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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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Форма поиска

Поддерживает ввод нескольких поисковых фраз (по одной на строку). При поиске обеспечивает поддержку морфологии русского и английского языка
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Применить Всего найдено 16676. Отображено 100.
05-01-2012 дата публикации

Resonator

Номер: US20120001700A1
Автор: Robert J. P. Lander
Принадлежит: NXP BV

A method of manufacturing a MEMS resonator formed from a first material having a first Young's modulus and a first temperature coefficient of the first Young's modulus, and a second material having a second Young's modulus and a second temperature coefficient of the second Young's modulus, a sign of the second temperature coefficient being opposite to a sign of the first temperature coefficient at least within operating conditions of the resonator. The method includes the steps of forming the resonator from the first material; applying the second material to the resonator; and controlling the quantity of the second material applied to the resonator by the geometry of the resonator.

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23-05-2017 дата публикации

Установка для получения изделий пропиткой пористых заготовок

Номер: RU0000171192U1

Полезная модель относится к области металлургии, а именно к устройствам для получения деталей сложной формы методом самопроизвольной пропитки жидкого расплава в пористый металлический, не металлический каркас.Технический результат - повышение качества пропитки за счет равномерного нагрева материалов, процесс происходит с большой скоростью, что не вызывает эрозионное разрушение поверхности каркаса, возможность пропитки крупногабаритных деталей, повышение производительности процесса.Загрузка пористых каркасов, с расположенным на них пропитывающим материалом, в установку происходит партией. Подача заготовок в область индукционного нагрева происходит поштучно, где пропитывающий материал и пористый каркас нагревают выше температуры плавления пропитывающего материала, выдерживают и охлаждают в холодильной установке. Процесс пропитки производится в вакууме.Установка для получения изделий методом пропитки содержит:1) блок для автоматической подачи заготовок на требуемую высоту представляет собой совокупность двух рычажных систем, движение которых осуществляется шаговым электродвигателем через зубчато-реечную передачу;2) блок для автоматической подачи заготовок в одну плоскость с индуктором представляет собой взаимодействие трех шаговых электродвигателей, двух рычажных механизмов с толкателями и ленточного транспортера;3) блок для автоматической подачи заготовки в область нагрева представляет собой взаимодействие шагового электродвигателя, конической зубчатой передачи, цепной передачи;4) блок охлаждения представляет собой совокупность ленточного транспортера, с движением от электродвигателя, и теплообменного аппарата, выполненного в виде медной трубки, обвитой вокруг внешней стороны холодильной камеры, по которой циркулирует вода.Блоки устройства отличаются простотой конструкции. РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 171 192 U1 (51) МПК B22F 3/26 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ФОРМУЛА ПОЛЕЗНОЙ МОДЕЛИ К ПАТЕНТУ РОССИЙСКОЙ ФЕДЕРАЦИИ (21)( ...

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14-11-2017 дата публикации

Пресс для экструзии электрода из титановой губки, легирующих компонентов, отходов титановых сплавов

Номер: RU0000174974U1

Полезная модель относится к порошковой металлургии и может быть использована при прессовании электродов для последующего переплава в слитки из шихтовых материалов титановых сплавов, а именно титановой губки и отходов, образующихся при производстве изделий из титановых сплавов.Гидравлический пресс для экструзии электрода, состоящий из следующих основных частей: станины-рамы, системы гидропривода, пресс-штемпеля, контейнера, втулки контейнера с конической матрицей, устройства подачи засыпаемых шихтовых материалов во втулку, глухой матрицы, запирающего мундштука пресса, центрирующей втулки и правящей втулки, правящая втулка постоянной длины делается сборной конструкцией из нескольких втулок.Обеспечивается упрощение конструкции узла контейнер-втулка-матрица. Ц 1 174974 ко РОССИЙСКАЯ ФЕДЕРАЦИЯ 19 11 зе а базе < (13 7 ВУ “174 974 1 (51) МПК ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ В22[ 3/20 (2006.01) (12) ОПИСАНИЕ ПОЛЕЗНОЙ МОДЕЛИ К ПАТЕНТУ (21)(22) Заявка: 2016150136, 20.12.2016 (24) Дата начала отсчета срока действия патента: 20.12.2016 Дата регистрации: 14.11.2017 Приоритет(ы): (22) Дата подачи заявки: 20.12.2016 (45) Опубликовано: 14.11.2017 Бюл. № 32 Адрес для переписки: 121614, Москва, ул. Осенний бульвар, 16, корп. 2, кв. 641, 642, Бондареву Андрею Борисовичу (72) Автор(ы): Бондарев Андрей Борисович (КО), Стадник Сергей Федорович (КП), Лукьянова Светлана Николаевна (КО), Монин Александр Ильич (КО) (73) Патентообладатель(и): Бондарев Андрей Борисович (КП) (56) Список документов, цитированных в отчете о поиске: КИ 2108881 СТ, 20.04.1998. АНДРЕЕВ А.Л. и др. Титановые сплавы. Плавка и литьё титановых сплавов, М., Металлургия, 1978, стр. 269-271. КУ 2090310 СТ, 20.09.1997. ВО 93712 01, 10.05.2010. КО 2120351 СТ, 20.10.1998. ГР 58130202 А, 03.08.1983. (54) ПРЕСС ДЛЯ ЭКСТРУЗИИ ЭЛЕКТРОДА ИЗ ТИТАНОВОЙ ГУБКИ, ЛЕГИРУЮЩИХ КОМПОНЕНТОВ, ОТХОДОВ ТИТАНОВЫХ СПЛАВОВ (57) Реферат: Полезная модель относится к порошковой металлургии и может быть использована при прессовании ...

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09-02-2012 дата публикации

Biodegradable implant and method for manufacturing same

Номер: US20120035740A1
Принадлежит: U&I CORP

This invention relates to a biodegradable implant including magnesium, wherein the magnesium contains, as impurities, (i) manganese (Mn); and (ii) one selected from the group consisting of iron (Fe), nickel (Ni) and mixtures of iron (Fe) and nickel (Ni), wherein the impurities satisfy the following condition: 0</(i)≦5, and an amount of the impurities is 1 part by weight or less but exceeding 0 parts by weight based on 100 parts by weight of the magnesium, and to a method of manufacturing the same.

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15-03-2012 дата публикации

Method of Making Porous Metal Articles

Номер: US20120065739A1
Принадлежит: Praxis Powder Technology Inc

In one embodiment, the present invention may be a method of making a porous biocompatible metal article by combining a metal powder with a homogenizing aid to form metal granules, including blending the metal granules and an extractable particulate to form a composite, forming the composite into a green article, removing the extractable particulate from the green article to form a metal matrix and pore structure, and sintering the metal matrix and pore structure. Furthermore the present invention may include a second homogenizing aid combined with the extractable particulate. The present invention also includes shaping the metal matrix and pore structure with or without the use of a binder.

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29-03-2012 дата публикации

Metal injection molding process and components formed therewith

Номер: US20120073303A1
Принадлежит: General Electric Co

A process of producing a metallic component having a desired shape that includes at least one nonuniform section, as well as metallic components produced by such a process. The process uses a composition containing a mixture of a polymeric binder and a metal powder that includes particles of an alloy having a reactive element that renders the alloy uncastable. The composition is metal injection molded to yield a green compact having a shape corresponding to the shape of the metallic component, including its at least one nonuniform section. A majority of the binder is then removed from the green compact, and then the green compact is sintered to remove a remainder of the binder and fuse particles of the metal powder together to form the metallic component and the nonuniform section thereof.

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12-04-2012 дата публикации

Collimators and methods for manufacturing collimators for nuclear medicine imaging systems

Номер: US20120085942A1
Автор: Yaron Hefetz, Yossi Birman
Принадлежит: Individual

Collimators and methods for manufacturing collimators for nuclear medicine (NM) imaging systems are provided. One method includes forming a plurality of collimator segments from powdered tungsten, wherein the plurality of collimator segments have opposing faces with edges therebetween. The method also includes sintering the powdered tungsten segments and joining the plurality of sintered powdered tungsten segments at least at one or more of the edges to form the collimator for the NM imaging system.

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10-05-2012 дата публикации

Rare earth magnet material and method for producing the same

Номер: US20120114515A1
Автор: Yuji Kaneko, Yukio Takada
Принадлежит: Toyota Central R&D Labs Inc

A method for producing a rare earth magnet material which allows efficient Dy or the like diffusion into an inside thereof. This method includes a preparation step of preparing a powder mixture of magnet powder including one or more rare earth elements including neodymium, boron, and the remainder being iron; and neodymium fluoride powder; a heating step of heating a compact of the powder mixture and causing oxygen around magnet powder particles to react with the fluoride powder, thereby obtaining a lump rare earth magnet material in which neodymium oxyfluoride is wholly distributed. The fluoride powder traps oxygen enclosed in the powder mixture and fixes the oxygen as stable NdOF. When Dy is diffused into this rare earth magnet material, Dy smoothly enters into its inside without being oxidized at grain boundaries. Consequently, coercivity of the entire rare earth magnet material can be efficiently increased without wasting scarce Dy.

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24-05-2012 дата публикации

Carbon molds for use in the fabrication of bulk metallic glass parts and molds

Номер: US20120125071A1
Принадлежит: UNIVERSITY OF CALIFORNIA, YALE UNIVERSITY

Novel molds and methods for Bulk Metallic Glass (BMG) molding using carbon templates obtained from pyrolyzed materials are provided. The method employs the Carbon MEMS (C-MEMS) technique to derive molds of different geometries and dimensions. The resultant carbon structures are stable at very high temperatures and have sufficient mechanical strength to be used as master molds for the thermoplastic forming of BMGs.

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31-05-2012 дата публикации

Method for co-processing components in a metal injection molding process, and components made via the same

Номер: US20120136400A1
Принадлежит: Maetta Sciences Inc

A method comprising molding a first component from a first feedstock comprising a first material powder and a first binder, molding a second component from a second feedstock comprising a second material powder and a second binder, placing the first component and the second component in physical communication with each other in order to form an assembled component, removing the first binder and the second binder from the assembled component and performing a sintering operation on the assembled component so as to bond the first component and the second component together.

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26-07-2012 дата публикации

Methods of forming molybdenum sputtering targets

Номер: US20120189483A1
Принадлежит: Individual

In various embodiments, tubular sputtering targets are produced by forming a tubular billet at least by pressing molybdenum powder in a mold and sintering the pressed molybdenum powder, working the tubular billet to form a worked billet, and heat treating the worked billet.

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27-09-2012 дата публикации

Earth-boring bits and other parts including cemented carbide

Номер: US20120240476A1
Принадлежит: TDY Industries LLC

A method of making an article of manufacture includes positioning a cemented carbide piece comprising at least 5% of the total volume of the article of manufacture, and, optionally, a non-cemented carbide piece in a void of a mold in predetermined positions to partially fill the void and define an unoccupied space. Inorganic particles are added to the mold to partially fill the unoccupied space and provide a remainder space. The cemented carbide piece, the non-cemented carbide piece if present, and the hard particles are heated and infiltrated with a molten metal or a metal alloy. The melting temperature of the molten metal or the metal alloy is less than the melting temperature of the inorganic particles. The molten metal or metal alloy in the remainder space solidifies and binds the cemented carbide piece, the non-cemented carbide piece if present, and the inorganic particles to form the article of manufacture.

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18-10-2012 дата публикации

Method for producing a fuel injection element having channels, and a fuel injection element

Номер: US20120261497A1
Автор: Arno Friedrichs
Принадлежит: Arno Friedrichs

The invention relates to a method for producing a fuel injection element having channels, as well as to a fuel injection element. A fuel injection element according to the invention has helically extending channels and is produced with use of an extrusion tool.

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18-10-2012 дата публикации

Methods for making aluminum nitride armor bodies

Номер: US20120263620A1
Автор: John Carberry
Принадлежит: Schott Corp

A method of making aluminum nitride armor bodies is provided. The method starts with low cost bulk raw material, in the form of aluminum or aluminum alloy, cryogenically mills the raw material into a precursor powder, which is essentially free of oxides and other undesirable impurities. The precursor powder is formed into a pre-form using low cost, short residence time molding processes. Finally, the pre-form is exposed to a nitriding process to convert the pre-form into the aluminum nitride armor body. In this manner, the method avoids the use of high cost aluminum nitride as a starting material and avoids the need for the high cost, single axis densification processes of the prior art.

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22-11-2012 дата публикации

Deposition and post-processing techniques for transparent conductive films

Номер: US20120292725A1

In one embodiment, a method is provided for fabrication of a semitransparent conductive mesh. A first solution having conductive nanowires suspended therein and a second solution having nanoparticles suspended therein are sprayed toward a substrate, the spraying forming a mist. The mist is processed, while on the substrate, to provide a semitransparent conductive material in the form of a mesh having the conductive nanowires and nanoparticles. The nanoparticles are configured and arranged to direct light passing through the mesh. Connections between the nanowires provide conductivity through the mesh.

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06-12-2012 дата публикации

Electromagnetically actuatable valve

Номер: US20120305816A1
Принадлежит: ROBERT BOSCH GMBH

An electrically actuatable valve for injecting fuel includes a magnetic actuator having multiple components, at least one component of the magnetic actuator having multiple sectors made of soft magnetic material and multiple insulating separating webs. A separating web is situated between each two neighboring sectors and entirely separates the neighboring sectors from one another electrically.

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28-02-2013 дата публикации

Turbine shroud segment

Номер: US20130052007A1
Принадлежит: Pratt and Whitney Canada Corp

A turbine shroud segment is metal injection molded (MIM) about a core to provide a composite structure. In one aspect, the core is held in position in an injection mold and then the MIM material is injected in the mold to form the body of the shroud segment about the core. Any suitable combination of materials can be used for the core and the MIM shroud body, each material selected for its own characteristics. The core may be imbedded in the shroud platform to provide a multilayered reinforced platform, which may offer resistance against crack propagation.

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07-03-2013 дата публикации

Degradable high shock impedance material

Номер: US20130055852A1
Автор: Zhiyue Xu
Принадлежит: Baker Hughes Inc

A selectively corrodible powder compact that may be used to make the components of a selectively corrodible perforating system is disclosed. The selectively corrodible powder compact includes a cellular nanomatrix comprising a nanomatrix material. The selectively corrodible powder compact also includes a plurality of dispersed particles comprising a particle core material having a density of about 7.5 g/cm 3 or more, dispersed in the cellular nanomatrix. The selectively corrodible powder compact further includes a bond layer extending throughout the cellular nanomatrix between the dispersed particles.

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21-03-2013 дата публикации

Method For Securing A Stop Member To A Seal Plate Configured For Use With An Electrosurgical Instrument

Номер: US20130071282A1
Автор: Monte S. Fry
Принадлежит: TYCO HEALTHCARE GROUP LP

A method for affixing a stop member to a seal plate for use with electrosurgical instruments is provided. An aperture is formed on a seal plate during a metal injection molding process thereof. A stop member is positioned within the aperture on the seal plate. The seal plate is, subsequently, sintered with the stop member positioned in the aperture.

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04-04-2013 дата публикации

Iron-based sintered sliding member and production method therefor

Номер: US20130084203A1
Принадлежит: Hitachi Powdered Metals Co Ltd

An iron-based sintered sliding member consists of, by mass %, 0.1 to 10% of Cu, 0.2 to 2.0% of C, 0.03 to 0.9% of Mn, 0.52 to 6.54% of S, and the balance of Fe and inevitable impurities. The iron-based sintered sliding member satisfies the following First Formula in which [S %] represents mass % of S and [Mn %] represents mass % of Mn in the overall composition. The iron-based sintered sliding member exhibits a metallic structure in which pores and sulfide particles are dispersed in the matrix that includes a martensite structure at not less than 50% by area ratio in cross section. The sulfide particles are dispersed at 3 to 30 vol. % with respect to the matrix. [S %]=0.6×[Mn %]+0.5 to 6.0  First Formula

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09-05-2013 дата публикации

Method for Manufacturing Resonance Tube, Resonance Tube, and Filter

Номер: US20130113578A1
Автор: Yanzhao Zhou
Принадлежит: Huawei Technologies Co Ltd

A method for manufacturing a resonance tube includes: mixing powder materials, to form homogeneous powder particles, where the powder materials comprise iron powder with a weight proportion of 50% to 90%, at least one of copper powder and steel powder with a weight proportion of 1% to 30%, and an auxiliary material with a weight proportion of 1% to 20%; pressing and molding the powder particles, to form a resonance tube roughcast; sintering the resonance tube roughcast in a protective atmosphere, to form a resonance tube semi-finished product; and electroplating the resonance tube semi-finished product, to form the resonance tube. In the method, the resonance tube, and the filter according to embodiments of the present invention, the resonance tube is manufactured by using multiple powder materials.

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16-05-2013 дата публикации

High Hardness, Corrosion Resistant PM Nitinol Implements and Components

Номер: US20130118312A1
Принадлежит: SUMMIT MATERIALS, LLC

A manufacturing method for making components includes: providing at least one of a prealloyed powder of a composition of Ni—Ti in the range of Ni-36Ti to Ni-45Ti or a mix of powders that forms a composition of Ni—Ti in the range of Ni-36Ti to Ni-45Ti; loading at least one of the prealloyed powder and the mix powders into a container; hot isostatically pressing (HIP) the container to full density to obtain a compact; rolling the compact in a mill with multiple passes to produce a sheet or other mill form material; and cutting blanks for the components from the sheet material to produce a component blank. 1. A manufacturing method for making components , comprising:providing at least one of a prealloyed powder of a composition of Ni—Ti in the range of Ni-36Ti to Ni-45Ti or a mix of powders that forms a composition of Ni—Ti in the range of Ni-36Ti to Ni-45Ti;loading at least one of the prealloyed powder or the mix of powders into a container;hot isostatically pressing (HIP) the container to full density to obtain a compact;rolling the compact in a mill with multiple passes to produce a sheet or other mill form material; andcutting blanks for the components from the sheet material to produce a component blank.2. The manufacturing method of claim 1 , wherein the mix of powders is a mix of nickel and titanium constitutive elemental powders that forms a composition of Ni—Ti in the range of Ni-36Ti to Ni-45Ti.3. The manufacturing method of claim 1 , wherein the container is manufactured from low carbon steel.4. The manufacturing method of claim 1 , wherein the container has one of a rectangular shape and a round shape.5. The manufacturing method of claim 1 , wherein pressures produced during the hot isostatically pressing (HIP) are between about 10 claim 1 ,000 psi and about 30 claim 1 ,000 psi.6. The manufacturing method of claim 1 , wherein a temperature during the hot isostatically pressing (HIP) ranges from about 1600° F. to about 2000° F.7. The manufacturing method of ...

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23-05-2013 дата публикации

Exchangeable insert seat member for cutting tool

Номер: US20130129435A1
Принадлежит: Sandvik Intellectual Property AB

The present invention relates to an exchangeable insert seat member for a metal cutting tool comprising a tool body and a cutting insert, wherein the exchangeable insert seat member is arranged to be placed between the tool body and the cutting insert wherein said exchangeable insert seat member is contacting said tool body and said cutting insert at contact areas arranged such that there is no direct contact between the tool body and the cutting insert and wherein said exchangeable insert seat member is produced by powder injection molding. The present invention also relates to a metal cutting tool comprising such an exchangeable insert seat member.

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23-05-2013 дата публикации

METHODS FOR PROCESSING NANOSTRUCTURED FERRITIC ALLOYS, AND ARTICLES PRODUCED THEREBY

Номер: US20130129556A1
Принадлежит: GENERAL ELECTRIC COMPANY

A formed article comprising a nanostructured ferritic alloy is provided. Advantageously, the article is not formed via extrusion, and thus, cost savings are provided. Methods are also provided for forming the article, and the articles so produced, exhibit sufficient continuous cycle fatigue crack growth resistance and hold time fatigue crack growth resistance to be utilized as turbomachinery components, and in particular, large, hot section components of a gas or steam turbine engines. In other embodiments, a turbomachinery component comprising an NFA is provided, and in some such embodiments, the turbomachinery component may be extruded. 1. A method of forming a turbomachinery component comprising a nanostructured ferritic alloy , the method comprising the steps:melting an alloy by vacuum induction melting to form a melt of the alloy where the alloy is any of martensitic, austenitic, duplex, or ferritic steel, atomizing the melt of the alloy to form an atomized powder of the alloy, milling the atomized powder of the alloy in the presence of an oxide until the oxide is dissolved into the alloy;hot isostatic pressing the powder under an inert environment to form a hot isostatic pressed nanostructured ferritic alloy preform, andforging the nanostructured ferritic alloy preform into a turbomachinery component wherein the steps are performed in the absence of extrusion.2. The method of claim 1 , wherein the atomizing comprises at least one of gas atomization claim 1 , water atomization claim 1 , rotating electrode atomization claim 1 , or combinations thereof.3. The method of claim 1 , wherein the oxide is selected from the group consisting of yttrium oxide claim 1 , aluminum oxide claim 1 , zirconium oxide claim 1 , hafnium oxide or combinations thereof.4. The method of claim 1 , wherein the hot isostatic pressing is continued to produce a nanostructured ferritic alloy preform having a density greater than 95% of theoretical density.5. The method of claim 1 , wherein ...

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30-05-2013 дата публикации

HIGH PRESSURE CARBIDE COMPONENT WITH SURFACES INCORPORATING GRADIENT STRUCTURES

Номер: US20130133531A1
Принадлежит: Smith International, Inc.

An anvil including a hard phase and a metal matrix in which the hard phase is dispersed, a concentration of the metal matrix phase varying according to a concentration gradient, is disclosed. The anvil may be used in a high pressure press. Methods of making an anvil including forming a hard phase dispersed in a metal matrix phase, a concentration of the metal matrix phase varying according to a concentration gradient, are also disclosed. 1. An anvil comprising:a hard phase; anda metal matrix phase in which the hard phase is dispersed, wherein a concentration of the metal matrix phase varies according to a concentration gradient.2. The anvil of claim 1 , wherein the hard phase comprises a hard material selected from the group consisting of tungsten carbide claim 1 , tantalum carbide claim 1 , titanium carbide and combinations thereof3. The anvil of claim 1 , wherein the metal matrix phase comprises a material selected from the group consisting of Co claim 1 , Fe claim 1 , Ni and combinations thereof4. The anvil of claim 1 , further comprising a working surface for applying high pressure claim 1 , wherein the concentration gradient extends from the working surface to a gradient depth within the anvil.5. The anvil of claim 4 , wherein a concentration of the metal matrix phase at the working surface is lower than a concentration of the metal matrix phase at the gradient depth within the anvil by an amount in a range of about 1 to about 2%.6. The anvil of claim 4 , wherein a concentration of the metal matrix phase at the working surface is lower than a concentration of the metal matrix phase at the gradient depth within the anvil by an amount in a range of about 2 to about 4%.7. The anvil of claim 4 , wherein a concentration of the metal matrix phase at the working surface is lower than a concentration of the metal matrix phase at the gradient depth within the anvil by an amount in a range of about 4 to about 6%.8. The anvil of claim 4 , wherein the concentration of the ...

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30-05-2013 дата публикации

NITRIDED SINTERED STEELS

Номер: US20130136646A1
Принадлежит: Höganas AB (publ)

The present invention concerns a method of producing sintered components, and sintered components by the method. The method provides a cost effective production of sintered steel parts with wear resistance properties comparable to those of components made from chilled cast iron. 1. A method of producing sintered components by single press/single sintering comprising the steps of:a) providing pre-alloyed iron-based steel powder comprising less than 0.3% by weight of Mn and at least one of Cr in an amount between 0.2-3.5% by weight, Mo in an amount between 0.05-1.20% by weight and V in an amount between 0.05-0.4% by weight, and maximum 0.5% incidental impurities, the balance being iron,b) mixing said pre-alloyed iron-based steel powder with lubricant and graphite, and optionally machining enhancing agent(s) and other conventional sintering additives,c) subjecting the mixed composition of step b) to compaction at pressures of 400-2000 MPa, thereby providing a compact,d) sintering said compact from step c) in a reducing atmosphere at a temperature between 1000-1400° C., thereby providing a sintered component,e) nitriding said sintered component of step d) in a nitrogen containing atmosphere, at a temperature of 400-600° C., with a soaking time of less than 3 hours,2. A method according to claim 1 , wherein the lubricant consists of composite lubricant particles comprising a core of 10-60% by weight of at least one primary fatty acid amide having more than 18 and not more than 24 carbon atoms and 40-90% by weight of at least one fatty acid bisamide claim 1 , said lubricant particles also comprising nanoparticles of at least one metal oxide adhered on the core.3. A method according to claim 1 , wherein the compact is not steam treated before nitriding in step e).4. A method according to claim 1 , wherein in step c) the compact is compacted to a green density of at least 7.10 g/cm.5. A method according to claim 1 , wherein in step d) the sintered component is sintered to a ...

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30-05-2013 дата публикации

POWDER-METALLURGICAL STEEL

Номер: US20130136647A1
Автор: ALBER Roland
Принадлежит: GUEHRING OHG

The invention relates to a method for producing powder-metallurgical steel. Said method consists of the following steps: a steel powder, preferably having a predetermined structure, is produced; the steel powder is mixed with a binding agent to form a plastically deformable raw material; the raw material is initially shaped to form a blank having a predefined spatial form; and the blank is sintered. 1. A method for producing a powder-metallurgical steel , particularly a tool steel , such as HSS or HSS-E steel , having the following process steps:producing steel powder have a predetermined microstructure;mixing the steel powder with a binding agent to form a plastically deformable raw mixture;preforming the raw mixture to form a blank having a predefined spatial form; andsintering the blank.2. The method according to claim 1 , characterized in that the steel powder undergoes processing to homogenize the geometry of the powder particles while it is being mixed with the binding agent.3. The method according to claim 1 , characterized in that the steel powder undergoes processing to homogenize the geometry of the powder particles before it is mixed with the binding agent.4. The method according to claim 3 , characterized in that the steel powder undergoes a selection process before mixing so that it has a predetermined particle size and/or particle size distribution when it undergoes the mixing process.5. The method according to claim 1 , characterized in that the steel powder is obtained by grinding or crushing steel particles.6. The method according to claim 1 , characterized in that the steel powder is mixed with a binding agent claim 1 , for example cobalt.7. The method according to claim 1 , characterized in that the blank undergoes a hot isostatic pressing (HIP) process before claim 1 , during or after sintering.8. The method according to claim 1 , characterized in that the blank undergoes a thermal treatment claim 1 , for example a hardening process claim 1 , ...

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30-05-2013 дата публикации

Method for producing composition for injection molding and composition for injection molding

Номер: US20130136926A1
Принадлежит: Seiko Epson Corp

A method for producing a composition for injection molding which contains an inorganic powder composed of at least one of a metal material and a ceramic material and a binder containing a polyacetal-based resin and a glycidyl group-containing polymer. The method includes: cryogenically grinding a first resin containing the polyacetal-based resin as a main component; cryogenically grinding a second resin containing the glycidyl group-containing polymer as a main component; mixing a powder obtained by grinding the first resin, a powder obtained by grinding the second resin, and the inorganic powder, thereby obtaining a mixed powder; and kneading the mixed powder.

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06-06-2013 дата публикации

PROCESS FOR PRODUCING A CU-CR MATERIAL BY POWDER METALLURGY

Номер: US20130140159A1
Принадлежит: PLANSEE POWERTECH AG

A process for producing a Cu—Cr material by powder metallurgy for a switching contact, in particular for vacuum switches, includes the steps of pressing a Cu—Cr powder mixture formed from Cu powder and Cr powder and sintering the pressed Cu—Cr powder mixture to form the material of the Cu—Cr switching contact. The sintering or a subsequent thermal treatment process is carried out with an alternating temperature profile, in which the Cu—Cr powder mixture or the Cu—Cr material is heated above an upper temperature limit value and cooled again below a lower temperature limit value at least twice in alternation. All of the steps are carried out at temperatures at which no molten phase forms. 112-. (canceled)13. A process for producing a Cu—Cr material by powder metallurgy for a switching contact or a vacuum switch contact , the process comprising the following steps:pressing a Cu—Cr powder mixture formed from Cu powder and Cr powder;sintering the pressed Cu—Cr powder mixture to form the material of the Cu—Cr switching contact; andcarrying out at least one of a sintering or subsequent thermal treatment process with an alternating temperature profile by heating the Cu—Cr powder mixture or the Cu—Cr material above an upper temperature limit value and cooling the Cu—Cr powder mixture or the Cu—Cr material again below a lower temperature limit value at least twice in alternation, and carrying out all of the steps at temperatures at which no molten phase forms.14. The process according to claim 13 , which further comprises setting the upper temperature limit value in a range between 1065° C. and 1025° C. and setting the lower temperature limit value at least 50° C. below the upper temperature limit value or at least 100° C. below the upper temperature limit value.15. The process according to claim 13 , which further comprises additionally performing a step of mixing Cu powder and Cr powder to form the Cu—Cr powder mixture.16. The process according to claim 13 , which further ...

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13-06-2013 дата публикации

Powder Material, Method for Manufacturing Communication Device, and Communication Device

Номер: US20130149184A1
Автор: Zhou Yanzhao
Принадлежит: Huawei Technologies Co., Ltd.

A powder material, a method for manufacturing a communication device, and a communication device are disclosed. The powder material according to an embodiment of the present invention includes quartz glass powder, tungsten powder, and an auxiliary material, where a weight proportion of the quartz glass powder is 5% to 90%, a weight proportion of the tungsten powder is 5% to 90%, and a weight proportion of the auxiliary material is 0 to 20%. The powder material according to another embodiment of the present invention includes titanium powder, tungsten powder, and iron powder, where a weight proportion of the titanium powder is 4% to 80%, a weight proportion of the tungsten powder is 5% to 90%, and a weight proportion of the iron powder is 4% to 80%. 1. A powder material comprising:quartz glass powder;tungsten powder; andan auxiliary material,wherein a weight proportion of the quartz glass powder is 5% to 90%,wherein a weight proportion of the tungsten powder is 5% to 90%, andwherein a weight proportion of the auxiliary material is 0% to 20%.2. The powder material according to claim 1 , wherein a maximum value of the weight proportion of the quartz glass powder is 75% to 90% claim 1 , wherein a minimum value of the weight proportion of the quartz glass powder is 5% to 10% claim 1 , wherein a maximum value of the weight proportion of the tungsten powder is 75% to 90% claim 1 , and wherein a minimum value of the weight proportion of the tungsten powder is 5% to 10%.3. The powder material according to claim 1 , wherein the weight proportion of the quartz glass powder is 15% to 70% claim 1 , and wherein the weight proportion of the tungsten powder is 15% to 70%.4. The powder material according to claim 3 , wherein a maximum value of the weight proportion of the quartz glass powder is 65% to 70% claim 3 , wherein a minimum value of the weight proportion of the quartz glass powder is 15% to 30% claim 3 , wherein a maximum value of the weight proportion of the tungsten ...

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20-06-2013 дата публикации

COMPOSITIONS COMPRISING NICKEL-TITANIUM, METHODS MANUFACTURE THEREOF AND ARTICLES COMPRISING THE SAME

Номер: US20130156627A1
Принадлежит:

Disclosing herein is a method for manufacturing nickel-titanium compositions. The method includes disposing a powdered composition in a mold; the powdered composition comprising nickel and titanium; the titanium being present in an amount of about 38 to about 42 wt % and the nickel being present in an amount of about 58 to about 62 wt %; sintering the powdered composition to produce a sintered preform; compacting the preform; machining the preform to form an article; heat treating the article; the annealing being conducted at a temperature of about 1650° F. to about 1900° F. at a pressure of about 3 Torr to about 5 Kg−f/cmfor a time period of about 10 minutes to about 5 hours; and quenching the article. 1. An article having a composition comprising:a first phase that comprises nickel and titanium in an atomic ratio of about 0.45:0.55 to about 0.55:0.45;a second phase that comprises nickel and titanium in an atomic ratio of about 0.70:0.30 to about 0.80:0.20; anda third phase that comprises nickel and titanium in an atomic ratio of about 0.52:0.48 to about 0.62:0.38; the article having no voids or pinholes and having a uniform surface hardness of about 40 to 62 HRC.2. The article of claim 1 , the article being a valve body claim 1 , a piston claim 1 , a piston ring claim 1 , a cylinder claim 1 , check valve balls claim 1 , balls for ball valves claim 1 , gates for gate valves claim 1 , tool bits claim 1 , parts for magnetic resonance imaging machines claim 1 , threaded fasteners claim 1 , locks claim 1 , safes claim 1 , quick connect couplings claim 1 , outer surfaces of submarines claim 1 , outer surfaces of ships claim 1 , wear plates claim 1 , articles used in space stations claim 1 , cutlery claim 1 , knives claim 1 , forks claim 1 , spoons claim 1 , saws claim 1 , shears claim 1 , razor blades claim 1 , drills claim 1 , drills and drill bits for offshore drilling claim 1 , drills and drill bits for oil well drilling claim 1 , tank turret bearings claim 1 , ...

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18-07-2013 дата публикации

Soft magnetic powder, granulated powder, dust core, electromagnetic component, and method for producing dust core

Номер: US20130181802A1
Принадлежит: Sumitomo Electric Industries Ltd

Provided are a soft magnetic powder for obtaining a dust core having a low iron loss, the dust core, and a method for producing a dust core. The present invention relates to a soft magnetic powder including a plurality of soft magnetic particles, each having an insulating layer. The Vickers hardness HV0.1 of a material constituting the soft magnetic particles is 300 or more, and the insulating layer contains Si, O, and at least one of an alkali metal and Mg. As long as the soft magnetic powder has such features, a material having a high electric resistance, such as an iron-based alloy, can be used. The eddy current loss can be reduced, and it is possible to effectively obtain a dust core having a low iron loss.

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25-07-2013 дата публикации

Method for producing sintered ndfeb magnet

Номер: US20130189426A1
Автор: Masato Sagawa
Принадлежит: Intermetallics Co Ltd

A method for producing a sintered NdFeB magnet having high coercivity and capable of being brought into applications without lowering its residual magnetic flux density or maximum energy product and without reprocessing. The method includes applying a substance containing dysprosium (Dy) and/or terbium (Tb) to the surface of the sintered NdFeB magnet forming a base body and then heating the magnet to diffuse Dy and/or Tb through the grain boundary and thereby increase the coercivity of the magnet. This method is characterized in that: (1) the substance containing Dy or Tb to be applied to the surface of the sintered NdFeB magnet is substantially a metal powder; (2) the metal powder is composed of a rare-earth element R and an iron-group transition element T, or composed of R, T and another element X, the element X capable of forming an alloy or intermetallic compound with R and/or T; and (3) the oxygen content of the sintered NdFeB magnet forming the base body is 5000 ppm or lower. The element T may contain nickel (Ni) or cobalt (Co) to produce an anticorrosion effect.

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01-08-2013 дата публикации

Embossed Metallic Flakes Process And Product

Номер: US20130192789A1
Принадлежит: ECKART AMERICA CORPORATION

A process for preparing embossed fine particulate thin metal flakes having high levels of brightness and color intensity. The process comprises forming a release coat on a flexible polymeric carrier film, embossing the release coat with a diffraction grating pattern that is monoruled at an angle above 45°, vacuum metalizing the embossed release surface with a highly reflective metal such as aluminum, and solubilizing the metalized release coat in a solvent for removing the metal from the carrier to form embossed metal flakes that replicate the embossment pattern. The flakes are recovered from the solution containing the solvent and release coat polymer while avoiding high shear, particle sizing or other application of energy that would excessively break up the flakes, so that the D50 particle size of the flakes is maintained at or above 75 microns. The flakes have application to coatings and printing inks that produce extremely high brightness characterized as an optically apparent glitter or sparkle effect in combination with high color intensity or chromaticity. 1. A process for making embossed fine particulate thin metallic flakes having brightness and color intensity , comprising providing a release surface on a carrier , embossing the release surface with a diffraction grating pattern having an angular ruling pattern greater than 45° , metalizing the embossed release surface with a thin reflective metal film , removing the metal film from the release surface to form a solvent dispersion of embossed metal flakes that have replicated the diffraction grating pattern , and controlling the particle size of the flakes contained in the dispersion to maintain the embossed flakes contained therein at a D50 particle size at or above 75 microns.2. The process according to in which the metal layer is applied to a polymeric release coat which is coated on the carrier and then embossed with the diffraction grating pattern.3. The process of forming a first coating containing ...

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01-08-2013 дата публикации

HIGH-STRENGTH MAGNESIUM ALLOY WIRE ROD, PRODUCTION METHOD THEREFOR, HIGH-STRENGTH MAGNESIUM ALLOY PART, AND HIGH-STRENGTH MAGNESIUM ALLOY SPRING

Номер: US20130195711A1
Принадлежит: NHK SPRING CO., LTD.

A high-strength magnesium alloy wire rod suitable for products in which at least one of bending stress and twisting stress primarily acts is provided. The wire rod has required elongation and 0.2% proof stress, whereby strength and formability are superior, and has higher strength in the vicinity of the surface. In the wire rod, the surface portion has the highest hardness in a cross section of the wire rod, the highest hardness is 170 HV or more, and the inner portion has a 0.2% proof stress of 550 MPa or more and an elongation of 5% or more. 1. A high-strength magnesium alloy wire rod used for members in which at least one of bending stress and twisting stress primarily acts , the wire rod comprising:a surface portion having the highest hardness in a cross section of the wire rod, the highest hardness being 170 HV or more;an inner portion having a 0.2% proof stress of 550 MPa or more and an elongation of 5% or more.2. The high-strength magnesium alloy wire rod according to claim 1 , whereinthe magnesium contains Mg as a main element and Ni and Y.3. The high-strength magnesium alloy wire rod according to claim 2 , whereinthe magnesium consists of 2 to 5 atomic % of Ni, 2 to 5 atomic % of Y, and the balance of Mg and inevitable impurities.4. The high-strength magnesium alloy wire rod according to claim 1 , wherein the portion having the highest hardness in the vicinity of the surface has an average grain diameter of 1 μm measured by an EBSD method.5. A production method for a high-strength magnesium alloy wire rod claim 1 , the method comprising:a step for yielding a raw material in a form of foil strips, foil pieces, or fibers of a magnesium alloy by a rapid solidification method,a sintering step for forming a billet by bonding, compressing, and sintering the raw material,{'claim-ref': {'@idref': 'CLM-00001', 'claim 1'}, 'a step for plastic forming the billet, thereby obtaining the wire rod according to .'}6. A production method for a high-strength magnesium alloy ...

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22-08-2013 дата публикации

PRESSURE FORMING OF METAL AND CERAMIC POWDERS

Номер: US20130218281A1
Принадлежит: Accellent Inc.

A method of pressure forming a brown part from metal and/or ceramic particle feedstocks includes: introducing into a mold cavity or extruder a first feedstock and one or more additional feedstocks or a green or brown state insert made from a feedstock, wherein the different feedstocks correspond to the different portions of the part; pressurizing the mold cavity or extruder to produce a preform having a plurality of portions corresponding to the first and one or more additional feedstocks, and debinding the preform. Micro voids and interstitial paths from the interior of the preform part to the exterior allow the escape of decomposing or subliming backbone component substantially without creating macro voids due to internal pressure. The large brown preform may then be sintered and subsequently thermomechanically processed to produce a net wrought microstructure and properties that are substantially free the interstitial spaces. 1. A method of producing a consolidated preform for a part , comprising: a first portion comprising a first metal and/or ceramic powder composition dispersed in a binder;', 'one or more additional portions, at least one of which shares a boundary with the first portion, each additional portion comprising a metal and/or ceramic powder composition dispersed in a binder that is different from at least the first portion; and, 'providing a green or brown preform comprisingsintering the preform to bind the powder particles to each other to produce a consolidated, unitary preform.2. The method of further performing a densification process on the preform subsequent to sintering to densify at least a portion of the consolidated claim 1 , unitary preform.3. The method of wherein at least one additional portion comprises a core that is substantially surrounded by the composition of the first portion.4. The method of wherein the core is completely surrounded by the first portion.5. The method of wherein the core comprises a majority of the part by ...

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05-09-2013 дата публикации

Method of forming an object using powder injection molding

Номер: US20130231427A1

A method of forming an object by powder injection molding, the object being formed from an injection molded integral body comprising a green part contiguous with an expendable part, the method comprising debinding the integral body at step 18 to obtain a debound green part contiguous with a debound expendable part; sintering the debound green part at step 20 at a sintering temperature, the debound expendable part configured to at least partially define the debound green part and has a melting point higher than the sintering temperature; and separating the debound expendable part from the sintered debound green part at step 22 to form the object.

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12-09-2013 дата публикации

Collimator for x-ray, gamma, or particle radiation

Номер: US20130235981A1
Принадлежит: Plansee Se

A collimator for x-ray, gamma, or particle radiation has a plurality of collimator elements made of a tungsten-containing material to reduce scattered radiation. At least one collimator element consists of a tungsten alloy having a tungsten content of 72 to 98 wt.-%, which contains 1 to 14 wt.-% of at least one metal of the group Mo, Ta, Nb and 1 to 14 wt.-% of at least one metal of the group Fe, Ni, Co, Cu. The collimator also has very homogeneous absorption behavior at very thin wall thicknesses of the collimator elements.

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12-09-2013 дата публикации

INDUSTRIAL METHOD FOR PRODUCING DISPERSION-STRENGTHENED IRON-BASED MATERIALS AT LOW COST AND IN LARGE-SCALE

Номер: US20130236349A1

The invention provides an industrial method for producing dispersion-strengthened iron-based materials at low cost and in large-scale. The industrial acid pickling waste solution is treated by spray roasting process after yttrium chloride is added. During the spray roasting process, the solution is atomized into fine droplets, the droplets are contacted with gas and dried into powders, which are heated in air to form metal oxides. The mixed powders of the metal oxides are reduced in hydrogen stream to obtain yttria dispersion-strengthened iron powders. High performance dispersion-strengthened iron materials are obtained by densifying the yttria dispersion-strengthened iron powders. The method has simple process and low cost, and is suitable for large-scale production due to the direct use of acid pickling waste solution from steel factory. 1. A method for industrially producing an iron-based dispersion strengthened material at low cost and on a large scale , wherein:step 1, adding yttrium chloride into a hydrochloric acid pickling waste liquor containing iron, so as to obtain a pickling waste liquor containing matrix metal ions, by which, a metal elementary substance is finally generated, and dispersed-phase metal ions, by which, an oxide as a dispersed phase is finally generated, wherein, when raw materials are converted into quality of the oxide as the dispersed phase and the matrix metal, mass fraction of the oxide as the dispersed phase in the total alloy is in the range of 0.1-2%;step 2, making the pickling waste liquor containing matrix metal ions and dispersed-phase metal ions get into a preconcentrator, and concentrating the waste acid;step 3, atomizing and spraying the concentrated waste acid to be tiny droplets by a nozzle on the top of a roasting furnace for roasting, in which, particles of ferric chloride in the concentrated acid is roasted into free hydrogen chloride and iron oxide in a burning gas, and yttrium chloride is roasted into free hydrogen ...

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19-09-2013 дата публикации

Electronic component element housing package

Номер: US20130240262A1
Автор: Masanori Nagahiro

An electronic component element housing package is produced by firing a ceramic substrate for housing an electronic component element and a metal layer for bonding to the ceramic substrate to form an electrical path, simultaneously in a reducing atmosphere. The ceramic substrate comprises alumina (Al 2 O 3 ), a partially stabilized zirconia by forming solid solution with yttria (Y 2 O 3 ) and a sintering agent. The sintering agent comprises magnesia (MgO), and at least 1 type selected from silica (SiO 2 ), calcia (CaO), or manganese oxides (MnO, MnO 2 , Mn 2 O 3 , Mn 3 O 4 ).

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26-09-2013 дата публикации

Method to Improve the Leaching Process

Номер: US20130247478A1
Принадлежит: Varel International Industries LP

A method to leach a component that includes a polycrystalline structure. The method includes obtaining the component having the polycrystalline structure. The polycrystalline structure includes catalyst material deposited therein. The method also includes performing a leaching process on the polycrystalline structure to an intermediate leaching depth. The leaching process removes at least a portion of the catalyst material from the polycrystalline structure and forms one or more by-product materials deposited therein. The method also includes performing a cleaning process on the polycrystalline structure, which removes at least a portion of the by-product materials. The leaching process and the cleaning process are iteratively continued until the intermediate leaching depth reaches a desired leaching depth, both of which are measured from one end of the polycrystalline structure. The desired leaching depth is greater than at least one intermediate leaching depth.

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10-10-2013 дата публикации

Method of Preparing Silver-Based Oxide Electrical Contact Materials with Fiber-like Arrangement

Номер: US20130266468A1
Принадлежит:

A method of preparing silver-based oxide electrical contact materials with fiber-like arrangement, includes the following steps of: (1) uniformly mixing the silver-metal alloy powders and graphite powders and then ball-milling; (2) internally oxidizing the ball-milled powders; (3) sieving; (4) placing the sieved powders and the matrix powders into the powder mixer for mixing; (5) cold-isostatically pressing; (6) sintering; (7) hot-pressing; and (8) hot-extruding, thereby obtaining the silver-based oxide electrical contact material with fiber-like arrangement. The method of the present invention can obtain the silver-based oxide electrical contact material having neat fiber-like arrangement with no specific requirement on processing deformation, plasticity and ductility of the reinforcing phase. The production process in this method is simple and is easy to operate. Besides, there is no particular requirement on the equipment. The method greatly improves the performance of contact materials in aspects of resistance to welding and arc erosion, conductivity, and processing performance 1. A method of preparing silver-based oxide electrical contact materials with fiber-like arrangement , comprising the steps of:(A) uniformly mixing silver-metal-additive alloy powders with graphite powders, and then placing the mixed powders into a high-energy ball milling tank for ball-milling, wherein the metal in the alloy powders can form alloy with Ag, a weight ratio of Ag to other metals in the alloy powders is calculated according to a composition of the preparation material and subsequent processing requirements, a content of the additive is calculated according to a content of the metal and subsequent processing requirements, and the additive is selected from a group consisting of Bi, In, Cu and rare earth elements;(B) internally oxidizing the powders obtained from the step (A) comprising firstly decarburizing in air atmosphere and then internally oxidizing in oxygen atmosphere;( ...

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10-10-2013 дата публикации

Method for near net shape manufacturing of high-temperature resistant engine components

Номер: US20130266469A1
Принадлежит: Rolls Royce Deutschland Ltd and Co KG

For near net shape manufacturing of a high-temperature resistant component of complex design a high melting-point part of an intermetallic phase provided as a metal powder is mixed with a binder, and from the feedstock such formed a green compact substantially matching the final contour is produced by metal injection moulding, into the pores of said compact that remain after removal of the binder the low melting-point part of the intermetallic phase is infiltrated. The brown compact thereby created is mechanically processed, if required, and subjected to a specific heat treatment depending on the metallic phases used in order to create the intermetallic phase. This permits engine components consisting of intermetallic phases and having a geometrically complex structure to be manufactured cost-efficiently.

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10-10-2013 дата публикации

METHOD FOR PRODUCING MAGNETIC GREEN COMPACTS, MAGNETIC GREEN COMPACT, AND SINTERED BODY

Номер: US20130266474A1
Автор: Kato Takeshi, Maeda Toru
Принадлежит: Sumitomo Electric Industries, Ltd.

A method is provided for producing magnetic green compacts. Material powder including a rare earth alloy and containing not less than 15 mass % of fine particles with particle diameter of not more than 2 μm is filled into a compacting mold, then compacted and compressed, and subjected to magnetic fields to give a green compact. A powder compact having a packing density 1.05 to 1.2 times the bulk density is subjected to a weak magnetic field of 1 to 2 T to give a compact. The magnetic field strength is increased to not less than 3 T at an excitation rate of 0.01 to 0.15 T/sec, and the strong magnetic field of not less than 3 T is applied to the compact by a high-temperature superconducting coil. The magnetic field is applied by the high-temperature superconducting coil in a direction opposite to a direction applied by a normal conducting coil. 1. A magnetic green compact used as a material for a sintered magnet and comprising powder including a rare earth alloy containing a rare earth and iron ,the powder containing 15 mass % to 100 mass % of fine particles with a particle diameter of not more than 2 μm,the green compact having a degree of crystal orientation of not less than 95%.2. A method for producing magnetic green compacts as materials for sintered magnets using powder including a rare earth alloy containing a rare earth and iron , the method comprising:a preparation step of providing material powder including the rare earth alloy and containing 15 mass % to 100 mass % of fine particles with a particle diameter of not more than 2 μm; anda compacting step of filling the material powder into a compacting mold, compacting and compressing the material powder, and applying a magnetic field to form a green compact;the compacting step comprising:a light compacting step of compacting and compressing the material powder filled in the compacting mold to fabricate a powder compact having a packing density that is 1.05 to 1.2 times the bulk density;a weak magnetic field ...

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10-10-2013 дата публикации

PROCESSING OF NICKEL-TITANIUM ALLOYS

Номер: US20130266817A1
Автор: Wojcik C. Craig
Принадлежит: ATI PROPERTIES, INC.

Processes for producing a nickel-titanium alloy are disclosed. The processes are characterized by the production of nickel-titanium alloy articles having improved microstructure. A pre-alloyed nickel-titanium alloy is melted and atomized to form molten nickel-titanium alloy particles. The molten nickel-titanium alloy particles are cooled to form nickel-titanium alloy powder. The nickel-titanium alloy powder is consolidated to form a fully-densified nickel-titanium alloy preform that is hot worked to form a nickel-titanium alloy article. Any second phases present in the nickel-titanium alloy article have a mean size of less than 10 micrometers measured according to ASTM E1245-03 (2008) or an equivalent method. 1. A nickel-titanium alloy article comprising:50.0 to 60.0 weight percent nickel based on the total weight of the article; andbalance titanium and residual elements;wherein the residual elements comprise greater than 300 ppm oxygen; andwherein second phases present in the nickel-titanium alloy article have a mean size of less than 10 micrometers measured according to ASTM E1245-03 (2008) or an equivalent method.2. The nickel-titanium alloy article of claim 1 , wherein the residual elements comprise greater than 350 ppm oxygen.3. The nickel-titanium alloy article of claim 1 , wherein the residual elements comprise greater than 100 ppm carbon.4. The nickel-titanium alloy article of claim 1 , wherein second phases present in the nickel-titanium alloy article have a mean size of less than 7.5 micrometers measured according to ASTM E1245-03 (2008) or an equivalent method.5. The nickel-titanium alloy article of claim 1 , wherein any second phases present in the nickel-titanium alloy article have a mean size of less than 5 micrometers measured according to ASTM E1245-03 (2008) or an equivalent method.6. The nickel-titanium alloy article of claim 1 , wherein any second phases present in the nickel-titanium alloy article have a mean size of less than 2.5 micrometers ...

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31-10-2013 дата публикации

MASTER BATCH FOR CERAMIC- OR METAL-POWDER INJECTION-MOLDING, AND METHOD FOR PREPARING SAID MASTER BATCH

Номер: US20130289184A1
Принадлежит:

The master batch for molding includes at least one inorganic powder, advantageously ceramic or metallic; an organic mixture, advantageously polymer, comprising: a stable polymer having good ductility features, from 30 to 90% by mass of the mixture; a lubricant, from 5 to 50% by mass of the mixture; a plasticizing polymer, from 5 to 30% by mass of the mixture; with a [% by mass of the lubricant]/[% by mass of the stable polymer] ratio smaller than or equal to 1, advantageously strictly smaller than 1. 1. A master hatch for molding , comprising:at least one inorganic powder, advantageously ceramic or metallic; an LLPDE as a stable polymer having good ductility features, from 30 to 90% by mass of the organic mixture;', 'a lubricant, from 5 to 50% by mass of the organic mixture;', 'a plasticizing polymer, from 5 to 30% by mass of the organic mixture;', 'with a [% by mass of the lubricant]/[% by mass of LLPDE] ratio smaller than or equal to 1, advantageously strictly smaller than 1., 'an organic mixture, advantageously polymer, comprising2. The master batch of claim 1 , wherein the organic mixture comprises:an LLDPE as a stable polymer having good ductility features, from 40 to 90% by mass of the organic mixture;a lubricant, from 5 to 40%, or even from 10 to 40% by mass of the organic mixture;a plasticizing polymer, from 5 to 30% by mass of the organic mixture.3. The master batch of claim 1 , wherein it contains neither solvent nor water.4. The master batch of claim 1 , wherein the lubricant is a paraffin wax.5. The master batch of claim 1 , wherein the plasticizing polymer is PEG.6. The master batch of claim 1 , wherein it further contains a dispersing agent claim 1 , advantageously stearic acid.7. The master batch of claim 6 , wherein the dispersing agent is added up to from 1 to 20% by mass of the organic mixture.8. The master batch of claim 1 , wherein the inorganic powder amounts to from 40 to 75% by volume of the master batch.9. A use of the master batch of to form ...

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07-11-2013 дата публикации

R-t-b sintered magnet

Номер: US20130293328A1
Автор: Futoshi Kuniyoshi
Принадлежит: Hitachi Metals Ltd

This sintered R-T-B based rare-earth magnet includes: R 2 Fe 14 B type compound crystal grains, including a light rare-earth element RL (which includes at least one of Nd and Pr) as a major rare-earth element R, as main phases; and a heavy rare-earth element RH (which includes at least one of Dy and Tb). Before its surface region is removed, the sintered R-T-B based rare-earth magnet has no layer including the rare-earth element R at a high concentration in that surface region. The sintered R-T-B based rare-earth magnet has a portion in which coercivity decreases gradually from its surface region toward its core portion. The difference in the amount of TRE between a portion of the sintered R-T-B based rare-earth magnet that reaches a depth of 500 μm as measured from its surface region toward its core portion and the core portion of the sintered R-T-B based rare-earth magnet is 0.1 through 1.0.

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14-11-2013 дата публикации

Composite soft magnetic material having low magnetic strain and high magnetic flux density, method for producing same, and electromagnetic circuit component

Номер: US20130298730A1
Принадлежит: Diamet Corp, Mitsubishi Materials Corp

A composite soft magnetic material having low magnetostriction and high magnetic flux density contains: pure iron-based composite soft magnetic powder particles that are subjected to an insulating treatment by a Mg-containing insulating film or a phosphate film; and Fe—Si alloy powder particles including 11%-16% by mass of Si. A ratio of an amount of the Fe—Si alloy powder particles to a total amount is in a range of 10%-60% by mass. A method for producing the composite soft magnetic material comprises the steps of: mixing a pure iron-based composite soft magnetic powder, and the Fe—Si alloy powder in such a manner that a ratio of the Fe—Si alloy powder to a total amount is in a range of 10%-60%; subjecting a resultant mixture to compression molding; and subjecting a resultant molded body to a baking treatment in a non-oxidizing atmosphere.

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14-11-2013 дата публикации

DISINTEGRABLE METAL CONE, PROCESS OF MAKING, AND USE OF THE SAME

Номер: US20130299185A1
Принадлежит: BAKER HUGHES INCORPORATED

A frustoconical member includes a metal composite that has a cellular nanomatrix comprising a metallic nanomatrix material; a metal matrix disposed in the cellular nanomatrix; and a first frustoconical portion. A process of making the frustoconical member includes combining a metal matrix powder, a disintegration agent, and metal nanomatrix material to form a composition; compacting the composition to form a compacted composition; sintering the compacted composition; and pressing the sintered composition to form the frustoconical member having a tapered portion on an outer surface of the frustoconical member. The frustoconical member can be used by contacting a frustoconical portion of the frustoconical member to a tapered surface of an article; applying pressure to the frustoconical member; urging the frustoconical member in a direction relative to the article to expand a radial dimension of the article; and contacting the frustoconical member with a fluid to disintegrate the frustoconical member. 1. A frustoconical member comprising:a first frustoconical portion; and a cellular nanomatrix comprising a metallic nanomatrix material; and', 'a metal matrix disposed in the cellular nanomatrix., 'a substrate comprising a metal composite which includes2. The frustoconical member of claim 1 , further comprising a second frustoconical portion.3. The frustoconical member of claim 2 , wherein the first frustoconical portion and second frustoconical portion are tapered in opposing directions to one another.4. The frustoconical member of claim 1 , further comprising an inner radial dimension and outer radial dimension such that the inner radial dimension is greater than 50% of the outer radial dimension.5. The frustoconical member of claim 1 , further comprising a seat disposed at an inner surface of the frustoconical member.6. The frustoconical member of claim 1 , wherein the seat includes a land which is sealingly engagable with a removable plug runnable thereagainst claim 1 ...

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14-11-2013 дата публикации

IRON BASED POWDERS FOR POWDER INJECTION MOLDING

Номер: US20130302202A1
Автор: Larsson Anna
Принадлежит: Höganas AB (publ)

An iron-based powder composition for metal injection molding having an average particle size of 20-60 μm, and having 99% of the particles less than 120 μm wherein the iron-based powder composition includes, by weight percent of the iron-based powder composition: Mo: 0.3-1.6, P: 0.1-0.6, optionally Cu: up to 3.0, optionally Si: up to 0.6, optionally Cr: up to 5, optionally, unavoidable impurities: up to 1.0, whereof carbon is less than 0.1, the balance being iron, and wherein the sum of Mo and 8*P content is within the range of 2-4.7. 1. An iron-based powder composition for metal injection molding having an average particle size of 20-60 μm , and having 99% of the particles less than 120 μm wherein the iron-based powder composition comprises by weight percent of the iron-based powder composition;Mo: 0.3-1.6,P: 0.1-0.6,optionally Cu: up to 3.0,optionally Si: up to 0.6,Cr: up to 5,Optionally unavoidable impurities: up to 1.0, whereof carbon is less than 0.1, the balance being iron, andwherein the sum of Mo and 8*P content is within the range of 2-4.7.2. An iron-based powder composition according to wherein the iron based composition includes an iron powder being prealloyed with Mo in such amounts that the powder composition includes 0.3-1.6% Mo by weight.3. An iron-based powder composition according to wherein P is present in the form of FeP powder.4. An iron-based powder composition according to wherein the content of Mo is 0.35-1.55% claim 1 , by weight of the iron-based powder composition.5. An iron-based powder composition according to wherein the content of P is 0.1-0-45% by weight of the iron-based powder composition.6. A metal injection molding feedstock composition comprising: the iron based powder composition according to and a binder.7. A metal injection molding feedstock according to wherein the binder is at least one organic binder in a concentration of 30-65% by volume of the feedstock composition.8. A method for producing a sintered component comprising ...

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14-11-2013 дата публикации

METHOD OF MANUFACTURING A BEARING

Номер: US20130302203A1
Принадлежит: Foxconn Technology Co., Ltd.

A method of manufacturing a bearing includes, firstly, injecting a mixture of metal powder into a mold to form a semi-finished product. Then the semi-finished product is sintered. After that, the sintered semi-finished product is fine machined, and then washed, to form the bearing. 1. A method of manufacturing a bearing , the method comprising:injecting a mixture of metal powder into a mold to form a semi-finished product;sintering the semi-finished product; andfine machining and washing the sintered semi-finished product to form the bearing.2. The method of claim 1 , wherein forming the semi-finished product comprises pressure molding.3. The method of claim 1 , wherein the semi-finished product is sintered in a mesh belt furnace.4. The method of claim 1 , wherein the sintered semi-finished product is fine machined in a sealed molding chamber using a shaping machine.5. The method of claim 1 , further comprising immersing the washed semi-finished product into oil in vacuum condition; and performing a deoiling process on the semi-finished product to separate the oil from the semi-finished product.6. The method of claim 5 , wherein the oil is antirust oil.7. The method of claim 5 , wherein a vacuum degree of the vacuum condition is in a range of from 0 millimeters mercury (mm Hg) to 5 mm Hg.8. The method of claim 1 , wherein the mixture of metal powder is a mixture of copper powder and iron powder.9. The method of claim 1 , wherein the formed bearing is configured for fixing a shaft on an impeller of a fan. 1. Technical FieldThe disclosure relates to methods of manufacturing bearings, and particularly to a method of manufacturing a bearing used in equipment such as spindle motors found in various electronic devices.2. Description of the Related ArtAt present, bearings are widely used in spindle motors, with the spindle motors applied in devices such as compact disc (CD) drives, digital video disc (DVD) drives, hard disk drives, laser beam printers, floppy disk drives ...

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26-12-2013 дата публикации

Material with high resistance to wear

Номер: US20130343944A1
Принадлежит: Boehler Edelstahl GmbH and Co KG

Material and method for the production of material with isotropic, mechanical properties and improved wear resistance and high hardness potential. Method includes producing in a powder metallurgical (PM) method a slug or ingot from a material of ledeburite tool steel alloy, and subjecting one of the slug or ingot or a semi-finished product produced from the slug or ingot to full annealing at a temperature of over 1100° C., but at least 10° C. below the fusing temperature of the lowest melting structure phase with a duration of over 12 hrs. In this manner, an average carbide phase size of the material is increased by at least 65%, a surface shape of the material is rounded and a matrix is homogenized. Method further includes subsequently processing the material into thermally tempered tools with high wear resistance occurs or into parts to which abrasive stress is applied.

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09-01-2014 дата публикации

DIRECT EXTRUSION OF SHAPES WITH L12 ALUMINUM ALLOYS

Номер: US20140010700A1
Автор: Pandey Awadh B.
Принадлежит:

A method for producing a high strength aluminum alloy brackets, cases, tubes, ducts, beams, spars and other parts containing L1dispersoids from an aluminum alloy powder containing the L1dispersoids. The powder is consolidated into a billet having a density of about 100 percent. The billet is extruded using an extrusion die shaped to produce the component. 1. A method for forming a high strength aluminum alloy component containing L1dispersoids , comprising the steps of:{'sub': 2', '2', '3, 'claim-text': about 0.1 to about 4.0 weight percent scandium, about 0.1 to about 20.0 weight percent erbium, about 0.1 to about 15.0 weight percent thulium, about 0.1 to about 25.0 weight percent ytterbium, and about 0.1 to about 25.0 weight percent lutetium;', 'at least one second element selected from the group comprising about 0.1 to about 20.0 weight percent gadolinium, about 0.1 to about 20.0 weight percent yttrium, about 0.05 to about 4.0 weight percent zirconium, about 0.05 to about 10.0 weight percent titanium, about 0.05 to about 10.0 weight percent hafnium, and about 0.05 to about 5.0 weight percent niobium; and', 'the balance substantially aluminum;, 'placing in a container a quantity of an aluminum alloy powder containing an L1dispersoid L1comprising AlX dispersoids wherein X is at least one first element selected from the group comprisingthe alloy powder having a mesh size of less than 450 mesh in a container,vacuum degassing the powder at a temperature of about 300° F. (149° C.) to about 900° F. (482° C.) for about 0.5 hours to about 8 days;sealing the degassed powder in the container under vacuum;heating the sealed container at about 300° F. (149° C.) to about 900° F. (482° C.) for about 15 minutes to eight hours;vacuum hot pressing the heated container to form a billet;removing the container from the formed billet; andextruding the billet into a component using an extrusion die shaped to form the component.2. The method of claim 1 , wherein the aluminum alloy ...

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06-03-2014 дата публикации

NOVEL METHOD OF IMPROVING THE MECHANICAL PROPERTIES OF POWDER METALLURGY PARTS BY GAS ALLOYING

Номер: US20140065003A1
Автор: Narasimhan Gopinath
Принадлежит:

The following specification describes a process for improving the hardness and other mechanical properties of iron and steel Powder Metallurgy (P/M) parts. The first stage of the novel process consists of heating to and holding at a temperature between 590° C. to 720° C. unalloyed or low alloyed P/M parts in an atmosphere containing a Nitrogen donor such as Ammonia in either batch or continuous furnaces. The concentration of ammonia during the first stage is maintained between 3% to 15%. The second stage of the inventive process is an ‘aging’ process which may be conducted either as an in-line process or as a stand-alone independent process that involves the heating of P/M parts that have fully or partially cooled after the first stage to a temperature between 180° C. and 660° C. in an atmosphere of plain air or Nitrogen. The first stage may be performed in varying concentrations of the nitrogen donor wherein the temperature and time duration may also be varied to control the depth of hardening in the said part. The conditions may be optimized to achieve through hardness of the part without embrittllement. The optional stage two of the technology is an aging process that does not involve “quenching,” thereby significantly lowering distortion of treated parts and eliminating pollution associated with liquid quenching. The technology improves process economy by using low temperatures and consequently fuel consumption. 1. A novel two stage process for heat treating unalloyed or low alloyed iron & steel P/M parts consisting of two major stages wherein the first stage is the alloying of the parts with Nitrogen gas which causes the formation of an austenitic phase in the metal matrix of the parts throughout the section thickness or to a controlled depth beneath the surface of the parts , in addition to the formation of hard transformation products and interstitial Nitrogen. This is followed in most but not all cases by a second stage of “aging” the P/M parts which causes ...

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27-03-2014 дата публикации

Corrosion-resistant magnet and method for producing the same

Номер: US20140083568A1
Принадлежит: Hitachi Metals Ltd

An object of the present invention is to provide an R—Fe—B based sintered magnet having on a surface thereof a chemical conversion film with higher corrosion resistance than a conventional chemical conversion film such as a phosphate film, and a method for producing the same. The corrosion-resistant magnet of the present invention as a means for achieving the object is characterized by comprising a chemical conversion film containing at least Zr, Nd, fluorine, and oxygen as constituent elements and not containing phosphorus directly on a surface of an R—Fe—B based sintered magnet, wherein R is a rare-earth element including at least Nd.

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10-04-2014 дата публикации

Electrode material for aluminum electrolytic capacitor, and process for producing same

Номер: US20140098460A1
Принадлежит: Toyo Aluminum KK

The present invention provides an electrode material for an aluminum electrolytic capacitor, which does not require any etching treatment and which has improved bending strength. Specifically, the present invention provides an electrode material for an aluminum electrolytic capacitor, which comprises, as constituent elements, a sintered body of a powder of at least one member selected from the group consisting of aluminum and aluminum alloys and an aluminum foil substrate that supports the sintered body thereon, which is characterized in that (1) the powder has an average particle size D 50 of 0.5 to 100 μm, (2) the sintered body is formed on one surface or both surfaces of the aluminum foil substrate and has a total thickness of 20 to 1,000 μm, and (3) the aluminum foil substrate has a thickness of 10 to 200 μm and an Si content of 10 to 3,000 ppm.

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04-01-2018 дата публикации

IMPLANTABLE MEDICAL DEVICE HOUSING HAVING INTEGRATED FEATURES

Номер: US20180001093A1
Принадлежит: Heraeus Deutschland GmbH & Co. KG

One aspect is a housing for an implantable medical device, including first housing portion of metal, an intermediate portion of metal and having first and second sides opposite one another and having integrated features, and a second housing portion of metal. The first housing portion is sealed to the first side of the intermediate portion and the second housing portion is sealed to the second side of the intermediate portion thereby forming an housing internal space within first and second housing portions and containing the intermediate portion and its features, such that the features are hermetically sealed within the housing relative to an external space that is outside the housing. 1. A housing for an implantable medical device comprising:a first housing portion comprising metal;an intermediate portion comprising metal and having first and second sides opposite one another and having integrated features; anda second housing portion comprising metal;wherein the first housing portion is sealed to the first side of the intermediate portion and the second housing portion is sealed to the second side of the intermediate portion thereby forming an housing internal space within first and second housing portions and containing the intermediate portion and its features, such that the features are hermetically sealed within the housing relative to an external space that is outside the housing.2. The housing of claim 1 , wherein the features comprise at least one of a group comprising walls claim 1 , ribs claim 1 , component cavities claim 1 , standoffs claim 1 , recesses claim 1 , knuckles claim 1 , and back-up bands.3. The housing of claim 1 , wherein the intermediate portion defines a first chamber between the first housing portion and the intermediate portion and a second chamber between the second housing portion and the intermediate portion.4. The housing of claim 3 , wherein the first and second chambers are hermetically sealed from each other by the intermediate ...

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04-01-2018 дата публикации

METHOD OF FABRICATING A HOUSING FOR AN IMPLANTABLE MEDICAL DEVICE HAVING INTEGRATED FEATURES

Номер: US20180001094A1
Принадлежит: Heraeus Deutschland GmbH & Co. KG

One aspect is a method of fabricating a housing for an implantable medical device, including forming a first housing portion of metal using an additive manufacturing process such that features are integrated into the first portion. A second housing portion of metal is also formed. The first and second housing portions are joining thereby sealing an internal space of the housing within first and second portions and fully containing the features such that they are hermetically sealed relative to an external space outside the housing. 1. A method of fabricating a housing for an implantable medical device , the method comprising:forming a first housing portion comprising metal using an additive manufacturing process such that features are integrated into the first portion;forming a second housing portion comprising metal; andjoining the first and second housing portions thereby sealed an internal space of the housing within first and second portions and fully containing the features such that they are hermetically sealed relative to an external space outside the housing.2. The method of claim 1 , wherein the additive manufacturing process comprises at least one of metal injection molding (MIM) claim 1 , direct metal laser sintering (DMLS) claim 1 , stereolithography (SLA) claim 1 , and three-dimensional printing (3D printing).3. The method of claim 2 , wherein additive manufacturing process comprises using at least one of Ti 6Al-4V (Grade 5 titanium) claim 2 , Ti 6Al-4V ELI (Grade 23 titanium) claim 2 , and Ti 3Al 2.5V (Grade 9 titanium) for the first and second housing portions.4. The method of claim 1 , wherein the features formed in first housing portion comprise at least one of a group comprising walls claim 1 , ribs claim 1 , component cavities claim 1 , standoffs claim 1 , recesses claim 1 , knuckles claim 1 , and back-up bands.5. The method of claim 1 , wherein joining the first and second housing portions further comprises welding along a connection line ...

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07-01-2021 дата публикации

NITROGEN SOLID SOLUTION TITANIUM SINTERED COMPACT AND METHOD FOR PRODUCING SAME

Номер: US20210001405A1
Автор: KONDOH Katsuyoshi
Принадлежит:

An nitrogen solid solution titanium sintered compact includes a matrix made of a titanium component having an α-phase, nitrogen atoms dissolved as a solute of solid solution in a crystal lattice of the titanium component, and metal atoms dissolved as a solute of solid solution in the crystal lattice of the titanium component. 115-. (canceled)16. A nitrogen solid solution titanium sintered compact comprising:a matrix made of a titanium component having an α-phase;nitrogen atoms dissolved as a solute of solid solution in a crystal lattice of a hexagonal close-packed structure of said titanium component; andmetal atoms dissolved as a solute of solid solution in the crystal lattice of a hexagonal close-packed structure of said titanium component.17. The nitrogen solid solution titanium sintered compact according to claim 16 , whereina compound of said titanium component and said metal atoms exceeding a solid solubility limit of dissolving into the α-phase is dispersed in said matrix.18. The nitrogen solid solution titanium sintered compact according to claim 16 , wherein a metal of said metal atoms is a metal selected from the group consisting of Al claim 16 , Si claim 16 , Cr claim 16 , V claim 16 , Mo claim 16 , Ta claim 16 , and Zr.19. A nitrogen solid solution titanium material sintered compact comprising:a matrix made of a titanium component having an α-phase;nitrogen atoms dissolved as a solute of solid solution in a crystal lattice of a hexagonal close-packed structure of said titanium component; anda metal component that is present by being dispersed in said matrix.20. The nitrogen solid solution titanium sintered compact according to claim 19 , wherein said metal component is made of metal atoms that are deposited in said matrix.21. The nitrogen solid solution titanium sintered compact according to claim 19 , wherein said metal component is a compound of metal atoms and said titanium component.22. The nitrogen solid solution titanium sintered compact according ...

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05-01-2017 дата публикации

METHOD FOR MANUFACTURING A CLADDED COMPONENT

Номер: US20170001244A1
Принадлежит:

A method for manufacturing a metallic component having a core and a metallic cladding by Hot Isostatic Pressing includes the steps of arranging a capsule and a core such that the capsule at least partially surrounds the core and a space is formed between at least a portion of the core and a portion of the capsule. The core, prior to the step of Hot Isostatic Pressing, is provided with at least one centering means for centering the solid body obtained in the step of Hot Isostatic Pressing in a metal machining apparatus. 1. A method for manufacturing a metallic component having a core and a metallic cladding , comprising the steps of:arranging a capsule and a core such that the capsule at least partially surrounds the core and such that a space is formed between at least a portion of the core and a portion of the capsule;filling the space with metallic cladding material such that the metallic cladding material covers at least a portion of the core;evacuating air from the capsule and sealing the capsule;subjecting the capsule to Hot Isostatic Pressing at a predetermined temperature, a predetermined pressure and for a predetermined time so that the metallic cladding material is bonded to the core forming a solid body; andsubjecting the solid body to a metal machining operation in which the metallic cladding material is machined in a metal machining apparatus into a metallic cladding of a predetermined thickness, wherein the core, prior to the step of Hot Isostatic Pressing, is provided with at least one centering means for centering the solid body obtained in the step of Hot Isostatic Pressing in the metal machining apparatus.2. The method according to claim 1 , wherein the centering means is a female centering means or a male centering means.3. The method according to claim 2 , wherein the male centering means is a truncated cone or a cone.4. The method according claim 2 , wherein the female centering means is a recess having the shape of a truncated cone or the shape ...

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04-01-2018 дата публикации

METHODS AND MULTI-PURPOSE POWDER REMOVAL FEATURES FOR ADDITIVE MANUFACTURING

Номер: US20180001384A1
Принадлежит:

The present disclosure generally relates to methods for additive manufacturing (AM) for fabricating multi-walled structures. A multi-walled structure includes a first wall having a first surface and a second wall having a second surface facing the first surface to define a passage having a width between the first surface and the second surface in a first direction. The multi-walled structure also includes an enlarged powder removal feature connecting the first wall and the second wall. The enlarged powder removal feature has an inner dimension greater than the width in the first direction and at least one open end in a direction transverse to the first width. 1. A method for fabricating an object , comprising:(a) irradiating a layer of powder in a powder bed with an energy beam in a series of scan lines to form a fused region;(b) providing a subsequent layer of powder over the powder bed by passing a recoater arm over the powder bed from a first side of the powder bed to a second side of the powder bed; and(c) repeating steps (a) and (b) until the object is formed in the powder bed,wherein the object includes:a first wall having a first surface,a second wall having a second surface facing the first surface to define a passage having a width between the first surface and the second surface in a first direction, andan enlarged powder removal feature connecting the first wall and the second wall, the enlarged powder removal feature having an inner dimension greater than the width in the first direction and at least one open end in a direction transverse to the first width.2. The method of claim 1 , further comprising:(d) removing unfused powder from the passage via the at least one open end.3. The method of claim 2 , further comprising:(e) passing an elongated object through the powder removal feature.4. The method of claim 1 , wherein the powder removal feature connects a first end of the first wall to a first end of the second wall.5. The method of claim 4 , wherein ...

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04-01-2018 дата публикации

ADDITIVE-MANUFACTURING SYSTEMS, APPARATUSES AND METHODS

Номер: US20180001548A1
Принадлежит:

Additive-manufacturing systems, surface-processing apparatuses, and methods of forming products using an additive-manufacturing head are provided. In one aspect, an additive-manufacturing system includes an additive-manufacturing head and a surface-processing device coupled to the additive-manufacturing head. In another aspect, a surface-processing apparatus for an additive-manufacturing head includes a housing configured to be coupled to the additive-manufacturing head and a surface-processing device coupled to the housing. In a further aspect, a method of forming a product using an additive-manufacturing head includes forming one or more layers of the product with the additive-manufacturing head and processing at least one of the one or more layers of the product with a surface-processing device coupled to the additive-manufacturing head. 1. A method of forming a product using an additive-manufacturing head , the method comprising:forming one or more layers of the product with the additive-manufacturing head; andprocessing at least one of the one or more layers of the product with a surface-processing device coupled to the additive-manufacturing head.2. The method of claim 1 , wherein processing at least the one of the one or more layers of the product comprises smoothing at least the one of the one or more layers of the product.3. The method of claim 2 , wherein smoothing at least the one of the one or more layers comprises smoothing at least the one of the one or more layers along at least one of an interior surface and an exterior surface of the product.4. The method of claim 3 , wherein smoothing at least the one of the one or more layers along at least the one of the interior surface or the exterior surface comprises melting a portion of at least the one of the one or more layers.5. The method of claim 3 , further comprising moving the surface-processing device relative to the additive-manufacturing head.6. The method of claim 1 , wherein processing includes ...

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03-01-2019 дата публикации

SHRINKING SUPPORT STRUCTURES

Номер: US20190001412A1
Принадлежит:

A variety of additive manufacturing techniques can be adapted to fabricate a substantially net shape object from a computerized model using materials that can be debound and sintered into a fully dense metallic part or the like. However, during sintering, the net shape will shrink as binder escapes and the base material fuses into a dense final part. If the foundation beneath the object does not shrink in a corresponding fashion, the resulting stresses throughout the object can lead to fracturing, warping, or other physical damage to the object resulting in a failed fabrication. To address this issue, a variety of techniques are disclosed for substrates and build plates that contract in a manner complementary to the object during debinding and sintering. 1. A method comprising:fabricating a support structure including a substrate for an object from a support material having at least one of a debind shrinkage rate and a sintering shrinkage rate matching a build material; andfabricating an object from the build material on the support structure, wherein the object has a net shape based on a computerized model, wherein the build material includes a powdered material for forming a final part and a binder system including one or more binders, wherein the one or more binders resist deformation of the object during a fabrication, a debinding, and a sintering of the object into the final part, and wherein the support structure is configured to match a shrinkage of the object during at least one of the debinding and the sintering.2. The method of further comprising fabricating the support structure on a build plate formed of a material that is debindable and sinterable.3. The method of wherein fabricating the support structure includes fabricating a build plate for use as the support structure by injection molding the build plate with the support material.4. The method of wherein fabricating the support structure includes fabricating a structural support for at least one of ...

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02-01-2020 дата публикации

3D PRINTER AND 3D PRINTING

Номер: US20200001537A1

A 3D printing system comprising: a selective solidification module to: form a printed article by processing a build material; and form a printed container encompassing the printed article and a portion of unused build material about the printed article, the printed container defining a first port and a second port fluidly connected to the first port. The 3D printing system further comprises a connector to couple to the first port or second port of the printed container; and a pump fluidly connected to the connector to cause a fluid to flow through the printed container from the first port to the second port such that the printed article is cooled by the fluid flow. 1. A 3D printing system comprising: form a printed article by processing a build material; and', 'form a printed container encompassing the printed article and a portion of unused build material about the printed article, the printed container defining a first port and a second port fluidly connected to the first port;, 'a selective solidification module toa connector to couple to the first port or second port of the printed container; anda pump fluidly connected to the connector to cause a fluid to flow through the printed container from the first port to the second port such that the printed article is cooled by the fluid flow.2. The 3D printing system of claim 1 , further comprising a post processing station to:receive a printed container; orreceive a printing bucket containing the printed container and unused build material surrounding the printed container;wherein the post processing station includes the connector and the pump.3. The 3D printing system of claim 1 , wherein the pump is a fluid injector to cause fluid to flow by injecting fluid into the printed container; orwherein the pump is a vacuum pump to cause the fluid to flow by pulling fluid through the printed container.4. The 3D printing system of claim 1 , further comprising a robotic arm to locate the printed container and drive the ...

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01-01-2015 дата публикации

PRECIPITATE STRENGTHENED NANOSTRUCTURED FERRITIC ALLOY AND METHOD OF FORMING

Номер: US20150004043A1
Принадлежит:

An alloy and method of forming the alloy are provided. The alloy includes a matrix phase, and a population of particulate phases dispersed within the matrix. The matrix includes iron and chromium; and the population includes a first subpopulation of particulate phases and a second subpopulation of particulate phases. The first subpopulation of particulate phases include a complex oxide, having a median size less than about 20 nm, and present in the alloy in a concentration from about 0.1 volume percent to about 5 volume percent. The second subpopulation of particulate phases have a median size in a range from about 30 nm to about 10 microns, and present in the alloy in a concentration from about 1 volume percent to about 15 volume percent. 1. An alloy , comprising: a first subpopulation of particulate phases comprising a complex oxide, having a median size less than about 20 nm, and present in the alloy in a concentration from about 0.1 volume percent to about 5 volume percent; and', 'a second subpopulation of particulate phases having a median size in a range from about 30 nm to about 10 microns, and present in the alloy in a concentration from about 1 volume percent to about 15 volume percent., 'a matrix phase comprising iron and chromium; and a population of particulate phases dispersed within the matrix, the population comprising2. The alloy of claim 1 , wherein the particulate phases of the first subpopulation comprise at least two elements of the following group: yttrium claim 1 , titanium claim 1 , aluminum claim 1 , zirconium claim 1 , hafnium claim 1 , and magnesium.3. The alloy of claim 2 , wherein the particulate phases of the first subpopulation comprise yttrium and titanium.4. The alloy of claim 1 , wherein the particulate phases of the first subpopulation have a median size less than about 10 nm.5. The alloy of claim 1 , wherein the concentration of the first subpopulation is in an amount from about 0.1 volume percent to about 3 volume percent of the ...

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01-01-2015 дата публикации

NANOSTRUCTURED FERRITIC ALLOY AND METHOD OF FORMING

Номер: US20150004044A1
Принадлежит: GENERAL ELECTRIC COMPANY

An alloy and method of forming the alloy are provided. The alloy includes a matrix phase, and a multimodally distributed population of particulate phases dispersed within the matrix. The matrix includes iron and chromium, and the population includes a first subpopulation of particulate phases and a second subpopulation of particulate phases. The first subpopulation of particulate phases include a complex oxide, having a median size less than about 15 nm, and present in the alloy in a concentration from about 0.1 volume percent to about 5 volume percent. The second subpopulation of particulate phases have a median size in a range from about 25 nm to about 10 microns, and present in the alloy in a concentration from about 0.1 volume percent to about 15 volume percent. Further embodiments include articles, such as turbomachinery components and fasteners, for example, that include the above alloy, and methods for making the alloy. 1. An alloy , comprising: a first subpopulation of particulate phases comprising a complex oxide, having a median size less than about 15 nm, and present in the alloy in a concentration from about 0.1 volume percent to about 5 volume percent; and', 'a second subpopulation of particulate phases having a median size in a range from about 25 nm to about 10 microns, and present in the alloy in a concentration from about 0.1 volume percent to about 15 volume percent., 'a matrix phase comprising iron and chromium; and a multimodally distributed population of particulate phases dispersed within the matrix, the population comprising2. The alloy of claim 1 , wherein the particulate phases of the first subpopulation comprise at least two elements of the following group: yttrium claim 1 , titanium claim 1 , aluminum claim 1 , zirconium claim 1 , hafnium claim 1 , and magnesium.3. The alloy of claim 2 , wherein the particulate phases of the first subpopulation comprise yttrium and titanium.4. The alloy of claim 1 , wherein the particulate phases of the ...

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04-01-2018 дата публикации

METALLURGICAL PROCESS AND ARTICLE WITH NICKEL-CHROMIUM SUPERALLOY

Номер: US20180002795A1
Автор: Das Gopal
Принадлежит:

A method of metallurgical processing includes, providing a workpiece that has been formed by additive manufacturing of a nickel-chromium based superalloy. The workpiece has an internal porosity and a microstructure with a columnar grain structure and delta phase. The workpiece is then hot isostatically pressed to reduce the internal porosity and to at least partially retain the columnar grain structure and the delta phase. The workpiece is then heat treated to at least partially retain the columnar grain structure and the delta phase. 1. A method of metallurgical processing , the method comprising:providing a workpiece that has been formed by additive manufacturing of a nickel-chromium based superalloy, the workpiece having an internal porosity and a microstructure with a columnar grain structure and delta phase;hot isostatically pressing the workpiece to reduce the internal porosity and to at least partially retain the columnar grain structure and the delta phase; andheat treating the workpiece after the hot isostatic pressing to at least partially retain the columnar grain structure and the delta phase.2. The method as recited in claim 1 , wherein the hot isostatic pressing of the workpiece forms new delta phase at grain boundaries in the columnar grain structure claim 1 , and the heat treating of the workpiece after the hot isostatic pressing forms additional new delta phase at grain boundaries in the columnar grain structure.3. The method as recited in claim 1 , wherein the nickel-chromium based superalloy has a composition including claim 1 , by weight: 50-55% Ni+Co claim 1 , 17-21% Cr claim 1 , 4.74-5.5% Nb+Ta claim 1 , 2.8-3.3% Mo claim 1 , 0.65-1.15 Ti claim 1 , 0.2-0.8 Al claim 1 , and a balance Fe and impurities.4. The method as recited in claim 1 , wherein the workpiece has a geometry of an aerospace component.5. The method as recited in claim 1 , wherein the hot isostatic pressing reduces the internal porosity by a relative percentage of least 40%.6. The ...

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03-01-2019 дата публикации

Gamma, gamma' cobalt based alloys for additive manufacturing methods or soldering, welding, powder and component

Номер: US20190003017A1
Принадлежит: SIEMENS AG

The invention relates to gamma, gamma'-cobalt-based alloys for additive manufacturing methods or soldering, welding, powder and component. By using a cobalt-based alloy based on Co-7W-7 Al-23Ni-2Ti-2Ta-12Cr-0.0IB-0.IC-(0-0.1Si), an alloy that is especially well-suited for additive manufacturing methods or high-temperature soldering is proposed.

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03-01-2019 дата публикации

HOT WORK TOOL STEEL

Номер: US20190003021A1
Принадлежит:

The invention relates hot work tool steel. The steel comprises the following main components (in wt. %): 5. A steel according claim 1 , wherein the content of primary precipitated MX is 0.2-3 vol. % claim 1 , preferably 0.3-1.0 vol. %.8. A steel according to claim 1 , wherein the matrix comprises tempered martensite and/or bainite and the amount of retained austenite is limited to 6 vol. %.9. A steel according to claim 1 , wherein the steel is provided in the form of a powder claim 1 , preferably having a size distribution in the range of 5-150 μm claim 1 , wherein the mean size of the powder particles is in the range of 25-50 μm.10. Use of a steel powder according to for additive manufacturing claim 9 , in particular for making of repairing injection moulding tools.11. A steel according to claim 1 , wherein the matrix comprises tempered martensite and/or bainite and the amount of retained austenite is limited to 5 vol. %.12. A steel according to claim 1 , wherein the matrix comprises tempered martensite and/or bainite and the amount of retained austenite is limited to 4 vol. %.13. A steel according to claim 1 , wherein the matrix comprises tempered martensite and/or bainite and the amount of retained austenite is limited to 2 vol. %.14. A steel according to claim 1 , wherein the steel is provided in the form of a powder claim 1 , having a size distribution in the range of 10-100 μm claim 1 , wherein the mean size of the powder particles is in the range of 25-50 μm.15. A steel according to claim 1 , wherein the steel is provided in the form of a powder claim 1 , having a size distribution in the range of 10-60 μm claim 1 , wherein the mean size of the powder particles is in the range of 25-50 μm. The invention relates to a hot work tool steel.Vanadium alloyed matrix tool steels have been on market for decades and attained a considerable interest because of the fact that they combine a high wear resistance with an excellent dimensional stability and because they have ...

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07-01-2021 дата публикации

Polymer Ammunition and Cartridge Primer Insert

Номер: US20210003373A1
Автор: Lonnie Burrow
Принадлежит: TRUE VELOCITY IP HOLDINGS LLC

The present invention provides polymer ammunition having a primer insert having: a top surface; a bottom surface opposite the top surface; a coupling element that extends from the bottom surface, wherein the coupling element comprises an interior surface and an exterior surface, wherein the interior surface comprises: a transition region that transitions from the bottom surface to a second segment wherein the transition region has a radius of from 0.02 to 0.2; a first segment extending from the second segment and terminates at a tip, wherein the first segment has a first segment distance from 0.02 to 0.18 inches and the second segment has a second segment distance from 0.02 to 0.18 inches, wherein the second segment has a second segment angle from +3 to −3 degrees relative to the first segment angle and the first segment has a first segment angle from +6 to −6 degrees from perpendicular to the top surface; a primer recess in the top surface that extends toward the bottom surface; a primer flash aperture positioned in the primer recess through the bottom surface; and a flash aperture groove in the primer recess and positioned around the primer flash aperture and adapted to receive a polymer overmolding through the primer flash aperture.

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05-01-2017 дата публикации

MAGNETIC COMPOSITE AND METHOD OF MANUFACTURING THE SAME

Номер: US20170004910A1
Автор: KIM In Gyu, Lee Seung Ho
Принадлежит: SAMSUNG ELECTRO-MECHANICS CO., LTD.

A magnetic composite and a method of manufacturing the same are provided. The magnetic composite includes a magnetic material including magnetic material particles and a metal alloy. 1. A magnetic composite comprising:a magnetic material comprising magnetic material particles; anda metal alloy.2. The magnetic composite of claim 1 , wherein the metal alloy is a eutectic alloy.3. The magnetic composite of claim 2 , wherein the eutectic alloy is a binary claim 2 , ternary claim 2 , quaternary claim 2 , or quinary alloy.4. The magnetic composite of claim 2 , wherein the eutectic alloy is an alloy comprising one or more elements selected from a group consisting of indium (In) claim 2 , tin (Sn) claim 2 , cadmium (Cd) claim 2 , bismuth (Bi) claim 2 , silver (Ag) claim 2 , gold (Au) claim 2 , lead (Pb) claim 2 , zinc (Zn) claim 2 , copper (Cu) claim 2 , germanium (Ge) claim 2 , silicon (Si) claim 2 , aluminum (Al) claim 2 , magnesium (Mg) claim 2 , calcium (Ca) claim 2 , and antimony (Sb).5. The magnetic composite of claim 1 , wherein the magnetic material particles are single phase particles dispersed in a binder comprising the metal alloy.6. The magnetic composite of claim 1 , wherein the magnetic material comprises at least one selected from a group consisting of a magnetocaloric material claim 1 , a soft magnetic material claim 1 , and a ferromagnetic material.7. The magnetic composite of claim 1 , wherein the magnetic material is an alloy claim 1 , an oxide claim 1 , or a nitride containing at least one selected from a group consisting of iron (Fe) claim 1 , manganese (Mn) claim 1 , cobalt (Co) claim 1 , nickel (Ni) claim 1 , niobium (Nb) claim 1 , yttrium (Y) claim 1 , lanthanum (La) claim 1 , cerium (Ce) claim 1 , praseodymium (Pr) claim 1 , neodymium (Nd) claim 1 , promethium (Pm) claim 1 , samarium (Sm) claim 1 , europium (Eu) claim 1 , gadolinium (Gd) claim 1 , terbium (Tb) claim 1 , dysprosium (Dy) claim 1 , holmium (Ho) claim 1 , erbium (Er) claim 1 , thulium ( ...

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04-01-2018 дата публикации

METAL MAGNETIC MATERIAL AND ELECTRONIC COMPONENT

Номер: US20180005738A1
Автор: Yamamoto Makoto
Принадлежит: MURATA MANUFACTURING CO., LTD.

Zinc is added to a metal magnetic alloy powder including iron and silicon. An element is formed using this magnetic material, and a coil is formed inside or on the surface of the element. 1. A metal magnetic material , comprisingzinc added to a metal magnetic alloy powder made of iron and silicon.2. A metal magnetic material , comprisingzinc added to a metal magnetic alloy powder made of iron and silicon, and whereina reaction product of the zinc and the metal magnetic alloy powder is generated by a heat treatment.3. A metal magnetic material , comprisingzinc added to a metal magnetic alloy powder made of iron and silicon, and whereina reaction product of the zinc and the metal magnetic alloy powder is generated by a heat treatment so that an oxide of the metal magnetic alloy powder due to the reaction product is present.4. A metal magnetic material , comprisingzinc added to a metal magnetic alloy powder made of iron and silicon, and whereina reaction product of the zinc and the metal magnetic alloy powder is generated by a heat treatment so that the reaction product is formed near a surface of the metal magnetic alloy powder.5. An electronic component , comprisingan element body formed of a metal magnetic material acquired by adding zinc to a metal magnetic alloy powder made of iron and silicon, whereina reaction product of the zinc and the metal magnetic alloy powder is generated in the element body, and whereina coil is formed inside, or on a surface of, the element body.6. An electronic component , comprisingan element body formed of a metal magnetic material acquired by adding zinc to a metal magnetic alloy powder made of iron and silicon, whereina reaction product of the zinc and the metal magnetic alloy powder is precipitated near a surface of the metal magnetic alloy powder, and whereina coil is formed inside, or on a surface of, the element body.7. An electronic component , comprisingan element body formed of a metal magnetic material acquired by adding ...

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07-01-2021 дата публикации

METHOD FOR MANUFACTURING RARE EARTH PERMANENT MAGNET

Номер: US20210005380A1
Принадлежит:

There is provided a method for manufacturing a rare earth sintered magnet having a stable magnetic performance, by uniformly distributing a heavy rear earth element to the surface of the magnet and the grain boundary inside of the magnet by using a mixture of a heavy rare earth compound or a heavy rare earth metal alloy and a rare earth magnet powder, to lower a decrease rate of the magnetic characteristics based on the temperature of the rare earth sintered magnet. 1. A method for manufacturing a rare earth sintered magnet comprising the steps of:preparing a rare earth alloy composed of xwt % RE-ywt % B-zwt % TM-bal.wt % Fe (wherein RE is a rare earth element, TM is a 3d transition element, x=28˜35, y=0.5˜1.5, z=0˜15) and pulverizing the prepared alloy to the size of 1.0˜5.0 μm;preparing a heavy rare earth compound or a heavy rare earth metal alloy and pulverizing the heavy rare earth compound or heavy rare earth metal alloy to the size of 1.0˜5.0 μm;mulling the pulverized rare earth alloy powder and the heavy rare earth compound powder or heavy rare earth metal alloy powder at the ratio of (100−H)wt %:Hwt %, to be mixed;aligning and compacting the mixed powder in a magnetic field, to be magnetized;loading the magnetized mixture powder into a heating furnace and diffusing a heavy rare earth element to a grain boundary of the rare earth alloy under a vacuum or in an inert gas atmosphere;sintering the alloy powder with the diffused heavy rare earth element; andperforming a heat treatment to the sintered alloy.2. The method for manufacturing a rare earth sintered magnet in claim 1 , wherein the heavy rare earth compound is one of the compounds which are Gd-Hydride claim 1 , Gd-Fluoride claim 1 , Gd-Oxide claim 1 , Gd-Oxyfluoride claim 1 , Nd-Hydride claim 1 , Ho-Fluoride claim 1 , Ho-Hydride claim 1 , Dy-Hydride claim 1 , Dy-Fluoride claim 1 , Tb-Hydride and Tb-Fluoride as powders.3. The method for manufacturing a rare earth sintered magnet in claim 1 , wherein the ...

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20-01-2022 дата публикации

A DEVICE FOR REMOVING FLAWS IN SITU DURING THE ADDITIVE PRINTING OF METAL PARTS

Номер: US20220016709A1
Принадлежит: Politecnico di Milano

A device for removing flaws in situ during the additive molding of metal parts forms the subject of the invention. The device comprises: a hopper adapted to contain metal powder; a printing platform, sliding along an axis; a metal powder releasing device, to allow the powder to fall from the hopper onto the printing platform; a doctor blade for distributing the powder onto the printing platform, forming a bed of powder; a laser source and associated laser beam scanning system, for selectively melting the bed of powder; a grinder for removing flawed layers and a monitoring system, configured to detect possible flaws in the layers, wherein said monitoring system is connected to an electronic control unit, configured to activate the aforesaid grinder in order to remove the flaws detected by the monitoring system. 1. A device for removing flaws in metal parts , in situ , said device comprising:a hopper adapted to contain metal powder;a printing platform sliding along an axis;a powder releasing device to allow the powder to fall from the hopper onto the printing platform;a doctor blade for distributing the powder onto the printing platform forming a bed of powder;a laser source for selectively melting the bed of powder; and the device further comprises:a grinder for removing flawed layers; anda monitoring system configured to detect possible flaws in the layers, wherein said monitoring system connected to an electronic control unit configured to activate the aforesaid grinder in order to remove the flaws detected by the monitoring system.2. The device according to claim 1 , wherein the grinder is mounted onto a grinder cart claim 1 , which allows a longitudinal feeding movement of the grinder.3. The device according to claim 1 , wherein the monitoring system comprises at least one sensor configured to inspect a melted pool of material in the bed of powder.4. The device according to claim 1 , wherein the monitoring system comprises at least one sensor outside the optical ...

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12-01-2017 дата публикации

WORKING ADDITIVELY MANUFACTURED PARTS

Номер: US20170008080A1
Автор: Xu JinQuan
Принадлежит:

A method of working an additively manufactured part includes applying a layer of wax to a part manufactured with an additive manufacturing process. Then a mold is formed over the layer of wax on the part. The wax is then removed from between the mold and the part. The part is then melted in the mold, and then the part is re-solidified in the mold. Finally, the mold is removed. 1. A method of working an additively manufactured part , the method comprising:applying a coating to a part manufactured with an additive manufacturing process;forming a mold over the coating on the part;removing the coating between the mold and the part;melting the part in the mold;re-solidifying the part in the mold; andremoving the mold.2. The method of claim 1 , wherein the part is manufactured with an additive manufacturing process selected from the group consisting of direct metal laser sintering claim 1 , electron beam freeform fabrication claim 1 , electron-beam melting claim 1 , selective laser melting claim 1 , selective laser sintering claim 1 , and combinations thereof.3. The method of claim 1 , wherein interior surfaces of the mold have an average surface roughness Requal to or less than 125 microinches (3.2 micrometers).4. The method of claim 3 , wherein interior surfaces of the mold have an average surface roughness Rbetween 60 microinches (1.5 micrometers) and 125 microinches (3.2 micrometers).5. The method of claim 1 , wherein the mold that is formed over the part is a ceramic mold.6. The method of claim 5 , wherein the ceramic mold and the part are placed in a furnace and heated to a temperature that is lower than the melting temperature of the part to sinter the mold.7. The method of claim 6 , wherein the ceramic mold and the part are heated in the furnace to a temperature that is greater than the melting temperature of the part to melt the part in the ceramic mold.8. The method of claim 1 , wherein the part is re-solidified on a chill block to control the crystallization of ...

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12-01-2017 дата публикации

TITANIUM POWDER CONTAINING SOLID-SOLUTED NITROGEN, TITANIUM MATERIAL, AND METHOD FOR PRODUCING TITANIUM POWDER CONTAINING SOLID-SOLUTED NITROGEN

Номер: US20170008087A1
Автор: KONDOH Katsuyoshi
Принадлежит:

A method for producing titanium powder containing a solid-soluted nitorogen comprises the step of heating titanium powder comprised of titanium particles in a nitrogen-containing atmosphere to dissolve nitrogen atoms and form a solid solution of nitrogen atom in a matrix of the titanium particle. 1. A method for producing titanium powder containing a solid-soluted nitrogen , the method comprising:heating titanium powder comprising titanium particles in a nitrogen-containing atmosphere to dissolve nitrogen atoms and form a solid solution of nitrogen atoms in a matrix of the titanium particles.2. The method for producing the titanium powder containing the solid-soluted nitrogen according to claim 1 , whereina heating temperature for forming the solid solution of the nitrogen atoms in the matrix of the titanium particles is 400° C. or more and 800° C. or less.3. A titanium powder containing the solid-soluted nitrogen produced by the method according to whereinthe titanium particles have a nitrogen content of 0.1 mass % or more and 0.65 mass % or less.4. A titanium material formed with the titanium powder containing the solid-soluted nitrogen according to into a predetermined shape.5. The titanium material according to claim 4 , whereinthe titanium material is an extruded material formed by extrusion of the titanium powder containing the solid-soluted nitrogen,the extruded material has a nitrogen content of 0.1 mass % or more and 0.65 mass % or less, andthe extruded material has an elongation to failure of 10% or more.6. The method for producing the titanium powder containing the solid-soluted nitrogen according to claim 1 , wherein the titanium powder is heated for a predetermined period of time to cause the titanium particles in the matrix of titanium particles to have a nitrogen content of 0.1 mass % or more and 0.65 mass % or less claim 1 , the nitrogen content being based claim 1 , at least in part claim 1 , on the predetermined period of time. The present ...

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27-01-2022 дата публикации

POROUS ELECTROLYZER GAS DIFFUSION LAYER AND METHOD OF MAKING THEREOF

Номер: US20220023946A1
Принадлежит:

A porous titanium sheet configured to function as an anode side gas diffusion layer of a proton exchange membrane (PEM) electrolyzer is formed by a powder technique, such as tape casting or powder metallurgy. 1. A porous titanium sheet configured to function as an anode side gas diffusion layer of a proton exchange membrane (PEM) electrolyzer , wherein the porous titanium sheet is formed by a powder technique.2. The porous titanium sheet of claim 1 , wherein a first major side of the porous titanium sheet has a higher porosity than an opposite second major side of the porous titanium sheet.3. The porous titanium sheet of claim 2 , wherein the first major side of the porous titanium sheet is configured to face an anode side flow plate claim 2 , and the second major side of the porous titanium sheet is configured to face an anode electrode.4. The porous titanium sheet of claim 2 , wherein the first major side of the porous titanium sheet has the porosity which is at least 10 percent higher than the opposite second major side of the porous titanium sheet.5. The porous titanium sheet of claim 1 , wherein a first major side of the porous titanium sheet includes a groove and an opposite second major side of the porous titanium sheet has a substantially planar surface which lacks a groove.6. The porous titanium sheet of claim 1 , wherein:the porous titanium sheet contains a titanium nitride coating on at least one surface thereof; andthe porous titanium sheet comprises pure titanium or an alloy of titanium containing more than 50 atomic percent titanium and less than 50 atomic percent of at least one of molybdenum, vanadium, niobium, tantalum, or zirconium.7. The porous titanium sheet of claim 1 , wherein the porous titanium sheet includes a bimodal pore size distribution comprising micropores having an average pore size in a range of 1 to 5 microns claim 1 , and macropores having an average pore size in a range of 30 to 40 microns.8. The porous titanium sheet of claim 1 , ...

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12-01-2017 дата публикации

PROCESS FOR PRODUCING A TARGET FORMED OF A SINTERING-RESISTANT MATERIAL OF A HIGH-MELTING POINT METAL ALLOY, SILICIDE, CARBIDE, NITRIDE OR BORIDE

Номер: US20170009335A1
Автор: Yamakoshi Yasuhiro
Принадлежит:

A target is formed of a sintering-resistant material of high-melting point metal alloy, high-melting point metal silicide, high-melting point metal carbide, high-melting point metal nitride or high-melting point metal boride comprising a structure in which a material formed of a sintering-resistant material of high-melting point metal alloy, high-melting point metal silicide, high-melting point metal carbide, high-melting point metal nitride or high-melting point metal boride and a high-melting point metal plate other than the target are bonded. A production method of such a target is provided. Further the generation of cracks during the target production and high power sputtering, and the reaction of the target raw material with the die during hot pressing can be inhibited effectively, and the warpage of the target can be reduced. 1. A production method of a composite sputtering target including a sputtering target comprising a sintered body formed of a powder of a sinter-resistant material of an alloy of high-melting point metals or a silicide , carbide , nitride or boride of a high-melting point metal , comprising the steps of:placing a secondary plate having a thickness of 2 to 6 mm and made of a high-melting point metal different from the high-melting point metals constituting the alloy or the high melting point metal of the silicide, carbide, nitride or boride of the sputtering target in a die;filling the die with powder formed of the alloy of high-melting point metals or the silicide, carbide, nitride or boride of the high-melting point metal of the sinter-resistant material of the sputtering target, the high-melting point metal or metals of the sputtering target having a melting point of 1700° C. or higher;additionally inserting a further secondary plate made of a high-melting point metal different from the metal or metals of the sputtering target on the filled powder to obtain a trilaminar structure;subsequently subjecting the trilaminar structure to ...

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14-01-2021 дата публикации

EXPEDITIONARY ADDITIVE MANUFACTURING (ExAM) SYSTEM AND METHOD

Номер: US20210008621A1
Принадлежит: Molyworks Materials Corp

An expeditionary additive manufacturing (ExAM) system for manufacturing metal parts includes a mobile foundry system configured to produce an alloy powder from a feedstock, and an additive manufacturing system configured to fabricate a part using the alloy powder. The additive manufacturing system includes a computer system having parts data and machine learning programs in signal communication with a cloud service. The parts data can include material specifications, drawings, process specifications, assembly instructions, and product verification requirements for the part. An expeditionary additive manufacturing (ExAM) method for making metal parts includes the steps of transporting the mobile foundry system and the additive manufacturing system to a desired location; making the alloy powder at the location using the mobile foundry system; and building a part at the location using the additive manufacturing system.

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14-01-2021 дата публикации

BLADE MANUFACTURING METHOD

Номер: US20210008627A1
Принадлежит:

Provided is a blade manufacturing method by which a blade of a stable quality can be manufactured. The present invention involves: a shaping process in which a blade is molded by means of metal injection molding by injecting metal powder toward a mold; a jig attaching process in which a jig serving as a mold, which is divided into at least two parts forming the shape of the blade therebetween, is attached to the blade by sandwiching the blade between the shape-forming surfaces; and a thermal treatment process in which a thermal treatment is applied to the blade to which the jig has been attached. 1. A blade manufacturing method comprising:a molding step of injecting a metal particle toward a mold and shaping a blade through metal injection molding;a jig attaching step of sandwiching the blade between shape-forming surfaces of a jig which is divided into at least two parts and serves as a mold in which a shape of the blade is formed, and attaching the jig to the blade; anda heat treatment step of performing heat treatment on the blade to which the jig is attached.2. The blade manufacturing method according to claim 1 ,wherein in the jig attaching step, a pressing unit that presses the jig in a direction sandwiching the blade is attached to the jig in a state where the jig sandwiches the blade, andin the heat treatment step, the heat treatment is performed in a state where the pressing unit is attached to the jig.3. The blade manufacturing method according to claim 1 ,wherein the metal particle is formed of a titanium aluminum alloy.4. The blade manufacturing method according to claim 1 ,wherein the jig has an insulator layer formed on a surface that comes into contact with the blade. The present invention relates to a blade manufacturing method.Metal injection molding (hereinafter, referred to as MIM as appropriate) is widely used in manufacturing mechanical components since productivity and dimensional accuracy are high. MIM is a processing method for obtaining a ...

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10-01-2019 дата публикации

SINTERED BODY, METHOD OF MANUFACTURING SINTERED BODY, COMBUSTOR PANEL, AND METHOD OF MANUFACTURING COMBUSTOR PANEL

Номер: US20190009340A1
Принадлежит:

By melting a shaping material in which a metal powder and a binder are mixed and by carrying out injection molding (primary shaping) in an injection mold, an injection molded body, or an intermediate shaped body are produced. The injection molded body or the intermediate shaped body is placed by a transfer mold and is subjected to a gravity shaping (secondary shaping) with a transformation. A sintered body is manufactured by carrying out debindering and sintering to the injection molded body. 16-. (canceled)7. A method of manufacturing a sintered body comprising:a debindering process of carrying out a debindering to an injection molded body produced by a primary shaping by injecting into an injection mold a shaping material in which a metal powder and a binder are mixed, to produce an intermediate shaped body;a sintering process of carrying out a sintering to the intermediate shaped body to produce a sintered body; anda secondary shaping process of transforming the injection molded body or the intermediate shaped body before the sintered body is produced.8. The method of manufacturing the sintered body according to claim 7 , wherein the secondary shaping process includes a process of pressing the injection molded body or the intermediate shaped body to a transfer mold by an action of gravity.9. The method of manufacturing the sintered body according to claim 8 , further comprising: 'wherein the debindering process includes carrying out the debindering to the injection molded body in a state that the injection molded body is placed on the transfer mold, to produce the intermediate shaped body,', 'an injection molded body placing process of placing the injection molded body on the transfer mold,'}wherein the secondary shaping process includes heating the intermediate shaped body to a shaping temperature in a state that the intermediate shaped body is placed on the transfer mold, to produce an intermediate shaped body after secondary shaping, andwherein the sintering ...

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09-01-2020 дата публикации

METHOD OF FORMING AN OBJECT USING 3D PRINTING

Номер: US20200009654A1
Принадлежит: Desktop Metal, Inc.

A 3D printer includes a build plate providing a surface on which an object is printed. Prior to printing, a sheet is fixed to the surface of the build plate. The sheet is composed of a material that adheres to a binder component of the feedstock used to print the object. During printing, the first layer of the printed object forms a bond with the sheet, which secures the location of the first layer and resists movement of the object during printing. Following printing and the object gaining sufficient rigidity, the object and sheet can be removed together from the printer. The sheet may then be peeled from the object, and the object can undergo debinding and/or sintering to create a finished object. 120-. (canceled)21. A method of forming an object using additive manufacturing , the method comprising:securing a base sheet to a top surface of a build plate of a three-dimensional (3D) printer, wherein an outer perimeter of the base sheet defines a print area;printing a first layer of a build material, including a metal powder and a binder material, in the print area;printing additional layers of the build material above the first layer layer-by-layer, wherein the first layer and the additional layers collectively form the object; andseparating the base sheet and the object,wherein the base sheet includes at least one component that is also included in the binder material, and wherein the at least one component in the base sheet adheres to the at least one component in the binder material.22. The method according to claim 21 , wherein the separating step includes removing the base sheet from the top surface of the build plate claim 21 , and peeling the base sheet from the object.23. The method according to claim 21 , further comprising:de-binding at least a portion of the binder material from the object after separating the base sheet and the object; andsintering the object.24. The method according to claim 21 , wherein the at least one component includes one or more ...

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09-01-2020 дата публикации

METHOD OF ADDITIVE MANUFACTURING OF COMPONENTS

Номер: US20200009656A1
Принадлежит:

A method of additive manufacturing a component. The method includes selecting powder characterization, depositing powder materials, inspecting the powder materials, selecting process and laser parameters for laser processing, laser processing the powder materials, performing layer cleanup, determining stress state and relieving, additionally inspecting the laser processed powder materials, and repeating steps until a buildup of the component is complete. 18-. (canceled)9. A method of additive manufacturing a component , the method comprising:selecting powder characterization;depositing powder materials for fabricating the component;inspecting, in-situ, the powder materials deposited to determine layer characteristics;selecting process and laser parameters for laser processing based on inspection results;laser processing the powder materials;performing layer cleanup on the laser processed powder materials;additionally inspecting, in-situ, the laser processed powder materials to determine material characteristics;inspecting via ultrasonic measurement process the laser processed powder materials to determine residual stress;upon determining residual stress is less than a threshold, repeating the above steps starting with the depositing step with additional powder materials until a buildup of the component is complete.10. The method of claim 9 , wherein the additional inspecting is via flash thermography utilizing heat powered via the preceding laser processing.11. The method of claim 9 , wherein the deposited powder layer differs in thickness from the deposited additional powder materials layer.12. The method of claim 9 , wherein inspection results identifies unacceptable characteristics claim 9 , and wherein the method further comprises repeating selecting claim 9 , laser processing claim 9 , and performing layer cleanup steps to reduce or eliminate the unacceptable characteristics before continuing on to the inspecting via ultrasonic measurement process step.13. The ...

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09-01-2020 дата публикации

Method and Device for Machining a Workpiece

Номер: US20200009659A1
Автор: Flögel Rupert
Принадлежит:

In a method for machining a workpiece (), the workpiece () is secured to a carrier element () by at least one connecting element () or is produced by a generative production method. In an embedding step, the workpiece () is introduced into a casting mould surrounding the workpiece () and a curing carrier material () surrounding the workpiece () is introduced into the casting mould, such that the workpiece () is embedded and fixed in the carrier material (). In an exposure step, the carrier material () is separated from the workpiece () and the workpiece () is exposed from a side facing the carrier element (), in order, in a subsequent second machining step, for it to be possible to machine the workpiece () partially embedded in the carrier material (). The workpiece () can be produced by a generative production method on the carrier element (), wherein at least one connecting element () that joins the workpiece () to the carrier element () is produced at the same time. Arranged on the carrier element () are protruding positioning elements (), which, when the workpiece () is introduced into the casting mould (), come into engagement with matching recesses in the casting mould, in order to define a position of the carrier element () with the workpiece () secured thereto relative to the casting mould and to allow subsequent referencing of the workpiece (). 121.-. (canceled)22. A method for machining a workpiece which is fixed on a carrier element by at least one connecting element , comprising:an embedding step, in which the workpiece is inserted into a casting mold enclosing the workpiece and a curing carrier material enclosing the workpiece is introduced into the casting mold, so that the workpiece is embedded and fixed in the carrier material;an exposure step, in which the carrier element is separated from the workpiece and the workpiece is exposed from a side facing the carrier element; anda subsequent machining step, in which the workpiece partially embedded in ...

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09-01-2020 дата публикации

SURFACE MODIFIED PARTICULATE AND SINTERED OR INJECTION MOLDED PRODUCTS

Номер: US20200009660A1
Автор: Heikkila Kurt
Принадлежит: Tundra Composites LLC

Disclosed are interfacially modified particulate and polymer composite material for use in injection molding processes, such as metal injection molding and additive process such as 3D printing. The composite material is uniquely adapted for powder metallurgy processes. Improved products are provided under process conditions through surface modified powders that are produced by extrusion, injection molding, additive processes such as 3D printing, Press and Sinter, or rapid prototyping. 124-. (canceled)25. A filament adapted for use in an additive manufacturing system , the system comprising a digitally controlled applicator that can deposit the filament in a controlled x-y plane and in a z-direction filament application to obtain a pre-form object; the filament comprising:(a) about 15 to 1 wt. % of a thermoplastic polymer; and(b) about 99 to 85 wt. % of a ferrous metal particulate, dispersed in the polymer, the particulate having a particle size of less than 500 microns, and an exterior coating of interfacial modifier on the particulate in an amount of about 0.005 to 2 wt. %, all percentages based on the weight of the filament.26. The filament of wherein the metal particulate comprises a blend of a first particle and a second particle with a size ratio of between about 2:1 to 7:1.27. The filament of wherein the first particle as a particle size of 4 to 100μ and the second particle as a particle of 5 to 50μ.28. The filament wherein the filament comprises a stainless steel particulate.29. The filament of wherein the filament comprises the stainless steel particulate dispersed in a polyolefin.30. The filament of wherein the filament comprises a generally circular cross-section with a diameter of about 0.1 to 5 millimeters.31. The filament wherein the interfacial modifier comprises an organometallic compound selected from the group of organo-titanium compound claim 25 , organo-zirconium compound or mixtures thereof.32. A thermoplastic pellet adapted for use in an ...

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12-01-2017 дата публикации

HIGH FREQUENCY INDUCTION HEATING METHOD

Номер: US20170010163A1
Автор: Yamashita Osamu
Принадлежит: TOYOTA JIDOSHA KABUSHIKI KAISHA

A high frequency induction heating method includes: providing a film containing a component, which melts at a preset heating temperature, on a surface of a workpiece before heating the workpiece by high frequency induction heating using a high-frequency coil; and heating the workpiece by high frequency induction heating. 1. A high frequency induction heating method comprising:providing a film containing a component, which melts at a preset heating temperature, on a surface of a workpiece before heating the workpiece by high frequency induction heating using a high-frequency coil; andheating the workpiece by high frequency induction heating.2. The high frequency induction heating method according to claim 1 , whereinthe workpiece is a sintered compact which is a rare earth magnet precursor, andthe sintered compact is heated by high frequency induction heating while performing hot working on the sintered compact.3. The high frequency induction heating method according to claim 1 , whereinthe film is formed of a graphite lubricating liquid and a melting component which is contained in the film.4. The high frequency induction heating method according to claim 3 , whereinthe film is formed by applying a solution, which is obtained by adding the melting component to the graphite lubricating liquid, to the surface of the workpiece and drying the solution.5. The high frequency induction heating method according to claim 1 , whereinthe workpiece has a Nd—Fe—B-based main phase with a nanocrystalline structure and a grain boundary phase of a Nd—X alloy, where X: metal element, the grain boundary phase being present around the main phase.6. The high frequency induction heating method according to claim 5 , whereinthe Nd—X alloy constituting the grain boundary phase is any one of Nd—Co, Nd—Fe, Nd—Ga, Nd—Co—Fe, and Nd—Co—Fe—Ga, or is a mixture of at least two of Nd—Co, Nd—Fe, Nd—Ga, Nd—Co—Fe, and Nd—Co—Fe—Ga; andthe Nd—X alloy is in a Nd rich state. The disclosure of Japanese ...

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14-01-2016 дата публикации

TURBINE WHEEL OF AN EXHAUST GAS TURBOCHARGER AND ASSOCIATED PRODUCTION METHOD

Номер: US20160010457A1
Принадлежит:

A turbine wheel for an exhaust gas turbocharger may include a body composed of a TiAl alloy via at least one of metal injection moulding, selective laser melting and electron beam melting. The body may include a plurality of blades each having an outlet blade root and an outlet blade tip disposed radially away from a rotation axis with respect to the outlet blade root. The body may have a quotient Q of a diameter ddefined by each of the outlet blade tips to a diameter ddefined by each of the oulet blade roots corresponding to the following relationship: Q=d/d 1. A turbine wheel for an exhaust gas turbocharger , comprising: a body composed of a TiAl alloy via at least one of metal injection moulding , selective laser melting and electron beam melting , the body including a plurality of blades each having an outlet blade root and an outlet blade tip disposed radially away from a rotation axis with respect to the outlet blade root , wherein the body has a quotient Q of a diameter ddefined by each of the outlet blade tips to a diameter ddefined by each of the outlet blade roots corresponding to the following relationship:{'br': None, 'i': Q=d', '/d, 'sub': S', 'N, '>3.85.'}2. An exhaust gas turbocharger , comprising: a turbine wheel composed of a TiAl alloy , the turbine wheel including a plurality of blades each having an outlet blade root and an outlet blade tip disposed radially away from a rotation axis with respect to the outlet blade root;{'sub': S', 'N, 'claim-text': {'br': None, 'i': Q=d', '/d, 'sub': S', 'N, '>3.85.'}, 'wherein the turbine wheel has a quotient Q of a diameter ddefined by each of the blade tips to a diameter ddefined by each of the outlet blade roots corresponding to the following relationship4. The method according to claim 3 , wherein the powdered metallurgy process is metal injection moulding claim 3 , and further comprising the steps of debinding and sintering the component.5. The method according to claim 3 , wherein the component is a ...

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11-01-2018 дата публикации

RIBBONS AND POWDERS FROM HIGH STRENGTH CORROSION RESISTANT ALUMINUM ALLOYS

Номер: US20180010216A1
Принадлежит:

Aluminum alloys, fabricated by a rapid solidification process, with high strength, high ductility, high corrosion resistance, high creep resistance, and good weldability. 1. An additively manufactured component manufactured by the method of .2. The method of claim 25 , wherein the alloy comprises a dispersion of nano-precipitates of AlZr with L1crystal structure in the aluminum matrix claim 25 , having an average diameter ranging from about 3 nm to about 50 nm.3. The method of claim 25 , the alloy further comprising about 0.3 to about 1.5% by weight of at least one of titanium claim 25 , hafnium claim 25 , vanadium claim 25 , niobium and tantalum.4. The method of claim 25 , wherein the alloy comprises a dispersion of AlZr primary precipitates claim 25 , having an average diameter ranging from about 0.05 μm to about 1.5 μm.5. (canceled)6. The method of claim 25 , wherein the alloy comprises as an impurity no more than about 0.05 wt. % of any one of scandium claim 25 , erbium claim 25 , thulium claim 25 , ytterbium claim 25 , or lutetium.7. The method of claim 25 , wherein the alloy is thermally stable up to an operating temperature of about 425° C.8. The method of claim 28 , wherein the alloy can be extruded at a thermal working window up to about 450° C.9. (canceled)10. The method of claim 25 , wherein the alloy has a fine grain structure with average grain diameters between about 200 nm and about 2 μm.11. An extruded component manufactured by the method of .12. The extruded component of claim 11 , wherein the extruded component is adapted for use in at least one application selected from a group consisting of aerospace claim 11 , automotive and marine applications.1316-. (canceled)17. A protective coating for magnesium or aluminum components claim 31 , the protective coating being manufactured by the method of .18. (canceled)19. The method of claim 25 , wherein the fabricating step comprises a gas-atomization process.20. An additively manufactured component ...

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12-01-2017 дата публикации

Cu-Ga ALLOY SPUTTERING TARGET AND METHOD FOR PRODUCING SAME

Номер: US20170011895A1
Принадлежит:

According to the present invention, a Cu—Ga alloy sputtering target which is a sintered body has a composition with 29.5 atom % to 43.0 atom % of Ga and a balance of Cu and inevitable impurities. A Cu—Ga alloy crystal particle in the sintered body has a structure in which γ phase particles are dispersed in a γ-phase crystal particle. A method for producing the sputtering target includes a step of performing normal pressure sintering by heating a molded body formed of a powder mixture of a pure Cu powder and a Cu—Ga alloy powder in a reducing atmosphere, and a step of cooling the obtained sintered body at a cooling rate of 0.1° C./min to 1.0° C./min, at a temperature having a range of 450° C. to 650° C. 1. A Cu—Ga alloy sputtering target , whereinthe Cu—Ga alloy sputtering target is a sintered body which has a composition with 29.5 atom % to 43.0 atom % of Ga and a balance of Cu and inevitable impurities, and{'sub': '1', 'a Cu—Ga alloy crystal particle in the sintered body has a structure in which γ phase particles are dispersed in a γ-phase crystal particle.'}2. The Cu—Ga alloy sputtering target according to claim 1 , wherein{'sub': '1', 'an average number of the γ phase particles in one γcrystal particle is 6 to 36, and'}{'sub': '1', 'an average particle diameter of γphase particles is 15.0 μm to 75.0 μm.'}3. The Cu—Ga alloy sputtering target according to claim 1 , whereinan amount of oxygen in the sintered body is equal to or less than 200 mass ppm.4. The Cu—Ga alloy sputtering target according to claim 1 , whereinthe sintered body further contains 0.05 atom % to 10.0 atom % of Na, anda Na compound phase is dispersed in the sintered body.5. The Cu—Ga alloy sputtering target according to claim 4 , wherein{'sub': 2', '2', '3', '6, 'the Na compound phase is formed of at least one of NaF, NaS, NaSe, and NaAlF.'}6. A method for producing the Cu—Ga alloy sputtering target according to claim 1 , the method comprising:a step of performing normal pressure sintering by ...

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10-01-2019 дата публикации

R-T-B-Ga-BASED MAGNET MATERIAL ALLOY AND METHOD OF PRODUCING THE SAME

Номер: US20190013122A1
Принадлежит:

Disclosed is an R-T-B—Ga-based magnet material ahoy where R is at least one element selected from rare earth metals including Y and excluding Gd, Tb, Dy, Ho, Er, TM, Yb, and Lu, and Tis one or more transition metals with Fe being an essential element. The R-T-B—Ga-based magnet material alloy includes: an RTB phase which is a principal phase, and an R-rich phase ( and ) which is a phase enriched with the R, wherein a non-crystalline phase in the R-rich phase has a Ga content (mass %) that is higher than a Ga content (mass %) of a crystalline phase in the R-rich phase. With this, it is possible to enhance the magnetic properties of rare earth magnets that are manufactured from the alloy and reduce variations in the magnetic properties thereof. 1. An R-T-B—Ga-based magnet material alloy (where R is at least one element selected from rare earth metals including Y and excluding Gd , Tb , Dy , Ho , Er , Tm , Yb , and Lu , and Tis one or more transition metals with Fe being n essential element) , the R-T-B—Ga-based magnet material alloy , comprising:{'sub': 2', '14, 'an RTB phase which is a principal phase; and'}an R-rich phase which is a phase enriched with the R, the R-rich phase including a on-crystalline phase and a crystalline phase, the non-crystalline phase having a Ga content in mass % that is higher than a Ga content in mass % of the crystalline phase.2. The R-T-B—Ga-based magnet material alloy according to claim 1 , wherein the R-T-B—Ga-based magnet material alloy has an average claim 1 , thickness in a range of 0.1 mm to 1.0 mm. The present invention relates to an alloy for use as a rare earth magnet material and a method of producing the same. More particularly, the present invention relates to an R-T-B—Ga-based magnet material alloy and a method of producing the same capable of enhancing the magnetic properties of rare earth magnets that are manufactured from the alloy and reducing variations in the magnetic properties thereof.R-T-B-based alloys, which exhibit ...

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03-02-2022 дата публикации

METHOD FOR PRODUCING A PISTON

Номер: US20220032371A1
Принадлежит:

The present invention relates to a method for producing a piston () for an internal combustion engine from a piston upper part () and a piston lower part (). 1. A method for producing a piston for an internal combustion engine , the method comprising:producing a piston upper part including a piston top, at least part of a ring section, and at least part of a cooling channel;producing a piston lower part and closing the part of the cooling channel arranged in the piston upper part via an additive method; 'wherein finish-machining the piston includes producing at least one annular groove in a ring support for receiving a piston ring.', 'finish-machining the piston; and'}2. The method according to claim 1 , wherein producing the upper piston part includes at least one of forging and casting the ring support into the piston upper part claim 1 , and wherein the ring support forms the annular groove.3. The method according to claim 1 , further comprising claim 1 , prior to producing the piston lower part via the additive method claim 1 , facing the piston upper part at least on a side facing the piston lower part.4. The method according to claim 1 , wherein producing the piston lower part via the additive method includes forming a second part of the cooling channel in a region of the piston lower part claim 1 , the second part of the cooling channel having a rougher surface than the part of the cooling channel arranged in the piston upper part claim 1 , wherein the rougher surface of the second part of the cooling channel is produced via the additive method.5. The method according to claim 1 , wherein the cooling channel has a non-rotationally symmetrical shape with respect to at least one of a piston vertical axis and a piston transverse axis.6. The method according to claim 1 , wherein producing the piston lower part via the additive method includes producing claim 1 , via the additive method claim 1 , a second part of the cooling channel in a region of the piston lower ...

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03-02-2022 дата публикации

Injection apparatus

Номер: US20220032520A1
Принадлежит: Japan Steel Works Ltd

An injection piston drives a screw. An injection hydraulic cylinder drives the injection piston and is partitioned into first and second chambers. A first oil discharge port is disposed in the injection hydraulic cylinder to be blocked by a piston part when the piston part of the injection piston advances to a pressure-holding switching position, and discharges hydraulic oil from the second chamber. A second oil discharge port is disposed in the injection hydraulic cylinder to be capable of discharging hydraulic oil from the second chamber regardless of the position of the injection piston. The injection piston has first and second members. The joint of the first and second members is disposed at a position separated from an end of the piston part on a side of the second chamber by a predetermined distance.

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19-01-2017 дата публикации

Magnesium base alloy tube and its manufacturing method

Номер: US20170014881A1
Принадлежит: Gohsyu Corp

[Problem] To present a small-diameter magnesium base alloy tube and its manufacturing method of long length, high dimensional precision, and excellent mechanical properties. [Solving Means] A raw material 1 of aluminum base alloy is extruded and formed by using a forming pattern comprising an upper pattern 2 having plural through-holes 21 for supplying the raw material into diaphragms of equal angles on the circumference and circular cylindrical protrusions 22 positioned in the center of plural through-holes 21 so as to be surrounded by plural through-holes 21 at the exit side of the through-holes 21, and a lower pattern 3 positioned in the concave portions commonly penetrating at the exit of the plural through-holes 21 of the upper pattern 2, having through-holes 32 for inserting the protrusions of circular circumference of the upper pattern by providing a tube forming gap, positioned in the center of concave portions 31 of the concave portions 31 in the circular columnar shape of the upper pattern 2.

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19-01-2017 дата публикации

METHOD FOR MANUFACTURING A LINE COMPONENT

Номер: US20170014887A1
Принадлежит:

According to the manufacturing method of the invention the line component. In particular an additively fabricated line component, comprises a line element for conducting a fluid from a first opening to a second opening, and a line branching connected with the line element for conducting the fluid to a third opening, wherein an outer region of the line component is designed load-compliant by means of a numerical optimization program and thereby includes a multitude of irregular topological structures in its outer region. In the manufacturing method of the line component a notch is incorporated on the inside of the line element, which serves to relieve a tension in a highly loaded state of the line component or the line element, a particle-filled gas stream is guided through the interior of the line component, in order to smooth the inside of the line component and/or the line component is subjected to a pressurization, in order to produce a plastic deformation on an inner surface of the line component. 1. A method for manufacturing a line component for conducting a fluid , the line component comprising:a line element for conducting a fluid from a first opening to a second opening, anda line branching connected with the line element for conducting the fluid to a third opening, whereinan outer region of the line component is designed load-compliant by means of a numerical optimization program and thereby includes a multitude of irregular topological structures in its outer region,wherein in the manufacturing method:a notch is incorporated on the inside of the line element, which serves to relieve a tension in a highly loaded state of the line component or the line element,a particle-filled gas stream is guided through the interior of the line component, in order to smooth the inside of the line component, and/orthe line component is subjected to a pressurization, in order to produce a plastic deformation on an inner surface of the line componentwherein the line ...

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19-01-2017 дата публикации

METHOD FOR REINFORCING METAL MATERIAL BY MEANS OF GRAPHENE

Номер: US20170014908A1

A method of reinforcing a metallic material includes adding graphene to an alcohol solution; subjecting the alcohol solution containing graphene to sonication; mixing a metal powder with the alcohol solution containing graphene; milling the metal powder and alcohol solution containing graphene mixture; drying the metal powder and alcohol solution containing graphene mixture to form a composite powder; subjecting the composite powder to a densification process followed by a hot isostatic pressing treatment to form a composite material; and molding the composite material by hot extrusion. 1. A method of reinforcing a metallic material , comprising:adding graphene to an alcohol solution;subjecting the alcohol solution containing graphene to sonication;mixing a metal powder with the alcohol solution containing graphene;milling the metal powder and alcohol solution containing graphene mixture;drying the metal powder and alcohol solution containing graphene mixture to form a composite powder;subjecting the composite powder to a densification process followed by a hot isostatic pressing treatment to form a composite material; andmolding the composite material by hot extrusion.2. The method of claim 1 , wherein the alcohol solution containing graphene is sonicated for about 30 minutes.3. The method of claim 1 , wherein a ratio of mass of metal powder added to a volume of the alcohol containing graphene solution is about 10:1 to 0.5:1.4. The method of claim 1 , wherein the densification process comprises:loading the composite powder into a sheath,vacuumizing the composite powder in the sheath; and{'sup': '−3', 'sealing the sheath by welding with the composite powder inside when the pressure reaches 1.0×10Pa.'}5. The method of claim 1 , wherein the hot isostatic pressing treatment is performed at 480° C. and 110 MPa for two hours.6. The method of claim 1 , wherein the molding by hot extrusion occurs at a temperature of 440° C. to 480° C. The present invention is a method of ...

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19-01-2017 дата публикации

METHOD FOR MANUFACTURING ADDITIVE MANUFACTURED OBJECT, AND MIXED MATERIAL

Номер: US20170014909A1
Принадлежит: KABUSHIKI KAISHA TOSHIBA

A method for manufacturing an additive manufactured object according embodiments includes supplying a powdered first material capable of being melted or sintered by irradiation with energy rays; supplying a powdered second material through which the energy rays are transmitted; melting or sintering the first material by irradiation with the energy rays; and solidifying the first material after melting or solidifying the first material by sintering. 1. (canceled)2. A method for manufacturing an additive manufactured object , the method comprising:supplying a powdered first material capable of being melted or sintered by irradiation with energy rays;supplying a powdered second material having absorptivity of the energy rays lower than the first material; andmelting or sintering the first material by irradiation with the energy rays, whereinthe first material and the second material are adjacent to each other.3. The method according to claim 2 , whereinthe supplying of the first material includes supplying the first material, andthe supplying of the second material includes supplying the second material to a second region adjacent to the first region.4. The method according to claim 3 , whereinthe first material includes a plurality of different first materials,the supplying of the first material includes the plurality of different first materials to the first region.5. The method according to claim 3 , wherein the first region claim 3 , and a third region being a part of the second region and being adjacent to the first region are irradiated with the energy rays claim 3 , in the melting or sintering of the first material.6. The method according to claim 2 , wherein the second material is removed claim 2 , after solidifying the first material after melting the first material claim 2 , or after sintering the first material.7. (canceled)8. A method for manufacturing an additive manufactured object claim 2 , the method comprising:supplying a powdered first material ...

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18-01-2018 дата публикации

Three-Dimensional Shaping Device

Номер: US20180015541A1
Принадлежит:

In a three-dimensional shaping device, a region of an elevatable/lowerable table for forming a powder layer and a region of a powder supply device are divided by a shield plate, an inert gas injection port is provided in the former region, the shield plate can be freely opened or closed so that a powder spraying squeegee traveling on the table is passed through, or a pipe which supplies powder from the powder supply device to the powder spraying squeegee which has traveled to the side of the shield plate penetrates through the shield plate, or a part of the shield plate is the powder supply port for the powder spraying squeegee which has traveled to the side of the shield plate and the pipe protrudes at a lower part and a sintering device applies a laser beam via a transparent region in a ceiling of a chamber. 1. A three-dimensional shaping device , comprising:at least one chamber,a region of an elevatable/lowerable table for forming a powder layer within the at least one chamber and a vicinity thereof,a region of a powder supply device and a vicinity thereof,a shield plate which divides the region of the elevatable/lowerable table from the region of the powder supply device,an inert gas injection port provided in the region of the elevatable/lowerable table,a powder spraying squeegee,the shield plate is constructed to be freely opened or closed so that the powder spraying squeegee traveling across the table is adapted to pass through the shield plate,a sintering device which applies a laser beam to a shaping region of a three-dimensional shaped article on the table via a transparent region in a ceiling of the at least one chamber,a horizontal-direction drive mechanism for the powder spraying squeegee, and a) a region of the horizontal-direction drive mechanism for the powder spraying squeegee and a vicinity thereof and', 'b) the region of the table and the vicinity thereof., 'the shield plate divides2. A three-dimensional shaping device , comprising:at least one ...

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18-01-2018 дата публикации

Method of Making Machine Component with Aluminum Alloy Under Temperature-Limited Forming Conditions

Номер: US20180015545A1
Принадлежит: CATERPILLAR INC.

A method of making a machine component includes extruding a supply of an aluminum alloy to produce an extrusion. The extrusion is formed under temperature-limited forming conditions of 275° C. or less to produce a blank. The blank is machined to at least one predetermined tolerance to produce the machine component. 1. A method of making a machine component , the method comprising:extruding a supply of an aluminum alloy to produce an extrusion;forming the extrusion under temperature-limited forming conditions of 275° C. or less to produce a blank;machining the blank to at least one predetermined tolerance to produce the machine component.2. The method of claim 1 , further comprising:producing the supply of the aluminum alloy via a rapid solidification process.3. The method of claim 2 , wherein the rapid solidification process comprises melt spinning.4. The method of claim 2 , wherein the rapid solidification process includes producing a ribbon of the aluminum alloy and chopping the ribbon of the aluminum alloy to form a plurality of flakes claim 2 , and wherein the plurality of flakes is extruded to produce the extrusion.5. The method of claim 1 , wherein the aluminum alloy includes aluminum and at least one strengthening metal.6. The method of claim 1 , wherein the aluminum alloy includes aluminum and up to 3.5 percent by weight of at least one element of a first group of elements claim 1 , the first group of elements consisting of Si claim 1 , Sc claim 1 , Ti claim 1 , V claim 1 , Cr claim 1 , Mn claim 1 , Fe claim 1 , Ni claim 1 , Cu claim 1 , Y claim 1 , Zr claim 1 , Mo claim 1 , Ce claim 1 , Nd claim 1 , Er claim 1 , Yb claim 1 , Ta claim 1 , W.7. The method of claim 6 , wherein the aluminum alloy includes between 3.5 percent and 9 percent by weight of at least one element of a second group of elements claim 6 , the second group of elements consisting of Ti and V.8. The method of claim 7 , wherein the aluminum alloy includes between 3.5 percent and 8.5 percent ...

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18-01-2018 дата публикации

METHOD FOR THE PRODUCTION OF A SINTERED GEAR

Номер: US20180015546A1
Принадлежит: MIBA SINTER AUSTRIA GMBH

The invention relates to a method for producing a sintered gear comprising a gear body on which at least one elastomer element is arranged, according to which a green compact is produced by pressing a powder, the green compact is sintered into a gear body and is hardened by carburization and subsequent quenching or sinter-hardening and subsequent quenching with a gas and afterwards the at least one elastomer element is vulcanized onto the gear body. 1. A method for producing a sintered gear comprising a gear body on which at least one elastomer element is arranged , according to which a green compact is produced by pressing a powder , the green compact is sintered into a gear body and is hardened by carburization and subsequent quenching or sinter-hardening and subsequent quenching and after this the at least one elastomer element is vulcanized onto the gear body , wherein the hardened gear body is quenched with a gas.2. The method as claimed in claim 1 , wherein the carburization of the gear body is performed by means of low-pressure carburization.3. The method as claimed in claim 1 , wherein a sinter-hardenable powder is used to produce the green compact.4. The method as claimed in claim 3 , wherein a sinter-hardenable powder is used which includes a proportion of chromium which is between 1 wt. % and 5 wt. %.5. The method as claimed in claim 1 , wherein the gear body is compacted to a density of between 6.8 g/cmand 7.4 g/cm.6110. The method as claimed in claim 1 , wherein the gear body is produced to have a roughness depth on its surface which is Rz and Rz.7. The method as claimed in claim 1 , wherein the carburization is performed to a depth of the gear body claim 1 , measured from its surface claim 1 , which is selected from a range of 100 μm to 2000 μm.8. The method as claimed in claim 1 , wherein the gas quenching is performed with N2 claim 1 , N2/H2 or He as the gas.9. The method as claimed in claim 1 , wherein the gear body is quenched at a quenching speed ...

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17-01-2019 дата публикации

GOLF HEAD AND MANUFACTURING METHOD THEREOF

Номер: US20190015709A1
Автор: CHEN Changchun
Принадлежит:

Disclosed is a golf head, comprising a head body and a weight balancing block welded onto the head body which is made of tungsten, nickel and copper and welded onto the titanium alloy head body which can prevent a brittle phase and increase the service life of the golf head; further, the head body is provided with a chamber in which the weight balancing block is placed, the weight balancing block has a surface provided with a welding bead groove towards an inner surface of the chamber which can prevent welding flux from falling off and thus increase welding stability of the weight balancing block. Further disclosed is a method of manufacturing the golf head, by metal injection moulding, the weight balancing block can be made into various complicated shapes matched with the shape of head body, with less moulding process, smooth moulding surface, high flatness and high production efficiency. 13.-. (canceled)5. The method of manufacturing the golf head according to claim 4 , wherein the binder in step A comprises polyformaldehyde claim 4 , high density polyethylene claim 4 , ethylene-vinyl acetate claim 4 , wax and stearic acid.6. The method of manufacturing the golf head according to claim 5 , wherein the step D comprises:step D1: discharging air in the catalytic degreasing furnace and filling nitrogen into the catalytic degreasing furnace; andstep D2: filling concentrated nitric acid after gas atomization into the furnace to decompose and discharge partial polyformaldehyde in the workblank of the weight balancing block in step C.7. The method of manufacturing the golf head according to claim 6 , wherein the catalyzing and degreasing is conducted at a temperature of 100 to 130° C. for 15 to 24 h.8. The method of manufacturing the golf head according to claim 5 , wherein the step E comprises:step E1, gasifying and discharging residual polyformaldehyde in the workblank after degreasing and other materials in the binder under a sintering temperature below 800° C.;step E2 ...

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