pure titanium or a titanium alloy formed into various shapes such as plates, strips, wires, and pipes by plastic processing such as rolling or forming.
- titanium alloys such as ⁇ alloy, a-j8 alloy, j8 alloy, etc., or pure titanium are used depending on the required properties (mechanical properties, etc.) of the application that do not limit the titanium material to be surface-treated. (JIS 1 to 4 types) can be used.
- Ti-1.5A1, Ti-0.5 Al-0.45Si-0.2Nb, 6-6A ⁇ 4V, Ti-3A1-2.5V, Ti-15V-3A and 3Sn-3Cr, Ti- lCu and other alloys with modified alloy components can be used.
- the titanium material itself which is the base material (base material)
- the base material must be excellent in high-temperature acid resistance against the above-mentioned commonly used titanium alloys or pure titanium. Preferred. Preferred and embodiments of these titanium materials excellent in high-temperature acid resistance are described below.
- the titanium alloy when the titanium alloy contains 0.12 to 2% by mass of Si, the high-temperature oxidation resistance at higher temperatures such as 850 ° C is improved. That is, it is preferable that the titanium alloy contains 0.12 to 2% by mass of Si, and the remaining titanium and inevitable impurity power.
- Si is effective in improving high-temperature acid resistance. It also improves high temperature strength. For this reason Contains 0.15% by mass or more of Si. On the other hand, when the Si content exceeds 2% by mass, it becomes difficult to form a titanium alloy into an exhaust pipe, where the formability deteriorates significantly.
- Nb, Mo, and Cr are also inferior in the effect of SU, but are effective in improving high-temperature acid resistance, and a synergistic effect can be expected by adding (coexisting) with Si. Therefore, one or more selected from Nb, Mo, and Cr may be included in a total content of 2% by mass or less with Si. If the total amount of these elements with Si exceeds 2% by mass, the formability deteriorates and it becomes difficult to form the exhaust pipe.
- the titanium material structure of the present invention is set as a preferred embodiment described below. That is, titanium selected from one or more of the following: increasing the average Si concentration on the outermost surface of the Si-containing titanium alloy, increasing the average crystal grain size of the titanium material structure, and making the titanium material a needle-like structure It is preferable to have an alloy structure. A synergistic effect can also be expected by using these tissues in appropriate combination with the above component composition.
- the additive of A1 induces peeling of the oxide scale in an acid environment of 800 ° C or higher, it is necessary to limit the amount of addition to, for example, less than 0.30% by mass.
- Addition of A1 for adjustment of mechanical properties at high temperatures, etc., can be actively performed, for example, at 0.30% by mass or more.
- the average concentration of Si on the outermost surface of the titanium alloy be 0.5 &% or more. Concentrated on this outermost surface, Si can be Si dissolved in titanium. Ti Si and other intermetallic compounds such as Ti Si and Si oxides and carbides are compounded.
- This Si concentration on the outermost surface basically increases with the Si content of the titanium alloy (base material), and satisfies the specified range of Si content. If you manufacture The average concentration of Si on the outermost surface of the titanium alloy may be increased to 0.5 at% or more. However, on the other hand, depending on the manufacturing method, a surface contamination layer such as oxygen or carbon may exist at a depth of several zm, and in such a case, the amount of Si present on the outermost surface There is a high possibility that the average concentration of Nb will be less than 0.5 at%, and an excellent effect of improving high-temperature acidity resistance cannot be expected. Therefore, the Si concentration on the outermost surface of the titanium alloy is not uniformly determined by the Si content of the titanium alloy. For this reason, when the average concentration of Si on the outermost surface of the titanium alloy is 0.5 at% or more, the production conditions such as V in which a surface contamination layer such as oxygen or carbon is not formed in the production of the titanium alloy. Especially preferred to choose.
- the final process may be a process in which the surface layer is removed. That is, pickling finish and polishing finish.
- the Si concentration on the outermost surface of this titanium alloy was determined by surface quantitative analysis using the wavelength dispersion method (Wave Dispersive Spectroscopy, abbreviated as WDS) in X-ray microanalysis analysis (EPMA, for short). It can be measured. More specifically, the analysis part on the outermost surface is expanded to X500 to X1000, first the existing elements are examined by qualitative analysis, and then each concentration is quantitatively determined by semi-quantitative analysis using the ZAF method. I can do it.
- the concentration on the outermost surface varies depending on the penetration depth of the electron beam at the time of analysis. By making the acceleration voltage at the time of analysis constant at 15 kv, the penetration depth of the electron beam is about 1 to 2.5 m. Therefore, the Si concentration on the outermost surface means the average concentration of Si from the surface to a depth of about 1 to 2.5 ⁇ m.
- the Si concentration on the outermost surface means the concentration defined in this way.
- the titanium material structure When manufactured by a conventional method, the titanium material structure becomes equiaxed grains. This equiaxed grain structure ensures properties such as formability and mechanical properties (strength) of the titanium alloy.
- the average crystal grain size greatly contributes to the high temperature acidity of titanium. That is, the resistance to high-temperature acidity is improved when the average crystal grain size is somewhat large. Specifically, this effect appears when the average grain size is 15 m or more, preferably 20 ⁇ m or more, more preferably 30 ⁇ m or more.
- the average result If the crystal grain size becomes excessively large, there will be a problem of rough skin at the time of molding.For applications where this problem is important, the upper limit of the average grain size is about 150 to 200 111, more preferably It is about 100 m.
- the rolling reduction in cold rolling which can be said to be a conventional method for producing titanium materials, is approximately 20 to 70%, although it varies depending on the material.
- the temperature of subsequent annealing is 600 to 800 ° C, and in the case of annealing such as vacuum annealing that takes a long time of several hours to tens of hours, the temperature on the low temperature side is about 600 to 700 ° C.
- the conditions are adopted, and in the short time treatment such as continuous annealing pickling, the temperature condition on the high temperature side of 700-800 ° C is adopted.
- the alloy element In the case of a titanium alloy, the alloy element often inhibits the grain growth, and within this range of conventional methods, even if the titanium material is cold-rolled and annealed, the average grain size should be 15 m or more. Is difficult.
- the rolling reduction of the cold rolling is reduced to 20% or less
- the annealing temperature is 825 ° C or more
- j8 The temperature rises to a temperature below the transformation point.
- the preferred rolling reduction is 15% or less, more preferably 10% or less.
- the preferable annealing temperature is 850 ° C. or more and j8 transformation point or less.
- the titanium material has a relatively coarse equiaxed grain structure with an average crystal grain size of 15 / zm or more, as described above, A1 is not restricted to less than 0.30% by mass. It's okay. In other words, the action of these relatively coarse equiaxed grain structures improves the high-temperature oxidation resistance, and therefore suppresses the high-temperature acidity reduction effect by A1. This effect increases as the average crystal grain size of the titanium material increases. [0189] (Method for measuring crystal grain size)
- the crystal grain size referred to in the present invention is an average crystal grain size of a cross section in the rolling (L) direction of a titanium material such as a titanium alloy or pure titanium.
- This crystal grain size was obtained by roughly polishing a cross section of a sample (test piece) taken from a titanium material by 0.05 to 0.1 mm, followed by mirror polishing, and then observing the etched surface using a 100 ⁇ optical microscope. Measured by the line intercept method in the vertical direction. The length of one measurement line is 0.95mm, and the total measurement line length is 0.95 x 15mm by observing a total of five fields with three lines per field. In this way, the average crystal grain size measured at any 10 locations in the center of the titanium material excluding the front and rear ends of the plate was further averaged to obtain the average crystal grain size of the titanium material. To do.
- the high temperature oxidation resistance is further improved.
- a needle-like thread and weave produced by heating the titanium material at the j8 transformation point or higher may be used.
- the structure of a titanium material is final annealed after the ⁇ -transformation point after cold rolling!
- the structure of the titanium material may be a needle-like structure that is not an equiaxed grain.
- This method of forming a needle-like structure can be obtained by heating a titanium material not particularly limited to a temperature above the j8 transformation point.
- a titanium material it can be produced by heating to 8 transformation points or higher and then cooling.
- the structure of the titanium material is such a needle-like structure that is not the above equiaxed crystal grain structure, the average crystal grain size cannot be obtained as in the case of the equiaxed structure.
- the needle-like structure itself is difficult to be defined by the normal average crystal grain size and aspect ratio, but is clearly defined by the manufacturing method which is the history of the needle-like structure.
- this acicular structure is defined as an acicular structure generated by heat treatment in which pure titanium or a titanium alloy is heated to the ⁇ transformation point or higher. It is. If the structure of the titanium material is this acicular structure, as described above, A1 may not be regulated to less than 0.30 mass%. Due to the improvement in high-temperature oxidation resistance due to these needle-like structures, the decrease in high-temperature oxidation resistance due to A1 is suppressed.
- this needle-like structure is not related to the rolling reduction rate of the cold rolling (even if the rolling reduction rate is not controlled), but finally the ⁇ transformation. It is inevitably (simple) obtained by cooling to a temperature above the point and then cooling. Depending on the product thickness constraints that come from the actual application, there may be cases where the cold rolling reduction cannot be freely selected and controlled. In such a case, in order to improve the high-temperature acid resistance, it is also useful to select this acicular structure regardless of the equiaxed grain structure. Note that the cooling after the heating does not require rapid cooling or forced cooling, which is good as it is allowed to cool.
- the structure of the titanium material is a relatively coarse equiaxed grain structure with an average crystal grain size of 15 m or more, or after cold rolling of the titanium material)) 8 transformation points
- A1 may not be regulated to less than 0.30% by mass. This is because the decrease in the high-temperature acidity resistance due to A1 is suppressed by the improvement in the high-temperature acidity resistance due to these relatively coarse equiaxed grain structure forces and needle-like structures. Therefore, when the titanium material has such a relatively coarse equiaxed grain structure force needle-like structure, it is allowed to contain A1 in a total content of 2% by mass or less with Si.
- the production method of the titanium material used in the present invention has preferable aspects of the above production method and conditions for structure preparation
- the process itself is ingot melting, hot forging, hot rolling, annealing, cold It can be produced by a conventional method that can be rolled, annealed or heat treated.
- the preferred structure for improving the high temperature acid resistance is changed by changing the cold rolling, annealing or heat treatment conditions.
- Example 3 Shot blasting using three kinds of aluminate powder particles (aggregates) a to c shown in Table 6 on one side of each titanium material test piece shown in Tables 7 and 8 Went. The shot blasted surface on one side of these specimens was evaluated for high-temperature oxidation resistance at higher temperatures exceeding 800 ° C.
- each titanium material about 120 g of ingots of each component composition were melted in a button arc furnace, and these ingots were subjected to hot forging, hot rolling, annealing, and cold rolling in a conventional manner.
- a cold-rolled sheet having a thickness of 2 mm was produced.
- the cold-rolled sheet was degreased and annealed at a predetermined temperature and condition to adjust the structure. Further, descaling was performed as necessary.
- the from the cold-rolled sheets were taken test piece 2mmt X 25mm w X 25mm 1.
- 21 to 24 general-purpose pure titanium and 25 to 29 general-purpose titanium alloys are commercially available. Among these, only 21 and 22 general-purpose pure titanium have a needle-like structure by the following heating. Only adjustments were made.
- the shot blasting conditions were performed under the projection pressure conditions shown in Tables 9 to 12, and the distance between the test piece and the shiyot blast nozzle was about 5 cm in common.
- each aluminum oxide particle powder was repeatedly injected and projected onto the surface of the titanium material at a high speed until the surface of the test piece became almost uniform shot blast skin.
- the projection time was 2 to 5 seconds on each side in common for each test piece.
- examples in which the average crystal grain size of the test specimen is 10 m or less indicate that the rolling reduction ratio of the titanium material is usually 40% within the scope of the law.
- the annealing conditions to be performed thereafter were also vacuum annealing at 800 ° C x soaking time of 6 minutes.
- the example in which the average crystal grain size of the test piece exceeds 15 m is different from the conventional method, and the rolling reduction of the titanium alloy is reduced depending on the desired average crystal grain size.
- the rate was reduced by selecting a range force of 20% or less, and the annealing temperature in vacuum annealing was selected by selecting a range of range force above 825 ° C and below the ⁇ transformation point.
- the soaking time was 6 minutes. Within this condition range, the rolling reduction of cold rolling is reduced and the annealing temperature is increased. However, the average crystal grain size becomes large.
- the rolling reduction of cold rolling was approximately 40% within the range of ordinary methods, and the cold-rolled sheet exceeded the j8 transformation point of titanium material.
- Vacuum heating was performed at ° C for a soaking time of 6 minutes. Only the commercially available general-purpose pure titanium 21 and 22 were adjusted to the needle-like structure by this heating.
- the entire structure of the test specimen collected from the test material was the acicular structure.
- the average concentration of Si on the outermost surface of the titanium alloy shown in Table 7 is 0.5 at% or more, and the example of concentration of the outermost surface Si is, after cold rolling with a rolling reduction of approximately 0%, instead of vacuum annealing, After atmospheric annealing at 850 ° C for 6 minutes, 600 ° C molten salt (NaNO 55% by mass, NaOH 35% by mass) so that a surface contamination layer such as oxygen or carbon does not exist up to a depth of several meters on the outermost surface of the titanium alloy. %,
- the average crystal grain size of the test piece under these production conditions is 10 ⁇ m or less, and an example in which the average crystal grain size of the test piece exceeds 15 m is that the reduction rate in cold rolling is 20% or less.
- the range force was also selected, and the reduction rate was made smaller to obtain a larger average grain size.
- the concentration of the outermost surface Si in the example in which the organization is a needle-like structure is performed by replacing only the above-described atmospheric annealing process with a condition of 950 ° C exceeding the 13 transformation point of the titanium alloy for 6 minutes. Is the concentration of the outermost Si The same process and conditions for ⁇ were carried out.
- the average Si concentration (at%) on the outermost surface of each test piece shown in Table 7 was analyzed by the following method.
- the titanium sample before analysis was subjected to ultrasonic cleaning with acetone for several minutes to adhere to the surface to remove contaminants such as oil, and then analyzed using an EPMA analyzer JXA-8900RL manufactured by JEOL Ltd. .
- the analysis magnification was X500
- the acceleration voltage was 15 kv
- the elements present on the surface were examined by qualitative analysis
- the abundance of the existing elements was determined by semi-quantitative analysis using the ZAF method.
- the average aluminum concentration (shown as average A1 content at% in the table) of the shot blasting layer shown in Tables 9 to 12 was also determined by the analysis method described above using an EPMA analyzer.
- the thickness of the shot blasting layer was in the range of a preferable average thickness of 1 m to 20 / z m in common in the measurement results obtained by the cross-sectional observation described above.
- the high temperature oxidation resistance of each test piece shown in Tables 9 to 12 was evaluated by a high temperature oxidation test. That is, when these specimens were exposed to a high-temperature atmosphere for 100 hours at 850 ° C exceeding 800 ° C, the weight increase (oxidation increase: mgZcm 2 ) before and after the high-temperature oxidation test was measured. Set. The smaller the weight increase, the better the high-temperature oxidation resistance at 850 ° C.
- the weight increase is 5 mg / cm 2 or less for exhaust mufflers, the high-temperature oxidation resistance is very excellent. ⁇ If the weight increase is 20 mg / cm 2 or less, the exhaust muffler As a result, the high-temperature acid resistance was evaluated as ⁇ . When the weight increase exceeded 20 mg / c, the high-temperature acid resistance for exhaust mufflers was rejected and evaluated as X.
- All of the invention examples shown in Table 9, all of the invention examples shown in Table 10, and all of the invention examples shown in Table 11 have a shot blast treatment layer made of aluminum oxide particles.
- the average concentration of aluminum is 4 at% or more, which satisfies the requirements of the present invention.
- the base material is the same as the titanium material, and there is no shot blasting layer made of aluminate particles.
- the pure titanium having the titanium material numbers 21 and 22 in the invention examples (comparative examples) shown in Table 11 has an equiaxed grain formed into a needle-like structure.
- inventive examples in which the base material titanium material was shot blasted with aluminate particles were high temperature oxidation resistance at 850 ° C. You can see that it is excellent.
- Each comparative example shown in Table 12 has a shot blasting layer of aluminate oxide particles.
- the projection pressure is as shown in Table 12 as the force using the powder of c in which the aluminate particles in the aggregate of aluminate particles to be shot blasted are less than 80% by mass.
- the shot blasting process is performed under conditions that are less than 2 atmospheres and less than 3 atmospheres, which are not preferable.
- the average aluminum concentration of the shot blasted layer is insufficient, being less than 4 at%.
- these comparative examples have excellent high-temperature acid resistance at 850 ° C due to the needle-like structure of the base material, but high-temperature acid resistance at 850 ° C due to the shot blast treatment layer. There is no improvement in sex.
- the particle size of the remainder (less than 10%) of the aluminum oxide particle size is less than 180 ii m
- the present invention it is possible to provide a titanium alloy and an engine exhaust pipe having excellent high-temperature oxidation resistance at higher temperatures such as 850 ° C exceeding 800 ° C.
- the engine exhaust pipe composed of the titanium alloy of the present invention includes all those having various joint structures such as a welded part structure and a mechanical joint structure. Further, the present invention is particularly excellent in acid resistance at higher temperatures exceeding 800 ° C., but even in an environment of 800 ° C. or less, it has superior oxidation resistance than conventional materials and is useful. Needless to say.
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Abstract
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DE112007000544.0T DE112007000544B4 (de) | 2006-03-30 | 2007-03-29 | Titanmaterial und Abgasrohr für Motor |
CN200780003745.1A CN101374967B (zh) | 2006-03-30 | 2007-03-29 | 钛合金和引擎排气管 |
US12/294,619 US8431231B2 (en) | 2006-03-30 | 2007-03-29 | Titanium Material and Exhaust Pipe for Engine |
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JP2006-095070 | 2006-03-30 | ||
JP2006095069A JP4157891B2 (ja) | 2006-03-30 | 2006-03-30 | 耐高温酸化性に優れたチタン合金およびエンジン排気管 |
JP2006095070A JP4157892B2 (ja) | 2006-03-30 | 2006-03-30 | 耐高温酸化性に優れた純チタンおよびエンジン排気管 |
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Cited By (3)
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CN112553554A (zh) * | 2020-12-17 | 2021-03-26 | 中国航发北京航空材料研究院 | 一种提高亚稳定的高氧超弹钛合金弹性应变极限的短时时效方法 |
WO2023181654A1 (ja) * | 2022-03-24 | 2023-09-28 | 株式会社神戸製鋼所 | チタン合金材及びチタン合金部品の製造方法 |
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Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH03193850A (ja) * | 1989-12-22 | 1991-08-23 | Nippon Steel Corp | 微細針状組織をなすチタンおよびチタン合金の製造方法 |
JPH04105659A (ja) * | 1990-08-27 | 1992-04-07 | Shinya Iwamoto | 生体用チタン合金およびその製造方法 |
JPH1088258A (ja) * | 1996-09-12 | 1998-04-07 | Sumitomo Metal Ind Ltd | 硫化水素環境用チタン材および製造方法 |
JPH1136029A (ja) * | 1997-05-21 | 1999-02-09 | Sumitomo Metal Ind Ltd | 高強度チタン合金鋳造品 |
JP2001089883A (ja) * | 1999-09-22 | 2001-04-03 | Daido Steel Co Ltd | チタン又はチタン合金製品の製造方法 |
JP2001089821A (ja) * | 1999-09-22 | 2001-04-03 | Sumitomo Metal Ind Ltd | 耐高温大気酸化性に優れた高強度、高延性チタン合金 |
JP2002003968A (ja) * | 2000-06-21 | 2002-01-09 | Sumitomo Metal Ind Ltd | 成形性に優れたチタン板とその製造方法 |
JP2004300569A (ja) * | 2003-03-20 | 2004-10-28 | Kobe Steel Ltd | 建材用純チタン材およびその製造方法 |
JP2005036311A (ja) * | 2003-06-27 | 2005-02-10 | Kobe Steel Ltd | チタン材、その製造方法および排気管 |
JP2005290448A (ja) * | 2004-03-31 | 2005-10-20 | Sumitomo Metal Ind Ltd | ハイドロフォーム用チタン管とその製造方法とハイドロフォーム成形品 |
JP2006009115A (ja) * | 2004-06-29 | 2006-01-12 | Kobe Steel Ltd | 耐酸化性に優れる表面処理チタン材及びその製造方法、エンジン排気管 |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS56165502A (en) * | 1980-05-23 | 1981-12-19 | Kobe Steel Ltd | Manufacture of cold rolled titanium sheet |
US5188677A (en) * | 1989-06-16 | 1993-02-23 | Nkk Corporation | Method of manufacturing a magnetic disk substrate |
JPH0688208A (ja) | 1992-09-03 | 1994-03-29 | Kobe Steel Ltd | 高耐食性表面処理金属材およびその製造方法 |
JP3151713B2 (ja) | 1993-02-03 | 2001-04-03 | 本田技研工業株式会社 | チタン材の表面処理方法 |
JPH09256138A (ja) | 1996-03-19 | 1997-09-30 | Kobe Steel Ltd | 耐酸化性および耐摩耗性に優れたTi基合金部材 |
EP0834586B1 (en) * | 1996-03-29 | 2002-09-04 | Kabushiki Kaisha Kobe Seiko Sho | High strength titanium alloy, product made therefrom and method for producing the same |
JPH1099976A (ja) | 1996-09-27 | 1998-04-21 | Daido Steel Co Ltd | Ti被覆クラッド板の製造方法 |
JP3361072B2 (ja) | 1998-02-20 | 2003-01-07 | 株式会社豊田中央研究所 | 耐酸化性に優れた金属製部材の製造方法 |
JP3967515B2 (ja) | 2000-02-16 | 2007-08-29 | 株式会社神戸製鋼所 | マフラー用チタン合金材およびマフラー |
US20040094241A1 (en) * | 2002-06-21 | 2004-05-20 | Yoji Kosaka | Titanium alloy and automotive exhaust systems thereof |
US20040187983A1 (en) | 2003-03-20 | 2004-09-30 | Kabushiki Kaisha Kobe Seiko Sho (Kobe Steel, Ltd.) | Pure titanium building material and method of manufacturing the same |
JP2005034581A (ja) | 2003-07-18 | 2005-02-10 | Kazuo Tsuruta | 座浴装置 |
JP4516440B2 (ja) | 2004-03-12 | 2010-08-04 | 株式会社神戸製鋼所 | 耐高温酸化性および耐食性に優れたチタン合金 |
EP1574589B1 (en) * | 2004-03-12 | 2012-12-12 | Kabushiki Kaisha Kobe Seiko Sho | Titanium alloy having excellent high-temperature oxidation and corrosion resistance |
-
2007
- 2007-03-29 WO PCT/JP2007/056799 patent/WO2007114218A1/ja active Application Filing
- 2007-03-29 DE DE112007000544.0T patent/DE112007000544B4/de active Active
- 2007-03-29 US US12/294,619 patent/US8431231B2/en active Active
Patent Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH03193850A (ja) * | 1989-12-22 | 1991-08-23 | Nippon Steel Corp | 微細針状組織をなすチタンおよびチタン合金の製造方法 |
JPH04105659A (ja) * | 1990-08-27 | 1992-04-07 | Shinya Iwamoto | 生体用チタン合金およびその製造方法 |
JPH1088258A (ja) * | 1996-09-12 | 1998-04-07 | Sumitomo Metal Ind Ltd | 硫化水素環境用チタン材および製造方法 |
JPH1136029A (ja) * | 1997-05-21 | 1999-02-09 | Sumitomo Metal Ind Ltd | 高強度チタン合金鋳造品 |
JP2001089883A (ja) * | 1999-09-22 | 2001-04-03 | Daido Steel Co Ltd | チタン又はチタン合金製品の製造方法 |
JP2001089821A (ja) * | 1999-09-22 | 2001-04-03 | Sumitomo Metal Ind Ltd | 耐高温大気酸化性に優れた高強度、高延性チタン合金 |
JP2002003968A (ja) * | 2000-06-21 | 2002-01-09 | Sumitomo Metal Ind Ltd | 成形性に優れたチタン板とその製造方法 |
JP2004300569A (ja) * | 2003-03-20 | 2004-10-28 | Kobe Steel Ltd | 建材用純チタン材およびその製造方法 |
JP2005036311A (ja) * | 2003-06-27 | 2005-02-10 | Kobe Steel Ltd | チタン材、その製造方法および排気管 |
JP2005290448A (ja) * | 2004-03-31 | 2005-10-20 | Sumitomo Metal Ind Ltd | ハイドロフォーム用チタン管とその製造方法とハイドロフォーム成形品 |
JP2006009115A (ja) * | 2004-06-29 | 2006-01-12 | Kobe Steel Ltd | 耐酸化性に優れる表面処理チタン材及びその製造方法、エンジン排気管 |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109750248A (zh) * | 2017-11-06 | 2019-05-14 | 中国科学院金属研究所 | 一种γ-TiAl表面喷丸处理促进Al2O3膜热生长的方法及应用 |
CN112553554A (zh) * | 2020-12-17 | 2021-03-26 | 中国航发北京航空材料研究院 | 一种提高亚稳定的高氧超弹钛合金弹性应变极限的短时时效方法 |
WO2023181654A1 (ja) * | 2022-03-24 | 2023-09-28 | 株式会社神戸製鋼所 | チタン合金材及びチタン合金部品の製造方法 |
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