EP1978119A1 - Titanium alloy for corrosion-resistant material - Google Patents

Titanium alloy for corrosion-resistant material Download PDF

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Publication number
EP1978119A1
EP1978119A1 EP06782010A EP06782010A EP1978119A1 EP 1978119 A1 EP1978119 A1 EP 1978119A1 EP 06782010 A EP06782010 A EP 06782010A EP 06782010 A EP06782010 A EP 06782010A EP 1978119 A1 EP1978119 A1 EP 1978119A1
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Prior art keywords
corrosion
mass
titanium alloy
resistant materials
titanium
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German (de)
French (fr)
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EP1978119B1 (en
EP1978119A4 (en
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Satoshi Matsumoto
Keisuke Nagashima
Takashi Maeda
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Nippon Steel Corp
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Sumitomo Metal Industries Ltd
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C14/00Alloys based on titanium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/16Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of other metals or alloys based thereon
    • C22F1/18High-melting or refractory metals or alloys based thereon
    • C22F1/183High-melting or refractory metals or alloys based thereon of titanium or alloys based thereon

Definitions

  • the present invention relates to a titanium alloy for corrosion-resistant materials.
  • Titanium forms thereon an oxidized film and therefore is not easily corroded as compared with general metals, so that it is widely used in a place requiring corrosion resistance.
  • titanium having more excellent corrosion resistance, and in order to deal with it, corrosion resistance is improved hitherto by adding another element to titanium.
  • Ti-Pd alloys which are also prescribed in JIS 11 type, 12 type and 13type, are known. These are alloys containing 0.12-0.25% by mass of Pd in pure titanium. Also, it is conventional to contain therein Co, Ni or the like other than Pd (cf. Patent Documents 1 and 2).
  • titanium has excellent characteristics as compared with general metals, and specifically it has not only excellent corrosion resistance but also a light weight and a high strength, and therefore various alloys are used in various applications, such as sports goods such as golf clubs and bicycles.
  • titanium alloys are expensive compared with general metals, and in these days, utilization of low cost, recycled titanium alloys, which are obtained by recycling not only sponge titanium produced from titanium ores, but also titanium alloys, which were once introduced into markets and had become out of use, are now being studied.
  • titanium alloys are expensive compared with general metals, and in these days, utilization of low cost, recycled titanium alloys, which are obtained by recycling not only sponge titanium produced from titanium ores, but also titanium alloys, which were once introduced into markets and had become out of use, are now being studied.
  • titanium alloys are not used for titanium alloys for corrosion-resistant materials.
  • titanium alloys for corrosion-resistant materials have been very expensive in the past.
  • conventional titanium alloys for corrosion-resistant materials have a problem in that they cannot be produced at low cost while maintaining the capability to suppress the deterioration of corrosion resistance.
  • a titanium alloy for corrosion-resistant materials which is characterized in that it contains 0.01-0.12% by mass in total of at least one of platinum group elements, at least one of Al, Cr, Zr, Nb, Si, Sn and Mn, and the residue comprising Ti and impurities, in which the total content of Al, Cr, Zr, Nb, Si, Sn and Mn is 5% by mass or less.
  • containing Al, Cr, Zr, Nb, Si, Sn and Mn in a titanium alloy is meant that Al, Cr, Zr, Nb, Si, Sn and Mn each are present in the titanium alloy in an amount exceeding the unavoidable level.
  • the content of each of these elements can be measured by using a conventionally used analytic instrument.
  • the contents, as the unavoidable levels, of these elements present in a titanium alloy are, at maximum, Al: 0.007% by mass, Cr: 0.007% by mass, Zr: 0.001% by mass, Nb: 0.001% by mass, Si: 0.004% by mass, Sn: 0.001% by mass and Mn: 0.001% by mass, respectively.
  • Al, Cr, Zr, Nb, Si, Sn and Mn in a titanium alloy is meant in the specification of this application that these elements each are present in the titanium alloy in an amount exceeding the corresponding amount.
  • Al, Cr, Zr, Nb, Si, Sn or Mn is contained in a titanium alloy for corrosion-resistant materials, so that it is possible to reuse recycled titanium alloys coming from products in which at least one of Al, Cr, Zr, Nb, Si, Sn and Mn is used.
  • 0.01-0.12% by mass in total of at least one of platinum group elements is contained in the titanium alloy for corrosion-resistant materials, and the total content of Al, Cr, Zr, Nb, Si, Sn and Mn is 5% by mass or less.
  • a titanium alloy for corrosion-resistant materials of this embodiment usually contains a platinum group element, any one or both of Co and Ni, at least one of Al, Cr, Zr, Nb, Si, Sn and Mn, and the residue comprising Ti and impurities.
  • the platinum group element is an essential component of a titanium alloy for corrosion-resistant materials, and the content thereof is 0.01-0.12% by mass.
  • the content of the platinum group element is 0.01-0.12% for the reason that when the platinum group element is less than 0.01% by mass, the corrosion resistance of the titanium alloy for corrosion-resistant materials does not reach a satisfactory level, which may cause corrosion, and on the other hand, even when the content thereof exceeds 0.12% by mass, it cannot be expected to have the corrosion resistance improved as the increase of the content thereof, and in addition, there is a possibility of increasing the cost of a titanium alloy for corrosion-resistant materials.
  • this platinum group element it is possible to use Ru, Rh, Pd, Os, Ir and Pt, and preferably use Pd.
  • Co and Ni are optional components, and the content thereof is 0.05-2.00% by mass. These may be contained in the titanium alloy for corrosion-resistant materials, in place of Ti contained in the titanium alloy as a residue of the essential components, such as the platinum group element and at least one of hereinafter described Al, Cr, Zr, Nb, Si, Sn and Mn. They are contained in the amount of 0.05-2.00% by mass, thereby producing an advantage of further improving the corrosion resistance while increasing the strength of the titanium alloy for corrosion-resistant materials. When the total amount of Co and Ni is less than 0.05% by mass, it is difficult to produce the advantage of further improving the corrosion resistance while increasing the strength of the titanium alloy.
  • the at least one of Al, Cr, Zr, Nb, Si, Sn and Mn is an essential component of a titanium alloy for corrosion-resistant materials, and the total content of Al, Cr, Zr, Nb, Si, Sn and Mn is 5% by mass or less.
  • These elements are contained in such a range for the reason that when the total content of Al, Cr, Zr, Nb, Si, Sn and Mn exceeds 5%, the corrosion resistance of the titanium alloy for corrosion-resistant materials is deteriorated, which causes corrosion. From these points of view, the total content of them is preferably 3% or less, and more preferably 2% or less.
  • impurities include unavoidable impurities such as C, O, H and Fe, and a small amount of another element may be contained in the titanium alloy for corrosion-resistant materials to such an extent as not to deteriorate the advantages of the present invention.
  • V, Mo and W are known as the elements causing less influences on the corrosion resistance, and can be contained in a titanium alloy for corrosion-resistant materials as long as the total content thereof is about 5% by mass or less.
  • the titanium alloy for corrosion-resistant materials mentioned above is preferably used for conduits, heat exchangers, electrolysis vessels and the like of such as a nickel refining plant, which are used in environments, in which they are exposed to concentrated sulfuric acid, nickel sulfate or nickel chloride at about 250°C.
  • Titanium alloys for corrosion-resistant materials are prepared by adjusting samples for evaluation on corrosion resistance of the respective Examples and Comparative Examples, using pure titanium and the respective components so as to have the components of Tables 1 and 2 contained in the amounts of Tables 1 and 2.
  • pure titanium is used for Comparative Example 1.
  • the titanium alloy of each composition is produced with a size having a thickness of 20 mm, a width of 70 mm and a length of 90 mm by melting through button arc melting. Then, the thus produced pieces each are hot rolled into 3 mm thickness, and then acid-washed, thereby removing scale from the surface, and cut into a test piece having a width of 50 mm and a length of 100 mm.
  • each sample for evaluation of corrosion resistance is prepared.
  • a titanium alloy for corrosion-resistant materials produced from sponge titanium or the like
  • a titanium alloy for corrosion resistance (Conventional Examples 1-4) containing the components shown in Table 3 are prepared and evaluated in the same manner as in Examples and Comparative Examples.
  • the weight of each sample for evaluation of corrosion resistance is measured before and after the immersion in the nickel chloride solution by using an electronic balance that is capable of measuring the weight with the unit of 0.1 mg, and the difference thereof is calculated as a weight reduction ( ⁇ M).
  • the titanium alloy for corrosion-resistant materials of the present invention is capable of suppressing deterioration of corrosion resistance even though it uses recycled titanium alloys or the like, and thus being produced at low cost while maintaining the capability to suppress the deterioration of corrosion resistance.

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  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Organic Chemistry (AREA)
  • Metallurgy (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Manufacture And Refinement Of Metals (AREA)
  • Cell Electrode Carriers And Collectors (AREA)
  • Prevention Of Electric Corrosion (AREA)
  • Catalysts (AREA)
  • Preventing Corrosion Or Incrustation Of Metals (AREA)
  • Investigating And Analyzing Materials By Characteristic Methods (AREA)

Abstract

An object is to provide a titanium alloy for corrosion-resistant materials that is capable of being produced at low cost while maintaining the capability to suppress the deterioration of corrosion resistance. According to the present invention, there is provided a titanium alloy for corrosion-resistant materials, which contains 0.01-0.12% by mass in total of at least one of platinum group elements, at least one of Al, Cr, Zr, Nb, Si, Sn and Mn, and the residue comprising Ti and impurities, in which the total content of Al, Cr, Zr, Nb, Si, Sn and Mn is 5% by mass or less.

Description

    FIELD OF THE INVENTION
  • The present invention relates to a titanium alloy for corrosion-resistant materials.
  • BACKGROUND OF THE INVENTION
  • Titanium forms thereon an oxidized film and therefore is not easily corroded as compared with general metals, so that it is widely used in a place requiring corrosion resistance. However, in this intended use, there is a demand for titanium having more excellent corrosion resistance, and in order to deal with it, corrosion resistance is improved hitherto by adding another element to titanium.
    For example, as titanium having improved corrosion resistance, Ti-Pd alloys, which are also prescribed in JIS 11 type, 12 type and 13type, are known. These are alloys containing 0.12-0.25% by mass of Pd in pure titanium. Also, it is conventional to contain therein Co, Ni or the like other than Pd (cf. Patent Documents 1 and 2).
  • Meanwhile, titanium has excellent characteristics as compared with general metals, and specifically it has not only excellent corrosion resistance but also a light weight and a high strength, and therefore various alloys are used in various applications, such as sports goods such as golf clubs and bicycles. However, titanium alloys are expensive compared with general metals, and in these days, utilization of low cost, recycled titanium alloys, which are obtained by recycling not only sponge titanium produced from titanium ores, but also titanium alloys, which were once introduced into markets and had become out of use, are now being studied.
    However, when even a small amount of another element is mixed in titanium for which corrosion resistance is required as mentioned above, corrosion may occur starting at such an element, and therefore recycled titanium alloys are not used for titanium alloys for corrosion-resistant materials. Furthermore, platinum group elements, such as Pd, are generally expensive compared with titanium and therefore titanium alloys for corrosion-resistant materials have been very expensive in the past.
    In other words, conventional titanium alloys for corrosion-resistant materials have a problem in that they cannot be produced at low cost while maintaining the capability to suppress the deterioration of corrosion resistance.
    • Patent Document 1: Japanese Patent No. 2132925
    • Patent Document 2: Japanese Patent Application Publication No. Hei-4-57735
    SUMMARY OF THE INVENTION PROBLEMS TO BE SOLVED BY THE INVENTION
  • In consideration of the above problems, it is an object of the present invention to provide a titanium alloy for corrosion-resistant materials that is capable of being produced at low cost while maintaining the capability to suppress the deterioration of corrosion resistance.
  • The present inventors intensively studied in order to solve the above problems, consequently found that it is possible to suppress the deterioration of corrosion resistance when a certain amount or less of at least one of Al, Cr, Zr, Nb, Si, Sn and Mn is contained in a titanium alloy, and thus achieved the present invention.
    Specifically, according to the present invention, there is provided a titanium alloy for corrosion-resistant materials, which is characterized in that it contains 0.01-0.12% by mass in total of at least one of platinum group elements, at least one of Al, Cr, Zr, Nb, Si, Sn and Mn, and the residue comprising Ti and impurities, in which the total content of Al, Cr, Zr, Nb, Si, Sn and Mn is 5% by mass or less.
  • By containing Al, Cr, Zr, Nb, Si, Sn and Mn in a titanium alloy is meant that Al, Cr, Zr, Nb, Si, Sn and Mn each are present in the titanium alloy in an amount exceeding the unavoidable level. The content of each of these elements can be measured by using a conventionally used analytic instrument. Usually, the contents, as the unavoidable levels, of these elements present in a titanium alloy are, at maximum, Al: 0.007% by mass, Cr: 0.007% by mass, Zr: 0.001% by mass, Nb: 0.001% by mass, Si: 0.004% by mass, Sn: 0.001% by mass and Mn: 0.001% by mass, respectively. Accordingly, by containing Al, Cr, Zr, Nb, Si, Sn and Mn in a titanium alloy is meant in the specification of this application that these elements each are present in the titanium alloy in an amount exceeding the corresponding amount.
  • ADVANTAGES OF THE INVENTION
  • According to the present invention, Al, Cr, Zr, Nb, Si, Sn or Mn is contained in a titanium alloy for corrosion-resistant materials, so that it is possible to reuse recycled titanium alloys coming from products in which at least one of Al, Cr, Zr, Nb, Si, Sn and Mn is used. In addition, according to the present invention, 0.01-0.12% by mass in total of at least one of platinum group elements is contained in the titanium alloy for corrosion-resistant materials, and the total content of Al, Cr, Zr, Nb, Si, Sn and Mn is 5% by mass or less. Whereby, it is possible to suppress the deterioration of corrosion resistance.
    In other words, it is possible to provide a titanium alloy for corrosion-resistant materials that is capable of being produced at low cost while maintaining the capability to suppress the deterioration of corrosion resistance.
  • DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT
  • Now, the description will be made for a preferred embodiment of a titanium alloy for corrosion-resistant materials. First, the description will be made for the amount of each element contained in a titanium alloy for corrosion-resistant materials and the reason for determining the amount thereof.
    A titanium alloy for corrosion-resistant materials of this embodiment usually contains a platinum group element, any one or both of Co and Ni, at least one of Al, Cr, Zr, Nb, Si, Sn and Mn, and the residue comprising Ti and impurities.
  • The platinum group element is an essential component of a titanium alloy for corrosion-resistant materials, and the content thereof is 0.01-0.12% by mass. The content of the platinum group element is 0.01-0.12% for the reason that when the platinum group element is less than 0.01% by mass, the corrosion resistance of the titanium alloy for corrosion-resistant materials does not reach a satisfactory level, which may cause corrosion, and on the other hand, even when the content thereof exceeds 0.12% by mass, it cannot be expected to have the corrosion resistance improved as the increase of the content thereof, and in addition, there is a possibility of increasing the cost of a titanium alloy for corrosion-resistant materials.
    As this platinum group element, it is possible to use Ru, Rh, Pd, Os, Ir and Pt, and preferably use Pd.
  • Co and Ni are optional components, and the content thereof is 0.05-2.00% by mass. These may be contained in the titanium alloy for corrosion-resistant materials, in place of Ti contained in the titanium alloy as a residue of the essential components, such as the platinum group element and at least one of hereinafter described Al, Cr, Zr, Nb, Si, Sn and Mn. They are contained in the amount of 0.05-2.00% by mass, thereby producing an advantage of further improving the corrosion resistance while increasing the strength of the titanium alloy for corrosion-resistant materials. When the total amount of Co and Ni is less than 0.05% by mass, it is difficult to produce the advantage of further improving the corrosion resistance while increasing the strength of the titanium alloy.
  • The at least one of Al, Cr, Zr, Nb, Si, Sn and Mn is an essential component of a titanium alloy for corrosion-resistant materials, and the total content of Al, Cr, Zr, Nb, Si, Sn and Mn is 5% by mass or less. These elements are contained in such a range for the reason that when the total content of Al, Cr, Zr, Nb, Si, Sn and Mn exceeds 5%, the corrosion resistance of the titanium alloy for corrosion-resistant materials is deteriorated, which causes corrosion. From these points of view, the total content of them is preferably 3% or less, and more preferably 2% or less.
  • Examples of impurities include unavoidable impurities such as C, O, H and Fe, and a small amount of another element may be contained in the titanium alloy for corrosion-resistant materials to such an extent as not to deteriorate the advantages of the present invention. Especially, V, Mo and W are known as the elements causing less influences on the corrosion resistance, and can be contained in a titanium alloy for corrosion-resistant materials as long as the total content thereof is about 5% by mass or less.
  • The titanium alloy for corrosion-resistant materials mentioned above is preferably used for conduits, heat exchangers, electrolysis vessels and the like of such as a nickel refining plant, which are used in environments, in which they are exposed to concentrated sulfuric acid, nickel sulfate or nickel chloride at about 250°C.
  • EXAMPLES
  • Now, the description will be made for the present invention in more detail with reference to examples without intention to limit the present invention thereto.
  • (Preparation of samples) (Examples 1 to 29, Comparative Examples 1 to 11)
  • Titanium alloys for corrosion-resistant materials are prepared by adjusting samples for evaluation on corrosion resistance of the respective Examples and Comparative Examples, using pure titanium and the respective components so as to have the components of Tables 1 and 2 contained in the amounts of Tables 1 and 2. For Comparative Example 1, pure titanium is used.
    First, the titanium alloy of each composition is produced with a size having a thickness of 20 mm, a width of 70 mm and a length of 90 mm by melting through button arc melting.
    Then, the thus produced pieces each are hot rolled into 3 mm thickness, and then acid-washed, thereby removing scale from the surface, and cut into a test piece having a width of 50 mm and a length of 100 mm. Then, one side of this test piece is polished with a #200 polishing sheet, while the lateral and rear sides thereof were sealed with a sealing agent, thereby allowing only the polished surface to be exposed to the surface. Thus, each sample for evaluation of corrosion resistance is prepared.
    As a conventional titanium alloy for corrosion-resistant materials produced from sponge titanium or the like, a titanium alloy for corrosion resistance (Conventional Examples 1-4) containing the components shown in Table 3 are prepared and evaluated in the same manner as in Examples and Comparative Examples.
  • [TABLE 1]
    Components (%) * Total
    Pd Co Ni Mn Sn Al Cr Zr Nb Si **
    Example 1 0.05 3 3
    Example 2 0.05 0.35 4 4
    Example 3 0.05 3 3
    Example 4 0.02 3 3
    Example 5 0.1 3 3
    Example 6 0.05 0.35 1 1 2
    Example 7 0.05 0.1 0.15 3 3
    Example 8 0.05 0.01 0.01 0.02
    Example 9 0.05 0.35 0.01 0.01 0.02
    Example 10 0.05 0.35 0.01 0.01 0.02
    Example 11 0.05 0.2 0.15 0.01 0.01 0.02
    Example 12 0.05 4 4
    Example 13 0.05 3.5 3.5
    Example 14 0.05 0.1 0.15 3 3
    Example 15 0.05 2 2 4
    Example 16 0.05 2 2
    Example 17 0.05 0.1 0.2 0.2 0.5
    Example 18 0.05 1 1
    Example 19 0.05 1 1
    Example 20 0.05 0.5 0.5 1
    Example 21 0.05 1 1 2
    Example 22 0.05 1 1 2
    Example 23 0.05 0.1 0.1
    Example 24 0.05 0.1 0.1
    Example 25 0.05 0.4 0.4
    Example 26 0.05 1 1
    Example 27 0.05 1 1
    Example 28 0.05 1.5 1.5
    Example 29 0.05 1 0.6 1.6
    * The numerals in Table are given in percent by mass.
    ** The total content of Mn, Sn, Al, Cr, Zr, Nb and Si is represented.
  • [TABLE2]
    Components (%) * Total
    Pd Co Ni Mn Sn Al Cr Zr Nb Si **
    Comparative Example 1 - 0
    Comparative Example 2 0.05 6 6
    Comparative Example 3 0.05 0.35 6 6
    Comparative Example 4 0.05 6 6
    Comparative Example 5 0.05 3 3 6
    Comparative Example 6 0.05 0.1 0.2 6 6
    Comparative Example 7 0.05 6 7 13
    Comparative Example 8 0.05 2 5 7
    Comparative Example 9 0.05 6 6
    Comparative Example 10 0.05 5.5 5.5
    Comparative Example 11 0.05 6 6
    * The numerals in Table are given in percent by mass.
    ** The total content of Mn, Sn, Al, Cr, Zr, Nb and Si is represented.
  • [TABLE 3]
    Components (%) * Total **
    Pd Co Ni Mn Sn Al Cr Zr Nb Si
    Conventional Example 1 0.05 0
    Conventional Example 2 0.05 0.35 0
    Conventional Example 3 0.05 0.35 0
    Conventional Example 4 0.02 0.2 0.15 0
    * The numerals in Table are given in percent by mass.
    ** The total content of Mn, Sn, Al, Cr, Zr, Nb and Si is represented.
  • (Nickel-chloride-resistance test)
  • The samples of Examples, Comparative Examples and Conventional Examples for evaluation on corrosion resistance each are immersed in 20% nickel chloride solution at 100°C for 100 hours, and the surface of each of the samples are observed by eyes and an optical microscope. Thus, the surface texture is evaluated. According to the result of the evaluation, it is determined as "○" for a sample in which no change is confirmed between its initial surface condition and its surface condition after the immersion in the nickel chloride solution, as "Δ" for a sample in which increase of unevenness or the like is slightly confirmed therebetween, and as "×" for a sample in which increase of unevenness or the like is apparently confirmed therebetween. The results are shown in Table 4.
    The weight of each sample for evaluation of corrosion resistance is measured before and after the immersion in the nickel chloride solution by using an electronic balance that is capable of measuring the weight with the unit of 0.1 mg, and the difference thereof is calculated as a weight reduction (ΔM). The reduced amount is calculated by the following expression based on the surface area (S) of each sample for evaluation of corrosion resistance before the immersion. Reduced amount g / m 2 = ΔM g / S m 2
    Figure imgb0001

    The results are shown in Table 4.
  • (Heated-sulfuric-acid-resistance test)
  • The samples of Examples, Comparative Examples and Conventional Examples for evaluation on corrosion resistance each are immersed in 5% sulfuric acid solution at 240°C for 1 hour, and the reduced amount is determined by calculation in the same manner as in the nickel-chloride-resistance test. The results are shown in Table 4.
  • (Heated-hydrochloric-acid-resistance test)
  • The samples of Examples, Comparative Examples and Conventional Examples for evaluation on corrosion resistance each are immersed in boiled 10% hydrochloric acid solution for 1 hour, and the reduced amount is determined by calculation in the same manner as in the nickel-chloride-resistance test. The results are shown in Table 4.
  • (Clearance-corrosion-resistance test)
  • Two samples of each of Examples, Comparative Examples and Conventional Examples are overlapped each other with the surfaces thereof facing each other, and are immersed in 20% NaCl solution at 90°C, adjusted to a pH value of 1 by hydrochloric acid, for 100 hours. Thus, the clearance-corrosion-resistance test is performed. In the same manner as in the nickel-chloride-resistance test, it is determined as "○" for a sample in which no change is confirmed between its surface conditions before and after the test, as "Δ " for a sample in which increase of unevenness or the like is slightly confirmed therebetween, and as "×" for a sample in which increase of unevenness or the like is apparently confirmed therebetween. The results are shown in Table 4.
  • [TABLE 4]
    Nickel-Chloride-Resistance Heated- Sulfuric-Acid-Resistance Heated- Hydrochloric-Acid Resistance Clearance-Corrosion-Resistance Nickel-Chloride-Resistance Heated-Sulfuric-Acid-Resistance Heated-Hydrochloric-Acid Resistance Clearance-Corrosion-Resistance
    Surface Texture Reduced Amount Reduced Amount Reduced Amount Surface Texture Surface Texture Reduced Amount Reduced Amount Reduced Ammmt Surface Texture
    Ex. 1 <0.10 0.76 1.5 Com. Ex. 1 × 0.26 13.5 41.2 ×
    Ex. 2 <0.10 0.61 1.8 Com. Ex. 2 Δ 0.14 1.01 2.5 Δ
    Ex. 3 <0.10 0.65 1.7 Com. Ex. 3 Δ 0.15 1.25 3.5 Δ
    Ex. 4 0.1 0.86 1.9 Com. Ex. 4 Δ 0.13 1.13 3.7 Δ
    Ex. 5 <0.10 0.35 1.1 Com. Ex. 5 Δ 0.14 1.01 2.5 Δ
    Ex. 6 <0.10 0.58 1.7 Com. Ex. 6 Δ 0.15 1.21 3.4 Δ
    Ex. 7 <0.10 0.58 1.6 Com. Ex. 7 Δ 0.25 1.81 4.2 Δ
    Ex. 8 <0.10 0.36 1.2 Com. Ex. 8 Δ 0.16 1.22 2.4 Δ
    Ex. 9 <0.10 0.42 1.3 Com. Ex. 9 Δ 0.15 1.1 2.2 Δ
    Ex. 10 <0.10 0.46 1.4 Com. Ex. 10 Δ 0.13 1.05 2.1 Δ
    Ex. 11 <0.10 0.57 1.4 Com. Ex. 11 Δ 0.14 1.11 2.2 Δ
    Ex. 12 <0.10 0.61 1.8
    Ex. 13 <0.10 0.62 1.7 Conv. Ex. 1 <0.10 0.36 1.2
    Ex. 14 <0.10 0.54 1.3 Conv. Ex. 2 <0.10 0.42 1.3
    Ex. 15 <0.10 0.7 1.8 Conv. Ex. 3 <0.10 0.46 1.4
    Ex. 16 <0.10 0.51 1.5 Conv. Ex. 4 <0.10 0.57 1.4
    Ex. 17 <0.10 0.58 1.3
    Ex. 18 <0.10 0.6 1.4
    Ex. 19 <0.10 0.63 1.4
    Ex. 20 <0.10 0.65 1.4
    Ex. 21 <0.10 0.7 1.5
    Ex. 22 <0.10 0.68 1.5
    Ex. 23 <0.10 0.63 1.3
    Ex. 24 <0.10 0.63 1.3
    Ex. 25 <0.10 0.65 1.3
    Ex. 26 <0.10 0.68 1.4
    Ex. 27 <0.10 0.68 1.4
    Ex. 28 <0.10 0.72 1.4
    Ex. 29 <0.10 0.72 1.4
    *The "reduced amount" in each test is given in g/m2. The "<0.10" is meant that the reduced amount is less than 0.10 g/m2.
  • From Table 4, it is also appreciated that a titanium alloy for corrosion-resistant materials containing 0.01-0.12% by mass in total of at least one of platinum group elements, at least one of Al, Cr, Zr, Nb, Si, Sn and Mn, and the residue comprising Ti and impurities, in which the total content of Al, Cr, Zr, Nb, Si, Sn and Mn is 5% by mass or less, or a titanium alloy for corrosion-resistant materials containing 0.01-0.12% by mass in total of at least one of platinum group elements, 0.05-2.00% by mass in total of any one or both of Co and Ni, at least one of Al, Cr, Zr, Nb, Si, Sn and Mn, and the residue comprising Ti and impurities, in which the total content of Al, Cr, Zr, Nb, Si, Sn and Mn is 5% by mass or less, is excellent in corrosion resistance compared with the respective Comparative Examples, and has corrosion resistance equivalent to that of a conventional titanium alloy for corrosion-resistant materials using sponge titanium.
  • In other words, it is appreciated that the titanium alloy for corrosion-resistant materials of the present invention is capable of suppressing deterioration of corrosion resistance even though it uses recycled titanium alloys or the like, and thus being produced at low cost while maintaining the capability to suppress the deterioration of corrosion resistance.

Claims (4)

  1. A titanium alloy for corrosion-resistant materials, which is characterized in that it contains 0.01-0.12% by mass in total of at least one of platinum group elements, at least one of Al, Cr, Zr, Nb, Si, Sn and Mn, and the residue comprising Ti and impurities, wherein the total content of Al, Cr, Zr, Nb, Si, Sn and Mn is 5% by mass or less.
  2. A titanium alloy for corrosion-resistant materials, which is characterized in that it contains 0.01-0.12% by mass in total of at least one of platinum group elements, 0.05-2.00% by mass in total of any one or both of Co and Ni, at least one of Al, Cr, Zr, Nb, Si, Sn and Mn, and the residue comprising Ti and impurities, wherein the total content of Al, Cr, Zr, Nb, Si, Sn and Mn is 5% by mass or less.
  3. A titanium alloy for corrosion-resistant materials according to claim 1, which is characterized in that it contains 0.01-0.12% by mass in total of at least one of platinum group elements, further contains in percent by mass at least one of Al: more than 0.007% but not more than 5%, Cr: more than 0.007% but not more than 5%, Zr: more than 0.001% but not more than 5%, Nb: more than 0.001% but not more than 5%, Si: more than 0.004% but not more than 5%, Sn: more than 0.001% but not more than 5% and Mn: more than 0.001% but not more than 5%, wherein the total content of Al, Cr, Zr, Nb, Si, Sn and Mn is 5% by mass or less, and the residue comprises Ti and impurities.
  4. A titanium alloy for corrosion-resistant materials according to claim 2, which is characterized in that it contains 0.01-0.12% by mass in total of at least one of platinum group elements, and 0.05-2.00% by mass in total of any one or both of Co and Ni, and further contains in percent by mass at least one of Al: more than 0.007% but not more than 5%, Cr: more than 0.007% but not more than 5%, Zr: more than 0.001% but not more than 5%, Nb: more than 0.001% but not more than 5%, Si: more than 0.004% but not more than 5%, Sn: more than 0.001% but not more than 5% and Mn: more than 0.001% but not more than 5%, wherein the total content of Al, Cr, Zr, Nb, Si, Sn and Mn is 5% by mass or less, and the residue comprises Ti and impurities.
EP06782010.0A 2005-12-28 2006-07-31 Titanium alloy for corrosion-resistant material Active EP1978119B1 (en)

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PL06782010T PL1978119T3 (en) 2005-12-28 2006-07-31 Titanium alloy for corrosion-resistant material

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JP2005377163A JP3916088B2 (en) 2005-12-28 2005-12-28 Titanium alloy for corrosion resistant materials
PCT/JP2006/315132 WO2007077645A1 (en) 2005-12-28 2006-07-31 Titanium alloy for corrosion-resistant material

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EP1978119A1 true EP1978119A1 (en) 2008-10-08
EP1978119A4 EP1978119A4 (en) 2014-07-02
EP1978119B1 EP1978119B1 (en) 2016-11-23

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EP (1) EP1978119B1 (en)
JP (1) JP3916088B2 (en)
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RU (1) RU2405850C2 (en)
WO (1) WO2007077645A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3575422A1 (en) * 2012-08-10 2019-12-04 Nippon Steel Corporation Titanium alloy material

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2426808C1 (en) * 2010-04-29 2011-08-20 Федеральное Государственное Унитарное Предприятие "Центральный Научно-Исследовательский Институт Конструкционных Материалов "Прометей" (Фгуп "Цнии Км "Прометей") Alloy on base of titanium
JP5348355B2 (en) * 2011-07-26 2013-11-20 新日鐵住金株式会社 Titanium alloy
JP5662928B2 (en) * 2011-12-26 2015-02-04 株式会社神戸製鋼所 Support device for solar cell module
RU2502819C1 (en) * 2012-04-19 2013-12-27 Федеральное Государственное Унитарное Предприятие "Центральный Научно-Исследовательский Институт Конструкционных Материалов "Прометей" (Фгуп "Цнии Км "Прометей") Titanium-base alloy
US9957836B2 (en) 2012-07-19 2018-05-01 Rti International Metals, Inc. Titanium alloy having good oxidation resistance and high strength at elevated temperatures
EP2889386B1 (en) 2013-01-25 2018-04-11 Nippon Steel & Sumitomo Metal Corporation Titanium alloy having excellent corrosion resistance in environment containing bromine ions
CN104878246A (en) * 2015-06-02 2015-09-02 张亚南 Alloy material for dental restoration and application of alloy material
US10441607B1 (en) 2016-02-22 2019-10-15 The Board Of Regents Of The University Of Texas System Multifunctional linker technology containing an N4 group
CN107576216A (en) * 2017-09-28 2018-01-12 江苏众众热能科技有限公司 A kind of heat-exchangers of the plate type titanium plate
CN107746997A (en) * 2017-10-23 2018-03-02 宝鸡市永盛泰钛业有限公司 A kind of corrosion resistant titanium alloy and preparation method thereof
CN108467970B (en) * 2018-03-23 2020-12-25 中国石油天然气集团公司管材研究所 Iron-containing titanium alloy pipe for high-corrosivity oil gas development and preparation method thereof
JP6927418B2 (en) 2018-04-10 2021-08-25 日本製鉄株式会社 Titanium alloy and its manufacturing method
CN108893651A (en) * 2018-07-25 2018-11-27 中南大学 A kind of high-strength high-ductility corrosion titanium alloy and preparation method thereof
CN110373571A (en) * 2019-08-28 2019-10-25 浙江海洋大学 A kind of wave key preparation method of light alloy
CN114555842B (en) 2019-10-30 2022-10-18 日本制铁株式会社 Titanium alloy
CN113584345B (en) * 2021-08-06 2022-03-08 东莞亿诚精密模具有限公司 Golf club head material, preparation process thereof and club head striking face
EP4617390A4 (en) 2022-11-09 2026-02-18 Nippon Steel Corp TITANIUM MATERIAL, COMPONENT OF A CHEMICAL DEVICE AND CHEMICAL DEVICE
CN116904799A (en) * 2023-06-02 2023-10-20 中国科学院金属研究所 Titanium alloy suitable for spent fuel post-treatment high Wen Xiaosuan environment and preparation method thereof
CN116516214B (en) * 2023-06-02 2026-03-27 中国科学院金属研究所 A titanium alloy resistant to high-temperature nitric acid corrosion and its preparation method

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61127844A (en) * 1984-11-22 1986-06-16 Nippon Mining Co Ltd Titanium alloy having superior corrosion resistance
JPS61194142A (en) * 1985-02-21 1986-08-28 Nippon Mining Co Ltd Titanium alloy having superior corrosion resistance
JPS6270543A (en) * 1985-09-25 1987-04-01 Nippon Mining Co Ltd Titanium-base alloy excellent in corrosion resistance
JPH0689423B2 (en) * 1985-11-05 1994-11-09 住友金属工業株式会社 Titanium alloy with excellent corrosion resistance
JPS62109936A (en) * 1985-11-08 1987-05-21 Nippon Mining Co Ltd Titanium alloy having superior corrosion resistance
JPS62199744A (en) * 1986-02-25 1987-09-03 Sumitomo Metal Ind Ltd Titanium alloy having superior crevice corrosion resistance
JPS63103045A (en) * 1986-10-20 1988-05-07 Kobe Steel Ltd Ti-ta alloy excellent in resistance to nitric-acid corrosion
JPH0196345A (en) * 1987-10-07 1989-04-14 Kobe Steel Ltd Ti-ru alloy having excellent nitric acid corrosion resistance
US4906436A (en) * 1988-06-27 1990-03-06 General Electric Company High strength oxidation resistant alpha titanium alloy
RU1621543C (en) * 1989-01-05 1994-08-15 ВНИИ авиационных материалов Titanium-base alloy
JPH03197638A (en) * 1989-12-26 1991-08-29 Sumitomo Metal Ind Ltd High strength and high corrosion-resistant titanium base alloy
DE69107758T2 (en) * 1990-10-01 1995-10-12 Sumitomo Metal Ind Process for improving the machinability of titanium and titanium alloys, and titanium alloys with good machinability.
JP2871867B2 (en) * 1991-01-16 1999-03-17 株式会社神戸製鋼所 Corrosion resistant Ti-based alloy
US5316722A (en) * 1992-07-09 1994-05-31 Kabushiki Kaisha Kobe Seiko Sho Corrosion resistant Ti-Cr-Ni alloy containing a platinum group metal
US5478524A (en) * 1992-08-24 1995-12-26 Nissan Motor Co., Ltd. Super high vacuum vessel
JP2000144287A (en) * 1998-11-06 2000-05-26 Daido Steel Co Ltd Titanium alloy for living body with excellent wear resistance
JP3878376B2 (en) * 1998-12-28 2007-02-07 株式会社神戸製鋼所 Corrosion resistant Ti alloy

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3575422A1 (en) * 2012-08-10 2019-12-04 Nippon Steel Corporation Titanium alloy material

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CN101316939A (en) 2008-12-03
EP1978119B1 (en) 2016-11-23
JP2006193829A (en) 2006-07-27
WO2007077645A1 (en) 2007-07-12
PL1978119T3 (en) 2017-06-30
RU2405850C2 (en) 2010-12-10
JP3916088B2 (en) 2007-05-16
EP1978119A4 (en) 2014-07-02
US20090004042A1 (en) 2009-01-01
RU2008130858A (en) 2010-02-10

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