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Небесная энциклопедия

Космические корабли и станции, автоматические КА и методы их проектирования, бортовые комплексы управления, системы и средства жизнеобеспечения, особенности технологии производства ракетно-космических систем

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Мониторинг СМИ

Мониторинг СМИ и социальных сетей. Сканирование интернета, новостных сайтов, специализированных контентных площадок на базе мессенджеров. Гибкие настройки фильтров и первоначальных источников.

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Поддерживает ввод нескольких поисковых фраз (по одной на строку). При поиске обеспечивает поддержку морфологии русского и английского языка
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01-11-2012 дата публикации

Alloy strip material and process for making same

Номер: US20120273094A1
Автор: Craig M. Eucken
Принадлежит: ATI Properties LLC

Methods for producing alloy strips including zirconium alloy strips that demonstrate improved formability are disclosed. The strips of the present disclosure have a purity and crystalline microstructure suitable for improved formability, for example, in the manufacture of certain articles such as panels for plate heat exchangers and high performance tower packing components. Other embodiments disclosed herein relate to formed alloy strip, articles of manufacture produced from the alloy strip, and methods for making the articles of manufacture.

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29-08-2013 дата публикации

Plasma Spray Method

Номер: US20130224393A1

The invention relates to a plasma spray method which can serve as a starting point for a manufacture of metal nanopowder, nitride nanopowder or carbide nanopowder or metal films, nitride films or carbide films. To achieve an inexpensive manufacture of the nanopowder or of the film, in the plasma spray in accordance with the invention a starting material (P) which contains a metal or silicon oxide is introduced into a plasma jet ( 113 ) at a process pressure of at most 1000 Pa, in particular at most 400 Pa. The starting material (P) contains a metal or silicon oxide which vaporizes in the plasma jet ( 113 ) and is reduced in so doing. After the reduction, the metal or silicon which formed the metal or silicon oxide in the starting material is thus present in pure form or in almost pure form. The metal or silicon can be deposited in the form of nanopowder or of a film ( 124 ). Nitride nanoparticles or films or carbide nanoparticles or films can be generated inexpensively by addition of a reactant (R) containing nitrogen or carbon.

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09-01-2014 дата публикации

Composites of bulk amorphous alloy and fiber/wires

Номер: US20140007986A1
Принадлежит: Apple Inc

A composite structure includes a matrix material having an intrinsic strain-to-failure rating in tension and a reinforcing material embedded in the bulk material. The reinforcing material is pre-stressed by a tensile force acting along one direction. The embedded reinforcing material interacts with the matrix material to place the composite structure into a compressive state. The compressive state provides an increased strain-to-failure rating in tension of the composite structure along a direction that is greater than the intrinsic strain-to-failure rating in tension of the matrix material along that direction. At least one of the matrix material and the reinforcing material is a bulk amorphous alloy (BAA). The reinforcing material can be a fiber or wire. In various embodiments, the matrix material may be a bulk amorphous alloy and/or the reinforcing material may be a bulk amorphous alloy.

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20-03-2014 дата публикации

METHOD FOR TREATING Cu THIN SHEET

Номер: US20140079891A1
Принадлежит: NGK Insulators Ltd

A method for treating a Cu thin sheet is provided. The method comprises the steps of: supplying a slurry in which a diffusion bonding aid (DBA), such as Ni powder, and a reinforcing material (RM), such as a carbide base metal compound, are dispersed in a solvent to a predetermined portion on a Cu or Cu base alloy thin sheet, drying the supplied slurry, and applying a laser to induce melting, solidification, and fixation, so as to form a buildup layer. In the method, the weight ratio of DBA to RM is specified to be 80:20 to 50:50, and the median diameters D 50 of both DBA and RM employed fall within 0.1 to 100 μm, the median diameter D 50 of DBA is larger than the median diameter D 50 of RM, and both the distribution ratio D 90 /D 10 of DBA and the distribution ratio D 90 /D 10 of RM are 4.0 or less.

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03-02-2022 дата публикации

CONGRUENTLY MELTING HIGH PURITY TITANIUM ALLOY FOR OPTICAL MOUNTS, FLEXURES, AND STRUCTURAL ELEMENTS REQUIRING COMPLIANCE

Номер: US20220035123A1
Принадлежит:

A flexure including a bipod strut pair extending from a base and a titanium-zirconium-niobium alloy, which includes titanium, about 13.5 to about 14.5 wt. % zirconium, and about 18 to about 19 weight % (wt. %) niobium. The titanium-zirconium-niobium alloy has a congruent melting temperature of about 1750 to about 1800° Celsius (° C.). 1. A flexure comprising:a bipod strut pair extending from a base;wherein the flexure includes a titanium-zirconium-niobium alloy comprising titanium, about 13.5 to about 14.5 wt. % zirconium, and about 18 to about 19 weight % (wt. %) niobium, the titanium-zirconium-niobium alloy having a congruent melting temperature of about 1750 to about 1800° Celsius (° C.).2. The flexure of claim 1 , wherein the flexure is coupled to a support structure claim 1 , and the support structure is further coupled to one or more flexures.3. The flexure of claim 2 , wherein the support base is coupled to a mirror.4. The flexure of claim 1 , wherein the titanium-zirconium-niobium alloy has an elastic modulus of about 7 to about 12 Megapounds per square inch (Msi).5. The flexure of claim 1 , wherein the titanium-zirconium-niobium alloy has an elongation at break of about 8% to about 30%.6. The flexure of claim 1 , wherein the titanium-zirconium-niobium alloy has an ultimate strength of about 115 to about 120 Kilopounds per square inch (Ksi) claim 1 , and an elastic modulus of about 9.6 to about 9.7 Msi.7. A flexure comprising:a circular body; anda plurality of attachment arms arranged on the circular body to couple the flexure to an optical element;wherein the flexure includes a titanium-zirconium-niobium alloy comprising titanium, about 13.5 to about 14.5 wt. % zirconium, and about 18 to about 19 weight % (wt. %) niobium, the titanium-zirconium-niobium alloy having a congruent melting temperature of about 1750 to about 1800° C.8. The flexure of claim 7 , wherein the circular body of the flexure has a diameter of about 5 to about 8 inches.9. The flexure of ...

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18-01-2018 дата публикации

Bulk Metallic Glass Interference Layers

Номер: US20180016661A1
Принадлежит:

BMG parts having an uniform and consistently thick metal oxide layer. The metal oxide layer, also known as an interference layer, exhibits a consistent color and durability over the entire surface of the part. Methods and devices involved in forming the BMG parts with uniformly thick interference layers are also provided. 1. A part comprising:a body composed of an amorphous alloy and defining a surface; andan interference layer formed on a portion of the surface, the interference layer having uniform thickness.2. The part of claim 1 , wherein the portion of the surface of the body is roughened.3. The part of claim 2 , wherein the roughened surface has an average roughness value (Ra) of from 0.005 to 3 μm.4. The part of claim 1 , wherein the uniform interference layer has a thickness that never varies by more than 10%.5. The part of claim 1 , wherein the uniform interference layer has a thickness that never varies by more than 5%.6. The part of claim 1 , wherein the uniform interference layer has a thickness that never varies by more than 1%.7. The part of claim 1 , wherein the amorphous alloy is a bulk metallic glass.8. The part of claim 7 , wherein the bulk metallic glass is at least 40 wt % zirconium.9. A portable electronic device comprising a housing and a cover glass claim 7 , wherein the housing has an external surface that is at least partially covered by an interference layer having an uniform thickness.10. The portable electronic device of claim 9 , wherein the housing is composed of a bulk metallic glass alloy having at least 40% by weight zirconium.11. The portable electronic device of claim 9 , wherein at least the external surface has an average roughness value (Ra) of from 0.005 to 3 μm.12. An anodization mold comprising:a thermally conductive block of material that defines a cavity defining a surface; andone or more heat zones defined in the block for heating of the block;wherein, the surface has an average roughness value of from 0.005 to 3 μm.13. A ...

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26-01-2017 дата публикации

DETECTION DEVICE COMPRISING AN IMPROVED COLD FINGER

Номер: US20170023412A1
Принадлежит:

The detection device comprises a cold finger which performs the thermal connection between a detector and a cooling system. The cold finger comprises at least one side wall at least partially formed by an area made from the amorphous metal alloy. Advantageously, the whole of the cold finger is made from the amorphous metal alloy. 2. The detection device according to claim 1 , wherein the area made from amorphous metal alloy forms a ring.3. The detection device according to claim 2 , wherein the at least one side wall is completely formed by an amorphous metal alloy.4. The detection device according to claim 3 , wherein the cold finger comprises a top formed from crystalline metal and connected to the readout circuit.5. The detection device according to claim 1 , wherein the amorphous metal alloy is chosen from Zirconium/Aluminium/Nickel/Copper alloys claim 1 , Zirconium/Titanium/Copper/Nickel/Beryllium alloys claim 1 , Iron/Nickel/Phosphorus/Boron alloys claim 1 , Iron/Boron alloys claim 1 , Iron/Nickel/Chromium/Phosphorus/Boron alloys claim 1 , Palladium/Nickel/Copper/Phosphorus alloys claim 1 , Palladium/Nickel/Phosphorus alloys claim 1 , Iron/Cobalt/Yttrium/Boron alloys claim 1 , and Cobalt/Nickel/Iron/Silicon/Boron alloys.6. The detection device according to claim 5 , wherein the amorphous metal alloy is chosen from ZrAlNiCualloys claim 5 , ZrTiCuNiBealloys claim 5 , FeBalloys claim 5 , FeNiPBand FeNiCrPBalloys claim 5 , PdNiCuPalloys claim 5 , PdNiPalloys claim 5 , Fe/Co/Y/Bor Fe/Co/Cr/Mo/C/B/Yor (Fe/Cr/Co/Mo/Mn/C/B)/Yalloys claim 5 , and CoNFeSiBalloys. This is a continuation of application Ser. No. 14/335,073 filed Jul. 18, 2014, and claims the benefit of French Application No. 1301711 filed Jul. 18, 2013. The entire disclosures of the prior applications are hereby incorporated by reference in their entirety.The invention relates to a detection device comprising a cold finger forming a cooling support of an infrared detector.In the field of detection devices, ...

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23-01-2020 дата публикации

STABLE BINARY NANOCRYSTALLINE ALLOYS AND METHODS OF IDENTIFYING SAME

Номер: US20200025697A1
Принадлежит: Massachusetts Institute of Technology

Identifying a stable phase of a binary alloy comprising a solute element and a solvent element. In one example, at least two thermodynamic parameters associated with grain growth and phase separation of the binary alloy are determined, and the stable phase of the binary alloy is identified based on the first thermodynamic parameter and the second thermodynamic parameter, wherein the stable phase is one of a stable nanocrystalline phase, a metastable nanocrystalline phase, and a non-nanocrystalline phase. In different aspects, an enthalpy of mixing of the binary alloy may be calculated as a first thermodynamic parameter, and an enthalpy of segregation of the binary alloy may be calculated as a second thermodynamic parameter. In another example, a diagram delineating a plurality of regions respectively representing different stable phases of at least one binary alloy is employed, wherein respective regions of the plurality of regions are delineated by at least one boundary determined as a function of at least two thermodynamic parameters associated with grain growth and phase separation of the at least one binary alloy. 143-. (canceled)44. An alloy comprising:a solvent element and a solute element;the alloy comprising at least one of Al—Pb, Co—Bi, Co—Cd, Co—Pb, Cr—Au, Cr—Bi, Cr—La, Cr—Na, Cr—Pb, Cr—Sc, Cr—Sn, Cr—Th, Cr—Y, Cu—Y, Fe—Ba, Fe—Bi, Fe—Ca, Fe—Cd, Fe—In, Fe—La, Fe—Mg, Fe—Pb, Hf—Mg, Hf—Ti, Ir—Cu, Ir—Ni, Ir—Rh, La—Mn, Mn—Ba, Mn—Ca, Mn—Cd, Mn—La, Mn—Mg, Mn—Pb, Mn—Sr, Mn—Tl, Mo—Au, Mo—Cr, Mo—In, Mo—Na, Mo—Sc, Mo—Th, Mo—V, Mo—Y, Nb—Bi, Nb—Cu, Nb—Ti, Nb—Tl, Nb—V, Ni—Pb, Ni—Sn, Ni—Tl, Os—Bi, Os—Co, Os—Ni, Os—Pb, Os—Pt, Os—Rh, Os—Ru, Pb—Al, Pd—Au, Pt—Au, Re—Bi, Re—Co, Re—La, Re—Ni, Re—Pd, Re—Rh, Re—Sb, Re—Sn, Re—Tc, Rh—Au, Rh—Co, Rh—Cu, Rh—Ni, Ru—Bi, Ru—Co, Ru—Hg, Ru—Ni, Ru—Pt, Ru—Sb, Ta—Bi, Ta—Cu, Ta—Hf, Ta—In, Ta—Ti, Ta—Tl, Ta—Zr, Tc—Ni, Tc—Pd, Tc—Rh, Th—La, Th—Sc, Th—Y, V—Bi, V—Cd, V—In, V—Ti, V—Tl, W—Au, W—Cr, W—In, W—Mn, W—Sb, W—Sc, W—Sn, W—Sr, W—Th, W—Ti, W—V, W ...

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02-02-2017 дата публикации

POWER MODULE SUBSTRATE, POWER MODULE SUBSTRATE WITH HEAT SINK, POWER MODULE, METHOD OF MANUFACTURING POWER MODULE SUBSTRATE, AND COPPER MEMBER-BONDING PASTE

Номер: US20170034905A1
Принадлежит:

This power module substrate includes a copper plate that is formed of copper or a copper alloy and is laminated on a surface of a ceramic substrate a nitride layer that is formed on the surface of the ceramic substrate between the copper plate and the ceramic substrate and an Ag—Cu eutectic structure layer having a thickness of 15 μm or less that is formed between the nitride layer and the copper plate. 1. A power module substrate , comprising:{'sub': 3', '4, 'a ceramic substrate that is formed of AlN or SiNand has a first surface;'}a copper plate that is formed of copper or a copper alloy and is laminated and bonded on the first surface of the ceramic substrate;a nitride layer that contains at least one nitride of elements selected from Ti, Hf, Zr, and Nb and is formed on the first surface of the ceramic substrate between the copper plate and the ceramic substrate; andan Ag—Cu eutectic structure layer that has a thickness of 15 μm or less and is formed between the nitride layer and the copper plate;wherein the thickness of the Ag—Cu eutectic structure layer is measured by a method comprising:obtaining a backscattered electron image of an interface between the copper plate and the ceramic substrate using an EPMA;based on the backscattered electron image, measuring the area of the Ag—Cu eutectic structure layer continuously formed on the bonding interface in a measurement visual field at a magnification of 2000 times;dividing the area of the Ag—Cu eutectic structure layer by the width of the measurement visual field, andobtaining the average of the thicknesses in five measurement visual fields as the thickness of the Ag—Cu eutectic structure layer.2. The power module substrate according to claim 1 , wherein the ceramic substrate is formed of AlN claim 1 , andthe thickness of the Ag—Cu eutectic structure layer is 14 μm or less.3. The power module substrate according to claim 1 , wherein{'sub': 3', '4, 'the ceramic substrate is formed of SiNand'}the thickness of the Ag ...

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11-02-2016 дата публикации

PROCEDURE FOR THE MECHANICAL ALLOYING OF METALS

Номер: US20160039007A1
Принадлежит:

The procedure for the mechanical alloying of metals comprises grinding at least a metal inside a grinding mill together with at least a control agent to obtain a powdered ground product, wherein: —the metal is selected from the list comprising: titanium, zirconium, hafnium, vanadium, niobium, tantalum, chromium, molybdenum, tungsten; and—the control agent is selected from the list comprising: magnesium, calcium and rare earths. 1. A procedure for the mechanical alloying of metals ,comprising grinding at least a metal inside a grinding mill together with at least a control agent to obtain a powdered ground product, wherein:said metal is selected from the list comprising: titanium, zirconium, hathium, vanadium, niobium, tantalum, chromium, molybdenum, tungsten; andsaid control agent is selected from the list comprising: magnesium, calcium and rare earths.2. The procedure according to claim 1 , wherein said grinding comprises grinding said metal and said control agent inside said grinding mill together with other alloy components.5. The procedure according to claim 1 , wherein claim 1 , before said grinding claim 1 , said control agent is in pure state.6. The procedure according to claim 2 , wherein claim 2 , before said grinding claim 2 , said control agent is bonded to said other alloy components.7. The procedure according to claim 1 , wherein said control agent is calcium.8. The procedure according to claim 1 , wherein said control agent is yttrium.9. The procedure according to claim 1 , wherein claim 1 , before said grinding claim 1 , said metal is in the form of powder aggregates.10. The procedure according claim 1 , wherein claim 1 , before said grinding claim 1 , said metal is in the form of a sponge.11. The procedure according to claim 1 , wherein claim 1 , before said grinding claim 1 , said metal is in the form of hydride.12. The procedure according to claim 1 , wherein said metal is titanium.13. The procedure according to claim 1 , wherein said metal is ...

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15-05-2014 дата публикации

Alloy strip material and process for making same

Номер: US20140130946A1
Автор: Craig M. Eucken
Принадлежит: ATI Properties LLC

Methods for producing alloy strips that demonstrate improved formability are disclosed. The strips have a crystalline microstructure suitable for improved formability in the manufacture of various articles such as panels for plate heat exchangers and high performance tower packing components.

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20-02-2020 дата публикации

Capacitor and forming method of capacitor

Номер: US20200058449A1
Принадлежит: Hokkaido University NUC, Tokin Corp

A capacitor includes an anode, an oxide layer, a dielectric layer and a cathode. The oxide layer is located between the anode and the dielectric layer. The anode is made of a Zr-alloy having a composition of ZrM, where M is a metal element capable of forming an oxide coating in an electrolytic solution. The oxide layer includes a composite oxide of ZrM having a hexagonal close-packed structure and having a composition of (ZrM)OY where Y<2. The dielectric layer includes another composite oxide of ZrM having a composition of (ZrM)O2.

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17-03-2016 дата публикации

PRODUCTS AND PROCESSES FOR MAKING BROADHEADS OF AMORPHOUS ALLOYS

Номер: US20160074932A1
Автор: MIZEK ROBERT
Принадлежит:

Embodiments of the present disclosure include broadhead assemblies and components for use with an archery bow and arrow. Embodiments of the present disclosure include products and methods of making broadhead assemblies and components using bulk solidifying amorphous alloys. 1. A method of making a broadhead assembly , comprising:a. providing a reusable mold defining an internal mold cavity matching the shape geometry of a broadhead assembly with a ferrule and a plurality of integrated blades with cutting edges, wherein the mold cavity profile net-to-shape size is less than 0.5% larger than the profile of the intended finished broadhead assembly, and wherein the mold defines a passageway to deliver liquid metal from an entry site to the mold cavity;b. heating a feedstock of metal to a liquid non-crystalline state;c. injecting the liquid-state non-crystalline metal into the mold cavity via the passageway to fill the mold cavity;d. rapidly cooling the liquid-state metal to an amorphous non-crystalline solid state;e. opening the mold and ejecting the finished broadhead assembly; and,f. sharpening the blade cutting edges.2. The method of claim 1 , wherein the amorphous alloy contains greater than 50% zirconium.3. The method of claim 1 , wherein the mold cavity profile net-to-shape size is less than 0.2% larger than the profile of the intended finished broadhead assembly.4. The method of claim 1 , wherein each blade cutting edge thickness is molded with a radius of approximately 10 microns or less claim 1 , and wherein the blade cutting edges are sharpened claim 1 , after ejection claim 1 , to a final cutting radius of approximately 2.0 microns or less.5. The method of claim 1 , wherein said mold is a two piece mold and said broadhead assembly has two blades.6. The method of claim 1 , wherein said mold is a three piece mold and said broadhead assembly has three blades.7. The method of claim 1 , wherein said mold defines a plurality of parting lines and wherein the shape ...

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11-03-2021 дата публикации

ZrNiSn-BASED HALF-HEUSLER THERMOELECTRIC MATERIAL AND PROCESS FOR MANUFACTURING SAME AND FOR REGULATING ANTISITE DEFECTS THEREIN

Номер: US20210074900A1
Принадлежит: Dalian University of Technology

The invention relates to a process for manufacturing a ZrNiSn-based half-Heusler thermoelectric material and regulating antisite defects therein, including the steps of: mixing zirconium (Zr), nickel (Ni), and stannum (Sn) at an atomic ratio of Zr: Ni: Sn=1:1:1; forming an ingot by melting the mixture in a levitation melting furnace; milling the ingot to form a milled powder followed by drying; sintering the dried powder by spark plasma sintering; and placing the sintered powder in a vacuum vessel to be subjected to heat treatment and then quenching treatment to obtain the ZrNiSn-based half-Heusler thermoelectric material. The process is simple, easy to control, and results in a single phase ZrNiSn-based half-Heusler thermoelectric material with antisite defects. 1. A process for manufacturing a ZrNiSn-based half-Heusler thermoelectric material and regulating antisite defects therein , comprising steps of:mixing zirconium (Zr), nickel (Ni), and stannum (Sn) at an atomic ratio of Zr:Ni:Sn=1:1:1;forming an ingot by melting the mixture in a levitation melting furnace;milling the ingot to form a milled powder followed by drying;sintering the dried powder by spark plasma sintering; andplacing the sintered powder in a vacuum vessel to be subjected to heat treatment and then quenching treatment to obtain the ZrNiSn-based half-Heusler thermoelectric material.2. The process according to claim 1 , comprising steps of:(1) mixing Zr, Ni, and Sn at an atomic ratio of Zr: Ni: Sn=1:1:1;(2) forming an ingot by melting the mixture in an argon atmosphere in a levitation melting furnace, with the mixture heated to a temperature of 1600 to 1800° C. and maintained at that temperature for 1 to 5 min;(3) ball-milling the ingot to form a ball-milled powder having a particle size of 0.5 to 2 μm followed by natural drying;(4) sintering the dried powder by spark plasma sintering at 900 to 1100° C. under 80 to 100 MPa for 5 to 20 min;(5) placing the sintered powder into a vacuum vessel;(6) ...

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17-03-2016 дата публикации

CRYSTALLINE ALLOY HAVING GLASS FORMING ABILITY, METHOD FOR MANUFACTURING SAME, ALLOY TARGET FOR SPUTTERING, AND METHOD FOR MANUFACTURING SAME

Номер: US20160076137A1
Принадлежит:

The purpose of the present invention is to provide a crystalline alloy having glass forming ability which has significantly superior thermal stability for being amorphous while having glass forming ability, and a manufacturing method for same. In addition, another purpose of the present invention is to provide an alloy target for sputtering, manufactured by using the crystalline alloy, and a method for manufacturing same. According to one aspect of the present invention, provided is the crystalline alloy having glass forming ability and comprising three or more elements having glass forming ability, wherein the average grain size of the alloy is 0.1-5 μm, and wherein the alloy comprises 67-78 atomic percentage of Zr, 4-13 atomic percentage of Al and/or Co, and 15-24 atomic percentage of Cu and/or Ni. 1. A crystalline alloy having amorphous forming ability , composed of three or more elements having an amorphous forming ability ,wherein the crystalline alloy has an average size of crystal grains in the range of 0.1 μm through 5 μm,wherein the alloy comprises 67 atomic % through 78 atomic % of Zr, 4 atomic % through 13 atomic % of one or more selected from Al and Co, and 15 atomic % through 24 atomic % of one or more selected from Cu and Ni.2. The crystalline alloy of claim 1 , wherein the alloy comprises 67 atomic % through 78 atomic % of Zr claim 1 , 4 atomic % through 12 atomic % of Co claim 1 , and 15 atomic % through 24 atomic % of one or more selected from Cu and Ni.3. The crystalline alloy of claim 1 , wherein the alloy comprises 67 atomic % through 78 atomic % of Zr claim 1 , 3 atomic % through 10 atomic % of Al claim 1 , 2 atomic % through 9 atomic % of Co claim 1 , and 17 atomic % through 23 atomic % of one or more selected from Cu and Ni.4. The crystalline alloy of claim 1 , wherein the alloy has capable to obtain an amorphous ribbon having casting thickness in the range of 20 μm through 100 μm when the melt of the alloy is casted with a cooling rate in the ...

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05-03-2020 дата публикации

ZIRCONIUM ALLOY HAVING EXCELLENT CORROSION RESISTANCE FOR NUCLEAR FUEL CLADDING TUBE AND METHOD OF MANUFACTURING THE SAME

Номер: US20200075181A1
Принадлежит: KEPCO NUCLEAR FUEL CO., LTD.

A zirconium alloy is manufactured through melting; solution heat treatment at 1,000 to 1,050° C. (β) for 30 to 40 min and β-quenching using water; preheating at 630 to 650° C. for 20 to 30 min and hot rolling at a reduction ratio of 60 to 65%; primary intermediate vacuum annealing at 570 to 590° C. for 3 to 4 hr and primarily cold-rolled at a reduction ratio of 30 to 40%; secondary intermediate vacuum annealing at 560 to 580° C. for 2 to 3 hr and secondarily cold-rolled at a reduction ratio of 50 to 60%; tertiary intermediate vacuum annealing at 560 to 580° C. for 2 to 3 hr and tertiarily cold-rolled at a reduction ratio of 30 to 40%; and final vacuum annealing at 460 to 590° C. for 7 to 9 hr. 1. A method of manufacturing a zirconium alloy for a nuclear fuel cladding tube , comprising steps of:(1) melting a mixture comprising 0.5 to 1.2 wt % of Nb, 0.4 to 0.8 wt % of Mo, 0.1 to 0.15 wt % of Cu, 0.15 to 0.2 wt % of Fe, and a balance of zirconium, thus preparing an ingot;(2) subjecting the ingot prepared in step (1) to solution heat treatment at 1,000 to 1,050° C. (β) for 30 to 40 min and then to β-quenching using water;(3) preheating the ingot treated in step (2) at 630 to 650° C. for 20 to 30 min and subjecting the ingot to hot rolling at a reduction ratio of 60 to 65%;(4) subjecting the material hot-rolled in step (3), to primary intermediate vacuum annealing at 570 to 590° C. for 3 to 4 hr and then to primarily cold-rolled at a reduction ratio of 30 to 40%;(5) subjecting the material primarily cold-rolled in step (4), to secondary intermediate vacuum annealing at 560 to 580° C. for 2 to 3 hr and then to secondarily cold-rolled at a reduction ratio of 50 to 60%;(6) subjecting the material secondarily cold-rolled in step (5), to tertiary intermediate vacuum annealing at 560 to 580° C. for 2 to 3 hr and then to tertiarily cold-rolled at a reduction ratio of 30 to 40%; and(7) subjecting the material tertiarily cold-rolled in step (6), to final vacuum annealing.2. The ...

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12-04-2018 дата публикации

STABLE NANOCRYSTALLINE ORDERING ALLOY SYSTEMS AND METHODS OF IDENTIFYING SAME

Номер: US20180100817A1
Принадлежит: Massachusetts Institute of Technology

Provided in one embodiment is a method of identifying a stable phase of an ordering binary alloy system comprising a solute element and a solvent element, the method comprising: determining at least three thermodynamic parameters associated with grain boundary segregation, phase separation, and intermetallic compound formation of the ordering binary alloy system; and identifying the stable phase of the ordering binary alloy system based on the first thermodynamic parameter, the second thermodynamic parameter and the third thermodynamic parameter by comparing the first thermodynamic parameter, the second thermodynamic parameter and the third thermodynamic parameter with a predetermined set of respective thermodynamic parameters to identify the stable phase; wherein the stable phase is one of a stable nanocrystalline phase, a metastable nanocrystalline phase, and a non-nanocrystalline phase. 144-. (canceled)45. An alloy comprising:a mixture of a solute element and a solvent element, the mixture having a phase including at least one of a stable nanocrystalline phase, a metastable nanocrystalline phase, and a non-nanocrystalline phase,the phase having a first thermodynamic parameter associated with grain boundary segregation of the alloy system, a second thermodynamic parameter associated with phase separation of the alloy system, and a third thermodynamic parameter associated with intermetallic compound formation of the alloy system,wherein the phase is stable when the first thermodynamic parameter, the second thermodynamic parameter, and the third thermodynamic parameter are within a predetermined region of a stability map of the alloy.46. The alloy of claim 45 , wherein an enthalpy of mixing is negative.47. The alloy of claim 45 , wherein the alloy includes an intermetallic compound.48. The alloy of claim 45 , wherein the alloy is an ordered binary alloy comprising at least one of Ag—Sc claim 45 , Ag—La claim 45 , Ag—Y claim 45 , Ba—Pd claim 45 , Ba—Pt claim 45 , Be— ...

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21-04-2016 дата публикации

Chromium-Aluminum Binary Alloy Having Excellent Corrosion Resistance and Method of Manufacturing Thereof

Номер: US20160108507A1

The present disclosure relates to a chromium-aluminum binary alloy with excellent corrosion resistance and a method of producing the same, and more particularly to a chromium-aluminum binary alloy with excellent corrosion resistance, including: 1 to 40% by weight of aluminum (Al), the balance of chromium (Cr), and other unavoidable impurities with respect to a total weight of the alloy, and a method of producing a chromium-aluminum binary alloy with excellent corrosion resistance, the method including: (Step 1 ) mixing and melting a raw material comprising: 1 to 40% by weight of aluminum (Al), the balance of chromium (Cr), and other unavoidable impurities with respect to a total weight of the alloy; and (Step 2 ) solution treating the alloy melted in Step 1. The chromium-aluminum binary alloy may be easily produced and has ductility, thus being highly applicable as a coating material for a material requiring high-temperature corrosion resistance and wear resistance.

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19-04-2018 дата публикации

Method of manufacturing zirconium nuclear fuel component using multi-pass hot rolling

Номер: US20180105915A1
Принадлежит: Kepco Nuclear Fuel Co Ltd

Disclosed is a method of manufacturing a zirconium alloy plate, wherein fine precipitates having an average size of 35 nm or less are uniformly distributed in a matrix through multi-pass hot rolling, thus increasing corrosion resistance and fatigue failure resistance, the method including forming a zirconium alloy ingot (step 1 ); subjecting the ingot of step 1 to beta annealing and rapid cooling (step 2 ); preheating the ingot of step 2 (step 3 ); forming a multi-pass hot-rolled plate through primary hot rolling and then air cooling during which secondary hot rolling is subsequently conducted (step 4 ); subjecting the multi-pass hot-rolled plate of step 4 to primary intermediate annealing and primary cold rolling (step 5 ); subjecting the rolled plate of step 5 to secondary intermediate annealing and secondary cold rolling (step 6 ); subjecting the rolled plate of step 6 to tertiary intermediate annealing and tertiary cold rolling (step 7 ); and finally annealing the rolled plate of step 7 (step 8 ).

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05-05-2016 дата публикации

DIE CASTING DEVICE AND METHOD FOR AMORPHOUS ALLOY

Номер: US20160121392A1
Автор: ZHANG Faliang
Принадлежит:

A die casting apparatus () for amorphous alloy and a method of die casting amorphous alloy may be provided. The die casting apparatus may comprise a stationary die () and a movable die (); a sealed cabin () defining a sealing chamber (); a protecting gas supplying device connected with the sealed cabin () for supplying the protecting gas into the sealing chamber (); a melting device () for receiving and melting amorphous alloy; a feed sleeve () having a molten material inlet (), with a plunger () positioned therein for injecting the molten amorphous alloy from the melting device () into a die chamber via the molten material inlet (); a driving device () connected with the plunger () for driving the plunger () in the feed sleeve (); and a gas purifying device () communicated with the sealed cabin () for purifying the gas from the sealed cabin (). 1. A method of die casting an amorphous alloy , comprising:treating gas in a sealing chamber defined in a sealed cabin;supplying a protecting gas into the sealing chamber to maintain the protecting gas in the sealing chamber to a pressure higher than an environmental pressure;feeding amorphous alloy into a melting device disposed inside the sealing chamber to obtain the molten amorphous alloy while the protecting gas filled within the sealing chamber overflowing outside;feeding the molten amorphous alloy into a die chamber defined by a mated stationary die and a movable die via a feed sleeve with a plunger positioned therein; andopening the mated stationary and movable dies to extract at least a component formed at least partially of the amorphous alloy from inside the die chamber while the protecting gas filled within the sealing chamber overflowing outside.2. The method of claim 1 , wherein the treating of the gas is performed by vacuum suction of the sealing chamber via a vacuum suction device or purifying gas inside the sealing chamber by a gas purifier.3. The method of claim 1 , wherein the protecting gas inside the ...

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07-05-2015 дата публикации

STABLE BINARY NANOCRYSTALLINE ALLOYS AND METHODS OF IDENTIFYING SAME

Номер: US20150125338A1
Принадлежит:

Identifying a stable phase of a binary alloy comprising a solute element and a solvent element. In one example, at least two thermodynamic parameters associated with grain growth and phase separation of the binary alloy are determined, and the stable phase of the binary alloy is identified based on the first thermodynamic parameter and the second thermodynamic parameter, wherein the stable phase is one of a stable nanocrystalline phase, a metastable nanocrystalline phase, and a non-nanocrystalline phase. 1. A method of identifying a stable phase of a binary alloy comprising a solute element and a solvent element , the method comprising:(A) determining at least two thermodynamic parameters associated with grain growth and phase separation of the binary alloy; and(B) identifying the stable phase of the binary alloy based on the first thermodynamic parameter and the second thermodynamic parameter by comparing the first thermodynamic parameter and the second thermodynamic parameter with a predetermined set of respective thermodynamic parameters to identify the stable phase;wherein the stable phase is one of a stable nanocrystalline phase, a metastable nanocrystalline phase, and a non-nanocrystalline phase.2. The method of claim 1 , wherein (A) further comprises at least one of:calculating an enthalpy of mixing of the binary alloy as a first thermodynamic parameter,calculating an enthalpy of segregation of the binary alloy as a second thermodynamic parameter, anddetermining a third thermodynamic parameter that is a free energy of mixing as a function of at least one of (i) concentration of grain boundary in the binary alloy, (ii) grain size of the binary alloy, (iii) concentration of the solute element in the binary alloy, and (iv) concentration of the solvent element in the binary alloy.3. (canceled)4. (canceled)5. The method of claim 1 , wherein the binary alloy has a positive enthalpy of mixing claim 1 , and at least one of the at least two thermodynamic parameters is ...

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04-05-2017 дата публикации

Systems and methods implementing wear-resistant copper-based materials

Номер: US20170121799A1
Принадлежит: California Institute of Technology

Systems and methods in accordance with embodiments of the invention implement copper-based materials in applications where resistance to wear is desired. In one embodiment, a wear-resistant gear includes a gear defined by a rotatable body having teeth disposed on an outer surface of the rotatable body, where the gear body is formed at least in part from a material including copper and X, where X is one of zirconium, titanium, hafnium, rutherfordium, and mixtures thereof and where the atomic ratio of copper to X is approximately between 2:3 and 3:2. 1. A wear-resistant alloy comprising:Cu, Zr, Al, Be and optionally Z,wherein Z is one of: Y, Nb, Ti, Cr, Fe, Co, Ni, Zn, B, C, Si, P, Mo, Pd, Ag, Sn, Sb, Hf, Ta, W, Pt, Au, and mixtures thereof;wherein the atomic % of Cu is at least 39.77;wherein the atomic % of Al is between approximately 3% and 10%;wherein the atomic % of Be is between approximately 3% and 10%;wherein the atomic ratio of Cu to Zr is approximately between 2:3 and 3:2; andwherein the alloy has the ability to form a metallic glass material.2. The wear resistant alloy of claim 1 , wherein the atomic ratio of Cu to Zr is approximately between 9:11 and 11:9.3. The wear resistant alloy of claim 2 , wherein Zr is replaced partially or entirely with one of: Ti claim 2 , Hf claim 2 , Rf claim 2 , and mixtures thereof.4. The wear resistant alloy of claim 1 , wherein the alloy composition is one of:{'sub': 43', '43', '7', '7', '40', '40', '10', '10', '39.77', '40.74', '6.79', '9.7', '3', '42.7', '42.7', '6.8', '4.9', '3', '41.7', '41.7', '6.8', '6.8', '3', '41', '40', '7', '7', '5', '42', '41', '7', '7', '3', '42', '41', '7', '7', '3', '44', '44', '5', '3', '4', '41.5', '41.5', '7', '10', '44', '44', '7', '5', '47', '47', '3', '3', '46', '46', '3', '5', '45', '45', '5', '5, 'CuZrAlBe, CuZrAlBe, CuZrAlBeNb, CuZrAlBeNb, CuZrAlBeNb, CuZrAlBeCo, CuZrAlBeCo, CuZrAlBeCr, CuZrAlNiBe, CuZrAlBe, CuZrAlBe, CuZrAlBe, CuZrAlBe, and CuZrAlBe.'}5. The wear resistant alloy of ...

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16-04-2020 дата публикации

MULTI-LAYERED NUCLEAR FUEL CLADDING AND METHOD FOR MANUFACTURING MULTI-LAYERED NUCLEAR FUEL CLADDING

Номер: US20200118697A1
Принадлежит:

Multi-layered nuclear fuel cladding, according to the present invention, comprises: an inner tube of zirconium alloy, of which both ends are open for providing an accommodation space into which a sintered nuclear fuel pellet is inserted; and an outer tube, disposed coaxially with the inner tube, having a greater diameter than the inner tube so as to surround the outer surface of the inner tube, wherein the outer tube and the inner tube are fixed to closely contact each other, and may be formed from metals different from each other. 1. A multi-layered nuclear fuel cladding comprising:an inner tube of zirconium alloy, of which both ends are open for providing an accommodation space into which a sintered body of nuclear fuel is inserted; andan outer tube, disposed coaxially with the inner tube, having a greater diameter than the inner tube so as to surround an outer surface of the inner tube,wherein the outer tube and the inner tube are fixed to closely contact each other, and are formed from metals different from each other.2. The multi-layered nuclear fuel cladding of claim 1 , wherein the metal configured to form the outer tube has a thermal expansion coefficient of 1 ppm/K to 40 ppm/K.3. The multi-layered nuclear fuel cladding of claim 1 , wherein the metal configured to form the outer tube has a thermal neutron absorption cross-sectional area of 0.0045 barn to 440 barn.4. The multi-layered nuclear fuel cladding of claim 1 , wherein the outer tube has greater ductility than the inner tube.5. The multi-layered nuclear fuel cladding of claim 1 , wherein the outer tube comprises a protective layer provided on an outer surface of the outer tube.6. The multi-layered nuclear fuel cladding of claim 5 , wherein the protective layer is a metal oxide or a metal nitride of the metal configured to form the outer tube.7. A method for manufacturing a multi-layered nuclear fuel cladding comprising:forming a preliminary cladding by inserting a preliminary inner tube of zirconium ...

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31-07-2014 дата публикации

Cutting insert

Номер: US20140212233A1
Принадлежит: TAEGUTEC LTD

A cutting insert has only cutting edge portion thereof made of SiC whisker reinforced ceramics brazed to the shank with active solder. This provides improved cutting performance by increased toughness and high strength of the SiC whisker reinforced ceramics without limitation in shape while reducing manufacturing costs. The cutting insert includes a cutting edge portion made of SiC whisker reinforced ceramics, and a shank to which the cutting edge portion is mounted. The cutting edge portion is brazed to the shank using an active solder, and the whiskers are disorderedly arranged and agglomerated in the cutting edge portion.

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12-05-2016 дата публикации

SHELL AND PREPARING METHOD AND USE OF THE SAME

Номер: US20160134729A1
Принадлежит:

The present disclosure provides a shell, a method of preparing the same and the use of the shell. The shell includes: a base () made of ceramic; and a bending part () disposed connected with an edge of the base () and made of an amorphous alloy. 1. A shell , comprising:a base made of ceramic; anda bending part connected with an edge of the base and made of an amorphous alloy.2. The shell of claim 1 , wherein the base has a thickness of about 0.35 millimeters to about 1 millimeter claim 1 , and the bending part has a thickness of about 0.35 millimeters to about 1 millimeter.3. The shell of claim 1 , wherein the base has a hardness of no less than 1000 Hv claim 1 , and the bending part has a hardness of no less than 450 Hv.4. The shell of any one of claim 1 , wherein the amorphous alloy comprises a Zr-based amorphous alloy.5. The shell of any one of claim 1 , wherein the bending part and the base are connected via a circular arc transition segment claim 1 , and a radius of the circular arc transition segment is about 2.5 millimeters to about 5 millimeters.6. The shell of any one of claim 1 , wherein the amorphous alloy is prepared by cooling a liquid alloy at a temperature of about 600 Celsius degrees to about 1000 Celsius degrees at a cooling rate of about 100 Celsius degrees per second to about 200 Celsius degrees per second.7. A method of preparing a shell claim 1 , comprising steps of:providing a base made of ceramic, andforming a bending part made of an amorphous alloy on an edge of the base.8. The method of claim 7 , wherein forming the bending part comprises:providing a liquid alloy at a temperature of about 600 Celsius degrees to about 1000 Celsius degrees under a first pressure;maintaining the liquid alloy under a second pressure greater than the first pressure for about 1 minute to about 10 minutes; andcooling the liquid alloy at a cooling rate of about 100 Celsius degrees per second to about 200 Celsius degrees per second.9. The method of claim 7 , wherein ...

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10-05-2018 дата публикации

ALLOYS FOR INERT MATRIX FUEL COMPOSITIONS, AND METHODS OF MAKING THE SAME

Номер: US20180130562A1
Принадлежит:

In one embodiment, an alloy includes: Zr; Fe; Cu; Ta in an amount from about 1 wt % to about 3 wt %; and one or more optional constituents selected from: Ti, Be, and Nb; and wherein the alloy comprises a ductile phase and a nanoprecipitate hard phase. According to another embodiment, a method of forming an inert matrix nuclear fuel includes: packing a hollow structure with fuel pellets and alloy precursor pellets; heating the fuel pellets and the alloy precursor pellets to at least a melting temperature of an alloy to be formed by melting the alloy precursor pellets; and solidifying the alloy into a matrix surrounding the fuel pellets. The alloy precursor pellets independently comprise: Zr; Fe; Cu; Ta present in an amount from about 1 to about 3 wt %; and one or more optional alloy constituents selected from: Ti, Be, and Nb. 1. An alloy , comprising:Zr;Fe;Cu;Ta in an amount from about 1 wt % to about 3 wt %; andone or more optional constituents selected from: Ti, Be, and Nb; andwherein the alloy comprises a ductile phase and a nanoprecipitate hard phase.2. The alloy as recited in claim 1 , wherein at least 95 vol % of the alloy is characterized by a body-centered-cubic (BCC) crystalline phase.3. The alloy as recited in claim 1 , wherein the nanoprecipitate hard phase occupies approximately 0.01 vol % to approximately 0.1 vol % of the alloy; andwherein the nanoprecipitate hard phase comprises one or more of the Fe and the Ti.4. The alloy as recited in claim 1 , wherein the alloy is formed into a matrix having particles of a fuel dispersed throughout the matrix.5. The alloy as recited in claim 4 , comprising a plurality of pores dispersed throughout the matrix.6. The alloy as recited in claim 4 , comprising a metal cladding surrounding the matrix.7. The alloy as recited in claim 6 , comprising a metallic coating layer between the matrix and the metal cladding.8. The alloy as recited in claim 1 , wherein the alloy is characterized by a formula ZrFeCuTa claim 1 , ...

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15-09-2022 дата публикации

ADDITIVE MANUFACTURING POWDERS WITH IMPROVED PHYSICAL CHARACTERISTICS, METHOD OF MANUFACTURE AND USE THEREOF

Номер: US20220288676A1
Автор: Cauchy Xavier, Rahma Hakim
Принадлежит:

In additive manufacturing operations, powders used in stereolithographic processes need to be precisely spread out in a uniform fashion at every pass of the stereolithographic process to ensure predictability in powder surface morphology. Typically, this is difficult to achieve with conventional powders because often these powders suffer from poor flowability, which may further deteriorate over time, and impairs the efficiency of the stereolithographic processes. The present disclosure describes additive manufacturing powders having improved physical characteristics such as flowability and tap density, which are less sensitive or insensitive to ambient humidity. For example, there is described a powder that includes spherical particles having a particle size distribution of less than 1000 micrometers and having a measurable flowability as determined in accordance with ASTM B213 at 75% relative humidity. 1. Additive manufacturing powder , comprising spherical particles having a particle size distribution (PSD) of from about 0 micrometers (μm) to about 1000 μm and having a flowability of ≤20 s determined in accordance with ASTM B213 at 30% relative humidity.2. The additive manufacturing powder according to claim 1 , having a flowability of ≤15 s determined in accordance with ASTM B213 at 30% relative humidity.3. The additive manufacturing powder according to or claim 1 , comprising particles having a PSD of 0 μm to 25 μm.4. The additive manufacturing powder according to or claim 1 , comprising particles having a PSD of 5 μm to 25 μm.5. The additive manufacturing powder according to or claim 1 , comprising particles having a PSD of 10 μm to 45 μm.6. The additive manufacturing powder according to or claim 1 , comprising particles having a PSD of 15 μm to 63 μm.7. The additive manufacturing powder according to or claim 1 , comprising particles having a PSD of 15 μm to 45 μm.8. The additive manufacturing powder according to or claim 1 , comprising particles having a PSD ...

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15-09-2022 дата публикации

METHODS AND APPARATUSES FOR PRODUCING METALLIC POWDER MATERIAL

Номер: US20220288684A1
Принадлежит:

A method of producing a metallic powder material comprises supplying feed materials to a melting hearth, and melting the feed materials on the melting hearth with a first heat source to provide a molten material having a desired chemical composition. At least a portion of the molten material is passed from the melting hearth either directly or indirectly to an atomizing hearth, where it is heated using a second heat source. At least a portion of the molten material from the atomizing hearth is passed in a molten state to an atomizing apparatus, which forms a droplet spray from the molten material. At least a portion of the droplet spray is solidified to provide a metallic powder material. 1. A method for producing a titanium alloy powder , the method comprising:supplying feed materials to a water-cooled copper melting hearth;melting the feed materials in the water-cooled copper melting hearth with a first plasma torch, thereby producing a molten titanium alloy material in the water-cooled copper melting hearth;passing at least a portion of the molten titanium alloy material from the water-cooled copper melting hearth to a water-cooled copper atomizing hearth;heating the molten titanium alloy material in the water-cooled copper atomizing hearth with a second plasma torch, wherein the water-cooled copper atomizing hearth comprises side walls, a bottom surface, and a drain outlet through a region of the bottom surface, wherein the bottom surface is not disconnectable from the side walls, and wherein the drain outlet is spaced away from the side walls; an inlet adjacent the water-cooled copper atomizing hearth and an outlet adjacent the gas-atomizing nozzle;', 'a melt container region receiving molten material from the water-cooled copper atomizing hearth, wherein one or more electrically conductive coils positioned at the inlet is adapted to selectively heat material within the melt container region; and', 'a passage comprising fluidly cooled walls communicating with ...

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11-06-2015 дата публикации

ZIRCONIUM-BASED AND BERYLLIUM FREE BULK AMORPHOUS ALLOY

Номер: US20150159249A1

The invention concerns a zirconium and/or hafnium based, beryllium free, bulk, amorphous alloy, with the addition of silver and/or gold and/or platinum to increase its critical diameter. 1. A bulk amorphous alloy , wherein the alloy comprises no beryllium and consists , in atomic percent values , of:a base comprising 50%-63% of zirconium and/or hafnium;1.5%-4.5% of at least one first additional metal, said at least one first additional metal being selected from the group consisting of titanium, niobium and tantalum, the niobium being less than or equal to 2.5%;0.5%-4.5% of at least one second additional metal, said at least one second additional metal being selected from the group consisting of silver, gold and platinum;8.5%-17.5% of at least one third additional metal, said at least one third additional metal being selected from the group consisting of nickel, cobalt, manganese and iron;9%-13% of aluminum; andcopper and inevitable impurities in a positive amount less than or equal to 18%.2. The alloy according to claim 1 , wherein the alloy comprises 2.5%-4.5% of said at least one first additional metal.3. The alloy according to claim 1 , wherein the alloy comprises 1.0%-4.0% of said at least one second additional metal.4. The alloy according to claim 3 , wherein the alloy comprises 1.5%-3.8% of said at least one second additional metal.5. The alloy according to claim 1 , wherein the alloy comprises 1.5%-2.5% of gold in atomic percentage.6. The alloy according to claim 1 , wherein the alloy comprises 1.5%-2.5% of platinum in atomic percentage.7. The alloy according to claim 1 , wherein the alloy comprises 1.0%-3.8% of silver in atomic percentage.8. The alloy according to claim 1 , wherein the alloy comprises less than or equal to 60% of zirconium and/or hafnium in the base.9. The alloy according to claim 1 , wherein the alloy comprises more than 10.0% of aluminum.10. The alloy according to claim 1 , wherein the alloy comprises a ratio of zirconium to copper claim 1 ...

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22-09-2022 дата публикации

CLADDED AMORPHOUS METAL PRODUCTS

Номер: US20220297227A1
Принадлежит:

An embodiment relates to a cladded composite comprising a cladding layer of a bulk metallic glass and a substrate; wherein the bulk metallic glass comprises approximately 0% crystallinity, approximately 0% porosity, less than 50 MPa thermal stress, approximately 0% distortion, approximately 0 inch heat affected zone, approximately 0% dilution, and a strength of about 2,000-3,500 MPa. 1. A cladded composite comprising a substrate and a cladding layer comprising a bulk metallic glass on the substrate; wherein the bulk metallic glass comprises 0-10% crystallinity , no porosity , less than 50 MPa thermal stress , no distortion , no heat affected zone , no dilution , and a bond strength of about 2 ,000-3 ,500 MPa;wherein the bulk metallic glass is a Ni based alloy; wherein the substrate comprises steel, aluminum or titanium.2. The cladded composite of claim 1 , wherein the Ni based alloy comprises Ni more than 90% wt.3. The cladded composite of claim 1 , wherein the cladding layer comprises a foil having a foil thickness of about 20-300 μm and the cladding layer has a thickness of about 0.02 mm to 5 mm.4. The cladded composite of claim 3 , wherein the cladding layer comprises multiple sheets of the foil.5. The cladded composite of claim 1 , wherein the bulk metallic glass comprises no crystallinity and no thermal stress.6. The cladded composite of claim 1 , wherein the cladded composite comprises a bond layer between the substrate and the cladding layer.7. The cladded composite of claim 1 , further comprising an interlayer claim 1 , wherein the interlayer and the substrate has a disjoint crystal of less than 1 micron in size.8. The cladded composite of claim 1 , wherein the Ni based alloy comprises Si.9. The cladded composite of claim 1 , wherein the Ni based alloy comprises phosphorus.10. A method comprising: modificating a surface of a bulk metallic glass to remove an oxide layer and cladding the bulk metallic glass on a substrate; wherein the cladding process is done ...

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24-06-2021 дата публикации

METHOD FOR HEAT TREATING A PREFORM MADE OF TITANIUM ALLOY POWDER

Номер: US20210187609A1
Принадлежит:

A method for heat treating a powder part preform including a titanium-based alloy, wherein the method includes the heat treatment of the preform in a furnace at a predetermined temperature, wherein the preform is on a holder during the heat treatment, wherein the holder includes a zirconium-based alloy having a zirconium content greater than or equal to 95% by weight, wherein the holder material has a melting temperature higher than the predefined temperature of the heat treatment, and wherein an anti-diffusion barrier is arranged between the preform and the holder in order to prevent welding of the preform to the holder. 1. A method for heat treating a powder part preform comprising a titanium-based alloy , wherein the method comprises the heat treatment of the preform in a furnace at a predetermined temperature , wherein the preform is on a holder during the heat treatment ,wherein the holder comprises a zirconium-based alloy having a zirconium content greater than or equal to 95% by weight,wherein the holder material has a melting temperature higher than the predefined temperature of the heat treatment, andwherein an anti-diffusion barrier is arranged between the preform and the holder in order to prevent welding of the preform to the holder.2. The method according to claim 1 , wherein the holder comprises a zirconium alloy selected from among the following: Zircaloy-2 claim 1 , Zircaloy-4.3. The method according to claim 1 , wherein the holder has a thickness of between 0.1 mm and 20 mm.4. The method according to claim 1 , wherein the anti-diffusion barrier comprises alumina or yttrium oxide.5. The method according to claim 1 , wherein the holder is stripped.6. The method according to claim 1 , wherein the heat treatment of the preform is sintering of the preform claim 1 , wherein the predefined temperature of the heat treatment is the temperature of a sintering step.7. A method for heat treating a powder part preform of a turbomachine part comprising a titanium ...

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29-09-2022 дата публикации

ROTORS FOR HIGH-PRESSURE COMPRESSORS AND LOW-PRESSURE TURBINE OF A GEARED TURBOFAN ENGINE AND METHOD FOR THE PRODUCTION THEREOF

Номер: US20220307377A1
Автор: KASTENHUBER Michael
Принадлежит:

A method for producing a rotary disk/blisk for a high-pressure compressor or a high-speed turbine and to a corresponding geared turbofan engine. The method involves providing a Ni base alloy comprising, in % by weight, 15.5-16.5 Cr, 14.0-15.5 Co, 4.75-5.25 Ti, 2.75-3.25 Mo. 2.25-2.75 Al, 1.00-1.50 W, as well as optionally 0.0250-0.0500 Zr, 0.0100-0.0200 B, 0.0100-0.0200 C, remainder Ni. The base alloy is shaped by forging to obtain a preform of the disk/blisk, the final contour thereof being produced by electrical discharge machining or electrochemical machining. 19.-. (canceled)10. A method for producing a rotary disk or a blisk for a high-pressure compressor or a high-speed turbine , wherein the method comprises providing a Ni base alloy comprising , in % by weight , from 15.5 to 16.5 Cr , from 14.0 to 15.5 Co , from 4.75 to 5.25 Ti , from 2.75 to 3.25 Mo , from 2.25 to 2.75 Al , from 1.00 to 1.50 W , optionally from 0.0250 to 0.0500 Zr , optionally from 0.0100 to 0.0200 B , optionally from 0.0100 to 0.0200 C , remainder Ni , the Ni base alloy being formed by forging to result in structure and a preform of the disk or blisk , a final contour of the disk or blisk being produced by electrical discharge machining or electrochemical machining.11. The method of claim 10 , wherein a rotary disk or a blisk for a low-pressure turbine of an aircraft engine is produced.12. The method of claim 11 , wherein a rotary disk or a blisk for a low-pressure turbine of a geared turbofan engine is produced.13. The method of claim 11 , wherein the rotary disk or blisk is designed and/or suitable and/or intended for an An≥4 claim 11 ,000 m/sin an Aerodynamic Design Point (ADP) range of the aircraft engine.14. The method of claim 13 , wherein An≥4 claim 13 ,500 m/s.15. The method of claim 13 , wherein An≥5 claim 13 ,000 m/s.16. The method of claim 10 , wherein the Ni base material comprises from 0.0250 to 0.0500 Zr.17. The method of claim 10 , wherein the Ni base material comprises from ...

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21-05-2020 дата публикации

Alloy for biomedical use and medical product

Номер: US20200157660A1

An alloy for biomedical use includes Zr as a main component, Nb the content of which is not less than 0.1% by weight and not greater than 25% by weight, Mo the content of which is not less than 0.1% by weight and not greater than 25% by weight, and Ta the content of which is not less than 0.1% by weight and not greater than 25% by weight. A tensile strength of the alloy is not less than 1000 MPa. A total content of Nb, Mo, and Ta in the alloy is not less than 2% by weight and not greater than 50% by weight. Mass susceptibility of the alloy is not greater than 1.50×10 −6 cm 3 /g. A Young's modulus of the alloy is not greater than 100 GPa. Also disclosed is a medical product including the alloy and a method for producing the alloy.

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28-06-2018 дата публикации

Hardfacing Containing Tungsten Carbide Particles with Barrier Coating and Methods of Making the Same

Номер: US20180178283A1
Автор: Wenhui Jiang
Принадлежит: Individual

A hardfacing composition comprising tungsten carbide particles having a barrier coating and a binder alloy is disclosed. The tungsten carbide particles comprise at least one kind of cast tungsten carbide, carburized tungsten carbide, macro-crystalline tungsten carbide, or sintered tungsten carbide. The barrier coating comprises at least one of metallic carbides, borides, nitrides, or their hybrid compounds. The hardfacing composition takes one of the forms selected from a welding/brazing tube, rod, rope, powder, paste, slurry, or cloth, which are suitable for being applied by various welding or brazing methods. The barrier coating would prevent or mitigate the degradation of the tungsten carbide particles due to attack of a molten binder alloy during a welding or brazing process. One of thermoreactive deposition/diffusion methods—halide activated pack cementation for making tungsten carbide particles having a barrier coating is disclosed.

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18-09-2014 дата публикации

SUPER ELASTIC ZIRCONIUM ALLOY FOR BIOLOGICAL USE, MEDICAL INSTRUMENT AND GLASSES

Номер: US20140271335A1
Принадлежит: University of Tsukuba

Provided is a super elastic alloy for biological use having a high biocompatibility, good processability and super elasticity, said super elastic alloy being a super elastic zirconium alloy for biological use comprising 27-54 mol % inclusive of titanium, 5-9 mol % inclusive of niobium which is a β phase-stabilizing element capable of stabilizing the β phase of zirconium, and 1-4 mol % inclusive in total of tin and/or aluminum which are ω phase-suppressing elements capable of suppressing the ω phase of zirconium, with the balance consisting of zirconium and inevitable impurities. 1. A super-elastic zirconium alloy for living tissues , comprises:titanium within a range of 27 mol %˜54 mol %;niobium within a range of 5 mol %-9 mol %, serving as a β phase stabilizing element for stabilizing the β phase of zirconium;at least one of tin and aluminum within a range of 1 mol %˜4mol %, serving as a ω phase inhibiting element for inhibiting the ω phase of zirconium;zirconium, which accounts for the remaining portion;inevitable impurities.2. A medical appliance claim 1 , made of the super-elastic zirconium alloy for living tissues according to .3. An eyeglasses claim 1 , having a frame made of the super-elastic zirconium alloy for living tissues according to . This application claims priority to PCT Application No. PCT/JP2012/005387, having a filing date of Aug. 28, 2012, the entire contents of which are hereby incorporated by reference.The present invention relates to a super-elastic zirconium alloy for living tissues, and medical appliance and eyeglasses that utilize the super-elastic zirconium alloy for living tissues.A variety of alloys for living tissues are used in surgeries and implants in the medical field.For example, Ti—Ni alloys have advantages such as high strength, wear resistance, corrosion resistance, and high compatibility with living tissues, etc., and are used as materials for living tissues in various medical appliances.However, Ti—Ni light alloys have poor ...

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13-06-2019 дата публикации

Systems and Methods Implementing Wear-Resistant Copper-Based Materials

Номер: US20190177826A1
Принадлежит: California Institute of Technology

Systems and methods in accordance with embodiments of the invention implement copper-based materials in applications where resistance to wear is desired. In one embodiment, a wear-resistant gear includes a gear defined by a rotatable body having teeth disposed on an outer surface of the rotatable body, where the gear body is formed at least in part from a material including copper and X, where X is one of zirconium, titanium, hafnium, rutherfordium, and mixtures thereof and where the atomic ratio of copper to X is approximately between 2:3 and 3:2. 1. A method for increasing the wear-resistance of a mechanical component comprising: [{'sup': '1/2', 'wherein at least an outer surface of the mechanical component is formed from a material having a fracture toughness of less than 80 MPa·m, a hardness of less than 450 Vickers and comprising CuZrXZ and optionally Z,'}, 'wherein X is at least one of Al and Be,', 'wherein Z is one of: Y, Nb, Ti, Cr, Fe, Co, Ni, Zn, B, C, Si, P, Mo, Pd, Ag, Sn, Sb, Hf, Ta, W, Pt, Au, and mixtures thereof,', 'wherein the atomic % of Cu is at least 39.77,', 'wherein the atomic % of Al, where present, is between approximately 3% and 10%,', 'wherein the atomic % of Be, where present, is between approximately 3% and 10%, and', 'wherein the atomic ratio of Cu to Zr is approximately between 2:3 and 3:2;, 'forming a mechanical component having at least one outer surface configured to engage with a mated component and subject to a wear-causing process;'}preparing the mechanical component such that a at least one outer surface has surface irregularities sufficiently small to prevent wear of greater than 15 μm in a single wear cycle; andconfiguring the mechanical component such that the wear-causing process from the mated component imparts a wear stress on the at least one outer surface of less than 5 MPa such that oxidation of the outer surface of the component is inhibited during operation of the wear-causing process.2. The method of claim 1 , wherein ...

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14-07-2016 дата публикации

MOLTEN ALUMINUM RESISTANT ALLOYS

Номер: US20160201170A1
Принадлежит:

Embodiments of methods for protection a material from a reaction from molten aluminum. In some embodiments, a coating can be applied over a substrate which has significantly less of a reaction rate with molten aluminum, thus preventing damage or chemical changes to the substrate. The coating alloy can be formed from cast iron in combination with niobium in some embodiments. 1. A method of protecting a component from molten aluminum reaction , the method comprising:coating a component formed from a base material with an alloy;wherein the alloy has a reaction level to molten aluminum of less than 38 atomic %, the reaction level being calculated by determining a minimum alloy content in a pseudo binary alloy/aluminum phase diagram where the liquidus temperature is at or above 1500K; andwherein the alloy has a minimum concentration of highly resistant secondary phases of 5 mole %.2. The method of claim 1 , wherein the alloy is a Nb—Zr alloy with 30-60 wt. % Zr.3. The method of claim 1 , wherein the alloy has a reaction rate to molten aluminum less than 50% than that of the base material.4. The method of claim 1 , wherein the alloy is a pseudo alloy of grey cast iron and niobium according to the formula: (grey cast iron)Nbwith x ranging from 10 to 30 wt. %.5. The method of claim 1 , wherein the alloy is a pseudo alloy of grey cast iron and niobium according to the formula: (grey cast iron)Nbwith x ranging from 0 to 10 wt. %.6. The method of claim 1 , wherein the alloy has a reaction rate less than 10% than that of the base material.7. The method of claim 1 , wherein the alloy has a reaction rate less than 5% than that of the base material.8. An alloy resistant to molten aluminum claim 1 , the alloy comprising:two or more elements;a reaction level of less than 38 atom %, wherein the reaction level is calculated by determining a minimum alloy content in a pseudo binary alloy/aluminum phase diagram where the liquidus temperature is at or above 1500K; anda minimum ...

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12-07-2018 дата публикации

Method for heat treating a preform made of titanium alloy powder

Номер: US20180193915A1

A method for heat treating a powder part preform including a titanium alloy, includes heat treating the preform in a furnace at a predefined temperature, wherein the preform is on a holder during the heat treatment. The holder includes a titanium alloy having a mass titanium content no lower than 45%, or a zirconium alloy having a mass zirconium content no lower than 95%, wherein the material making up the holder has a melting temperature higher than the predefined heat treatment temperature, and an antidiffusion barrier is arranged between the preform and the holder to prevent the preform from becoming welded to the holder.

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13-07-2017 дата публикации

METHOD FOR PRODUCING A COMPONENT FROM A METAL ALLOY WITH AN AMORPHOUS PHASE

Номер: US20170197246A1
Принадлежит:

The invention relates to a method for producing a component from an at least partially amorphous metal alloy, comprising the following steps: providing a powder from an at least partially amorphous metal alloy; producing a shaped semi-finished product from the powder in that the powder is applied in layers and the powder particles of each newly applied layer, at least at the surface of the semi-finished product to be shaped, are fused and/or melted by targeted local heat input and bond to one another as they cool again; and hot pressing the semi-finished product, wherein the hot pressing is performed at a temperature that is between the transformation temperature and the crystallisation temperature of the amorphous phase of the metal alloy, wherein a mechanical pressure is exerted onto the semi-finished product during the hot pressing and the semi-finished product is compacted during the hot pressing. 1. A method for producing a component from an at least partially amorphous metal alloy , comprising the following steps:providing a powder from an at least partially amorphous metal alloy, wherein the powder consists of spherical powder particles;producing a shaped semi-finished product from the powder in that the powder is applied in layers and the powder particles of each newly applied layer, at least at the surface of the semi-finished product to be shaped, are fused and/or melted by targeted local heat input and bond to one another as they cool again; andhot pressing the semi-finished product, wherein the hot pressing is performed at a temperature that is between the transformation temperature and the crystallisation temperature of the amorphous phase of the metal alloy, wherein a mechanical pressure is exerted onto the semi-finished product during the hot pressing and the semi-finished product is compacted during the hot pressing.2. The method according to claim 1 , wherein:the hot pressing of the semi-finished product is carried out by a hot isostatic pressing of ...

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14-07-2016 дата публикации

HYDROGEN STORAGE ALLOY AND NEGATIVE ELECTRODE AND NI-METAL HYDRIDE BATTERY EMPLOYING SAME

Номер: US20160204429A1
Принадлежит:

A hydrogen storage alloy having a higher electrochemical hydrogen storage capacity than that predicted by the alloy's gaseous hydrogen storage capacity at 2 MPa. The hydrogen storage alloy may have an electrochemical hydrogen storage capacity 5 to 15 times higher than that predicted by the maximum gaseous phase hydrogen storage capacity thereof. The hydrogen storage alloy may be selected from alloys of the group consisting of AB, AB, AB, AB, AB, ABand AB. The hydrogen storage alloy may further be selected from the group consisting of: a) Zr(VNi); wherein 0 Подробнее

20-07-2017 дата публикации

FEEDBACK-ASSISTED RAPID DISCHARGE HEATING AND FORMING OF METALLIC GLASSES

Номер: US20170203358A1
Принадлежит:

The disclosure is directed to an apparatus comprising feedback-assisted control of the heating process in rapid discharge heating and forming of metallic glass articles. 1. A rapid discharge heating and forming (RDHF) apparatus comprising: a source of electrical energy;', 'a metallic glass sample;', 'at least two electrodes connecting the source of electrical energy to a sample of metallic glass feedstock;', 'a feedback control loop comprising:', 'a temperature-monitoring device disposed in temperature monitoring relationship with the sample configured to generate a signal indicative of the temperature of the sample;', {'sub': o', 'o, 'a computing device in signal communication with the temperature-monitoring device configured to convert the signal from the temperature-monitoring device to a sample temperature T, compare T to a predefined temperature value T, and generate a current terminating signal when T substantially matches T; and'}, 'a current interrupting device electrically connected with the source of electrical energy and in signal communication with the computing device, and where the current interrupting device is configured to terminate the electrical current generated by the source of electrical energy when the current terminating signal is received from the computing device; and, 'an electrical circuit comprisinga shaping tool disposed in forming relation to the metallic glass sample.2. The RDHF apparatus of claim 1 , wherein the temperature-monitoring device is selected from a group consisting of thermocouple claim 1 , pyrometer claim 1 , thermographic camera claim 1 , and resistance temperature detector claim 1 , or combinations thereof.3. The RDHF apparatus of claim 1 , wherein the current interrupting device is selected from a group consisting of gate turn-off thyristor claim 1 , power metal oxide semiconductor field emission transistor (MOSFET) claim 1 , integrated gate-commutated thyristor claim 1 , and insulated gate bipolar transistor claim 1 ...

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28-07-2016 дата публикации

Getter, mems device and method of forming the same

Номер: US20160214077A1

A getter is provided. The getter consists essentially of from about 0% to 50% of titanium, from about 0% to 50% zirconium, and from about 5% to 50% of tantalum. A MEMS device is provided. The MEMS device includes a substrate and a getter over the substrate. The getter consists essentially of from about 0% to 50% of titanium, from about 0% to 50% zirconium, and from about 5% to 50% of tantalum. A method of forming a MEMS device is provided. The method includes the following operations: providing a substrate; and providing a getter over the substrate, wherein the getter consists essentially of from about 0% to 50% of titanium, from about 0% to 50% zirconium, and from about 5% to 50% of tantalum, and wherein all of the percentages are atomic percentages.

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04-07-2019 дата публикации

BIOCOMPATIBLE ALLOY AND MEDICAL PRODUCT

Номер: US20190201576A1
Принадлежит:

Provided is a biocompatible alloy having low magnetic susceptibility and excellent mechanical properties. The biocompatible alloy according to the present invention contains: Zr as a main component; Nb of not less than 0.1% by mass and not greater than 25% by mass; Mo of not less than 0.1% by mass and not greater than 25% by mass; and Ta of not less than 0.1% by mass and not greater than 25% by mass. A total content of Nb, Mo, and Ta in the biocompatible alloy is not less than 2% by mass and not greater than 50% by mass. The biocompatible alloy has a mass susceptibility of not greater than 1.50×10cm/g. The biocompatible alloy has a Young's Modulus of not greater than 100 GPa. Various biocompatible implants and medical devices can be manufactured from the biocompatible alloy. 1. A biocompatible alloy comprising:Zr as a main component;Nb of not less than 0.1% by mass and not greater than 25% by mass;Mo of not less than 0.1% by mass and not greater than 25% by mass; andTa of not less than 0.1% by mass and not greater than 25% by mass.2. The biocompatible alloy according to claim 1 , whereina total content of Nb, Mo, and Ta is not less than 2% by mass and not greater than 50% by mass.3. The biocompatible alloy according to claim 1 , whereinthe Nb content is not less than 0.5% by mass and not greater than 25% by mass,the Mo content is not less than 0.1% by mass and not greater than by mass, andthe Ta content is not less than 1.0% by mass and not greater than 15% by mass.4. The biocompatible alloy according to claim 1 , whereinthe Nb content is not less than 12% by mass and not greater than 16% by mass,the Mo content is not less than 0.5% by mass and not greater than 5% by mass, andthe Ta content is not less than 3% by mass and not greater than 12% by mass.5. The biocompatible alloy according to claim 1 , whereina ratio (PMo/PTa) of PMo, which is the Mo content (% by mass), to PTa, which is the Ta content (% by mass), is not less than 1/20 and not greater than 1/3.6. The ...

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23-10-2014 дата публикации

BULK METALLIC GLASS FORMING ALLOY

Номер: US20140311630A1
Принадлежит:

A bulk metallic glass forming alloy having the following composition x(aZr bHf cM dNb eO) yCu zAI and its preparation from an alloy L=(aZr bHf cM dNb eO), Cu, and Al as well as the use thereof is described. 2. The bulk metallic glass forming alloy according to claim 1 , wherein x=71.9 wt % claim 1 , y=24.4 wt % claim 1 , and z=3.7 wt %.3. A method of preparing the bulk metallic glass forming alloy claim 1 , wherein 70.5-73.5 wt % of a pre-formed alloy L=aZr bHf cM dNb eO wherein a claim 1 , b claim 1 , c claim 1 , d claim 1 , e and M are defined above claim 1 , 23.3-25.5 wt % of Cu claim 1 , and 3.4-4.2 wt % of Al are provided and under an inert gas atmosphere claim 1 , are heated to a temperature higher than the liquidus temperature of the pre-formed alloy L claim 1 , homogenized at a temperature of about 50 to about 100 K above the liquidus temperature of the resulting alloy and cast into a metallic mold.4. The method of claim 3 , wherein x=71.9 wt % claim 3 , y=24.4 wt % claim 3 , and z=3.7 wt %.5. Use of the bulk metallic glass forming alloy of in the manufacture of products by means of gravity casting claim 1 , suction casting claim 1 , spray casting claim 1 , die casting claim 1 , high-pressure die casting claim 1 , or thermoplastic forming.6. Use of the bulk metallic glass forming alloy prepared according to in the manufacture of products by means of gravity casting claim 3 , suction casting claim 3 , spray casting claim 3 , die casting claim 3 , high pressure die casting claim 3 , or thermoplastic forming.7. A product manufactured using a process selected from gravity casting claim 1 , suction casting claim 1 , spray casting claim 1 , die casting claim 1 , high pressure die casting claim 1 , and thermoplastic forming claim 1 , which utilizes the bulk glass forming alloy of .8. A product manufactured using a process selected from gravity casting claim 3 , suction casting claim 3 , spray casting claim 3 , die casting claim 3 , high pressure die casting claim 3 ...

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11-08-2016 дата публикации

Hydrogen Storage Alloys

Номер: US20160230253A1
Автор: Nei Jean, Wong Diana, Young Kwo
Принадлежит:

Hydrogen storage alloys comprising a) at least one main phase, b) a storage secondary phase and c) a catalytic secondary phase, where the weight ratio of the catalytic secondary phase abundance to the storage secondary phase abundance is ≧3; or comprising a) at least one main phase, b) from 0 to about 13.3 wt % of a storage secondary phase and c) a catalytic secondary phase, where the alloy comprises from 0.05 at % to 0.98 at % of one or more rare earth elements; or comprising a) at least one main phase, b) from 0 to about 13.3 wt % of a storage secondary phase and c) a catalytic secondary phase, where the alloy comprises for example i) one or more elements selected from the group consisting of Ti, Zr, Nb and Hf and ii) one or more elements selected from the group consisting of V, Cr, Mn, Ni, Sn, Al, Co, Cu, Mo, W, Fe, Si, Sn and rare earth elements, where the atomic ratio of ii) to i) is from about 1.80 to about 1.98, exhibit improved electrochemical properties, for instance improved low temperature electrochemical performance. 1. A hydrogen storage alloy comprising at least one main phase and at least one secondary phase , where the main phase or phases in total are present at a higher abundance by weight than each of the secondary phases ,where the alloy comprises from about 0.05 at % to about 0.98 at % of one or more rare earth elements andwhich alloy exhibits an improvement of surface catalytic ability at{'sub': 2', '12.0', '21.5', '10.0', '7.5', '8.1', '32.2', '0.3', '0.4', '8.0, '−40° C., defined as the product of charge transfer resistance (R) and double layer capacitance (C), of at least 10%, relative to the ABalloy TiZrVCrMnNiSnAlCo; and/or'}which exhibits a charge transfer resistance at −40 C of ≦60 Ω·g; and/orwhich exhibits a surface catalytic ability at −40° C., defined as the product of charge transfer resistance (R) and double layer capacitance (C), of ≦30 seconds.2. An alloy according to comprisinga) at least one main phase,b) optionally a storage ...

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11-08-2016 дата публикации

Hydrogen Storage Alloys

Номер: US20160230254A1
Автор: Nei Jean, Wong Diana, Young Kwo
Принадлежит:

Hydrogen storage alloys comprising a) at least one main phase, b) a storage secondary phase and c) a catalytic secondary phase, where the weight ratio of the catalytic secondary phase abundance to the storage secondary phase abundance is ≧3; or comprising a) at least one main phase, b) from 0 to about 13.3 wt % of a storage secondary phase and c) a catalytic secondary phase, where the alloy comprises from 0.05 at % to 0.98 at % of one or more rare earth elements; or comprising a) at least one main phase, b) from 0 to about 13.3 wt % of a storage secondary phase and c) a catalytic secondary phase, where the alloy comprises for example i) one or more elements selected from the group consisting of Ti, Zr, Nb and Hf and ii) one or more elements selected from the group consisting of V, Cr, Mn, Ni, Sn, Al, Co, Cu, Mo, W, Fe, Si, Sn and rare earth elements, where the atomic ratio of ii) to i) is from about 1.80 to about 1.98, exhibit improved electrochemical properties, for instance improved low temperature electrochemical performance. 1. A hydrogen storage alloy which exhibits{'sub': 2', '12.0', '21.5', '10.0', '7.5', '8.1', '32.2', '0.3', '0.4', '8.0, 'an improvement of surface catalytic ability at −40° C., defined as the product of charge transfer resistance (R) and double layer capacitance (C), of at least 10%, relative to the ABalloy TiZrVCrMnNiSnAlCo; and/or'}a charge transfer resistance at −40° C. of ≦60 Ω·g; and/ora surface catalytic ability at −40° C., defined as the product of charge transfer resistance (R) and double layer capacitance (C), of ≦30 seconds.2. An alloy according to which exhibitsa charge transfer resistance at −40° C. of ≦30 Ω·g; and/ora surface catalytic ability at −40° C. of ≦8.0 seconds.3. An alloy according to comprising at least one main phase and at least one secondary phase claim 1 , where the main phase or phases in total are present at a higher abundance by weight than each of the secondary phases.4. An alloy according to comprisinga) at ...

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11-08-2016 дата публикации

Hydrogen Storage Alloys

Номер: US20160230255A1
Автор: Diana Wong, Jean NEI, Kwo Young
Принадлежит: BASF Corp

Hydrogen storage alloys comprising a) at least one main phase, b) a storage secondary phase and c) a catalytic secondary phase, where the weight ratio of the catalytic secondary phase abundance to the storage secondary phase abundance is ≧3; or comprising a) at least one main phase, b) from 0 to about 13.3 wt % of a storage secondary phase and c) a catalytic secondary phase, where the alloy comprises from 0.05 at % to 0.98 at % of one or more rare earth elements; or comprising a) at least one main phase, b) from 0 to about 13.3 wt % of a storage secondary phase and c) a catalytic secondary phase, where the alloy comprises for example i) one or more elements selected from the group consisting of Ti, Zr, Nb and Hf and ii) one or more elements selected from the group consisting of V, Cr, Mn, Ni, Sn, Al, Co, Cu, Mo, W, Fe, Si, Sn and rare earth elements, where the atomic ratio of ii) to i) is from about 1.80 to about 1.98, exhibit improved electrochemical properties, for instance improved low temperature electrochemical performance.

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18-08-2016 дата публикации

Non-evaporable getter alloys particularly suitable for hydrogen and carbon monoxide sorption

Номер: US20160237533A1
Принадлежит: SAES Getters SpA

Getter devices with improved sorption rate, based on powders of quaternary alloys particularly suitable for hydrogen and carbon monoxide sorption, are described. Quaternary alloys having a composition comprising zirconium, vanadium, titanium and aluminum as main constituent elements are also described.

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18-08-2016 дата публикации

ZIRCONIUM BASED BULK METALLIC GLASSES WITH HAFNIUM

Номер: US20160237538A1
Принадлежит:

Various embodiments of zirconium based bulk metallic glass with hafnium are described herein. In one embodiment, an alloy composition includes zirconium (Zr), hafnium (Hf), copper (Cu), aluminum (Al), at least one element from a group consisting of niobium (Nb) and titanium (Ti), and at least one element from a group consisting of nickel (Ni), iron (Fe), and cobalt (Co). 1. An article formed from a metallic glass composition having zirconium (Zr) , hafnium (Hf) , copper (Cu) , aluminum (Al) , at least one element from a group consisting of niobium (Nb) and titanium (Ti) , and at least one element from a group consisting of nickel (Ni) , iron (Fe) , and cobalt (Co) , the metallic glass composition having a formula of ZrHf(Nb ,Ti)Cu(Ni ,Fe ,Co)Al , wherein ,a is from about 35 to about 60;b is from about 8 to about 20;c is from about 0 to about 8;d is from about 0 to about 40;e is from about 0 to about 30; andf is from about 5 to about 25.2. The article of wherein:a is from about 40 to about 60;b is from about 8 to about 16;c is from about 0 to about 6;d is from about 0 to about 40;e is from about 0 to about 20; andf is from about 7 to about 15.3. The article of wherein:a is from about 45 to about 55;b is from about 8 to about 14;c is from about 2 to about 5;d is from about 0 to about 35;e is from about 0 to about 20; andf is from about 8 to about 11.4. The article of wherein:a+b is from about 40 to about 55; andd+e is from about 20 to about 50.5. The article of wherein:a+b is from about 55 to about 70; andd+e is from about 10 to about 40.6. The article of wherein the metallic glass composition has a formula of ZrHfNbCuNiAlor ZrHfNbCuFeAl.7. The article of wherein a ratio of Hf/(Ti+Nb) is from about 2 to about 5.8. The article of wherein a bend ductility of the article is about 4% when a smallest section thickness of about 4 mm claim 1 , or about 8% with a smallest section thickness of about 2 mm.9. The article of wherein a density of the article is about 7.0 to about ...

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27-11-2014 дата публикации

Crystalline alloy having glass-forming ability, preparation method thereof, alloy target for sputtering, and preparation method thereof

Номер: US20140346038A1

Provided are a crystalline alloy having significantly better thermal stability than an amorphous alloy as well as glass-forming ability, and a method of manufacturing the crystalline alloy. The present invention also provides an alloy sputtering target that is manufactured by using the crystalline alloy, and a method of manufacturing the alloy target. According to an aspect of the present invention, provided is a crystalline alloy having glass-forming ability which is formed of three or more elements having glass-forming ability, wherein the average grain size of the alloy is in a range of 0.1 μm to 5 μm and the alloy includes 5 at % to 20 at % of aluminum (Al), 15 at % to 40 at % of any one or more selected from copper (Cu) and nickel (Ni), and the remainder being zirconium (Zr).

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27-11-2014 дата публикации

STABLE NANOCRYSTALLINE ORDERING ALLOY SYSTEMS AND METHODS OF IDENTIFYING SAME

Номер: US20140348203A1
Принадлежит: Massachusetts Institute of Technology

Provided in one embodiment is a method of identifying a stable phase of an ordering binary alloy system comprising a solute element and a solvent element, the method comprising: determining at least three thermodynamic parameters associated with grain boundary segregation, phase separation, and intermetallic compound formation of the ordering binary alloy system; and identifying the stable phase of the ordering binary alloy system based on the first thermodynamic parameter, the second thermodynamic parameter and the third thermodynamic parameter by comparing the first thermodynamic parameter, the second thermodynamic parameter and the third thermodynamic parameter with a predetermined set of respective thermodynamic parameters to identify the stable phase; wherein the stable phase is one of a stable nanocrystalline phase, a metastable nanocrystalline phase, and a non-nanocrystalline phase. 1. A method of identifying a stable phase of an ordering binary alloy system comprising a solute element and a solvent element , the method comprising:(A) determining at least three thermodynamic parameters associated with grain boundary segregation, phase separation, and intermetallic compound formation of the ordering binary alloy system; and(B) identifying the stable phase of the ordering binary alloy system based on the first thermodynamic parameter, the second thermodynamic parameter and the third thermodynamic parameter by comparing the first thermodynamic parameter, the second thermodynamic parameter and the third thermodynamic parameter with a predetermined set of respective thermodynamic parameters to identify the stable phase;wherein the stable phase is one of a stable nanocrystalline phase, a metastable nanocrystalline phase, and a non-nanocrystalline phase.2. The method of claim 1 , wherein (A) further comprises calculating a free energy of formation of an intermetallic compound of the ordering binary alloy system as the first thermodynamic parameter.3. The method of ...

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15-09-2016 дата публикации

HOT ISOSTATIC PRESSING PROCESS FOR SUPERALLOY POWDER

Номер: US20160263655A1

Hot isostatic press (HIP) process for superalloy powder, to form a superalloy member. A first step HIP temperature is higher than an initial melting temperature of low-melting-point alloy powder and more than 15° C. lower than a solidus of completely homogenized alloy. Pressure is ≧90 MPa, and time is 20 minutes≦t≧1 hour. Heating is stopped after the first step to cool material until temperature is below initial melting temperature of low-melting-point phase. There is temperature keeping for ≧2 hours, to ensure low-melting-point phase, formed during cooling after first step, is completely dissolved. Alloy is cooled after second step to room temperature as furnace pressure keeping continues. Formation of an original particle boundary is prevented or there is significantly reduced the number of precipitated phases on the original particle boundary in HIP procedure, to obtain compact alloy with microscopic structures as equiaxed crystals. 1. A hot isostatic pressing method for superalloy powder , which is characterized in that:the process comprises the following steps:(1) preparing superalloy powder by gas atomization or other methods; sieving the powder to obtain the powder with size less than or equal to 155 μm; loading the sieved powder into a carbon steel or stainless steel capsule; hot degassing and then sealing the capsule;(2) putting the powder capsule prepared in step (1) into a hot isostatic pressing apparatus; starting hot isostatic press compaction after reaching the presupposed conditions in a manner of heating and pressuring simultaneously or heating firstly and then pressuring;wherein the parameters for the hot isostatic press are: the hot isostatic pressing temperature is within the range between the incipient melting temperature of the low-melting-point phase in the powder particles and the solidus of completely homogenized alloy plus 15° C.; the pressure is higher than or equal to 90 MPa; the holding time in this stage is longer than or equal to 20 ...

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22-08-2019 дата публикации

STABLE NANOCRYSTALLINE ORDERING ALLOY SYSTEMS AND METHODS OF IDENTIFYING SAME

Номер: US20190257775A1
Принадлежит: Massachusetts Institute of Technology

Provided in one embodiment is a method of identifying a stable phase of an ordering binary alloy system comprising a solute element and a solvent element, the method comprising: determining at least three thermodynamic parameters associated with grain boundary segregation, phase separation, and intermetallic compound formation of the ordering binary alloy system; and identifying the stable phase of the ordering binary alloy system based on the first thermodynamic parameter, the second thermodynamic parameter and the third thermodynamic parameter by comparing the first thermodynamic parameter, the second thermodynamic parameter and the third thermodynamic parameter with a predetermined set of respective thermodynamic parameters to identify the stable phase; wherein the stable phase is one of a stable nanocrystalline phase, a metastable nanocrystalline phase, and a non-nanocrystalline phase. 144-. (canceled)45. An alloy comprising:a solvent element and a solute element;the alloy comprising at least one of Ag—Sc, Ag—La, Ag—Y, Ba—Pd, Ba—Pt, Be—Ti, Bi—Pd, Ca—Pt, Cd—Pd, Co—Al, Co—As, Co—Ga, Co—Ge, Co—Hf, Co—Nb, Co—Sc, Co—Ta, Co—Ti, Co—Y, Co—Zr, Cr—Pt, Fe—Al, Fe—As, Fe—Hf, Fe—Sc, Fe—Zr, Hf—Ag, Hf—Bi, Hf—Co, Hf—Ni, Hf—Re, Hf—Tl, Ir—Cd, Ir—Cr, Ir—Ge, Ir—In, Ir—Mg, Ir—Mn, Ir—Sb, Ir—Zn, La—Ag, La—Au, La—Ir, La—Rh, La—Zn, Mn—Ga, Mn—Pd, Mn—Sb, Mo—Al, Mo—Ge, Mo—Pd, Nb—Co, Nb—Ga, Nb—Ni, Nb—Re, Nb—Sb, Nb—Sn, Nb—Zn, Ni—Ga, Ni—Ge, Ni—Hf, Ni—In, Ni—La, Ni—Mg, Ni—Nb, Ni—Ta, Ni—Th, Ni—Y, Ni—Zn, Os—As, Os—Ga, Os—Ge, Os—P, Os—V, Os—Y, Os—Zn, Pd—Mn, Pt—Bi, Pt—K, Pt—Mn, Pt—Na, Pt—Tl, Re—Al, Re—As, Re—Ga, Re—Ge, Re—Hf, Re—Nb, Re—Sc, Re—Ta, Re—Ti, Rh—Bi, Rh—Cd, Rh—In, Rh—Mg, Rh—Mn, Rh—Sb, Rh—Sn, Rh—Tl, Rh—Zn, Ru—Ga, Ru—Ge, Ru—La, Ru—Y, Ru—Zn, Sc—Ag, Sc—Ni, Sc—Os, Sc—Ru, Sc—Tc, Sn—Pd, Sr—Pd, Sr—Pt, Ta—Al, Ta—Fe, Ta—Ga, Ta—Ni, Ta—Re, Ta—Sb, Ta—Sn, Ta—Zn, Tc—Ge, Tc—La, Tc—Th, Tc—V, Tc—Y, Tc—Zn, Th—Ir, Th—Rh, Ti—Be, Ti—Bi, Ti—Cd, Ti—Co, Ti—In, Ti—Ni, Ti—Pb, Ti—Sn, Ti—Zn, V—Ga, V—Ru, V—Sb, V—Tc, W ...

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09-12-2021 дата публикации

ZIRCONIUM-BASED METAL GLASS ALLOY

Номер: US20210381083A1
Принадлежит:

According to the present invention, provided is a zirconium-based metal glass alloy including, in atomic %, 62% or more and 67% or less of zirconium (Zr), 1% or more and 5% or less of niobium (Nb), 0.5% or more and 2% or less of titanium (Ti), 12% or more and 15% or less of copper (Cu), 8% or more and 10% or less of nickel (Ni), and 7.5% or more and 8.5% or less of aluminum (Al), the zirconium-based metal glass alloy having a composition represented by ZrNbTiCuNiAl. 1. A zirconium-based metal glass alloy comprising , in atomic % , 62% or more and 67% or less of zirconium (Zr) , 1% or more and 5% or less of niobium (Nb) , 0.5% or more and 2% or less of titanium (Ti) , 12% or more and 15% or less of copper (Cu) , 8% or more and 10% or less of nickel (Ni) , and 7.5% or more and 8.5% or less of aluminum (Al) , the zirconium-based metal glass alloy having a composition represented by ZrNbTiCuNiAl.2. The zirconium-based metal glass alloy according to claim 1 , wherein the total sum of the contents of Zr claim 1 , Nb claim 1 , and Ti (Zr+Nb+Ti) in atomic % is 65% or more and 70% or less.3. The zirconium-based metal glass alloy according to claim 1 , wherein the sum of the contents of Nb and Ti (Nb+Ti) in atomic % is 5% or less claim 1 , and the ratio of the contents of Nb and Ti (Nb/Ti) is 1.0 or more and 8.0 or less.4. The zirconium-based metal glass alloy according to claim 1 , wherein a supercooled liquid region (ΔTx) obtained by difference between crystallization temperature Tx and glass transition temperature Tg (crystallization temperature Tx−glass transition temperature Tg) is 85 K or more.5. The zirconium-based metal glass alloy according to claim 1 , wherein plastic strain (ε) is 10% or more.6. The zirconium-based metal glass alloy according to claim 2 , wherein the sum of the contents of Nb and Ti (Nb+Ti) in atomic % is 5% or less claim 2 , and the ratio of the contents of Nb and Ti (Nb/Ti) is 1.0 or more and 8.0 or less.7. The zirconium-based metal glass alloy ...

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15-10-2015 дата публикации

ZIRCONIUM ALLOY COMPOSITION HAVING LOW HYDROGEN PICK-UP RATE AND HIGH HYDROGEN EMBRITTLEMENT RESISTANCE AND METHOD OF PREPARING THE SAME

Номер: US20150292071A1
Принадлежит: KEPCO NUCLEAR FUEL CO., LTD.

Disclosed herein are zirconium alloy compositions having a low hydrogen pick-up rate and high hydrogen embrittlement resistance. This zirconium alloy composition can be usefully used as a nuclear fuel components in a nuclear power plant because it has a very low hydrogen pick-up rate and high hydrogen embrittlement resistance under operation environments of nuclear power plant. 1. A method of preparing a zirconium alloy having a low hydrogen pick-up rate and high hydrogen embrittlement resistance , comprising the steps of:1) melting a mixture of compositions of a zirconium alloy to prepare an ingot;2) β-annealing the ingot at 1000˜1050° C. for 30˜40 min and then rapidly cooling (β-quenching) the annealed ingot with water;3) preheating the heat-treated ingot to 630˜650° C. for 20˜30 min and then hot-rolling the preheated ingot at a reduction ratio of 60˜65%;4) primarily intermediate-vacuum-heat-treating the hot-rolled product at 560˜580° C. for 3˜4 hours and then primarily cold-rolling the product at a reduction ratio of 50˜60%;5) secondarily intermediate-vacuum-heat-treating the primarily cold-rolled product at 570˜590° C. for 2˜3 hours and then secondarily cold-rolling the product at a reduction ratio of 50˜60%;6) thirdly intermediate-vacuum-heat-treating the secondarily cold-rolled product at 570˜590° C. for 2˜3 hours and then thirdly cold-rolling the product at a reduction ratio of 55˜65%; and7) finally heat-treating the thirdly cold rolled product in vacuum at 460˜470° C. for 8˜9 hours.2. A zirconium alloy composition having low hydrogen pick-up rate and high hydrogen embrittlement resistance , comprising: niobium 1.0˜1.4 wt %; scandium 0.1˜0.3 wt %; aluminum 0.04˜0.06 wt %; tin 0.1˜0.3 wt %; iron 0.04˜0.06 wt %; and a residue of zirconium.3. A zirconium alloy composition having low hydrogen pick-up rate and high hydrogen embrittlement resistance , comprising: niobium 1.0˜1.4 wt %; scandium 0.1˜0.3 wt %; aluminum 0.04˜0.06 wt %; copper 0.04˜0.08 wt %; and a ...

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06-10-2016 дата публикации

METHOD FOR MANUFACURING AMORPHOUS ALLOY FILM AND METHOD FOR MANUFACTURING NANOSTRUCTURED FILM COMPRISING NITORGEN

Номер: US20160289813A1
Принадлежит:

The purpose of the present invention is to provide a nanostructured composite thin film showing low friction properties and a method for manufacturing same, and a member with low friction properties and a method for manufacturing same, wherein the thin film shows an exceptionally low value of friction coefficient but also shows high hardness and adhesion in comparison with conventional thin films, and the member has such a nanostructured composite thin film formed on the surface thereof. Provided, according to one aspect of the present invention, is a nanostructured composite thin film having low friction properties which has a composite structure in which a nitride phase comprising Zr and Al as a nitride component and at least one metallic phase are mixed, and has the size of a crystal grain in the range of 5 nm to 30 nm. Here, the nitride phase has a crystal structure of Zr nitride, and the metallic phase can comprise one or more selected from Cu and Ni. 1. A method of manufacturing a nanostructured film comprising nitrogen , the method comprising:forming a nanostructured film having nitrogen on a substrate by sputtering an alloy target with injection of a reactive gas having nitrogen or nitrogen gas (N2) or nitrogen (N) into a sputtering apparatus,wherein the alloy target is formed by annealing an amorphous alloy or a nano-crystalline alloy composed of three or more metal elements having an amorphous forming ability at a temperature in the range of equal to or more than crystallization starting temperature of the amorphous alloy or the nano-crystalline alloy and less than melting temperature of the amorphous alloy or the nano-crystalline alloy,wherein the alloy target has a microstructure in which crystal grains having an average size in the range of 0.1 μm through 5 μm are uniformly distributed,wherein the amorphous alloy or nano-crystalline alloy has 5 atomic % through 20 atomic % of Al, 15 atomic % through 40 atomic % of one or more selected from Cu and Ni, ...

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05-10-2017 дата публикации

Nuclear fuel claddings, production method thereof and uses of same against oxidation/hydriding

Номер: US20170287578A1

The invention relates to a nuclear fuel cladding comprising: i) a substrate containing a zirconium-based inner layer, optionally coated with at least one intermediate layer formed by at least one intermediate material selected from among tantalum, molybdenum, tungsten, niobium, vanadium, hafnium or the alloys thereof; and ii) at least one protective outer layer placed on the substrate and formed by a protective material selected from either chromium or an alloy of chromium. The nuclear fuel cladding produced using the method of the invention has improved resistance to oxidation/hydriding. The invention also relates to the method for the production of the nuclear fuel cladding by ion etching of the surface of the substrate and deposition of the outer layer on the substrate with a high power impulse magnetron sputtering method (HiPIMS), as well as to the use thereof to protect against oxidation and/or hydriding.

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22-10-2015 дата публикации

ASSEMBLY HAVING AT LEAST TWO CERAMIC BODIES JOINED WITH ONE ANOTHER, ESPECIALLY A PRESSURE MEASURING CELL, AND METHOD FOR JOINING CERAMIC BODIES BY MEANS OF AN ACTIVE HARD SOLDER, OR BRAZE

Номер: US20150298264A1
Принадлежит: Friedrich-Schiller-Universitat Jena

An assembly comprising: two ceramic bodies, which are joined by means of a joint of an active hard solder, or braze, wherein the active hard solder, or braze, has a continuous core volume, which is spaced, in each case, from the ceramic bodies by at least 1 μm, and an average composition Cwith a liquidus temperature T(C), wherein the composition Chas a coefficient of thermal expansion α(C), wherein α(C)=m·α(K), wherein m≦1.5, especially m≦1.3 and preferably m≦1.2, wherein α(K) is the average coefficient of thermal expansion of the ceramic material of the ceramic bodies, wherein the joint has boundary layers, which border on the ceramic body, wherein at least one of the boundary layers, which lies outside of the core volume, has an average composition Cwith a liquidus temperature T(C), which lies not less than 50 K, preferably not less than 100 K, and especially preferably not less than 200 K, under the liquidus temperature T(C) of the average composition Cof the core volume. 116-. (canceled)18. The assembly as claimed in claim 17 , wherein:said at least one boundary layer has a thickness of no more than 3 μm, especially no more than 2 μm and preferably no more than 1 μm.19. The assembly as claimed in claim 17 , wherein:{'sub': B', 'l', 'B', 'l', 'e', 'e, 'the composition Chas a liquidus temperature T(C), which lies no more than 300 K, preferably no more than 150 K, and preferably no more than 50 K above the liquidus temperature T(C) of the eutectic point, respectively of the nearest intersection with a eutectic valley having a composition Cin the composition space,'}{'sub': e', 'e1', 'eN', 'e', 'ei', 'i, 'wherein C:=(c, . . . , c), wherein |C|=1, and wherein the care the stoichiometric fractions of the components Kwith i=1, . . . , N at the eutectic point, respectively a nearest intersection with a eutectic valley.'}20. The assembly as claimed in claim 17 , wherein:{'sub': e', 'e', 'e1', 'eN', 'e', 'ei', 'i', 'e', 'B', 'eB', 'e', 'B', 'eB', 'eB', 'eB', 'K', 'B', 'KB ...

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22-10-2015 дата публикации

DIELECTRIC AND METHOD FOR PRODUCING THE SAME, AND ELECTROLYTIC CAPACITOR

Номер: US20150299887A1
Принадлежит:

There are provided a dielectric and an electrolytic capacitor that have a small amount of leakage current, and have high reliability also in a high temperature environment. A dielectric containing at least zirconium, titanium, and a carbon atom, wherein a concentration of the carbon atom is 100 ppm or more and 10,000 ppm or less, and an atomic ratio of the titanium to a sum of the zirconium and the titanium is 30% or more and 90% or less. 1. A dielectric comprising at least zirconium , titanium , and a carbon atom , whereina concentration of the carbon atom is 100 ppm or more and 10,000 ppm or less, andan atomic ratio of the titanium to a sum of the zirconium and the titanium is 30% or more and 90% or less.2. A method for producing the dielectric according to claim 1 , comprising:mixing an alloy of zirconium and titanium with an organic binder to obtain a mixture;sintering the mixture to obtain a sintered body; andanodizing the sintered body.3. The method for producing the dielectric according to claim 2 , wherein the organic binder is at least one selected from the group consisting of an acrylic resin claim 2 , a polyvinyl alcohol resin claim 2 , a styrenic resin claim 2 , and camphor.4. A method for producing the dielectric according to claim 1 , comprising:heat-treating an alloy of zirconium and titanium in a gas comprising organic compound A; andanodizing the alloy after the heat treatment.5. A method for producing the dielectric according to claim 1 , comprising:anodizing an alloy of zirconium and titanium in a solution comprising organic compound B.6. A dielectric produced by the method according to .7. A dielectric produced by the method according to .8. A dielectric produced by the method according to .9. A dielectric produced by the method according to .10. An electrolytic capacitor comprising the dielectric according to .11. An electrolytic capacitor comprising the dielectric according to .12. An electrolytic capacitor comprising the dielectric according ...

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20-10-2016 дата публикации

ZIRCONIUM ALLOY HAVING EXCELLENT CORROSION RESISTANCE AND CREEP RESISTANCE AND METHOD OF MANUFACTURING THE SAME

Номер: US20160304991A1
Принадлежит: KEPCO NUCLEAR FUEL CO., LTD.

A zirconium alloy is manufactured through melting; solution heat treatment at 1,000 to 1,050° C. for 30 to 40 min and β-quenching using water; preheating at 630 to 650° C. for 20 to 30 min and hot rolling at a reduction ratio of 60 to 65%; primary intermediate vacuum annealing at 570 to 590° C. for 3 to 4 hr and primarily cold-rolled at a reduction ratio of 30 to 40%; secondary intermediate vacuum annealing at 560 to 580° C. for 2 to 3 hr and secondarily cold-rolled at a reduction ratio of 50 to 60%; tertiary intermediate vacuum annealing at 560 to 580° C. for 2 to 3 hr and tertiarily cold-rolled at a reduction ratio of 30 to 40%; and final vacuum annealing at 440 to 650° C. for 7 to 9 hr. 1. A zirconium alloy , comprising:1.1 to 1.2 wt % of Nb, 0.01 to 0.2 wt % of P, 0.2 to 0.3 wt % of Fe, and a balance of Zr.2. The zirconium alloy of claim 1 , wherein P is added in an amount of 0.02 to 0.07 wt %.3. The zirconium alloy of claim 1 , further comprising 0.01 to 0.15 wt % of Ta.4. The zirconium alloy of claim 3 , wherein Ta is added in an amount of 0.03 to 0.1 wt %.5. A method of manufacturing a zirconium alloy claim 3 , comprising steps of:(1) melting a mixture comprising 1.1 to 1.2 wt % of Nb, 0.01 to 0.2 wt % of P, 0.2 to 0.3 wt % of Fe, and a balance of Zr, thus preparing an ingot;(2) subjecting the ingot prepared in step (1) to solution heat treatment at 1,000 to 1,050° C. (β-phase range) for 30 to 40 min and then to β-quenching using water;(3) preheating the ingot treated in step (2) at 630 to 650° C. for 20 to 30 min and subjecting the ingot to hot rolling at a reduction ratio of 60 to 65%;(4) subjecting the material hot-rolled in step (3), to primary intermediate vacuum annealing at 570 to 590° C. for 3 to 4 hr and then to primarily cold-rolled at a reduction ratio of 30 to 40%;(5) subjecting the material primarily cold-rolled in step (4), to secondary intermediate vacuum annealing at 560 to 580° C. for 2 to 3 hr and then to secondarily cold-rolled at a ...

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29-10-2015 дата публикации

Zirconium based bulk metallic glasses with hafnium

Номер: US20150307975A1
Принадлежит: Washington State University WSU

Various embodiments of zirconium based bulk metallic glass with hafnium are described herein. In one embodiment, an alloy composition includes zirconium (Zr), hafnium (Hf), copper (Cu), aluminum (Al), at least one element from a group consisting of niobium (Nb) and titanium (Ti), and at least one element from a group consisting of nickel (Ni), iron (Fe), and cobalt (Co).

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29-10-2015 дата публикации

ZIRCONIUM ALLOYS WITH IMPROVED CORROSION/CREEP RESISTANCE DUE TO FINAL HEAT TREATMENTS

Номер: US20150307976A1
Принадлежит: WESTINGHOUSE ELECTRIC COMPANY, LLC.

The invention relates to zirconium-based alloys and articles produced therefrom, such as tubing or strips, which have at least one of excellent corrosion resistance to water or steam and creep resistance at elevated temperatures in a nuclear reactor. The alloys include from about 0.2 to 1.5 weight percent niobium, from about 0.01 to 0.6 weight percent iron, from about 0.0 to 0.8 weight percent tin, from about 0.0 to 0.5 weight percent chromium, from about 0.0 to 0.3 weight percent copper, from about 0,0 to 0.3 weight percent vanadium, and from about 0.0 to 0.1 weight percent nickel with the balance at least 97 weight percent zirconium, including impurities. Further, the articles are formed by processes that include final heat treatment of (i) SRA or PRXA (0-33% RXA), or (ii) RXA or PRXA (80-100% RXA). 1. A zirconium-based alloy having one of improved corrosion resistance and improved creep resistance , for use in an elevated temperature environment of a nuclear reactor , comprising an alloying composition:0.2 to 1.5 weight percent niobium;0.01 to 0.6 weight percent iron;0.0 to 0.8 weight percent tin;0.0 to 0.5 weight percent chromium;0.0 to 0.3 weight percent copper;0.0 to 0.3 weight percent vanadium;0.0 to 0.1 weight percent nickel; anda balance at least 97 weight percent zirconium, including impurities, the zirconium-based alloy formed by a process, comprising:(a) melting the alloying composition to produce a melted alloy material;(b) forging the melted alloy material to produce a forged alloy material;(c) quenching the forged alloy material to produce a quenched alloy material;(d) extruding the quenched alloy material to produce a tube-shell alloy material;(e) pilgering the tube-shell alloy material to produce a reduced tube-shell alloy material;(f) annealing the reduced tube-shell alloy material to produce an annealed alloy material;(g) repeating steps (e) and (f) to produce a final alloy material; and(h) subjecting the final alloy material to a final heat ...

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20-10-2016 дата публикации

ZIRCONIUM ALLOY HAVING EXCELLENT CORROSION RESISTANCE FOR NUCLEAR FUEL CLADDING TUBE AND METHOD OF MANUFACTURING THE SAME

Номер: US20160307651A1
Принадлежит: KEPCO NUCLEAR FUEL CO., LTD.

A zirconium alloy is manufactured through melting; solution heat treatment at 1,000 to 1,050° C. (β) for 30 to 40 min and β-quenching using water; preheating at 630 to 650° C. for 20 to 30 min and hot rolling at a reduction ratio of 60 to 65%; primary intermediate vacuum annealing at 570 to 590° C. for 3 to 4 hr and primarily cold-rolled at a reduction ratio of 30 to 40%; secondary intermediate vacuum annealing at 560 to 580° C. for 2 to 3 hr and secondarily cold-rolled at a reduction ratio of 50 to 60%; tertiary intermediate vacuum annealing at 560 to 580° C. for 2 to 3 hr and tertiarily cold-rolled at a reduction ratio of 30 to 40%; and final vacuum annealing at 460 to 590° C. for 7 to 9 hr. 1. A zirconium alloy for a nuclear fuel cladding tube , comprising:0.5 to 1.2 wt % of Nb, 0.4 to 0.8 wt % of Mo, 0.1 to 0.15 wt % of Cu, 0.15 to 0.2 wt % of Fe, and a balance of zirconium.2. The zirconium alloy for a nuclear fuel cladding tube of claim 1 , 0.5 to 0.6 wt % of Nb claim 1 , 0.4 to 0.5 wt % of Mo.3. The zirconium alloy for a nuclear fuel cladding tube of claim 1 , 1.1 to 1.2 wt % of Nb claim 1 , 0.4 to 0.5 wt % of Mo.4. The zirconium alloy for a nuclear fuel cladding tube of claim 1 , 0.5 to 0.6 wt % of Nb claim 1 , 0.7 to 0.8 wt % of Mo.5. A method of manufacturing a zirconium alloy for a nuclear fuel cladding tube claim 1 , comprising steps of:(1) melting a mixture comprising 0.5 to 1.2 wt % of Nb, 0.4 to 0.8 wt % of Mo, 0.1 to 0.15 wt % of Cu, 0.15 to 0.2 wt % of Fe, and a balance of zirconium, thus preparing an ingot;(2) subjecting the ingot prepared in step (1) to solution heat treatment at 1,000 to 1,050° C. (β) for 30 to 40 min and then to β-quenching using water;(3) preheating the ingot treated in step (2) at 630 to 650° C. for 20 to 30 min and subjecting the ingot to hot rolling at a reduction ratio of 60 to 65%;(4) subjecting the material hot-rolled in step (3), to primary intermediate vacuum annealing at 570 to 590° C. for 3 to 4 hr and then to ...

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02-11-2017 дата публикации

METAL-CERAMIC COMPOSITE STRUCTURE AND FABRICATION METHOD THEREOF

Номер: US20170312817A1
Принадлежит:

The present disclosure provides a metal-ceramic composite structure and a fabrication method thereof. The metal-ceramic composite structure includes a ceramic substrate having a groove on a surface thereof; a metal member filled in the groove, including a main body made of zirconium base alloy, and a reinforcing material dispersed in the main body and selected from at least one of W, Mo, Ni, Cr, stainless steel, WC, TiC, SiC, ZrC, ZrO, BN, SiN, TiN and AlO; a luminance value L of the metal member surface is in a range of 36.92-44.07 under a LAB Chroma system. 1. A metal-ceramic composite structure , comprising:a ceramic substrate, having a groove on a surface of the ceramic substrate; anda metal member, filled in the groove and comprising:a main body, made of zirconium base alloy;{'sub': 2', '3', '4', '2', '3, 'a reinforcing material, dispersed in the main body, and selected from at least one of W, Mo, Ni, Cr, stainless steel, WC, TiC, SiC, ZrC, ZrO, BN, SiN, TiN and AlO,'}wherein a luminance value L of the metal member surface is in a range of 36.92-44.07 under a LAB Chroma system.2. The metal-ceramic composite structure according to claim 1 , wherein claim 1 , based on a total volume of the metal member claim 1 , a volume percentage of the reinforcing material is in a range of 5%-30%.3. The metal-ceramic composite structure according to claim 1 , wherein the reinforcing material has particle shape claim 1 , and a D50 particle size of the reinforcing material is in a range of 0.1 μm-100 μm.4. The metal-ceramic composite structure according to claim 1 , wherein the zirconium base alloy is a zirconium base amorphous alloy.5. The metal-ceramic composite structure according to claim 4 , wherein the ceramic substrate is a zirconia ceramic.6. The metal-ceramic composite structure according to claim 5 , wherein claim 5 , a thermal expansion coefficient of the reinforcing material is in a range of 3×10K−10×10K claim 5 , a thermal expansion coefficient of the zirconium base ...

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10-11-2016 дата публикации

ENTROPY-CONTROLLED BCC ALLOY HAVING STRONG RESISTANCE TO HIGH-TEMPERATURE NEUTRON RADIATION DAMAGE

Номер: US20160326616A1
Принадлежит:

Disclosed is an entropy-controlled solid solution matrix BCC alloy having strong resistance to high-temperature neutron radiation damage. The entropy-controlled solid solution matrix BCC alloy includes three or more multicomponent main elements selected from the element group consisting of Zr, Al, Nb, Mo, Cr, V, and Ti selected based on a neutron absorption cross-sectional area and a mixing enthalpy. Each of the elements is included in an amount of 5 to 35 at %, and the entropy-controlled solid solution matrix BCC alloy is a BCC-structure solid solution matrix alloy in a medium-entropy to high-entropy state. In this invention, damage caused by neutron radiation is reduced, and entropy is controlled to thus ensure a solid solution matrix BCC structure having a slow diffusion speed, and accordingly, resistance to void swelling due to radioactive rays is high. 1. An entropy-controlled solid solution matrix BCC alloy having strong resistance to high-temperature neutron radiation damage , comprising:three or more elements selected from the element group consisting of Zr, Al, Nb, Mo, Cr, V, and Ti, selected based on a neutron absorption cross-sectional area and a mixing enthalpy,wherein each of the elements is included in an amount of 5 to 35 at %, and the entropy-controlled solid solution matrix BCC alloy is a BCC-structure solid solution matrix alloy, which includes multicomponent main elements, in a medium-entropy to high-entropy state.2. The entropy-controlled solid solution matrix BCC alloy of claim 1 , wherein the entropy-controlled solid solution matrix BCC alloy includes one or more elements selected from Zr claim 1 , Al claim 1 , and Nb claim 1 , and one or more elements selected from Cr claim 1 , Ti claim 1 , Mo claim 1 , and V claim 1 , and a ratio of each of the elements is in a range of 5 to 35 at %.3. The entropy-controlled solid solution matrix BCC alloy of claim 1 , wherein the entropy-controlled solid solution matrix BCC alloy includes two or more ...

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17-11-2016 дата публикации

METHODS AND APPARATUSES FOR PRODUCING METALLIC POWDER MATERIAL

Номер: US20160332232A1
Принадлежит:

A method of producing a metallic powder material comprises supplying feed materials to a melting hearth, and melting the feed materials on the melting hearth with a first heat source to provide a molten material having a desired chemical composition. At least a portion of the molten material is passed from the melting hearth either directly or indirectly to an atomizing hearth, where it is heated using a second heat source. At least a portion of the molten material from the atomizing hearth is passed in a molten state to an atomizing apparatus, which forms a droplet spray from the molten material. At least a portion of the droplet spray is solidified to provide a metallic powder material. 1. A method of producing a metallic powder material , the method comprising:supplying feed materials to a melting hearth;melting the feed materials in the melting hearth with a heat source, thereby producing a molten material;passing at least a portion of the molten material from the melting hearth directly or indirectly to an atomizing hearth;heating the molten material in the atomizing hearth with a second heat source;passing at least a portion of the molten material from the atomizing hearth in a molten state to an atomizing nozzle; andforming a droplet spray of the molten material with the atomizing nozzle, whereafter at least a portion of the droplet spray is solidified to provide a metallic powder material.2. The method of claim 1 , where the at least a portion of the molten material passes from the melting hearth through at least one additional hearth prior to entering the atomizing hearth.3. The method of claim 1 , wherein the first heat source and the second heat source each independently comprises at least one of a plasma torch claim 1 , an electron beam generator claim 1 , a heating device generating electrons claim 1 , a laser claim 1 , an electric arc device claim 1 , and an induction coil.4. The method of claim 1 , wherein the molten material is at least one of ...

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26-11-2015 дата публикации

COMPOSITION FOR REACTIVE MATERIAL

Номер: US20150337414A1
Автор: Alven David A.
Принадлежит: Aerojet Rocketdyne, Inc.

A composition includes an alloy that has, by weight, 25-65% zirconium, 25-65% tungsten, and 6-25% of a combined amount of nickel in at least one of iron and cobalt. The alloy may be formed into a geometric body that has a density of 7.8 grams per cubic centimeter to 11.4 grams per cubic centimeter. 1. A composition of matter comprising: 25-65% zirconium;', '25-65% tungsten; and', '6-25% of a combined amount of nickel and at least one of iron and cobalt., 'an alloy including, by weight2. The composition as recited in claim 1 , wherein the alloy includes 5-20% nickel.3. The composition as recited in claim 1 , wherein the alloy includes 1-5% of at least one of iron and cobalt.4. The composition as recited in claim 1 , wherein the alloy includes iron and excludes cobalt.5. The composition as recited in claim 1 , wherein the alloy includes cobalt and excludes iron.6. The composition as recited in claim 1 , wherein the zirconium claim 1 , tungsten claim 1 , nickel claim 1 , and at least one of iron and cobalt are distributed throughout the alloy.7. The composition as recited in claim 1 , wherein the alloy consists of:25-65% zirconium;25-65% tungsten; and6-25% of a combined amount of nickel and at least one of iron and cobalt.8. The composition as recited in claim 1 , wherein the alloy consists essentially of:25-65% zirconium;25-65% tungsten; and6-25% of a combined amount of nickel and at least one of iron and cobalt.9. An article comprising:a geometric body formed of an alloy having a density of 7.8 grams per cubic centimeter to 11.4 grams per cubic centimeter, the density being selected with respect to a kinetic energy parameter of the geometric body, the alloy including zirconium, tungsten, nickel, and at least one of iron and cobalt.10. The article as recited in claim 9 , wherein the alloy claim 9 , by weight claim 9 , includes:25-65% zirconium;25-65% tungsten; and6-25% of a combined amount of nickel and at least one of iron and cobalt.11. The article as recited in ...

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24-11-2016 дата публикации

ZIRCONIUM-BASED AMORPHOUS ALLOY AND MANUFACTURING METHOD THEREOF

Номер: US20160340765A1
Принадлежит:

A Zr-based amorphous alloy has the following formula: ZrCuAlNiTiM. a, b, c, d, e, and f of the formula are corresponding atomic percents with 50≦a≦55, 25≦b≦30, 15≦c≦24, 0.1≦d≦9, 0.1≦e≦5, 0.1≦f≦5, and a+b+c+d+e+f≦100. M is selected from one or more of the following group consisting of Sc, Ce, Pr, Nd, Pm, Sm, Eu, Gd, Tb, Dy, Ho, Er, Tm, Yb, Lu, and mixtures thereof. 1. A Zr-based amorphous alloy having the following formula: ZrCuAlNiTiM , wherein the a , b , c , d , e , and f of the formula are corresponding atomic percents with 50≦a≦55 , 25≦b≦30 , 15≦c≦24 , 0.1≦d≦9 , 0.1≦e≦5 , 0.1≦f≦5 , and a+b+c+d+e+f≦100; M is selected from one or more of the following group consisting of Sc , Ce , Pr , Nd , Pm , Sm , Eu , Gd , Tb , Dy , Ho , Er , Tm , Yb , Lu , and mixtures thereof.2. The Zr-based amorphous alloy of claim 1 , wherein the Zr-based amorphous alloy has one of the following formulas: ZrCuAlNiTiSm claim 1 , ZrCuAlNiTiCe claim 1 , ZrCuAlNiTiHo claim 1 , ZrCuAlNiTiPrNd claim 1 , ZrCuAlNiTiPrNd claim 1 , ZrCuAlNiTiTb claim 1 , ZrCuAlNiTiEr claim 1 , ZrCuAlNiTiEu claim 1 , ZrCuAlNiTiSC claim 1 , ZrCuAlNiTiDy claim 1 , ZrCuAlNiTiPm claim 1 , ZrCuAlNiTiDy.3. The Zr-based amorphous alloy of claim 1 , wherein the Zr-based amorphous alloy has one of the following formulas: ZrCuAlNiTiEr claim 1 , ZrCuAlNiTiCe claim 1 , ZrCuAlNiTiPrNd claim 1 , ZrCuAlNiTiCe claim 1 , ZrCuAlNiTiEr claim 1 , ZrCuAlNiTiLu claim 1 , ZrCuAl1NiTiPrNd claim 1 , ZrCuAlNiTiSc.4. The Zr-based amorphous alloy of claim 1 , wherein the Zr-based amorphous alloy has one of the following formulas: ZrCuAlNiTiPrNd claim 1 , ZrCuAlNiTiEr claim 1 , ZrCuAlNiTiCe claim 1 , ZrCuAlNiTiPrNd claim 1 , ZrCuAlNiTiCe claim 1 , ZrCuAlNiTiYb claim 1 , ZrCuAlNiTiGd claim 1 , ZrCuAlNiTiSc claim 1 , ZrCuAlNiTiPrNd claim 1 , ZrCuAlNiTiTm.5. The Zr-based amorphous alloy of claim 1 , wherein the Zr-based amorphous alloy has a glass forming ability of 2.5 millimeters.6. A method for manufacturing a Zr-based amorphous alloy claim 1 , ...

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15-10-2020 дата публикации

ULTRASONIC ADDITIVE MANUFACTURING OF CLADDED AMORPHOUS METAL PRODUCTS

Номер: US20200324362A1
Принадлежит:

An embodiment relates to an ultrasonic additive manufacturing process, comprising joining a foil comprising a bulk metallic glass to a substrate; and forming a cladded composite comprising the foil and the substrate; wherein a thickness of the cladded composite is greater than a critical casting thickness of the bulk metallic glass, wherein the cladded composite comprises a cladding layer of the bulk metallic glass on the substrate and the bulk metallic glass comprises approximately 0% crystallinity, approximately 0% porosity, less than 50 MPa thermal stress, approximately 0% distortion, approximately 0 inch heat affected zone, approximately 0% dilution, and a strength of about 2,000-3,500 MPa. 1. An ultrasonic additive manufacturing process , comprising:joining a foil comprising a bulk metallic glass to a substrate; andforming a cladded composite comprising the foil and the substrate;wherein a thickness of the cladded composite is greater than a critical casting thickness of the bulk metallic glass.2. The ultrasonic additive manufacturing process of claim 1 , wherein the thickness of the cladded composite is greater than the critical casting thickness of the bulk metallic glass by a factor of at least 15.3. The ultrasonic additive manufacturing process of claim 1 , wherein the ultrasonic additive manufacturing process comprises an amplitude in range of 30 μm to 40 μm and a speed in range of 50 inch per minute to 150 inch per minute.4. The ultrasonic additive manufacturing process of claim 1 , wherein no interlayer is between the bulk metallic glass and the substrate.5. The ultrasonic additive manufacturing process of claim 1 , where an interlayer is between the bulk metallic glass and the substrate.6. The ultrasonic additive manufacturing process of claim 1 , wherein the bulk metallic glass and the substrate has an interface; wherein the interface is amorphous.7. The ultrasonic additive manufacturing process of claim 1 , wherein the bulk metallic glass and the ...

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10-12-2015 дата публикации

TREATMENT PROCESS FOR A ZIRCONIUM ALLOY, ZIRCONIUM ALLOY RESULTING FROM THIS PROCESS AND PARTS OF NUCLEAR REACTORS MADE OF THIS ALLOY

Номер: US20150354030A1
Принадлежит: AREVA NP

A treatment process for a zirconium alloy is provided. The process includes the following steps: 111-. (canceled)12. A treatment process for a zirconium alloy for use in a nuclear reactor , comprising: 0.40%≦Nb≦1.05%;', 'traces≦Sn≦2%;', '(0.5Nb−0.25)%≦Fe≦0.50%;', 'traces≦Ni≦0.10%;', 'traces≦(Cr+V)%≦0.50%;', 'traces≦S≦35 ppm;', '600 ppm≦O≦2000 ppm;', 'traces≦Si≦120 ppm;', 'traces≦C≦150 ppm; and', 'If 0.50%≦Nb≦1.05%, then (Cr+V)%≦(0.2+3/4Fe−1/4Nb)%; and', 'the remaining being Zr and unavoidable impurities;, 'preparing a zirconium alloy ingot, the zirconium alloy ingot having a composition of which is in weight % or weight ppmat least one step of reheating and hot shaping the zirconium alloy ingot;at least one cycle of cold rolling-annealing steps on the zirconium alloy ingot after the at least one step of reheating and hot shaping, a last annealing of the at least one cycle of cold rolling-annealing steps being a final annealing step which gives a product formed therefrom a final stress-relieved, partially recrystallized or completely recrystallized condition,the annealing of at least one of the cold rolling-annealing steps being performed at a temperature comprised between 600° C. and the lowest of either 700° C. or (710−20×Nb %)° C., and the annealings of the other cold rolling-annealing steps, if any, being performed at a temperature not higher than 600° C.13. The treatment process as recited in wherein the at least one step of reheating and hot shaping the zirconium alloy ingot includes a reheating and quenching step following a hot shaping step.14. The treatment process as recited in further comprising an annealing the ingot after the at least one step of reheating and hot shaping the zirconium alloy ingot.15. The treatment process as recited in wherein (0.02+1/3Fe)%≦(Cr+V)%.16. The treatment process as recited in wherein 0.50%≦Nb≦1.05% claim 12 , and (0.02+1/3Fe)%≦(Cr+V)%≦(0.2+3/4Fe−1/4Nb)%.17. The treatment process as recited in wherein the at least one cycle ...

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29-11-2018 дата публикации

Hypoeutectic Amorphous Metal-Based Materials for Additive Manufacturing

Номер: US20180339338A1
Принадлежит: California Institute of Technology

Systems and methods for developing tough hypoeutectic amorphous metal-based materials for additive manufacturing, and methods of additive manufacturing using such materials are provided. The methods use 3D printing of discrete thin layers during the assembly of bulk parts from metallic glass alloys with compositions selected to improve toughness at the expense of glass forming ability. The metallic glass alloy used in manufacturing of a bulk part is selected to have minimal glass forming ability for the per layer cooling rate afforded by the manufacturing process, and may be specially composed for high toughness. 1. A method of additive manufacturing a bulk amorphous metal part comprising:providing a metallic glass forming alloy based on a metallic glass-forming alloy system with two or more components where a eutectic exists between two of the components that results in a eutectic metallic glass forming alloy having a critical casting thickness, and wherein the amount of at least the most abundant component of the metallic glass-alloy system is increased at the expense of the sum of the other components such that the metallic glass forming alloy is hypoeutectic and has a critical casting thickness less than the eutectic metallic glass forming alloy;disposing molten layers of the hypoeutectic metallic glass forming alloy atop one another additively, and allowing said layers to cool to a bulk amorphous metal part having an amorphous fraction of at least 10% by volume, having an overall thickness of at least 1 mm; andwherein the most abundant component of the metallic glass forming alloy comprises at least 70% atomic the metallic glass forming alloy.2. The method of claim 1 , where the metallic glass forming alloy is heated to above its melting temperature and then cooled at an initial cooling rate faster than 1 claim 1 ,000 K/s such that each layer being disposed cools sufficiently rapidly so as to form at least a partially amorphous metal layer.3. The method of ...

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06-12-2018 дата публикации

High Toughness Metallic Glass-Based Composites for Additive Manufacturing

Номер: US20180345366A1
Автор: Hofmann Douglas C.
Принадлежит: California Institute of Technology

Methods and alloy systems for non-Be BMG matrix composite materials that can be used to additively manufacturing parts with superior mechanical properties, especially high toughness and strength, are provided. Alloys are directed to BMGMC materials comprising a high strength BMG matrix reinforced with properly scaled, soft, crystalline metal dendrite inclusions dispersed throughout the matrix in a sufficient concentration to resist fracture. 1. A method for forming a bulk metallic glass matrix composite utilizing powder-based additive manufacturing comprising:mixing a powder of a bulk metallic glass composition with a powder of at least one additional metallic composition wherein the at least one additional metallic composition forms a reinforcing crystalline ductile phase configured to inhibit crack propagation in a bulk metallic glass matrix formed from the bulk metallic glass composition, and wherein the volume fraction of the at least one metallic crystalline phase is from between 15-95% by volume of the bulk metallic glass matrix composite;melting the mixed powder of the bulk metallic glass composition and the at least one additional metallic composition using an additive manufacturing heating source such that the at least one additional metallic composition is partially melted such that a native oxide layer disposed within the bulk metallic glass matrix composition is dissolved; and{'sup': '1/2', 'solidifying the melt formed from the mixed powders in a layer by layer printing process to form the bulk metallic glass matrix composite having at least one property selected from the group of a porosity of equal to or less than 2% by volume, an overall strength of at least 50% of the strength of the bulk metallic glass composition when formed into a bulk part, a fracture toughness that is at least 5% larger than bulk metallic glass composition, a tension ductility that is at least 1% larger than the bulk metallic glass composition, and a notch toughness larger than ...

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15-12-2016 дата публикации

OXIDIZED-ZIRCONIUM-ALLOY ARTICLE AND METHOD THEREFOR

Номер: US20160362777A1
Принадлежит:

Described are articles having, at least, an outer surface comprising unalloyed oxidized Zirconium with Niobium having a thickness and configurations suitable for sports equipment, golf clubs, aircraft, boat hulls, motor vehicle, propellers, helicopter rotors, and various other non-medical applications. 1. A method of producing at least an outer surface for a golf club head , the method comprising:providing an article made from an alloy consisting of about between 70-98 with percent unalloyed Zirconium and about 2-30 weight percent Niobium;heating the article in an oxygen at atmosphere to a temperature of between about 200° Celsius and 880° Celsius, for a duration of between about 10 minutes to 110 minutes; andforming the article in the shape, size and thickness of the at least the outer surface of the golf club head.2. The method of claim 1 , where the at least the outer surface is a face portion of the golf club head.3. The method of claim 1 , wherein the at least the outer surface is between about 5μm and 10 μm thick.4. The method of claim 1 , wherein the at least the outer surface is between about 10 μm and two centimeters thick.5. A method of producing a surface or skin of an aircraft part claim 1 , the method comprising:providing an article made from an alloy consisting of about between 70-90 weight percent unalloyed Zirconium and about 10-30% weight percent Niobium;heating the article in an oxygen at atmosphere to a temperature of between about 200° Celsius and 880° Celsius, for a duration of between about 10 minutes to 110 minutes; andforming the article in the shape, size and thickness of the surface or skin of the aircraft part.6. The method of claim 5 , wherein the aircraft part is a propeller of an aircraft.7. The method of claim 5 , wherein the aircraft part is a helicopter rotor.8. A method of producing at least claim 5 , an outer surface of an article claim 5 , the method comprising:providing an article made from an alloy consisting of about between 70 ...

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29-10-2020 дата публикации

Ti-Zr Alloy Powder And Anode Containing The Same

Номер: US20200343052A1
Принадлежит: Global Advanced Metals USA, Inc.

A Ti—Zr alloy in powder form is described. Sintered pellets containing the Ti—Zr alloy powder of the present invention, as well as capacitor anodes, are further described. 1. A titanium-zirconium (Ti—Zr) alloy powder comprising an atomic ratio of Ti and Zr of from 10:90 to 90:10 , and having an average primary particle size of from 550 nm to 2 microns.2. The titanium-zirconium alloy powder of claim 1 , wherein said titanium-zirconium alloy powder further comprises a Ti—Zr oxide layer on said titanium-zirconium alloy powder.3. The titanium-zirconium alloy powder of claim 2 , wherein said Ti—Zr oxide layer further comprises phosphorus.4. The titanium-zirconium alloy powder of claim 2 , wherein said Ti—Zr oxide layer further comprises phosphorus at a level of from about 50 ppm to about 5 claim 2 ,000 ppm.5. The titanium-zirconium alloy powder of claim 2 , wherein said Ti—Zr oxide layer further comprises phosphorus at a level of from about 200 ppm to about 5 claim 2 ,000 ppm.6. The titanium-zirconium alloy powder of claim 1 , wherein said titanium-zirconium alloy powder further comprises a Ti—Zr oxide layer on said titanium-zirconium alloy powder and said Ti—Zr oxide layer has a thickness of from about 5 nm to about 20 nm.7. The titanium-zirconium alloy powder of claim 1 , wherein said titanium-zirconium alloy powder further comprises a Ti—Zr oxide layer that fully encapsulates said titanium-zirconium alloy powder.8. The titanium-zirconium alloy powder of claim 1 , wherein said titanium-zirconium alloy powder are particles consisting of a single phase homogeneous solid solution of Ti and Zr.9. The titanium-zirconium alloy powder of claim 1 , wherein said titanium-zirconium alloy has less than 50 ppm carbon.10. The titanium-zirconium alloy powder of claim 1 , wherein said titanium-zirconium alloy has less than 500 ppm of individual grains of titanium or zirconium or both.11. The titanium-zirconium alloy powder of claim 1 , wherein said titanium-zirconium alloy powder has ...

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22-12-2016 дата публикации

Ceramic pressure measuring cell and method for its manufacture

Номер: US20160370241A1
Автор: Berlinger Andrea
Принадлежит: Endress + Hauser GmbH + Co. KG

A method for manufacturing a pressure measuring cell, which has a ceramic platform and a ceramic measuring membrane, wherein the measuring membrane is joined with the platform pressure tightly by means of an active hard solder, or braze, wherein the method includes: providing the platform, the measuring membrane and the active hard solder, or braze, positioning the active hard solder, or braze, between the platform and the measuring membrane; melting the active hard solder, or braze, by irradiating the active hard solder, or braze, by means of a laser, wherein the irradiating of the active hard solder, or braze, occurs through the measuring membrane; and letting the active hard solder, or braze, solidify by cooling. 115-. (canceled)16. A method for manufacturing a pressure measuring cell , which has a ceramic platform and a ceramic measuring membrane , wherein the measuring membrane is joined with the platform pressure tightly by means of an active hard solder , or braze , the method comprising the steps of:providing the platform, the measuring membrane and the active hard solder, or braze;positioning the active hard solder, or braze, between the platform and the measuring membrane;melting the active hard solder, or braze, by irradiating the active hard solder, or braze, by means of a laser, wherein the irradiating of the active hard solder, or braze, occurs through the measuring membrane; andletting the active hard solder, or braze, solidify by cooling.17. The method as claimed in claim 16 , wherein:said melted of the active hard solder, or braze, is held at or above the liquidus temperature not more than 1 minute, especially not more than 30 seconds, preferably not more than 15 seconds.18. The method as claimed in claim 16 , wherein:said letting of the active hard solder, or braze, solidify by cooling occurs down to the solidus temperature with an average cooling rate of not less than 20 K/minute, especially not less than 40 K/minute, preferably not less than 1 K/ ...

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28-11-2019 дата публикации

NON-EVAPORABLE GETTER ALLOYS PARTICULARLY SUITABLE FOR HYDROGEN AND CARBON MONOXIDE SORPTION

Номер: US20190360076A1
Принадлежит: SAES GETTERS S.P.A.

Getter devices with improved sorption rate based on powders of ternary alloys particularly suitable for hydrogen and carbon monoxide sorption are described, said alloys having a composition comprising zirconium, vanadium and aluminum as main constituent elements. 115-. (canceled)16: Non-evaporable getter alloy consisting of:a. vanadium from 18 to 40% by atoms;b. aluminum from 5 to 25% by atoms;c. optionally one or more additional element selected from the group consisting of iron, chromium, manganese, cobalt, and nickel; andd. zirconium in the amount to balance the alloy to 100% by atoms,wherein, if present, said one or more additional element is in an amount comprised between 0.1 and 3% with respect to the alloy, said amount being lower than 10% of the aluminum atomic percentage content in the alloy.17: The non-evaporable getter alloy according to claim 16 , wherein zirconium and vanadium have a ratio Zr/V of their respective atomic amount comprised between 1 and 2.5.18: The non-evaporable getter alloy according to claim 16 , wherein claim 16 , if present claim 16 , said one or more additional element is in an amount comprised between 0.1 and 2% with respect to the alloy.19: Non-evaporable getter alloy consisting of:i) vanadium from 18 to 40% by atoms;ii) aluminum from 5 to 25% by atoms;iii) optionally one or more additional element selected from the group consisting of iron, chromium, manganese, cobalt, and nickel;iv) impurities in an amount lower than 1% by atoms with respect to the alloy,v) zirconium in the amount to balance the alloy to 100% by atoms; andwherein, if present, said one or more additional element is in an amount comprised between 0.1 and 3% with respect to the alloy, said amount being lower than 10% of the aluminum atomic percentage content in the alloy.20: The non-evaporable getter alloy according to claim 16 , which is in the form of a powder.21: A mixture claim 16 , comprising:{'claim-ref': {'@idref': 'CLM-00020', 'claim 20'}, 'the non- ...

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26-11-2020 дата публикации

DIAMOND BLADE AND METHOD OF MANUFACTURING THE SAME

Номер: US20200368856A1
Автор: Chu Jinn P., LAI Bo-Zhang

A diamond blade includes a base and a thin film metallic glass. The base includes a plurality of diamond particles, and the plurality of diamond particles protrude from a surface of the base. The thin film metallic glass is formed on the surface of the base, and the plurality of diamond particles are exposed on the thin film metallic glass. 1. A diamond blade , comprising:a base comprising a plurality of diamond particles, the plurality of diamond particles protruding from a surface of the base; anda thin film metallic glass formed on the surface of the base, wherein the plurality of diamond particles are exposed on the thin film metallic glass.2. The diamond blade of claim 1 , wherein the thin film metallic glass is a continuous thin film without a columnar structure.3. The diamond blade of claim 2 , wherein the thin film metallic glass is deposited on the surface of the base by a high-power impulse magnetron sputtering process.4. The diamond blade of claim 1 , wherein the thin film metallic glass comprises a zirconium-based metallic glass material.5. The diamond blade of claim 4 , wherein the zirconium-based metallic glass material comprises a ZrCuAlNialloy claim 4 , wherein a is 61.7±0.2 at % claim 4 , b is 24.6±0.1 at % claim 4 , c is 7.7±0.1 at % and d is 6.0±0.1 at % claim 4 , and wherein a+b+c+d=100.6. The diamond blade of claim 1 , wherein the base comprises an edge with a chamfer angle claim 1 , and the chamfer angle is 60±2 degrees.7. The diamond blade of claim 1 , wherein the plurality of diamond particles are fixed on the surface of the base by bonding.8. A method of manufacturing the diamond blade as recited in claim 1 , comprising:providing a base comprising a plurality of diamond particles, the plurality of diamond particles protruding from a surface of the base;performing a first dressing of the base;depositing a thin film metallic glass on the surface of the base; andperforming a second dressing of the base to remove a redundant part of the thin ...

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19-12-2019 дата публикации

METHODS AND APPARATUSES FOR PRODUCING METALLIC POWDER MATERIAL

Номер: US20190381571A1
Принадлежит:

A method of producing a metallic powder material comprises supplying feed materials to a melting hearth, and melting the feed materials on the melting hearth with a first heat source to provide a molten material having a desired chemical composition. At least a portion of the molten material is passed from the melting hearth either directly or indirectly to an atomizing hearth, where it is heated using a second heat source. At least a portion of the molten material from the atomizing hearth is passed in a molten state to an atomizing apparatus, which forms a droplet spray from the molten material. At least a portion of the droplet spray is solidified to provide a metallic powder material. 144.-. (canceled)45. A method for producing a titanium alloy powder , the method comprising:supplying feed materials to a water-cooled copper melting hearth;melting the feed materials in the water-cooled copper melting hearth with a first plasma torch, thereby producing a molten titanium alloy material in the water-cooled copper melting hearth;passing at least a portion of the molten titanium alloy material from the water-cooled copper melting hearth to a water-cooled copper atomizing hearth;heating the molten titanium alloy material in the water-cooled copper atomizing hearth with a second plasma torch; a passage in direct fluid communication with the water-cooled copper atomizing hearth and the gas-atomizing nozzle, the passage comprising a water-cooled wall containing molten titanium alloy material received from the water-cooled copper atomizing hearth; and', 'an induction coil that selectively heats at least a portion of the molten titanium alloy material contained in the passage and controls solidification and flow of the molten titanium alloy material in the passage;, 'passing at least a portion of the molten titanium alloy material directly from the water-cooled copper atomizing hearth through a cold induction guide to a gas-atomizing nozzle, wherein the cold induction guide ...

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16-11-2000 дата публикации

Nb-Ti-Zr-Mo ALLOYS FOR MEDICAL AND DENTAL DEVICES

Номер: WO2000068448A1
Принадлежит: Davitech, Inc.

The present invention is a medical implant or device (2) fabricated, in any manner, from a niobium (Nb) - titanium(Ti) - zirconium(Zr) - Molybednum(Mo) alloy (NbTiZrMo alloy). The implant or device has components at least partially fabricated from a metal alloy comprising a) between about 29 and 70 weight percent Nb; b) between about 10 and 46 weight percent Zr; c) between about 3 and 15 percent Mo; and a balance of titanium. The inventive alloy provides for a uniform beta structure which is corrosion resistant, and can be readily processed to develop high-strength and low-modulus, with the ability for conversion oxidation or nitridization surface hardening of the medical implant or device.

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17-11-2005 дата публикации

Sputter targets and methods of forming same by rotary axial forging

Номер: WO2005108639A1
Принадлежит: CABOT CORPORATION

A method of making sputter targets using rotary axial forging is described. Other thermomechanical working steps can be used prior to and/or after the forging step. Sputter targets are further described which can have unique grain size and/or crystal structures.

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24-12-2001 дата публикации

The hypo-stoichiometric Zr-Ni based hydrogen storage alloy for anode material of Ni/MH secondary battery

Номер: KR100317556B1
Принадлежит: 윤덕용, 한국과학기술원

본 발명은 Ni-MH 2차전지용 고용량, 고성능 수소저장합금에 관한 것으로서 본 발명의 Zr계 수소저장합금은 하기 일반식 (Ⅰ)로 표시된다. The present invention relates to a high capacity, high performance hydrogen storage alloy for Ni-MH secondary batteries, wherein the Zr-based hydrogen storage alloy of the present invention is represented by the following general formula (I). Zr 1-X Ti X (Mn U V V Cr Y Ni 1-U-V-Y ) Z ( I ) Zr 1-X Ti X (Mn U V V Cr Y Ni 1-UVY ) Z (I) 상기식에서, In the above formula, 아래 첨자 X, U, V, Y 및 Z는 각각 합금 조성 원소들의 원자분율로서 Subscripts X, U, V, Y and Z are the atomic fractions 0 < X ≤ 0.4, 0.3 ≤ U ≤ 0.4, 0.1 ≤ V ≤ 0.2, 0.0 ≤ Y ≤ 0.2, 0.45 ≤ U+V+Y ≤ 0.65, 1.6 ≤ Z ≤ 1.9 을 만족하는 값이다. 0 <X ≦ 0.4, 0.3 ≦ U ≦ 0.4, 0.1 ≦ V ≦ 0.2, 0.0 ≦ Y ≦ 0.2, 0.45 ≦ U + V + Y ≦ 0.65, and 1.6 ≦ Z ≦ 1.9. 상기 본 발명의 Zr계 수소저장합금은 기존의 상용화되고 있는 Co 원소를 포함한 수소저장합금(Mn-Ni계)을 대체할 수 있으며, 또한 기존의 Ni/MH 2차전지의 성능 및 에너지밀도를 향상시킴으로써 전기자동차의 개발에 필요한 고용량, 고성능의 2차전지 제조를 가능하게 한다. The Zr-based hydrogen storage alloy of the present invention can replace a conventional hydrogen storage alloy (Mn-Ni-based) containing Co commercially available, and also improve the performance and energy density of the existing Ni / MH secondary battery. By doing so, it is possible to manufacture high capacity, high performance secondary batteries required for the development of electric vehicles.

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28-07-2015 дата публикации

Polycrystalline alloy having glass forming ability, method of fabricating the same, alloy target for sputtering and method of fabricating the same

Номер: KR101539647B1
Принадлежит: 한국생산기술연구원

본 발명은 비정질 형성능을 가지면서도 열적 안정성이 비정질에 비해 현저하게 우수한 비정질 형성능을 가지는 결정질 합금 및 그 제조방법의 제공을 목적으로 한다. 또한 본 발명은 상기 결정질 합금을 이용하여 제조한 스퍼터링용 합금타겟 및 그 제조방법의 제공을 또 다른 목적으로 한다. 본 발명의 일 관점에 의하면, 비정질 형성능을 가지는, 네 금속원소 이상으로 이루어진 합금으로서, 상기 합금의 결정립 평균크기는 0.1㎛ 내지 5㎛ 범위에 있고, 상기 합금은 Al이 5원자% 내지 20원자%; Cu 및 Ni 중에서 선택된 어느 하나 이상이 15원자% 내지 40원자%; Cr, Mo, Si, Nb, Co, Sn, In, Bi, Zn, V, Hf, Ag, Ti 및 Fe 중에서 선택되는 어느 하나 이상의 합이 8원자% 이하(0초과); P 및 S 중에서 선택된 적어도 하나 이상; 및 잔부가 Zr;으로 이루어진, 비정질 형성능을 가지는 결정질 합금이 제공된다. An object of the present invention is to provide a crystalline alloy having an amorphous forming ability and a thermal stability that is remarkably superior to that of amorphous, and a method for producing the same. Another object of the present invention is to provide an alloy target for sputtering manufactured using the crystalline alloy and a method of manufacturing the same. According to one aspect of the present invention, there is provided an amorphous alloy having an amorphous forming ability, the average grain size of the alloy being in a range of 0.1 탆 to 5 탆, wherein the alloy contains 5 atom% to 20 atom% ; 15 atom% to 40 atom% of at least one selected from Cu and Ni; At least one selected from the group consisting of Cr, Mo, Si, Nb, Co, Sn, In, Bi, Zn, V, Hf, Ag, Ti and Fe is not more than 8 atomic% P and S; And the remainder being Zr, is provided.

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10-05-2010 дата публикации

Non evaporating gas absorbing alloys for hydrogen trapping

Номер: RU2388839C2
Принадлежит: Саес Геттерс С.П.А.

FIELD: metallurgy. ^ SUBSTANCE: invention refers to non evaporating gas absorbing alloys actuated at relatively low temperatures and capable to trap hydrogen. The invention can be implemented at fabrication of thermal flasks, solar collectors, lamps of discharge voltage, and generating X-ray tubes. The alloy has the following composition, wt %: Zr 50-80, Y 10-20, M 5-40, where M is chosen from Al, Fe, Cr, Mn, V or mixtures of these elements. The region of alloy contents is limited with polygon determined with points on triple diagram, wt %: a) Zr 50 % - Y 10 % - M 40 %; b) Zr 50 % - Y 20 % - M 30 %; c) Zr 75 % - Y 20 % - M 5 %; d) Zr 80 % - Y 15 % - M 5 %; e) Zr 80 % - Y 10 % - M 10 %. ^ EFFECT: improved characteristics of equilibrium pressure of hydrogen and temperature of activation relative to known materials. ^ 12 cl, 7 dwg, 1 tbl, 6 ex РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) 2 388 839 (13) C2 (51) МПК C22C 16/00 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ, ПАТЕНТАМ И ТОВАРНЫМ ЗНАКАМ (12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ (21), (22) Заявка: 2007123562/02, 18.11.2005 (24) Дата начала отсчета срока действия патента: 18.11.2005 (43) Дата публикации заявки: 27.12.2008 (56) Список документов, цитированных в отчете о поиске: WO 01/92590 A1, 06.12.2001. WO 2004/024965 A2, 25.03.2004. JP 01-140094 A, 01.06.1989. RU 2118231 C1, 27.08.1998. 2 3 8 8 8 3 9 R U (86) Заявка PCT: IT 2005/000673 (18.11.2005) C 2 C 2 (85) Дата перевода заявки PCT на национальную фазу: 25.06.2007 (87) Публикация PCT: WO 2006/057020 (01.06.2006) Адрес для переписки: 129090, Москва, ул. Б.Спасская, 25, стр.3, ООО "Юридическая фирма Городисский и Партнеры", пат.пов. А.В.Мицу (54) НЕИСПАРЯЮЩИЕСЯ ГАЗОПОГЛОТИТЕЛЬНЫЕ СПЛАВЫ ДЛЯ СОРБЦИИ ВОДОРОДА (57) Реферат: Изобретение относится к неиспаряющимся газопоглотительным сплавам, активируемым при относительно низких температурах и способным эффективно сорбировать водород, и может быть использовано при изготовлении термических колб, солнечных ...

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23-10-2014 дата публикации

비정질 형성능을 가지는 결정질 합금, 그 제조방법, 스퍼터링용 합금타겟 및 그 제조방법

Номер: KR101452879B1
Принадлежит: 한국생산기술연구원

본 발명은 비정질 형성능을 가지면서도 열적 안정성이 비정질에 비해 현저하게 우수한 비정질 형성능을 가지는 결정질 합금 및 그 제조방법의 제공을 목적으로 한다. 또한 본 발명은 상기 결정질 합금을 이용하여 제조한 스퍼터링용 합금타겟 및 그 제조방법의 제공을 또 다른 목적으로 한다. 본 발명의 일 관점에 의하면, 비정질 형성능을 가지는 3원소 이상으로 이루어진 합금으로서 상기 합금의 결정립 평균크기는 0.1 내지 5㎛ 범위에 있고, 상기 합금은 Al이 5 내지 20원자%, Cu 및 Ni 중에서 선택된 어느 하나 이상이 15 내지 40원자%, 잔부가 Zr으로 이루어진, 비정질 형성능을 가지는 결정질 합금이 제공된다.

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14-11-2017 дата публикации

一种用于贮存氚的ab型储氢合金及其制备方法

Номер: CN105568110B
Принадлежит: Institute of Materials of CAEP

本发明提供了一种用于贮存氚的AB型储氢合金及其制备方法,涉及储氢合金技术领域。该用于贮存氚的AB型储氢合金,其组分通式为Zr 1‑ x Ti x Co 1‑y Fe y ,其中0.1≤x≤0.4,0.1≤y≤0.2。本发明提供的储氢合金具有良好的抗氢致歧化性能,优异的吸放氢动力学性能及室温氢化物平衡压力,其制备方法简单易行,易于实现,制备效率高,实用性高。

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23-10-2018 дата публикации

Неиспаряемые геттерные сплавы, особенно подходящие для сорбции водорода и монооксида углерода

Номер: RU2670511C2
Принадлежит: Саес Геттерс С.П.А.

Группа изобретений относится к геттерному устройству для сорбции водорода и монооксида углерода. Геттерное устройство содержит композицию порошков неиспаряемого геттерного сплава, которая содержит цирконий, ванадий, титан и алюминий. Указанный неиспаряемый геттерный сплав необязательно содержит по меньшей мере один дополнительный химический элемент в суммарном количестве менее 8 ат.% от общей композиции неиспаряемого геттерного сплава, являющейся суммой циркония, ванадия, титана, алюминия и указанных необязательно присутствующих дополнительных элементов, сбалансированных до 100 ат.%. В качестве дополнительных химических элементов указанный неиспаряемый геттерный сплав содержит по меньшей мере один металл, выбранный из группы, состоящей из железа, хрома, марганца, кобальта и никеля, в количестве от 0,1 до 7 ат.% от упомянутой общей композиции неиспаряемого геттерного сплава и необязательно содержит незначительные количества других химических элементов в количестве менее 1% относительно упомянутой общей композиции сплава. 3 н. и 12 з.п. ф-лы, 2 табл., 10 ил. РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 2 670 511 C2 (51) МПК C22C 16/00 (2006.01) C22C 1/04 (2006.01) C22C 30/00 (2006.01) H01J 7/18 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ (52) СПК C22C 1/0458 (2006.01); C22C 16/00 (2006.01); C22C 30/00 (2006.01); H01J 61/26 (2006.01); H01J 7/183 (2006.01); B01D 2253/1122 (2006.01); B01D 2257/108 (2006.01); B01D 53/04 (2006.01) (21)(22) Заявка: 2016120582, 19.11.2014 19.11.2014 Дата регистрации: 23.10.2018 (56) Список документов, цитированных в отчете о поиске: US 4839085 A1, 13.06.1989. WO 20.11.2013 IT MI2013A001921 (43) Дата публикации заявки: 30.11.2017 Бюл. № 34 (45) Опубликовано: 23.10.2018 Бюл. № 30 2004024965 A2, 25.03.2004. EP 719609 A3, 03.07.1996. US 4360445 A1, 23.11.1982. RU 2253695 C2, 10.06.2005. RU 2260069 C2, 10.09.2005. RU 2388839 C2, 10.05.2010. C 2 C 2 (85) Дата начала рассмотрения заявки PCT на ...

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23-02-2011 дата публикации

合金、大块金属玻璃以及形成合金、大块金属玻璃的方法

Номер: CN101297053B
Принадлежит: NATIONAL UNIVERSITY OF SINGAPORE

具有通式(Zr,Ti) 100-X-U (Cu 100-a Ni a ) X Al U 的合金,其中X、U和a是下列范围的原子百分数:37≤X≤48,3≤U≤14,以及3≤a≤30。

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10-09-2005 дата публикации

Nonvaporizing getter alloys

Номер: RU2260069C2
Принадлежит: Саес Геттерс С.П.А.

FIELD: metallurgy; getter devices made from getter alloys. SUBSTANCE: proposed nonvaporizing getter alloy has high sorption capacity of gases, especially nitrogen containing zirconium, vanadium and iron; it also additionally contains manganese and at least one element selected from yttrium, lanthanum, lanthanides and any mixture of them at the following ratio of components, mass-%: zirconium, from 60 to 85; vanadium, from 2 to 20; iron, from 0.5 to 10; manganese, from 2.5 to 30; yttrium, lanthanum, lanthanides or their mixture, from 1 to 6. Device contains powder getter material of nonvaporizing getter alloy. EFFECT: enhanced sorption of gases, especially nitrogen. 15 cl, 11 dwg, 18 ex ÐÎÑÑÈÉÑÊÀß ÔÅÄÅÐÀÖÈß (19) RU (51) ÌÏÊ 7 (11) 2 260 069 (13) C2 C 22 C 16/00, H 01 J 7/18, 41/16 ÔÅÄÅÐÀËÜÍÀß ÑËÓÆÁÀ ÏÎ ÈÍÒÅËËÅÊÒÓÀËÜÍÎÉ ÑÎÁÑÒÂÅÍÍÎÑÒÈ, ÏÀÒÅÍÒÀÌ È ÒÎÂÀÐÍÛÌ ÇÍÀÊÀÌ (12) ÎÏÈÑÀÍÈÅ ÈÇÎÁÐÅÒÅÍÈß Ê ÏÀÒÅÍÒÓ (21), (22) Çà âêà: 2002105025/02, 28.05.2001 (72) Àâòîð(û): ÒÎÈß Ëóêà (IT), ÁÎÔÔÈÒÎ Êëàóäèî (IT) (24) Äàòà íà÷àëà äåéñòâè ïàòåíòà: 28.05.2001 (30) Ïðèîðèòåò: 30.05.2000 IT MI2000A001200 (73) Ïàòåíòîîáëàäàòåëü(ëè): ÑÀÅÑ ÃÅÒÒÅÐÑ Ñ.Ï.À. (IT) R U (43) Äàòà ïóáëèêàöèè çà âêè: 20.08.2003 (45) Îïóáëèêîâàíî: 10.09.2005 Áþë. ¹ 25 2 2 6 0 0 6 9 (56) Ñïèñîê äîêóìåíòîâ, öèòèðîâàííûõ â îò÷åòå î ïîèñêå: US 4312669 À, 26.01.1982. RU 2122518 C1, 27.11.1998. RU 2118231 Ñ1, 27.08.1998. US 5961750 A, 05.10.1999. US 4668424 A, 26.05.1987. (85) Äàòà ïåðåâîäà çà âêè PCT íà íàöèîíàëüíóþ ôàçó: 28.02.2002 2 2 6 0 0 6 9 R U (87) Ïóáëèêàöè PCT: WO 01/92590 (06.12.2001) C 2 C 2 (86) Çà âêà PCT: IT 01/00269 (28.05.2001) Àäðåñ äë ïåðåïèñêè: 129010, Ìîñêâà, óë. Á. Ñïàññêà , 25, ñòð.3, ÎÎÎ "Þðèäè÷åñêà ôèðìà Ãîðîäèññêèé è Ïàðòíåðû", ïàò.ïîâ. Þ.Ä.Êóçíåöîâó, ðåã.¹ 595 (54) ÍÅÈÑÏÀÐßÅÌÛÅ ÃÅÒÒÅÐÍÛÅ ÑÏËÀÂÛ (57) Ðåôåðàò: Èçîáðåòåíèå îòíîñèòñ ê îáëàñòè ìåòàëëóðãèè, à èìåííî ê ãåòòåðíûì óñòðîéñòâàì, èçãîòîâëåííûì èç ãåòòåðíûõ ñïëàâîâ. Ïðåäëîæåí íåèñïàð åìûé ãåòòåðíûé ñïëàâ è ãåòòåðíîå óñòðîéñòâî. Ñïëàâ èìååò âûñîêóþ ...

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20-04-2007 дата публикации

Process for the manufacture of zirconium?alloy cladding tube having excellent corrosion resistance for a nuclear fuel rod

Номер: KR100709389B1
Принадлежит: 학교법인 한양학원

본 발명은 핵반응기의 핵연료봉에 사용되는 지르코늄 합금재의 피복관(Nuclear Fuel Cladding)에 관한 것이다. 이 피복관은 핵연료를 수용하기 위한 신장된 중공의 금속성 관으로, 상기 금속성관은 지르코늄 합금재이며, 상기 관의 외측면에는 두께 0.5~3.7㎛의 지르코늄 산화피막이 형성된 것이다. 이 피복관의 제조방법 역시 제공된다. 피복관의 외측면에 고온에서 형성된 보호성 산화피막에 의해 내부식성이 개선된다. The present invention relates to a nuclear fuel cladding of a zirconium alloy material used for nuclear fuel rods of a nuclear reactor. The cladding tube is an elongated hollow metallic tube for accommodating nuclear fuel. The metallic tube is a zirconium alloy material, and a zirconium oxide film having a thickness of 0.5 to 3.7 μm is formed on the outer surface of the tube. A method for producing this cladding tube is also provided. Corrosion resistance is improved by a protective oxide film formed at a high temperature on the outer surface of the cladding tube. 핵연료봉, 피복관, 지르코늄 합금, 지르코늄 산화피막, 내부식성 Fuel rods, cladding, zirconium alloy, zirconium oxide, corrosion resistance

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20-03-2000 дата публикации

Nonvaporizing getter alloy and device containing such alloy

Номер: RU2146722C1
Принадлежит: Саес Геттерс С.П.А.

FIELD: nonvaporizing getter alloys. SUBSTANCE: nonvaporizing getter alloy contains zirconium, cobalt and one or several components A selected from group including yttrium, lanthanum or rare-earth metal. In this case content of alloy components expressed in weight per cent is comprised in polygon on triple alloy diagram governed by points: (a) Zr 81 - Co 9 - A 10; (b) Zr 68 - Co 22 - A 10; (c) Zr 74 - Co - 24 - A 2; (d) Zr 88 - Co 10 - A 2. Alloy possesses properties of sorption of various gases having comparatively low activation temperature and applicable in production of heat-insulating vessels such as thermoses, Dewar flasks, or pipeline for transportation of oil, cleaners of inert gases or lamps. EFFECT: production of nonvaporizing getter alloys widely used and safe for environment. 16 cl, 10 dwg, 1 tbl, 8 ex ССЛДЭ9УсС ПЧ ГЭ (19) РОССИЙСКОЕ АГЕНТСТВО ПО ПАТЕНТАМ И ТОВАРНЫМ ЗНАКАМ ВИ” 2 146 722 ' (51) МПК? 13) СЛ С 22 С 16/00, Е 17 С 3/08 12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ РОССИЙСКОЙ ФЕДЕРАЦИИ (21), (22) Заявка: 98105967/02, 02.04.1998 (24) Дата начала действия патента: 02.04.1998 (30) Приоритет: 03.04.1997 1Т М!97АОО0769 (46) Дата публикации: 20.03.2000 (56) Ссылки: КУ 94045979 АЛ, 10.08.1996. ЦЗ 4973369 А, 27.11.1990. ЕР 0382475 АЗ, 16.08.1990. ЕР 0653796 АЛ, 17.05.1995. Дегмет{ рибЙсаНоп: оп4оп, опй!пе МР! оп ОЧЕЗТЕЕ. АМ 76-69461Х, меек З7, 51086284. Дегмепт{ рибЙсаНоп: оп4оп, оп!пе МР! оп ОЧЕЗТЕЕ. АМ 95-232456, меек 31, ОЕ 4342941. Дегмет{ рибЙсаНоп: оп4оп, оп!пе РИ оп ОЧЕЗТЕЕ. АМ 87-162952, меек 23, ($ 4668424. (98) Адрес для переписки: 129010, Москва, ул.Б.Спасская, 25, стр.3, ООО "Городисский и партнеры" (71) Заявитель: Саес Геттерс С.п.А. (1Т) (72) Изобретатель: Клаудио Боффито (1!Т), Алессио Корацца (1Т), Стефано Томинетги (1Т) (73) Патентообладатель: Саес Гетгерс С.п.А. (1Т) (54) НЕИСПАРЯЮЩИЙСЯ ГАЗОПОГЛОТИТЕЛЬНЫЙ СПЛАВ И УСТРОЙСТВО, СОДЕРЖАЩЕЕ ТАКОЙ СПЛАВ (57) Реферат: Неиспаряющийся газопоглотительный сплав содержит цирконий, кобальт и один или ...

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18-09-2019 дата публикации

Non-evaporable getter alloys particularly suitable for hydrogen and carbon monoxide sorption

Номер: KR102022755B1
Принадлежит: 사에스 게터스 에스.페.아.

수소 및 일산화탄소 수착에 특히 적합한, 4원 합금의 분말을 기재로 하는 개선된 수착 속도를 갖는 게터 장치이며, 상기 합금은 주요 구성 원소로서 지르코늄, 바나듐, 티타늄 및 알루미늄을 포함하는 조성을 갖는 것인 게터 장치가 기재되어 있다. A getter device having an improved sorption rate based on powders of quaternary alloys, which is particularly suitable for hydrogen and carbon monoxide sorption, the alloy having a composition comprising zirconium, vanadium, titanium and aluminum as main constituents. Is described.

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11-09-2015 дата публикации

Polycrystalline alloy having glass forming ability, method of fabricating the same, alloy target for sputtering and method of fabricating the same

Номер: KR101552242B1
Принадлежит: 한국생산기술연구원

본 발명은 비정질 형성능을 가지면서도 열적 안정성이 비정질에 비해 현저하게 우수한 비정질 형성능을 가지는 결정질 합금 및 그 제조방법의 제공을 목적으로 한다. 또한 본 발명은 상기 결정질 합금을 이용하여 제조한 스퍼터링용 합금타겟 및 그 제조방법의 제공을 또 다른 목적으로 한다. 본 발명의 일 관점에 의하면, 비정질 형성능을 가지는 3원소 이상으로 이루어진 합금으로서 상기 합금의 결정립 평균크기는 0.1㎛ 내지 5㎛ 범위에 있고, 상기 합금은 Al이 5원자% 내지 20원자%, Cu 및 Ni 중에서 선택된 어느 하나 이상이 15원자% 내지 40원자%, P 및 S 중에서 선택된 적어도 하나 이상, 및 잔부가 Zr으로 이루어진, 비정질 형성능을 가지는 결정질 합금이 제공된다. An object of the present invention is to provide a crystalline alloy having an amorphous forming ability and a thermal stability that is remarkably superior to that of amorphous, and a method for producing the same. Another object of the present invention is to provide an alloy target for sputtering manufactured using the crystalline alloy and a method of manufacturing the same. According to one aspect of the present invention, the average grain size of the alloy is in the range of 0.1 탆 to 5 탆, and the alloy contains Al at 5 atom% to 20 atom%, Cu and And Ni is 15 atomic% to 40 atomic%, at least one selected from P and S, and the remainder is Zr.

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23-09-2019 дата публикации

Method for production of ingots out of zirconium alloys based on magnesium-thermal sponge

Номер: RU2700892C2

FIELD: metallurgy. SUBSTANCE: invention relates to production of ingots from zirconium alloys based on zirconium magnesium-thermal sponge containing alloying elements. Method involves obtaining ligatures tablets, forming consumable electrodes and casting ingots. Ligature tablets are obtained by mixing and pressing alloying components in pure form, or in form of their compounds, or with addition of electrolytic zirconium powder or zirconium magnesium-thermal sponge. Method comprises pressing briquettes from a mixture containing zirconium-containing materials in the form of zirconium magnesium-thermal sponge, ground zirconium iodide and/or zirconium production, and obtained ligature tablets are uniformly distributed in charge by mechanical mixing. Formation of consumable electrodes is carried out by welding briquettes between each other. EFFECT: high chemical homogeneity of ingots from zirconium alloys based on magnesium-thermal sponge. 5 cl, 2 tbl РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 2 700 892 C2 (51) МПК C22B 9/20 (2006.01) C22C 16/00 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ (52) СПК C22B 9/20 (2018.08); C22C 16/00 (2018.08); B22F 3/02 (2018.08) (21)(22) Заявка: 2018105420, 13.02.2018 (24) Дата начала отсчета срока действия патента: Дата регистрации: 23.09.2019 (43) Дата публикации заявки: 13.08.2019 Бюл. № 23 (45) Опубликовано: 23.09.2019 Бюл. № 27 2 7 0 0 8 9 2 R U (56) Список документов, цитированных в отчете о поиске: JP 61030637 A, 12.02.1986. JP 58161735 A, 26.09.1983. US 4164420 A1, 14.08.1979. RU 2313591 C2, 27.12.2007. RU 2365464 C2, 27.08.2009. (54) СПОСОБ ПОЛУЧЕНИЯ СЛИТКОВ ИЗ СПЛАВОВ ЦИРКОНИЯ НА ОСНОВЕ МАГНИЕТЕРМИЧЕСКОЙ ГУБКИ (57) Реферат: Изобретение относится к получению слитков содержащей цирконийсодержащие материалы в из сплавов циркония на основе циркониевой виде циркониевой магниетермической губки, магниетермической губки, содержащих измельченного йодидного циркония и/или легирующие ...

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04-02-2009 дата публикации

Sputtering target and method for production thereof

Номер: CN100457963C
Принадлежит: Nippon Mining and Metals Co Ltd

本发明涉及一种具有平均结晶尺寸为1nm~50nm的组织的烧结体溅射靶,特别是由3元系以上的合金组成,以从Zr、Pd、Cu、Co、Fe、Ti、Mg、Sr、Y、Nb、Mo、Tc、Ru、Rh、Ag、Cd、In、Sn、Sb、Te、稀土类金属中选择的至少一种元素作为主要成分的烧结体溅射靶。通过烧结喷雾粉制造该靶。能够代替结晶组织粗糙,且通过成本高的把溶融金属粹火得到的块状金属玻璃,提供具有通过烧结法得到的高密度的极其微细且均匀的组织的靶。

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13-08-2019 дата публикации

METHOD FOR PRODUCING INGOTS FROM ZIRCONIUM ALLOYS BASED ON MAGNETIC THERMAL SPONGE

Номер: RU2018105420A

РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 2018 105 420 A (51) МПК C22B 9/20 (2006.01) C22C 16/00 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ЗАЯВКА НА ИЗОБРЕТЕНИЕ (21)(22) Заявка: 2018105420, 13.02.2018 (71) Заявитель(и): Акционерное общество "Чепецкий механический завод" (RU) Приоритет(ы): (22) Дата подачи заявки: 13.02.2018 (43) Дата публикации заявки: 13.08.2019 Бюл. № 23 где mл.к. - масса легирующих компонентов на один брикет, кг; mт - масса таблетки лигатуры, размеры которой сравнимы со средней фракцией губки, кг; Стр.: 1 A 2 0 1 8 1 0 5 4 2 0 R U A (57) Формула изобретения 1. Способ получения слитков из сплавов циркония на основе магние-термической губки, содержащих тугоплавкие и/или легкоплавкие легирующие элементы, включающий получение таблеток лигатуры, прессование брикетов из шихты на основе цирконийсодержащих материалов, формирование расходуемых электродов и выплавку слитка, отличающийся тем, что перед прессованием брикетов полученные таблетки лигатуры равномерно распределяют в шихте путем механического перемешивания, а формирование расходуемого электрода осуществляют путем сварки брикетов между собой. 2. Способ по п. 1, отличающийся тем, что в качестве легирующих компонентов используют легирующие элементы в чистом виде или в виде их соединений. 3. Способ по п. 1, отличающийся тем, что таблетки лигатуры получают смешиванием и прессованием легирующих компонентов в чистом виде или в виде соединений отдельно или с добавлением по результатам расчета электролитического порошка циркония или губки циркония фракцией не более 2 мм. 4. Способ по п. 1, отличающийся тем, что необходимое количество таблеток лигатуры на один брикет рассчитывают по формулам: 2 0 1 8 1 0 5 4 2 0 (54) СПОСОБ ПОЛУЧЕНИЯ СЛИТКОВ ИЗ СПЛАВОВ ЦИРКОНИЯ НА ОСНОВЕ МАГНИЕТЕРМИЧЕСКОЙ ГУБКИ R U Адрес для переписки: 427622, Удмуртская Респ., г. Глазов, ул. Белова, 7, АО ЧМЗ, Технологическая служба (72) Автор(ы): Александров Александр Владимирович (RU), Аржакова Валентина ...

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20-11-1999 дата публикации

Zirconium-base alloy

Номер: RU2141539C1

FIELD: zirconium-base alloys. SUBSTANCE: zirconium-base alloy contains the following components, wt. %: niobium 0.5-3.0; iron 0.005-0.5; oxygen 0.03-0.2; carbon 0.001-0.04; silicon 0.002-0.1; nickel 0.003-0.02; the balance, zirconium. In this case, alloy microstructure is characterized by particles of beta-niobium-containing phases sizing not in excess of 0.1 mcm with content of niobium in amount of 60-95% uniformly distributed in alpha-solution. Invention allows production of zirconium-base material whose articles used in active zone of nuclear reactor possess more stable properties such as corrosion resistance, strength, resistance to irradiation growth and creepage, high resistance to nodular corrosion that enhances service life of articles in active zone of nuclear reactors. EFFECT: higher efficiency. 6 cl, 3 tbl 69 ГУС ПЧ Го РОССИЙСКОЕ АГЕНТСТВО ПО ПАТЕНТАМ И ТОВАРНЫМ ЗНАКАМ (19) (51) МПК ВИ” 2441 539 ' 13) СЛ С 22С 16/00, С 21С 3/07 12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ РОССИЙСКОЙ ФЕДЕРАЦИИ (21), (22) Заявка: 99107802102, 22.04.1999 (24) Дата начала действия патента: 22.04.1999 (46) Дата публикации: 20.11.1999 (56) Ссылки: ЕР 0720177 А, 03.07.1996. КЦ 2032759 СЛ, 04.10.1995. ЕР 0538778 АЛ, 28.04.1993. ЕР 0532830 АД, 24.03.1993. 4$ 5366690 А, 22.11.1994. ($ 5125985 А, 30.06.1992. 4Р 01301830 А, 12.06.1989. (98) Адрес для переписки: 123060, Москва, а/я 369 ВНИИНМ (71) Заявитель: Государственный научный центр РФ Всероссийский научно-исспедовательский институт неорганических материалов им.акад.А.А.Бочвара (72) Изобретатель: Никулина А.В., Шебалдов П.В., Шишов В.Н., Перегуд М.М. ‚ Агеенкова Л.Е., Рождественский В.В. , Солонин М.И., Бибилашвили Ю.К. ‚ Лавренюк П.И., Лосицкий А.Ф., Ганза Н.А. , Кузьменко Н.В., Котрехов В.А., Шевнин Ю.П., Маркелов В.А. (73) Патентообладатель: Государственный научный центр РФ Всероссийский научно-исследовательский институт неорганических материалов им.акад.А.А.Бочвара (54) СПЛАВ НА ОСНОВЕ ЦИРКОНИЯ (57) Реферат: Сплав на основе циркония ...

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30-11-2017 дата публикации

EVAPORABLE HETTER ALLOYS, SPECIALLY SUITABLE FOR SORPTION OF HYDROGEN AND CARBON MONOXIDE

Номер: RU2016120582A
Принадлежит: Саес Геттерс С.П.А.

А 2016120582 ко РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) 11 3 3 < ВО ^° 20%: (50) МПК С22С 104 (2006.01) а воз А Хх Эх $ 55 м 5 ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ЗАЯВКА НА ИЗОБРЕТЕНИЕ (21)(22) Заявка: 2016120582, 19.11.2014 (71) Заявитель(и): САЕС ГЕТТЕРС С.П.А. (ТГ) Приоритет(ы): (30) Конвенционный приоритет: (72) Автор(ы): 20.11.2013 Т М12013А001921 КОДА Альберто (ТТ), ГАЛЛИТОНЬОТТА Алессандро (ТТ), 4 : 30.11.2017 Бюл. № 34 (43) Дата публикации заявки юл. № БОНУЧЧИ Антонио (РЕ), (85) Дата начала рассмотрения заявки РСТ на КОНТЕ Андреа ([Т) национальной фазе: 25.05.2016 (86) Заявка РСТ: [В 2014/066169 (19.11.2014) (87) Публикация заявки РСТ: УГО 2015/075648 (28.05.2015) Адрес для переписки: 109012, Москва, ул. Ильинка, 5/2, ООО "Союзпатент" (54) НЕИСПАРЯЕМЫЕ ГЕТТЕРНЫЕ СПЛАВЫ, ОСОБЕННО ПОДХОДЯЩИЕ ДЛЯ СОРБЦИИ ВОДОРОДА И МОНООКСИДА УГЛЕРОДА (57) Формула изобретения 1. Геттерное устройство, содержащее порошки неиспаряемого геттерного сплава, имеющие высокую эффективность сорбции газа, в частности, водорода и монооксида углерода, характеризующееся тем, что указанные порошки сплава содержат в качестве элементов композиции цирконий, ванадий, титан и алюминий, и имеют содержание указанных элементов в атомных процентах, которое может варьировать в следующих диапазонах: а. цирконий от 38 до 44,8% Ь. ванадий от 14 до 29% с. титан от 13 до 15% 4. алюминий от 11,5 до 35%, причем указанные диапазоны атомных процентов выражены относительно суммы циркония, ванадия, титана и алюминия в неиспаряемом геттерном сплаве, указанный неиспаряемый геттерный сплав необязательно содержит один или несколько дополнительных элементов с содержанием в атомных процентах менее 8% относительно общей композиции сплава, при этом указанный один или несколько дополнительных элементов, выбраны из группы, состоящей из железа, хрома, марганца, кобальта или никеля, с содержанием в атомных процентах от 0,1 до 7% относительно общей композиции сплава, в то время как незначительные количества других ...

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26-01-2018 дата публикации

Method and apparatus for manufacturing metal powder material

Номер: CN107635701A
Принадлежит: ATI Properties LLC

一种制造金属粉末材料的方法包括:将进料供应至熔化炉;以及利用第一热源熔化所述熔化炉上的所述进料以提供具有所需化学组成的熔化材料。将所述熔化材料的至少一部分从所述熔化炉直接或间接地传递至雾化炉,在所述雾化炉中使用第二热源加热所述熔化材料。将所述熔化材料的至少一部分以熔化状态从所述雾化炉传递至雾化设备,所述雾化设备由所述熔化材料形成小滴喷雾。使所述小滴喷雾的至少一部分凝固以提供金属粉末材料。

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09-01-2017 дата публикации

Method for surface processing a zirconium of hafnium alloy, and component processed in this manner

Номер: KR101690202B1
Автор: 도미니크 허츠
Принадлежит: 아레바 엔피

지르코늄 혹은 하프늄 합금 재질의 부품의 적어도 일부를 표면 가공하는 방법으로서, 합금 표면층을 나노구조화 하여 합금의 두께를 적어도 5㎛가 되게 하는 적어도 하나의 공정을 포함하고 이때 합금의 입자크기는 100nm 이하이며, 상기 나노구조화는 부품 제작시 사전에 거친 마지막 열처리 공정의 온도와 같거나 이보다 낮은 온도에서 행하는 것으로 된 표면 가공법에 대해 기술한다. 상기 방식으로 가공된 지르코늄 혹은 하프늄 합금 재질의 부품에 대해서도 기술한다. A method of surface processing at least a portion of a zirconium or hafnium alloy material component, the method comprising at least one step of nanostructuring the alloy surface layer to a thickness of at least 5 micrometers, wherein the alloy has a particle size of 100 nm or less, The nanostructuring describes a surface processing method which is performed at a temperature equal to or lower than the temperature of the last annealing process which was roughly preheated at the time of manufacturing the part. Parts of the zirconium or hafnium alloy material processed in the above manner will also be described.

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17-11-2020 дата публикации

Tough corrosion-resistant titanium alloy and preparation method thereof

Номер: CN108893632B
Принадлежит: YANSHAN UNIVERSITY

本发明提供一种强韧耐蚀钛合金及其制备方法,该强韧耐蚀钛合金,按质量含量计,包括Al 5.56~6.75%、Ru 0.08~0.14%、V 3.5~4.5%、Zr(0,50%]和余量的Ti。本发明通过合金化,提高钛合金的强度和耐蚀性能,Zr与Ti形成无限固溶体,从而实现固溶强化,且Zr的致钝电位较Ti更负,即使在弱氧化条件环境中依然可以发生钝化,提高了表面生成致密氧化膜的能力,提升了其耐腐蚀性能;元素Al极大的提高了α相的稳定性和β‑α转变温度,合金在淬火后获得的均为细小的α相,实现细晶强化;同时微量元素Ru的添加也使合金耐蚀性的提高。

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