US20040238076A1 - Fe-ni based alloy for shadow mask raw material excellent in corrosion resistance and shadow mask material - Google Patents
Fe-ni based alloy for shadow mask raw material excellent in corrosion resistance and shadow mask material Download PDFInfo
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- US20040238076A1 US20040238076A1 US10/488,257 US48825704A US2004238076A1 US 20040238076 A1 US20040238076 A1 US 20040238076A1 US 48825704 A US48825704 A US 48825704A US 2004238076 A1 US2004238076 A1 US 2004238076A1
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- shadow mask
- alloy
- corrosion resistance
- based alloy
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- 229910045601 alloy Inorganic materials 0.000 title claims abstract description 65
- 239000000956 alloy Substances 0.000 title claims abstract description 65
- 230000007797 corrosion Effects 0.000 title claims abstract description 39
- 238000005260 corrosion Methods 0.000 title claims abstract description 39
- 239000000463 material Substances 0.000 title claims abstract description 29
- 239000002994 raw material Substances 0.000 title description 5
- 229910001030 Iron–nickel alloy Inorganic materials 0.000 claims abstract description 26
- 229910052748 manganese Inorganic materials 0.000 claims abstract description 12
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 4
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 3
- 239000012535 impurity Substances 0.000 claims abstract description 3
- 229910052759 nickel Inorganic materials 0.000 claims abstract description 3
- 229910052758 niobium Inorganic materials 0.000 claims abstract description 3
- 239000013078 crystal Substances 0.000 claims description 19
- 239000010955 niobium Substances 0.000 claims description 15
- 239000000203 mixture Substances 0.000 claims description 9
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 claims description 6
- 239000002131 composite material Substances 0.000 claims description 6
- 229910052761 rare earth metal Inorganic materials 0.000 claims description 6
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 5
- 229910052735 hafnium Inorganic materials 0.000 claims description 5
- 229910052715 tantalum Inorganic materials 0.000 claims description 5
- 229910052719 titanium Inorganic materials 0.000 claims description 5
- 229910052720 vanadium Inorganic materials 0.000 claims description 5
- 229910052726 zirconium Inorganic materials 0.000 claims description 5
- 229910052593 corundum Inorganic materials 0.000 claims description 4
- 229910001845 yogo sapphire Inorganic materials 0.000 claims description 4
- 229910052799 carbon Inorganic materials 0.000 claims description 3
- URLJKFSTXLNXLG-UHFFFAOYSA-N niobium(5+);oxygen(2-) Chemical compound [O-2].[O-2].[O-2].[O-2].[O-2].[Nb+5].[Nb+5] URLJKFSTXLNXLG-UHFFFAOYSA-N 0.000 claims description 3
- 229910052596 spinel Inorganic materials 0.000 claims description 3
- 239000011029 spinel Substances 0.000 claims description 3
- 229910003271 Ni-Fe Inorganic materials 0.000 claims description 2
- JEIPFZHSYJVQDO-UHFFFAOYSA-N iron(III) oxide Inorganic materials O=[Fe]O[Fe]=O JEIPFZHSYJVQDO-UHFFFAOYSA-N 0.000 abstract description 22
- 238000000137 annealing Methods 0.000 abstract description 18
- 239000007858 starting material Substances 0.000 abstract description 12
- 238000004519 manufacturing process Methods 0.000 abstract description 7
- 239000002344 surface layer Substances 0.000 description 11
- 229910000990 Ni alloy Inorganic materials 0.000 description 8
- 230000000052 comparative effect Effects 0.000 description 6
- 230000000694 effects Effects 0.000 description 4
- 229910000831 Steel Inorganic materials 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 3
- 238000005530 etching Methods 0.000 description 3
- 238000005096 rolling process Methods 0.000 description 3
- 239000010959 steel Substances 0.000 description 3
- 229910000655 Killed steel Inorganic materials 0.000 description 2
- 238000005097 cold rolling Methods 0.000 description 2
- 238000009792 diffusion process Methods 0.000 description 2
- 238000004090 dissolution Methods 0.000 description 2
- 238000010894 electron beam technology Methods 0.000 description 2
- 229910021645 metal ion Inorganic materials 0.000 description 2
- 238000007670 refining Methods 0.000 description 2
- 229910001374 Invar Inorganic materials 0.000 description 1
- UCKMPCXJQFINFW-UHFFFAOYSA-N Sulphide Chemical compound [S-2] UCKMPCXJQFINFW-UHFFFAOYSA-N 0.000 description 1
- RQMIWLMVTCKXAQ-UHFFFAOYSA-N [AlH3].[C] Chemical compound [AlH3].[C] RQMIWLMVTCKXAQ-UHFFFAOYSA-N 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052681 coesite Inorganic materials 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 229910052906 cristobalite Inorganic materials 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 229910000484 niobium oxide Inorganic materials 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 239000000377 silicon dioxide Substances 0.000 description 1
- 238000004513 sizing Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
- 238000004544 sputter deposition Methods 0.000 description 1
- 229910052682 stishovite Inorganic materials 0.000 description 1
- 238000005482 strain hardening Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 229910052905 tridymite Inorganic materials 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/02—Ferrous alloys, e.g. steel alloys containing silicon
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/004—Very low carbon steels, i.e. having a carbon content of less than 0,01%
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/04—Ferrous alloys, e.g. steel alloys containing manganese
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/08—Ferrous alloys, e.g. steel alloys containing nickel
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/12—Ferrous alloys, e.g. steel alloys containing tungsten, tantalum, molybdenum, vanadium, or niobium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/48—Ferrous alloys, e.g. steel alloys containing chromium with nickel with niobium or tantalum
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J29/00—Details of cathode-ray tubes or of electron-beam tubes of the types covered by group H01J31/00
- H01J29/02—Electrodes; Screens; Mounting, supporting, spacing or insulating thereof
- H01J29/06—Screens for shielding; Masks interposed in the electron stream
- H01J29/07—Shadow masks for colour television tubes
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J2229/00—Details of cathode ray tubes or electron beam tubes
- H01J2229/07—Shadow masks
- H01J2229/0727—Aperture plate
- H01J2229/0733—Aperture plate characterised by the material
Definitions
- This invention relates to a Fe—Ni based alloy for a shadow mask having an excellent corrosion resistance, which is used in a cathode tube for a color television or the like, and a shadow mask material, and more particularly to a Fe—Ni based alloy having an excellent corrosion resistance, a high stiffness and a low thermal expansion, which is less in the generation of rust even when being exposed to an atmosphere after the bright annealing at a production step of a starting material, and a shadow mask material using this alloy.
- a low carbon aluminum killed steel sheet is used as a shadow mask material.
- This steel sheet is produced, for example, by subjecting a steel sheet after a middle cold rolling to a stress relief middle annealing in a continuous annealing furnace or a batch annealing furnace and then to a finish cold rolling and a temper rolling (including dull rolling).
- a material for a cathode tube or display of a high-quality color television for example, a shadow mask for the cathode tube of the color television is sometimes heated to a temperature reaching to about 80° C. because not more than 1 ⁇ 3 of electron beams pass through openings of the shadow mask and the remaining electron beams collide with the shadow mask.
- the shadow mask material is strained by thermal expansion and brings about the deterioration of color purity.
- Fe-36 Ni based invar alloy being less in the influence of thermal expansion is recently used instead of the above aluminum killed steel sheet.
- Fe—Ni based alloy plates a low thermal expansion Fe-36 Ni based alloy plate reducing Mn as an alloying element (JP-A-5-186853), an alloy plate having a high strength by adding of Nb (U.S. Pat. No. 3,150,831) and the like with the recent flattening and large-sizing of display face.
- the low thermal expansion Fe-36 Ni based alloy having a reduced Mn and the high-strength Fe-36 Ni based alloy added with Nb are not exposed to corrosion environment in the cathode tube because the atmosphere is vacuum, but are exposed in air for a long time in the course of circulation and transportation after the bright annealing as a middle step in the production of the raw material, so that there is caused a case that rust is generated not to provide a product and there is left a problem in the rust prevention.
- the inventors have made various studies with respect to conditions of Fe—Ni based alloys hardly generating rust even when it is exposed to air after the bright annealing as a middle step in the production of the starting material and obtained the following knowledge. It has been found that the rust generated in the starting material (Fe—Ni based alloy) is apt to be easily caused after the bright annealing and also the rust is apt to be generated in low thermal expansion Fe-36 Ni alloy having a reduced Mn rather than the usual Fe-36 Ni alloy.
- the S concentration in the alloy ranging from its surface to a depth of 150 ⁇ is considerably higher than that of a bulk portion (interior portion).
- S is enriched in such a surface layer portion
- S promotes the dissolution of a metal ion and induces the rust.
- such a phenomenon may be solved when the surface layer portion of the alloy plate is removed mechanically and chemically, but it is difficult to conduct this treatment in a commercial scale.
- the inventors attempt to control the enrichment of S in the surface layer of the alloy plate.
- the enrichment of S in the surface layer portion of the Fe-36 Ni alloy plate is zero in the Fe—Ni based alloy having a high Mn content but is conspicuous in the low thermal expansion type Fe-36 Ni alloy having a low Mn content, and that S is entrapped into Mn based inclusion of the Fe—Ni based alloy having the high Mn content, but the enriched amount of S decreases in inverse proportion to the Mn content in the low thermal expansion type Fe-36 Ni alloy having the low Mn content.
- the corrosion resistance of Fe—Ni alloy is largely dependent upon the crystal grain size. That is, it has been confirmed that the corrosion resistance after the bright annealing largely depends on the crystal grain size of the starting material and particularly the corrosion resistance of the material is improved as the crystal grain size becomes small (crystal grain number (ASTM) becomes large). This is considered due to the fact that as the crystal grain size becomes small, the area of the crystal grain boundary increases and the diffusion distance of S becomes long.
- the non-metallic inclusion is effective to include one or more selected from silica (SiO 2 ), spinel (MgO Al 2 O 3 ) and niobium oxide (Nb 2 O 5 ) in addition to MnO—FeO—SiO 2 —Nb 2 O 5 —MgO—Al 2 O 3 -CaO base composite oxide.
- the invention is based on the above knowledge and the gist and construction thereof are as follows.
- the invention is a Fe—Ni based alloy for a shadow mask having an excellent corrosion resistance comprising C ⁇ 0.01 wt %, Si: 0.01-0.1 wt %, Mn: 0.01-0.1 wt %, Ni: 35-37 wt %, Cr ⁇ 0.1 wt %, Nb: 0.01-1.0 wt %, S ⁇ 0.0020 wt %, Al ⁇ 0.005 wt % and the balance being Fe and inevitable impurity.
- the alloy of the invention is preferable to contain 0.005-1.0% in total of one or more selected from Ti, V, Zr, Ta, Hf and REM in addition to the above component composition.
- a maximum value of S concentration in a region ranging from a surface of the alloy to 150 ⁇ is not more than 20 times of a bulk.
- a crystal grain size is not less than No. 9 of ASTM grain size number.
- the alloy of the invention is preferable to contain one or more selected from silica (SiO 2 ), spinel (MgO. Al 2 O 3 ) and niobium oxide (Nb 2 O 5 ) in addition to MnO—FeO—SiO 2 -Nb 2 O 5 -MgO—Al 2 O 3 -CaO base composite oxide.
- silica SiO 2
- spinel MgO. Al 2 O 3
- Nb 2 O 5 niobium oxide
- the invention proposes a shadow mask material having a high corrosion resistance, a high rigidity and a low thermal expansion comprised of the above Ni—Fe based alloy and having a proof strength at 0.2% of not less than 300 N/mm 2 and a thermal expansion coefficient of not more than 1.0 ⁇ 10 ⁇ 6 /OC.
- C is an element contributing to strengthen the material through solid solution and work hardening action.
- the content thereof exceeds 0.01 wt %, a great amount of carbide is precipitated to deteriorate the etching property, press formability, graphitizing property and low thermal expansion property. Therefore, the C content is limited to not more than 0.01 wt %. Preferably, it is not more than 0.005 wt %.
- Mn 0.01-0.1 wt %
- Mn is useful as a solid-soluting element and further is required to add in an amount of not less than 0.01 wt % as a deoxidizing material in the refining of the alloy.
- the addition amount exceeds 0.1 wt %, the thermal expansion is increased, so that the amount is limited to a range of 0.01-0.1 wt %.
- it is 0.01-0.05 wt %.
- Mn is added to produce Mn inclusion, which fixes S diffused in the bright annealing, so that a constant amount of Mn inclusion is required. Therefore, it is necessary that the relation of Mn and S is controlled to satisfy Mn/S ⁇ 25 in view of the corrosion resistance.
- Ni is an element largely exerting upon the thermal expansion property of the Fe—Ni alloy. When the Ni content is 36 wt %, the thermal expansion is minimum, so that Ni is limited to 35-37 wt %.
- Cr is an element considerably improving the corrosion resistance.
- the content exceeds 0.1 wt %, the thermal expansion coefficient becomes high and also the graphitizing property is deteriorated, so that it is limited to not more than 0.1 wt %.
- Nb 0.01-1.0 wt %
- Nb increases the proof strength at 0.2% when being added to the alloy. Also, it has an effect that the crystal gain size is remarkably fined to increase the area of the crystal boundary and to prolong the diffusion distance of S to control the enrichment of S on the surface. Also, not only the toughness, etching property and press formability but also the graphitizing property are improved.
- Nb is required to be added in an amount of at least 0.01 wt %. Preferably, it is added in an amount of not less than 0.10 wt %. However, when the amount exceeds 1.0 wt %, the toughness, press formability and low thermal expansion property rather lower, so that it is limited to 0.01-1.0 wt %.
- S is an element characterizing the alloy according to the invention and is an element largely affecting the corrosion resistance.
- S diffuses near to the neighborhood of the surface of the raw material after the bright annealing and hence the S concentration in a region from the surface of the raw material to a depth of 150 ⁇ (surface layer portion) considerably rises to a bulk to thereby deteriorate the corrosion resistance.
- the S content is limited to not more than 0.0020 wt %, and is preferably not more than 0.0010 wt %.
- Al is a relatively active element, so that if it is included in a great amount, oxidation is preferentially caused on the surface of the steel sheet to obstruct the graphitizing property. Further, Al based oxide is increased to obstruct the etching property. Particularly, when it exceeds 0.005 wt %, the low thermal expansion property lowers, so that it is limited to 0.005 wt %.
- Ti, V, Zr, Ta, Hf and REM are elements contributing to finely divide crystal grains by bonding to C and N to form carbide and nitride and contribute to corrosion resistance by bonding to S to form sulfide.
- one or more selected from Ti, V, Zr, Ta, Hf and REM is less than 0.005 wt % alone or in total, the above effect is insufficient. While when it exceeds 1.0 wt %, the solid soluted amount of the element becomes too large and the low thermal expansion property lowers, so that the amount is limited to 0.005-1.0 wt %.
- the S concentration in a region ranging from the surface of the alloy sheet to 150 ⁇ is made to not more than about 20 times. Because, if the degree of S enriched in the surface layer exceeds 20 times the S concentration of a bulk (base), the dissolution of the metal ion is promoted and the rust is induced. Moreover, the S concentration is preferably not more than 18 times.
- the crystal grain size it is effective to make the crystal grain size to not less than No. 9 as an ASTM grain size number in addition to the above composition planning.
- the corrosion resistance after the bright annealing largely depends upon the crystal grain size of the starting material, and particularly the corrosion resistance of the material is improved as the crystal grain size becomes small (the grain size number becomes large).
- the proof strength at 0.2% largely depends upon the crystal grain size, it is desirable that the crystal grain size is not less than ASTM No. 9 in order to obtain excellent corrosion resistance and rigidity.
- the control of the non-metallic inclusion is further conducted in the invention. That is, the non-metallic inclusion included in the alloy of the invention is required to be a non-metallic inclusion further containing one or more selected from SiO 2 , MgO. Al 2 O 3 and Nb 2 O 5 in addition to MnO—FeO—SiO 2 —Nb 2 O 3 —MgO—Al 2 O 3 —CaO base composite oxide. According to the inventors' studies, it has been confirmed that if acid-soluble MgO single inclusion or CaO single inclusion is produced, the corrosion resistance in the dewing in air is deteriorated.
- a material to be tested is produced by adjusting the components of the alloy so as to have a component composition shown in the following Table 1, and the test material is melted in an air induction furnace to prepare an ingot. Then, the ingot is subjected to a hot forging work at a temperature of 1000-1150° C., hot rolled at a rolling reduction of not less than 80% and then subjected to a solid-soluting heat treatment at 900° C. for 60 seconds in an atmosphere of 30% H 2 +N 2 having a dew point of ⁇ 40° C. Thereafter, it is gradually cooled to obtain a Fe—Ni alloy having a thickness of 0.12 mm.
- the thermal expansion coefficient shown in the table is measured in a range of from room temperature to 300° C. and is determined by an average thermal expansion coefficient at 30-100° C., and the proof strength at 0.2% is measured by a tension test. Also, a maximum value of S enriched amount in a region ranging from the surface of the sheet to 150 ⁇ is carried out by sputtering at an interval of 50 ⁇ through an OJ electron spectroscopic apparatus and conducting an elementary analysis every time to calculating an atomic concentration of S to show a ratio to bulk (the bulk in this examples is a value chemically reviewing of the starting material as a whole). The corrosion resistance is evaluated by a rust generating area ratio at a corrosion state after the exposure in an outdoor air exposure test.
- the alloys adaptable in the invention have sufficient properties such as corrosion resistance, rigidity and low thermal expansion property. That is, the test materials according to the invention have a high rigidity as the proof strength at 0.2% is not less than 300 N/mm 2 , and are low thermal expansion as the thermal expansion coefficient is not more than 1.0 ⁇ 10 ⁇ 16 /° C. Also, they have an excellent corrosion resistance as the rust generating area ratio after the exposure test in air is not more than 0.5%. On the contrary, the comparative materials 19, 20 are poor in the corrosion resistance because the S amount in the bulk is large. Also, the comparative materials 21, 22 are poor in the corrosion resistance because the form of the inclusion contains MgO single body or CaO single body.
- the comparative material 23 is poor in the corrosion resistance and rigidity because the crystal grain size is large.
- the comparative material 24 is poor in the corrosion resistance because the maximum value of the S enriched amount in the region from the sheet surface to 150 ⁇ is not less than 20.
- the Fe—Ni based alloy according to the invention can be produced as a material for shadow mask without generating the rust after the bright annealing.
- the starting material for shadow mask having a high rigidity and a low thermal expansion can be produced, in which the proof strength at 0.2% is not less than 300 N/mm 2 and the thermal expansion coefficient is not more than 1.0 ⁇ 10 ⁇ 6 /° C. as a quality of the material before the formation of the mask.
- the shadow mask material in a cathode tube for a color television or display can be surely produced in a high yield.
Abstract
There is provided a Fe—Ni based alloy for shadow mask having high corrosion resistance, high rigidity and low thermal expansion and hardly generating rust even if being exposed in air in the course of circulation and transportation after the bright annealing as a middle step of the starting material production and a shadow mask material. A Fe—Ni based alloy for a shadow mask having an excellent corrosion resistance comprises C≦0.01 wt %, Si: 0.01-0.1 wt %, Mn: 0.01-0.1 wt %, Ni: 35-37 wt %, Cr≦0.1 wt %, Nb: 0.01-1.0 wt %, S≦0.0020 wt %, Al≦0.005 wt % and the balance being Fe and inevitable impurity, and a shadow mask material is comprised of the alloy having a proof strength at 0.2% of not less than 300 N/mm2 and a thermal expansion coefficient of not more than 1.0×10−6/° C.
Description
- This invention relates to a Fe—Ni based alloy for a shadow mask having an excellent corrosion resistance, which is used in a cathode tube for a color television or the like, and a shadow mask material, and more particularly to a Fe—Ni based alloy having an excellent corrosion resistance, a high stiffness and a low thermal expansion, which is less in the generation of rust even when being exposed to an atmosphere after the bright annealing at a production step of a starting material, and a shadow mask material using this alloy.
- Heretofore, a low carbon aluminum killed steel sheet is used as a shadow mask material. This steel sheet is produced, for example, by subjecting a steel sheet after a middle cold rolling to a stress relief middle annealing in a continuous annealing furnace or a batch annealing furnace and then to a finish cold rolling and a temper rolling (including dull rolling).
- In general, a material for a cathode tube or display of a high-quality color television, for example, a shadow mask for the cathode tube of the color television is sometimes heated to a temperature reaching to about 80° C. because not more than ⅓ of electron beams pass through openings of the shadow mask and the remaining electron beams collide with the shadow mask. As a result, the shadow mask material is strained by thermal expansion and brings about the deterioration of color purity. For this end, as a material of the shadow mask material, it is advantageous to use a raw material having a small thermal expansion coefficient. In this connection, Fe-36 Ni based invar alloy being less in the influence of thermal expansion is recently used instead of the above aluminum killed steel sheet.
- Among the Fe—Ni based alloy plates are used a low thermal expansion Fe-36 Ni based alloy plate reducing Mn as an alloying element (JP-A-5-186853), an alloy plate having a high strength by adding of Nb (U.S. Pat. No. 3,150,831) and the like with the recent flattening and large-sizing of display face.
- However, the low thermal expansion Fe-36 Ni based alloy having a reduced Mn and the high-strength Fe-36 Ni based alloy added with Nb are not exposed to corrosion environment in the cathode tube because the atmosphere is vacuum, but are exposed in air for a long time in the course of circulation and transportation after the bright annealing as a middle step in the production of the raw material, so that there is caused a case that rust is generated not to provide a product and there is left a problem in the rust prevention.
- It is an object of the invention to provide a Fe—Ni based alloy for a high-rigidity, low-thermal expansion shadow mask material being less in the occurrence of rust even when it is exposed to an air over a long time for circulation and transportation after the bright annealing as a middle step in the production of the starting material as well as a shadow mask material.
- As to the above object, the inventors have made various studies with respect to conditions of Fe—Ni based alloys hardly generating rust even when it is exposed to air after the bright annealing as a middle step in the production of the starting material and obtained the following knowledge. It has been found that the rust generated in the starting material (Fe—Ni based alloy) is apt to be easily caused after the bright annealing and also the rust is apt to be generated in low thermal expansion Fe-36 Ni alloy having a reduced Mn rather than the usual Fe-36 Ni alloy. As a result of further examination on this knowledge, it is discovered that in the low-Mn, Fe—Ni based alloy, the S concentration in the alloy ranging from its surface to a depth of 150 Å (surface layer portion) is considerably higher than that of a bulk portion (interior portion). As is generally known, as S is enriched in such a surface layer portion, S promotes the dissolution of a metal ion and induces the rust. Moreover, such a phenomenon may be solved when the surface layer portion of the alloy plate is removed mechanically and chemically, but it is difficult to conduct this treatment in a commercial scale.
- The inventors attempt to control the enrichment of S in the surface layer of the alloy plate. As a result of the inventors' studies, it has been found that the enrichment of S in the surface layer portion of the Fe-36 Ni alloy plate is zero in the Fe—Ni based alloy having a high Mn content but is conspicuous in the low thermal expansion type Fe-36 Ni alloy having a low Mn content, and that S is entrapped into Mn based inclusion of the Fe—Ni based alloy having the high Mn content, but the enriched amount of S decreases in inverse proportion to the Mn content in the low thermal expansion type Fe-36 Ni alloy having the low Mn content. That is, it has been confirmed that a great amount of S not entrapped into the Mn based inclusion is existent in the low thermal expansion Fe-36 Ni alloy having the low Mn content and such an S is enriched by diffusing near to the surface layer in the bright annealing.
- On the other hand, the inventors have found that in order to prevent the occurrence of such a rust, it is required to control a ratio of Mn as an element producing the Mn inclusion to S, and made further studies. As a result, it has been found that the rust hardly occurs when a relation between Mn and S satisfies Mn/S=25-70. Also, it has been found that the rust is not particularly generated when the S concentration in a zone ranging from the surface of the alloy to 150 Å (surface layer portion) is not more than 20 times of that in the bulk portion (interior portion).
- Furthermore, it has been found that the corrosion resistance of Fe—Ni alloy is largely dependent upon the crystal grain size. That is, it has been confirmed that the corrosion resistance after the bright annealing largely depends on the crystal grain size of the starting material and particularly the corrosion resistance of the material is improved as the crystal grain size becomes small (crystal grain number (ASTM) becomes large). This is considered due to the fact that as the crystal grain size becomes small, the area of the crystal grain boundary increases and the diffusion distance of S becomes long.
- Moreover, it has been found that in order to suppress the occurrence of the rust, it is effective to control the non-metallic inclusion in addition to the above countermeasure. As acid-soluble MgO single inclusion or CaO single inclusion is produced, the corrosion resistance in the bedewing in air is deteriorated, and further in case of Nb-containing Fe-36 Ni alloy, the corrosion resistance is confirmed to be deteriorated when MgO single inclusion or CaO single inclusion is included in MnO—FeO—SiO2-Nb2O5-MgO—Al2O3-CaO base composite oxide produced by controlling the formation of alumina based inclusion.
- On the other hand, when an alloy plate has an inclusion composition not including the MgO single inclusion or CaO single inclusion, there is no problem in the corrosion resistance, so that it has been found that the non-metallic inclusion is effective to include one or more selected from silica (SiO2), spinel (MgO Al2O3) and niobium oxide (Nb2O5) in addition to MnO—FeO—SiO2—Nb2O5—MgO—Al2O3-CaO base composite oxide.
- The invention is based on the above knowledge and the gist and construction thereof are as follows.
- That is, the invention is a Fe—Ni based alloy for a shadow mask having an excellent corrosion resistance comprising C≦0.01 wt %, Si: 0.01-0.1 wt %, Mn: 0.01-0.1 wt %, Ni: 35-37 wt %, Cr≦0.1 wt %, Nb: 0.01-1.0 wt %, S≦0.0020 wt %, Al≦0.005 wt % and the balance being Fe and inevitable impurity.
- Moreover, the alloy of the invention is preferable to contain 0.005-1.0% in total of one or more selected from Ti, V, Zr, Ta, Hf and REM in addition to the above component composition.
- Also, the alloy of the invention is preferable to be an alloy wherein a relation of Mn and S satisfies Mn/S=25-70.
- Furthermore, it is preferable that a maximum value of S concentration in a region ranging from a surface of the alloy to 150 Å is not more than 20 times of a bulk.
- In the alloy of the invention, it is also preferable that a crystal grain size is not less than No. 9 of ASTM grain size number.
- Further, the alloy of the invention is preferable to contain one or more selected from silica (SiO2), spinel (MgO. Al2O3) and niobium oxide (Nb2O5) in addition to MnO—FeO—SiO2-Nb2O5-MgO—Al2O3-CaO base composite oxide.
- Also, the invention proposes a shadow mask material having a high corrosion resistance, a high rigidity and a low thermal expansion comprised of the above Ni—Fe based alloy and having a proof strength at 0.2% of not less than 300 N/mm2 and a thermal expansion coefficient of not more than 1.0×10−6/OC.
- The reason why the composition of the Fe—Ni based alloy according to the invention is limited to the above range will be described below.
- C≦0.01 wt %
- C is an element contributing to strengthen the material through solid solution and work hardening action. When the content thereof exceeds 0.01 wt %, a great amount of carbide is precipitated to deteriorate the etching property, press formability, graphitizing property and low thermal expansion property. Therefore, the C content is limited to not more than 0.01 wt %. Preferably, it is not more than 0.005 wt %.
- Si: 0.01-0.1 wt %
- Although it is required to add not less than 0.01 wt % of Si as a deoxidizing material in the refining of the alloy, if the addition amount thereof exceeds 0.1 wt %, the thermal expansion is increased, so that the amount is limited to a range of 0.01-0.1 wt %. Preferably, it is 0.02-0.05 wt %.
- Mn: 0.01-0.1 wt % Mn is useful as a solid-soluting element and further is required to add in an amount of not less than 0.01 wt % as a deoxidizing material in the refining of the alloy. However, when the addition amount exceeds 0.1 wt %, the thermal expansion is increased, so that the amount is limited to a range of 0.01-0.1 wt %. Preferably, it is 0.01-0.05 wt %.
- Also, Mn is added to produce Mn inclusion, which fixes S diffused in the bright annealing, so that a constant amount of Mn inclusion is required. Therefore, it is necessary that the relation of Mn and S is controlled to satisfy Mn/S≧25 in view of the corrosion resistance.
- Ni: 35-37 wt %
- Ni is an element largely exerting upon the thermal expansion property of the Fe—Ni alloy. When the Ni content is 36 wt %, the thermal expansion is minimum, so that Ni is limited to 35-37 wt %.
- Cr≦0.1 wt %
- Cr is an element considerably improving the corrosion resistance. When the content exceeds 0.1 wt %, the thermal expansion coefficient becomes high and also the graphitizing property is deteriorated, so that it is limited to not more than 0.1 wt %.
- Nb: 0.01-1.0 wt %
- Nb increases the proof strength at 0.2% when being added to the alloy. Also, it has an effect that the crystal gain size is remarkably fined to increase the area of the crystal boundary and to prolong the diffusion distance of S to control the enrichment of S on the surface. Also, not only the toughness, etching property and press formability but also the graphitizing property are improved.
- In order to obtain the above effect, and particularly provide the corrosion resistance and the proof strength at 0.2%, therefore, Nb is required to be added in an amount of at least 0.01 wt %. Preferably, it is added in an amount of not less than 0.10 wt %. However, when the amount exceeds 1.0 wt %, the toughness, press formability and low thermal expansion property rather lower, so that it is limited to 0.01-1.0 wt %.
- S≦0.0020 wt %
- S is an element characterizing the alloy according to the invention and is an element largely affecting the corrosion resistance. When the content of S exceeds 0.0020 wt %, S diffuses near to the neighborhood of the surface of the raw material after the bright annealing and hence the S concentration in a region from the surface of the raw material to a depth of 150 Å (surface layer portion) considerably rises to a bulk to thereby deteriorate the corrosion resistance. For this end, the S content is limited to not more than 0.0020 wt %, and is preferably not more than 0.0010 wt %.
- However, it is required to satisfy Mn/S=25-70 in view of the relation of Mn and S.
- Al≦0.005 wt %
- Al is a relatively active element, so that if it is included in a great amount, oxidation is preferentially caused on the surface of the steel sheet to obstruct the graphitizing property. Further, Al based oxide is increased to obstruct the etching property. Particularly, when it exceeds 0.005 wt %, the low thermal expansion property lowers, so that it is limited to 0.005 wt %.
- Ti, V, Zr, Ta, Hf and REM
- Ti, V, Zr, Ta, Hf and REM are elements contributing to finely divide crystal grains by bonding to C and N to form carbide and nitride and contribute to corrosion resistance by bonding to S to form sulfide. When one or more selected from Ti, V, Zr, Ta, Hf and REM is less than 0.005 wt % alone or in total, the above effect is insufficient. While when it exceeds 1.0 wt %, the solid soluted amount of the element becomes too large and the low thermal expansion property lowers, so that the amount is limited to 0.005-1.0 wt %.
- Mn/S=25-70
- In the Fe—Ni alloy according to the invention, Mn and S are required to adjust so as to satisfy a relation of the following equation:
- Mn/S=25-70.
- That is, it is important that S content badly affecting the corrosion resistance is controlled with Mn by adjusting the Mn content in accordance with the S content. when the ratio Mn/S is less than 25, the S content including in Mn based inclusion is less and hence S diffuses near to the surface layer and is enriched in the bright annealing and rust is apt to be caused. A preferable upper limit is about 70.
- In the Fe—Ni alloy according to the invention, the S concentration in a region ranging from the surface of the alloy sheet to 150 Å is made to not more than about 20 times. Because, if the degree of S enriched in the surface layer exceeds 20 times the S concentration of a bulk (base), the dissolution of the metal ion is promoted and the rust is induced. Moreover, the S concentration is preferably not more than 18 times.
- Crystal Grain Size
- In the invention, it is effective to make the crystal grain size to not less than No. 9 as an ASTM grain size number in addition to the above composition planning. According to the inventors' studies, it has been confirmed that the corrosion resistance after the bright annealing largely depends upon the crystal grain size of the starting material, and particularly the corrosion resistance of the material is improved as the crystal grain size becomes small (the grain size number becomes large). Also, since the proof strength at 0.2% largely depends upon the crystal grain size, it is desirable that the crystal grain size is not less than ASTM No. 9 in order to obtain excellent corrosion resistance and rigidity.
- Non-Metallic Inclusion
- In addition to the above composition planning and the crystal grain size adjustment, the control of the non-metallic inclusion is further conducted in the invention. That is, the non-metallic inclusion included in the alloy of the invention is required to be a non-metallic inclusion further containing one or more selected from SiO2, MgO. Al2O3 and Nb2O5 in addition to MnO—FeO—SiO2—Nb2O3—MgO—Al2O3—CaO base composite oxide. According to the inventors' studies, it has been confirmed that if acid-soluble MgO single inclusion or CaO single inclusion is produced, the corrosion resistance in the dewing in air is deteriorated. Further, it has been confirmed that in Nb-containing Fe-36 Ni alloy, when MgO single inclusion or CaO single inclusion is contained in the MnO—FeO—SiO2—Nb2O5—MgO—Al2O3—CaO base composite oxide produced in the control of the alumina inclusion formation, the corrosion resistance is also deteriorated. On the other hand, the inclusion composition containing no MgO single inclusion and CaO single inclusion does not cause problems in the corrosion resistance, so that the inclusion is rendered into the above composition.
- The action and effect of the alloys according to the invention will be concretely described with reference to the examples, but the invention is not limited to only the examples mentioned below.
- A material to be tested is produced by adjusting the components of the alloy so as to have a component composition shown in the following Table 1, and the test material is melted in an air induction furnace to prepare an ingot. Then, the ingot is subjected to a hot forging work at a temperature of 1000-1150° C., hot rolled at a rolling reduction of not less than 80% and then subjected to a solid-soluting heat treatment at 900° C. for 60 seconds in an atmosphere of 30% H2+N2 having a dew point of −40° C. Thereafter, it is gradually cooled to obtain a Fe—Ni alloy having a thickness of 0.12 mm.
- The thermal expansion coefficient shown in the table is measured in a range of from room temperature to 300° C. and is determined by an average thermal expansion coefficient at 30-100° C., and the proof strength at 0.2% is measured by a tension test. Also, a maximum value of S enriched amount in a region ranging from the surface of the sheet to 150 Å is carried out by sputtering at an interval of 50 Å through an OJ electron spectroscopic apparatus and conducting an elementary analysis every time to calculating an atomic concentration of S to show a ratio to bulk (the bulk in this examples is a value chemically reviewing of the starting material as a whole). The corrosion resistance is evaluated by a rust generating area ratio at a corrosion state after the exposure in an outdoor air exposure test. Moreover, when the rust generating area ratio is not less than 0.5%, rust is generated by exposing to air for a long period of time after the bright annealing as a middle step of the starting material production, and hence such a starting material is unsuitable. These results are shown in Table 2.
- As seen from Table 2, it can be said that the alloys adaptable in the invention have sufficient properties such as corrosion resistance, rigidity and low thermal expansion property. That is, the test materials according to the invention have a high rigidity as the proof strength at 0.2% is not less than 300 N/mm2, and are low thermal expansion as the thermal expansion coefficient is not more than 1.0×10−16/° C. Also, they have an excellent corrosion resistance as the rust generating area ratio after the exposure test in air is not more than 0.5%. On the contrary, the comparative materials 19, 20 are poor in the corrosion resistance because the S amount in the bulk is large. Also, the comparative materials 21, 22 are poor in the corrosion resistance because the form of the inclusion contains MgO single body or CaO single body. The comparative material 23 is poor in the corrosion resistance and rigidity because the crystal grain size is large. The comparative material 24 is poor in the corrosion resistance because the maximum value of the S enriched amount in the region from the sheet surface to 150 Å is not less than 20. Moreover, the Fe—Ni based alloy according to the invention can be produced as a material for shadow mask without generating the rust after the bright annealing. Particularly, the starting material for shadow mask having a high rigidity and a low thermal expansion can be produced, in which the proof strength at 0.2% is not less than 300 N/mm2 and the thermal expansion coefficient is not more than 1.0×10−6/° C. as a quality of the material before the formation of the mask.
TABLE 1 Alloy Chemical components Form of Number C Si Mn Ni Cr Nb S Al others Mn/S inclusion Invention alloys 1 0.003 0.03 0.01 35.89 0.01 0.17 0.0003 0.002 — 33 1 2 0.004 0.04 0.03 35.96 0.02 0.18 0.0008 0.001 — 38 1 3 0.003 0.03 0.05 36.01 0.01 0.22 0.0010 0.003 — 50 1 4 0.003 0.04 0.03 35.97 0.05 0.21 0.0012 0.002 — 25 1 5 0.003 0.08 0.08 35.89 0.03 0.20 0.0012 0.004 67 1 6 0.004 0.05 0.05 35.97 0.04 0.02 0.0015 0.003 33 1 7 0.005 0.02 0.03 35.95 0.05 0.50 0.0010 0.001 30 1 8 0.003 0.03 0.04 36.02 0.01 0.95 0.0013 0.004 31 1 9 0.004 0.03 0.03 36.03 0.01 0.19 0.0012 0.003 Ti 0.05 25 1 10 0.003 0.05 0.05 36.20 0.05 0.15 0.0018 0.002 V 0.07 28 1 11 0.002 0.06 0.02 36.15 0.04 0.18 0.0008 0.003 Ti 0.03 25 1 V 0.01 12 0.003 0.02 0.03 36.25 0.03 0.16 0.0011 0.004 Ta 0.05 27 1 13 0.003 0.03 0.04 36.33 0.02 0.21 0.0015 0.001 Zr 0.08 27 1 14 0.004 0.03 0.05 35.98 0.05 0.18 0.0010 0.003 Ta 0.03 50 1 Zr 0.07 15 0.005 0.03 0.02 36.62 0.06 0.20 0.0008 0.002 Hf 0.05 25 1 16 0.003 0.04 0.03 35.99 0.01 0.21 0.0012 0.003 REM 0.05 25 1 17 0.003 0.04 0.03 35.95 0.08 0.19 0.0012 0.002 — 25 2 18 0.004 0.03 0.03 36.26 0.03 0.21 0.0011 0.002 — 27 3 Comparative alloys 19 0.004 0.02 0.02 36.00 0.02 0.10 0.0022 0.004 — 9 1 20 0.004 0.03 0.03 36.07 0.04 0.21 0.0030 0.003 — 10 1 21 0.004 0.05 0.04 35.85 0.05 0.18 0.0016 0.002 — 25 4 22 0.003 0.08 0.06 36.05 0.01 0.20 0.0020 0.002 — 30 5 23 0.003 0.03 0.05 35.97 0.04 0.02 0.0015 0.003 — 33 1 24 0.003 0.02 0.05 35.96 0.01 0.22 0.0020 0.002 — 25 1 -
TABLE 2 Maximum value of Thermal S concentration Rust Proof expansion Crystal in a region from Relative generating area Alloy strength at coefficient grain S amount of surface layer to ratio ratio after air Number 0.2% (N/mm2) (× 10−6/° C.) size No. bulk (A) 150 Å (B) (B/A) exposing test (%) Invention alloys 1 315 0.81 11 0.0003 0.0050 16.8 0.26 2 316 0.84 10 0.0008 0.0013 16.1 0.24 3 320 0.88 11 0.0010 0.0152 15.2 0.25 4 318 0.89 10 0.0012 0.0218 18.2 0.30 5 319 0.88 11 0.0012 0.0160 13.3 0.24 6 305 0.83 9 0.0015 0.0260 17.3 0.26 7 340 0.92 10 0.0010 0.0170 17.0 0.27 8 351 0.95 10 0.0013 0.0224 17.2 0.29 9 321 0.88 11 0.0012 0.0223 18.6 0.31 10 318 0.85 10 0.0018 0.0311 17.3 0.32 11 316 0.87 11 0.0008 0.0146 18.3 0.31 12 322 0.85 11 0.0011 0.0193 17.5 0.30 13 319 0.89 11 0.0015 0.0252 16.8 0.30 14 317 0.87 11 0.0010 0.0153 15.3 0.27 15 335 0.93 11 0.0008 0.0145 18.1 0.30 16 309 0.86 11 0.0012 0.0226 18.8 0.32 17 312 0.88 11 0.0012 0.0223 18.6 0.33 18 319 0.89 11 0.0011 0.0187 17.0 0.30 Comparative alloys 19 319 0.85 10 0.0022 0.1118 50.8 0.97 20 315 0.88 11 0.0030 0.1458 48.6 0.92 21 316 0.83 10 0.0025 0.0770 30.8 0.60 22 319 0.85 11 0.0035 0.0990 25.7 0.52 23 290 0.80 7 0.0015 0.0260 17.3 0.51 24 320 0.88 11 0.0020 0.0430 21.5 0.50 - As mentioned above, according to the invention, there can be provided Fe—Ni based alloys for shadow mask having high corrosion resistance, high rigidity and low thermal expansion and hardly generating rust even if being exposed in air in the course of circulation and transportation after the bright annealing as a middle step of the starting material production. Therefore, the shadow mask material in a cathode tube for a color television or display can be surely produced in a high yield.
Claims (7)
1) A Fe—Ni based alloy for a shadow mask having an excellent corrosion resistance comprising C≦0.01 wt %, Si: 0.01-0.1 wt %, Mn: 0.01-0.1 wt %, Ni: 35-37 wt %, Cr≦0.1 wt %, Nb: 0.01-1.0 wt %, S≦0.0020 wt %, Al≦0.005 wt %, and Mn/S=25-70 and the balance being Fe and inevitable impurity and having a thermal expansion coefficient at 30-100° C. of not more than 1.0×10−6/° C.
2) A Fe—Ni based alloy for a shadow mask according to claim 1 , wherein a relation of Mn and S is rendered into Mn/S≧25.
3) A Fe—Ni based alloy for a shadow mask according to claim 1 , wherein the alloy contains 0.005-1.0% in total of one or more selected from Ti, V, Zr, Ta, Hf and REM in addition to the above component composition.
4) A Fe—Ni based alloy for a shadow mask according to claim 1 , wherein a maximum value of S concentration in a region ranging from a surface of the alloy to 150□ is not more than 20 times of a bulk.
5) A Fe—Ni based alloy for a shadow mask according to claim 1 , wherein a crystal grain size is not less than No. 9 of ASTM grain size number.
6) A Fe—Ni based alloy for a shadow mask having an excellent corrosion resistance according to claim 1 , wherein the alloy contains a non-metallic inclusion comprising one or more selected from silica (SiO2), spinel (MgO□Al2O3) and niobium oxide (Nb2O5) in addition to MnO—FeO—SiO2—Nb2O5—MgO—Al2O3—CaO base composite oxide.
7) A shadow mask material having a high corrosion resistance, a high rigidity and a low thermal expansion comprised of a Ni—Fe based alloy as claimed in claim 1 , and having a proof strength at 0.2% of not less than 300 N/mm2 and a thermal expansion coefficient of not more than 1.0×10−6/° C.
Applications Claiming Priority (3)
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JP2001323145A JP3854121B2 (en) | 2001-10-22 | 2001-10-22 | Fe-Ni alloy for shadow mask material with excellent corrosion resistance and shadow mask material |
JP2001-323145 | 2001-10-22 | ||
PCT/JP2002/010718 WO2003035920A1 (en) | 2001-10-22 | 2002-10-16 | Fe-Ni BASE ALLOY FOR SHADOW MASK RAW MATERIAL EXCELLENT IN CORROSION RESISTANCE AND SHADOW MASK MATERIAL |
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US20040238076A1 true US20040238076A1 (en) | 2004-12-02 |
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US10/488,257 Abandoned US20040238076A1 (en) | 2001-10-22 | 2002-10-16 | Fe-ni based alloy for shadow mask raw material excellent in corrosion resistance and shadow mask material |
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US (1) | US20040238076A1 (en) |
EP (1) | EP1445341A4 (en) |
JP (1) | JP3854121B2 (en) |
KR (1) | KR100595393B1 (en) |
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Cited By (2)
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CN115976395A (en) * | 2022-12-28 | 2023-04-18 | 北冶功能材料(江苏)有限公司 | Preparation method of invar alloy for metal mask |
EP4083249A4 (en) * | 2019-12-27 | 2023-11-29 | Nippon Steel Corporation | Alloy |
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KR101668529B1 (en) | 2014-12-23 | 2016-10-31 | 주식회사 포스코 | Encapsulant for packaging an organic electric device for display with low thermal expansion coefficient |
KR101677352B1 (en) | 2014-12-26 | 2016-11-18 | 주식회사 포스코 | Encapsulant for packaging an organic electric device for display with low thermal expansion coefficient |
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- 2002-10-16 WO PCT/JP2002/010718 patent/WO2003035920A1/en active Application Filing
- 2002-10-16 EP EP02777848A patent/EP1445341A4/en not_active Withdrawn
- 2002-10-16 CN CNB028207742A patent/CN100343405C/en not_active Expired - Fee Related
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Also Published As
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KR100595393B1 (en) | 2006-06-30 |
WO2003035920A1 (en) | 2003-05-01 |
EP1445341A4 (en) | 2004-12-15 |
JP3854121B2 (en) | 2006-12-06 |
EP1445341A1 (en) | 2004-08-11 |
JP2003129185A (en) | 2003-05-08 |
CN100343405C (en) | 2007-10-17 |
KR20040045877A (en) | 2004-06-02 |
CN1571857A (en) | 2005-01-26 |
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