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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 9049. Отображено 100.
10-11-2016 дата публикации

Установка для диффузионной сварки и пайки

Номер: RU0000165822U1

Установка для диффузионной сварки и пайки, содержащая установленную на основание колпаковую камеру, верхнюю плиту, опирающуюся на две колонны, вынесенные за пределы камеры, а также гидропривод, включающий силовой гидроцилиндр, смонтированный на верхней плите с возможностью воздействия штоком на охлаждаемый шток механизма сжатия, расположенный под штоком силового гидроцилиндра соосно последнему, отличающаяся тем, что она снабжена тензодатчиком, размещенным между штоком силового гидроцилиндра и штоком механизма сжатия и оснащена двумя возвратными гидроцилиндрами, смонтированными на фланце штока механизма сжатия, причем гидропривод содержит автоматизированную гидросистему управления силовым гидроцилиндром, включающую гидронасос и соответствующий по расходу насоса пропорциональный предохранительный клапан, размещенный между гидронасосом и гидрораспределителем. РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 165 822 U1 (51) МПК B23K 20/14 (2006.01) B23K 20/26 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ТИТУЛЬНЫЙ (21)(22) Заявка: ЛИСТ ОПИСАНИЯ ПОЛЕЗНОЙ МОДЕЛИ К ПАТЕНТУ 2015157054/02, 29.12.2015 (24) Дата начала отсчета срока действия патента: 29.12.2015 (72) Автор(ы): Лисовский Николай Павлович (RU) Приоритет(ы): (22) Дата подачи заявки: 29.12.2015 (45) Опубликовано: 10.11.2016 Бюл. № 31 1 6 5 8 2 2 R U (57) Формула полезной модели Установка для диффузионной сварки и пайки, содержащая установленную на основание колпаковую камеру, верхнюю плиту, опирающуюся на две колонны, вынесенные за пределы камеры, а также гидропривод, включающий силовой гидроцилиндр, смонтированный на верхней плите с возможностью воздействия штоком на охлаждаемый шток механизма сжатия, расположенный под штоком силового гидроцилиндра соосно последнему, отличающаяся тем, что она снабжена тензодатчиком, размещенным между штоком силового гидроцилиндра и штоком механизма сжатия и оснащена двумя возвратными гидроцилиндрами, смонтированными на фланце штока механизма сжатия, причем гидропривод ...

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26-01-2012 дата публикации

Process for joining carbon steel part and zirconia ceramic part and composite articles made by same

Номер: US20120021245A1

A process for joining a carbon steel part and a zirconia ceramic part, comprising steps of: providing a metal part made of carbon steel, a ceramic part made of zirconia ceramic, and a titanium foil; bringing the metal part, ceramic part, and titanium foil into contact, with the titanium foil inserted between the metal part and ceramic part; applying a joining pressure of about 10˜50 MPa to the parts to be joined; and simultaneously applying a pulse electric current to the parts while the joining pressure is applied for heating up the parts to a joining temperature of about 800° C. to about 1100° C. at a rate of about 50˜600° C./min, maintaining the joining temperature for about 10˜50 minutes.

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09-02-2012 дата публикации

Bonding unit control unit and multi-layer bonding method

Номер: US20120031557A1
Принадлежит: Mitsubishi Heavy Industries Ltd

A multi-layer bonding method of the present invention includes: forming a first bonded substrate by bonding a first substrate and an intermediate substrate in a bonding chamber; conveying a second substrate inside said bonding chamber when said first bonded substrate is arranged inside said bonding chamber; and forming a second bonded substrate by bonding said first bonded substrate and said second substrate in said bonding chamber. According to such a multi-layer bonding method, the upper-side substrate can be bonded with an intermediate substrate and then a first bonded substrate is bonded with a lower-side substrate without taking out the first bonded substrate from the bonding chamber. For this reason, a second bonded substrate can be produced at high speed and at a low cost.

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09-02-2012 дата публикации

Low deflection bi-metal rotor seals

Номер: US20120032404A1
Принадлежит: Dresser Rand Co

A seal assembly for use in a turbomachine is provided. The seal assembly has an annular division wall with outside and inside surfaces, a carrier ring disposed adjacent the inside surface of the annular division wall, and a sealing substrate metallurgically-bonded to an inner-most surface of the carrier ring. The sealing substrate is machined to form a seal surface that can be disposed proximate a rotor and maintained substantially parallel thereto during operation of the turbomachine.

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19-07-2012 дата публикации

Laminate armor and related methods

Номер: US20120180630A1
Принадлежит: Battelle Energy Alliance Llc

Laminate armor and methods of manufacturing laminate armor are disclosed. Specifically, laminate armor plates comprising a commercially pure titanium layer and a titanium alloy layer bonded to the commercially pure titanium outer layer are disclosed, wherein an average thickness of the titanium alloy inner layer is about four times an average thickness of the commercially pure titanium outer layer. In use, the titanium alloy layer is positioned facing an area to be protected. Additionally, roll-bonding methods for manufacturing laminate armor plates are disclosed.

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09-08-2012 дата публикации

Tin-silver bonding and method thereof

Номер: US20120199635A1
Принадлежит: National Central University

A Sn—Ag bonding and a method thereof are revealed. By means of a bonding layer formed by tin and silver between wafers, the stress released by diffusion and bonding between tin(Sn) and silver(Ag) is larger than the stress released by diffusion and bonding of conventional gold-silver bonding. Moreover, a Sn—Ag bonding method of the present invention forms Sn—Ag bonding at low temperature and releases more stress so as to reduce thermal stress generated during wafer bonding effectively. And after wafer bonding, the high temperature processes can be performed.

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10-01-2013 дата публикации

Joined heterogeneous materials and joining method therefor

Номер: US20130011183A1
Принадлежит: Honda Motor Co Ltd

Disclosed is a joined heterogeneous material in which a carbon steel material ( 11 ) and an aluminum material ( 12 ) have joined via friction-stir welding. The region of a weld zone ( 15 ) with a low lift-up amount in a plastic flow area ( 17 ) created during friction-stir welding is located on one side of the aluminum material ( 12 ) with respect to the weld zone ( 15 ), created by a welding probe ( 14 ). The region of the weld zone ( 15 ) with a high plastic flow area ( 17 ) lift-up amount is located on the other side of the aluminum material ( 12 ).

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13-06-2013 дата публикации

Method and arrangement for welding electrical conductors

Номер: US20130146644A1
Принадлежит: SCHUNK SONOSYSTEMS GMBH

A method and apparatus for welding lines having metallic braids or strands to form an end node or transit node by introducing a first portion of each line into a compression space of an ultrasonic welding apparatus, wherein the first portions run along a straight line, wherein at least one line has a component at a distance from the end node or transit node to be welded, and at least the line which has the component is attenuated between the compression space and the contact element in a second portion by a change in profile of the line which is imposed using a deflection device. To this end, the line which has the component is oriented in extension of the straight line.

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15-08-2013 дата публикации

METAL BONDING METHOD

Номер: US20130206821A1
Принадлежит: SANYO ELECTRIC CO., LTD.

After a first coating portion formed on a bonding face of a first bonding portion and a second coating portion formed on a bonding face of a second bonding portion are removed by reverse sputtering, copper sputtering is performed to form first and second copper films. The gap between the oxide film on the outermost face of the first copper film and the oxide film on the outermost face of the second copper film is filled with a solution into which copper oxide can be eluted, thereby eluting copper oxide contained in the oxide film in the solution. By applying pressure and heat, the components contained in the solution are removed except for copper, thereby bonding the outermost face of the first copper film and the outermost face of the second copper film to each other by means of copper solid-phase diffusion. 1. A metal bonding method comprising:preparing a first bonding portion containing, as a principal component, a metal component other than copper or an inorganic compound, and a second bonding portion containing, as a principal component, a metal component that is the same as or otherwise differs from the metal component that is a principal component of the first bonding portion;forming a copper film on an exposed face of the first bonding portion and on an exposed face of the second bonding portion;filling a gap between the copper film formed on the first bonding portion and the copper film formed on the second bonding portion with a material into which copper oxide can be eluted; andapplying pressure to the first bonding portion and the second bonding portion so as to reduce the distance between them, thereby bonding the first bonding portion and the second bonding portion via copper.2. A metal bonding method according to claim 1 , further comprising heating the first bonding portion and the second bonding portion before pressure is applied to the first bonding portion and the second bonding portion claim 1 , during a period of time in which pressure is ...

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29-08-2013 дата публикации

BURRING APPARATUS FOR FRICTION WELDING MACHINE

Номер: US20130221070A1
Принадлежит: NITTAN VALVE CO., LTD.

A burring apparatus for a friction welding machine comprises a clamp unit provided at the front end of a horizontal main spindle, for holding work piece W coaxial with the main spindle, a clamp unit provided at the front end of a slide movable to and away from the main spindle in the direction of the axis of the main spindle and a doughnut-shaped cutter for shearing off a burr. Work piece W is moved forward together with the slide until work piece W comes into contact with work piece W so that the mated ends of work pieces W and W are friction welded together to form a joint work piece W. The burr formed on the jointed work piece W is sheared off by the cutter. The jointed work piece W is then liberated from the main spindle. 1. A burring apparatus for a friction welding machine that includes: a horizontally arranged main spindle; a first work holding , provided at the front end portion (nose) of the main spindle , for gripping a first rod shape work piece coaxially with the main spindle; a slide movable to and away from the main spindle along the axis of the main spindle; and a second work holding , arranged at the front end of the slide in opposition to the nose of the main spindle , for gripping a second rod shape work piece of the same diameter as the first rod shape work piece coaxially with the first rod shape work piece , the friction welding machine adapted to friction weld the first and second rod shape work pieces by pressing one end of the second rod shape work piece gripped by the slide onto one end of the first rod shape work piece while the first rod shape work piece is in rotation together with the main spindle , the burring apparatus characterized by comprising a doughnut shape cutter having an inner diameter slightly larger than the outer diameter of the rod shape work pieces , and movable in the axial direction of the main spindle , the doughnut shape cutter arranged in a region ahead of the main spindle and the first rod shape work piece gripped ...

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05-09-2013 дата публикации

METHODS AND SYSTEMS FOR ALIGNING TOOLING ELEMENTS OF ULTRASONIC BONDING SYSTEMS

Номер: US20130228611A1
Принадлежит: Orthodyne Electronics Corporation

A method of aligning a subject tooling element of a material handling system of an ultrasonic bonding system is provided. The method includes the steps of: a) providing an overlay defining a relative position of at least a portion of a reference tooling element; b) viewing an image of at least a portion of the subject tooling element combined with a corresponding portion of the overlay; and c) adjusting a position of at least a portion of the subject tooling element by referring to the overlay in the image. 1. A method of aligning a subject tooling element of a material handling system of an ultrasonic bonding system , the method comprising the steps of:a) providing an overlay defining a relative position of at least a portion of a reference tooling element;b) viewing an image of at least a portion of the subject tooling element combined with a corresponding portion of the overlay; andc) adjusting a position of at least a portion of the subject tooling element by referring to the overlay in the image.2. The method of wherein step a) includes providing the overlay defining the relative position of at least the portion of the reference tooling element with respect to at least one reference position of a reference material handling system.3. The method of wherein the at least one reference position is a position of at least one of (1) a portion of a rail member of the reference material handling system claim 2 , and (2) a portion of a riser member of the reference material handling system configured for raising a workpiece in connection with an ultrasonic bonding operation.4. The method of wherein step a) includes providing the overlay defining the relative position of at least the portion of the reference tooling element with respect to at least one reference position of a workpiece positioned by a material handling system of the ultrasonic bonding system.5. The method of wherein step a) includes providing the overlay defining the relative position of at least the ...

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31-10-2013 дата публикации

METAL BONDING APPARATUS

Номер: US20130284794A1
Принадлежит: SANYO ELECTRIC CO., LTD.

The metal bonding apparatus comprises: a solution supply unit configured to supply a solution which is able to elute an oxide with copper oxide as a principal component, to at least one of a first bonding portion and a second bonding portion; a pressing unit configured to apply pressure to the first bonding portion and the second bonding portion so as to sandwich the solution between the first bonding portion and the second bonding portion, and in a direction in which a distance between the first bonding portion and the second bonding portion is reduced; and a heating unit configured to heat the first bonding portion and the second bonding portion, wherein the first bonding portion and the second bonding portion are bonded by the pressure applied by the pressing unit and the heat from the heating unit. 1. A metal bonding apparatus comprising:a solution supply unit configured to supply a solution which is able to elute an oxide with copper oxide as a principal component, to at least one of a first bonding portion and a second bonding portion;a pressing unit configured to apply pressure to the first bonding portion and the second bonding portion so as to sandwich the solution between the first bonding portion and the second bonding portion, and in a direction in which a distance between the first bonding portion and the second bonding portion is reduced; anda heating unit configured to heat the first bonding portion and the second bonding portion,wherein the first bonding portion and the second bonding portion are bonded by the pressure applied by the pressing unit and the heat from the heating unit.2. A metal bonding apparatus according to claim 1 ,wherein the first bonding portion comprises a first base portion formed of a metal with copper as a principal component and the first coating portion formed of an oxide with copper oxide as a principal component and configured to coat a surface of the first base portion,wherein the second bonding portion comprises a second ...

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07-11-2013 дата публикации

SYSTEMS AND METHODS FOR PROCESSING RIBBON AND WIRE IN ULTRASONIC BONDING SYSTEMS

Номер: US20130292456A1
Автор: Safavi Ardebili Vahid
Принадлежит: Orthodyne Electronics Corporation

An ultrasonic bonding system is provided. The system includes: a) a bond head assembly carrying an ultrasonic bonding tool; b) a conductive material supply; c) a conductive material feeding system for guiding a length of the conductive material supply to a position proximate the ultrasonic bonding tool; and d) a vapor generation system for supplying a vapor proximate the ultrasonic bonding tool, the vapor including a carrier gas and a lubricating vapor. 1. An ultrasonic bonding system comprising:a) a bond head assembly carrying an ultrasonic bonding tool;b) a conductive material supply;c) a conductive material feeding system for guiding a length of the conductive material supply to a position proximate the ultrasonic bonding tool; andd) a vapor generation system for supplying a vapor proximate the ultrasonic bonding tool, the vapor including a carrier gas and a lubricating vapor.2. The ultrasonic bonding system of wherein the lubricating vapor comprises methanol.3. The ultrasonic bonding system of wherein the carrier gas includes at least one of compressed air claim 1 , nitrogen claim 1 , and argon.4. The ultrasonic bonding system of wherein the vapor generation system includes a bubbler feeding the vapor to an outlet proximate the ultrasonic bonding tool.5. The ultrasonic bonding system of wherein the outlet is carried by the bond head assembly.6. The ultrasonic bonding system of wherein the vapor generation system supplies the vapor within a vapor containment structure claim 1 , the vapor containment structure substantially enclosing the bond head assembly.7. The ultrasonic bonding system of wherein the conductive material supply includes at least one of a conductive ribbon supply and a wire supply.8. An ultrasonic bonding system comprising:a) a bond head assembly carrying an ultrasonic bonding tool;b) a conductive material supply;c) a conductive material feeding structure for guiding a length of a conductive material from the conductive material supply to a ...

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07-11-2013 дата публикации

METHOD OF MAKING A METAL-STRIP LAMINATE

Номер: US20130295443A1
Автор: STUTH Bernhard
Принадлежит:

A metal laminate is made by first laying at least one first metal strip of at least one first metal having a thickness of 40 μm to 750 μm on at least one second metal strip of a second metal different from the first metal to form a multilayer stack having a total thickness between 2 mm and 15 mm. Then the first and second strips of the multilayer stack are bonded together by rolling. Finally a finished laminate is formed by reducing a thickness of the bonded-together first and second strips by rolling in at least one pass such that the one first metal strip has a thickness of 0.5 to 10 μm. 1. A method of making a metal laminate , the method comprising the steps of sequentially:a) laying at least one first metal strip of at least one first metal having a thickness of 40 μm to 750 μm on at least one second metal strip of a second metal different from the first metal to form a multilayer stack having a total thickness between 2 mm and 15 mm;b) bonding together the first and second strips of the multilayer stack by rolling; andc) forming a finished laminate by reducing a thickness of the bonded-together first and second strips by rolling in at least one pass such that the one first metal strip has a thickness of 0.5 to 10 μm.2. The method defined in claim 1 , wherein the multilayer stack has a total thickness between 5 and 7 mm.3. The method defined in claim 1 , further comprising the step of:diffusion annealing the stack prior to step c) to produce between the first and second strip a diffusion layer that is also reduced in thickness during thickness reduction.4. The method defined in claim 1 , wherein the stack is comprised of only the first strip and the second strip.5. The method defined in claim 4 , wherein prior to step c) the thickness of the one second metal strip is 5 to 10 mm and the thickness of a first metal strip is 0.8-15% of the thickness of the individual singular second metal strip.6. The method defined in claim 4 , wherein the first metal strip is a ...

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14-11-2013 дата публикации

DISPOSABLE MANDREL FOR FRICTION STIR JOINING

Номер: US20130299560A1
Принадлежит:

A system and method for providing a mandrel that can be used to react the loads that are created by a friction stir joining tool as it performs friction stir joining of tubulars, the mandrel selected from a disposable mandrel, a partially disposable mandrel, a reusable mandrel, and a mandrel that is partially disposable and partially reusable. 1. A mandrel for use in friction stir joining , said mandrel comprised of:a hard mandrel portion that provides support for friction stir joining; anda supporting mandrel portion that is at least partially dissolvable, the supporting mandrel portion providing support for the hard mandrel portion.2. The mandrel as defined in wherein the hard mandrel portion is coupled to the supporting mandrel portion by at least one attaching means selected from the group of attaching means including adhesive and an interference fit.3. The mandrel as defined in wherein the supporting mandrel portion includes a channel in which the hard mandrel portion is disposed.4. The mandrel as defined in wherein the hard mandrel portion is comprised of at least one hard mandrel segment.5. The mandrel as defined in wherein the at least one hard mandrel segment is comprised of a plurality of hard mandrel segments.6. The mandrel as defined in wherein the hard mandrel portion is comprised of a material that can be fractured.7. The mandrel as defined in wherein the supporting mandrel portion has an aperture through a length thereof.8. The mandrel as defined in wherein the supporting mandrel is formed as a plurality of wedges claim 1 , wherein the hard mandrel segments are disposed on an outer perimeter of the wedges claim 1 , and wherein the wedges are coupled using an adhesive.9. A method for performing friction stir joining using a mandrel claim 1 , said method comprising:1) providing a hard mandrel portion that provides support for friction stir joining;2) supporting the hard mandrel portion with a supporting mandrel portion;3) placing the mandrel inside ...

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14-11-2013 дата публикации

FRICTION STIR JOINING OF CURVED SURFACES

Номер: US20130299561A1
Принадлежит:

A system and method for joining curved surfaces such as pipes by obtaining pipes having additional rough stock material on the pipe ends, the rough stock material being precision machine processed to prepare complementary face profiles on each of the curved surfaces and then performing friction stir joining of the pipes to obtain a joint that has fewer defects than joints created from conventional welding. 1. A method for preparing curved surfaces for friction stir joining , said method comprising:1) obtaining a first curved surface having a first end and a second curved surface having a first end, the first end of the first curved surface and the first end of the second curved surface including rough stock material;2) precision machine processing a face profile into the first end of the first curved surface and the first end of the second curved surface, removing at least a portion of the rough stock material; and3) aligning the first end of the first curved surface and the first end of the second curved surface together to form a joint.2. The method as defined in wherein the method further comprises positioning a mandrel under the joint.3. The method as defined in wherein the method further comprises performing friction stir joining on the joint between the first end of the first curved surface and the first end of the second curved surface using a friction stir joining tool.4. The method as defined in wherein the method further comprises performing friction stir joining on the joint between the first end of the first curved surface and the first end of the second curved surface using a stationary shoulder friction stir joining tool.5. The method as defined in wherein performing friction stir joining further comprises using a shielding gas at the joint to prevent corrosion during friction stir joining.6. The method as defined in wherein the method further comprises forming the rough stock material on the first curved surface and the second curved surface using a ...

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12-12-2013 дата публикации

PROCESS FOR ELECTRIC BONDING OF AN ALUMINUM WIRE

Номер: US20130327814A1
Принадлежит:

A process for electric bonding of an aluminum wire to a contact area which wire, provided with an oxide layer on its outer surface, is wrapped with an insulating lacquer and ultrasonic bonded to said contact area, wherein insulation is removed from the aluminum wire section to be connected to the contact area prior to the ultrasonic bonding process by removing the insulating layer which surrounds the outer surface of the wire with oxide layer by means of an electric plasma. 1. Process for electric bonding of an aluminum wire to a contact area which wire , provided with an oxide layer on its outer surface , is wrapped with an insulating lacquer comprising:removing insulation from the aluminum wire section to be connected to the contact area prior to the ultrasonic bonding process by removing the insulating layer which surrounds the outer surface of the wire with oxide layer by means of an electric plasma, andultrasonic bonding the aluminum wire to the contact area.2. The process according to claim 1 , wherein the electric plasma has a defined temperature of more than 200° C. and less than 620° C.3. The process according to claim 1 , wherein the insulation is removed from the aluminum wire section in a cycle mode first and the aluminum wire is ultrasonic bonded thereafter.4. The process according to claim 3 , wherein the cycle time is shorter than 10 seconds.5. The process according to claim 1 , wherein insulation removal from the aluminum wire section and subsequent bonding of the aluminum wire are carried out in direct succession with a time difference of less than 300 seconds between termination of insulation removal from the aluminum wire section and aluminum wire feeding for ultrasonic bonding.6. The process according to claim 1 , wherein insulating lacquer is removed from a plurality of aluminum wire sections simultaneously.7. The process according to claim 1 , wherein insulation is removed from two aluminum wire sections at a time.8. The process according to ...

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23-01-2014 дата публикации

Method for welding aluminum alloy materials and aluminum alloy panel produced thereby

Номер: US20140023874A1
Принадлежит: Sumitomo Light Metal Industries Ltd

First and second aluminum alloy materials ( 2, 3 ), each comprised of a 5000-series aluminum alloy containing second phase particles having a diameter less than 5 μm in a distribution density of less than or equal to 10,000 second phase particles/mm 2 , are welded together by abutting portions of the first and second aluminum alloy materials, and friction stir welding along the abutted portions ( 5 ) to form an integrally-welded aluminum alloy panel ( 1 ). The friction stir welding is performed using a tool ( 8 ) having a shoulder ( 10 ) under the following conditions: (i) the shoulder of the tool has a diameter (d) in the range of 3 mm≦d≦8 mm and (ii) the revolution number (r) of the tool is 6<r≦20, wherein r is tool revolutions/length of the weld ( 4 ) in millimeters.

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20-02-2014 дата публикации

Bonding-substrate fabrication method, bonding substrate, substrate bonding method, bonding-substrate fabrication apparatus, and substrate assembly

Номер: US20140048805A1

[Problem] To provide a substrate bonding technique having a wide range of application. [Solution] A silicon thin film is formed on a bonding surface, and the interface with the substrate is surface-treated using energetic particles/metal particles.

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13-03-2014 дата публикации

System for friction stir welding including a mobile counter-bearing

Номер: US20140069984A1
Принадлежит: AIRBUS OPERATIONS SAS

System for friction stir welding of two parts which includes a welding unit which includes at least one welding head fitted with a rotating pin and a counter-bearing unit which has a support surface to support the parts against a pressure exerted by the welding head, and wherein each welding head can be moved relative to the support surface in a first direction parallel to an axis of rotation of the rotating pin and in a second direction orthogonal to the axis of rotation, and wherein the support surface can be moved in the second direction and is formed of two coaxial clamp rollers which are set apart from each other.

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13-03-2014 дата публикации

Friction stir spot welding device and friction stir spot welding method

Номер: US20140069986A1
Принадлежит: Kawasaki Jukogyo KK

A tool driving section of a friction stir spot welding device is configured to advance and retract each of a pin member and a shoulder member. A tool driving control section is configured to control the tool driving section such that an absolute value of a tool average position Tx defined by a following equation: Ap·Pp+As·Ps=Tx, where Ap is a cross-section area of a front end surface of the pin member, As is a cross-section area of a front end surface of the shoulder member, Pp is a press-fit depth of the pin member press-fitted from a front surface of an object to be welded, and Ps is a press-fit depth of the shoulder member press-fitted from the front surface of the object to be welded, is small.

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27-03-2014 дата публикации

Method for joining substrates

Номер: US20140083597A1

The invention relates to a method of joining substrates. It is the object of the invention in this respect to join substrates of substrate materials together without having to exert an increased effort for a coating with additional coating processes to be carried out and to be able to achieve a good quality of the join connection in so doing. In the method in accordance with the invention a pretreatment of at least one join surface of a substrate to be joined is carried out in low pressure oxygen plasma prior to the actual joining. On the joining, a contact force acts on the substrates to be joined in the range 2 kPa to 5 MPa and in this process a heat treatment is carried out at an elevated temperature of at least 100° C. and at under pressure conditions of a maximum of 10 mbar, preferably <10 −3 mbar.

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07-01-2016 дата публикации

METHOD FOR PRODUCING A CIRCUIT CARRIER AND FOR CONNECTING AN ELECTRICAL CONDUCTOR TO A METALLIZATION LAYER OF A CIRCUIT CARRIER

Номер: US20160001393A1
Принадлежит:

One aspect of the invention relates to a method for producing a circuit carrier. For this purpose, an electrically insulating carrier is provided, having an upper side and also an underside opposite from the upper side. A first metal foil and a hardening material are likewise provided. Then, an upper metallization layer, which is arranged on the upper side and has a hardening area, is produced. In this case, at least one contiguous portion of the hardening area is created by at least part of the hardening material being diffused into the first metal foil. 1. A method for producing a circuit carrier , comprising the steps of:providing an electrically insulating carrier, which has an upper side and also an underside opposite from the upper side;providing a first metal foil;providing a hardening material; andproducing an upper metallization layer arranged on the upper side and having a hardening area, at least one contiguous portion of the hardening area being created by at least part of the hardening material being diffused into the first metal foil.2. The method as claimed in claim 1 , in which the contiguous portion has a thickness of at least 5 μm and/or of at most 100 μm.3. The method as claimed in claim 1 , in which the contiguous portion has a base area of at least 1 mm.4. The method as claimed in claim 1 , in which the contiguous portion has at every location:a first hardness, which is greater than a second hardness of the first metal foil.5. The method as claimed in claim 1 , in which the carrier provided is formed as a ceramic layer or as a green sheet.6. The method as claimed in claim 1 , in which claim 1 , before the diffusion claim 1 , the hardening material is applied to the side of the first metal foil that is facing away from the carrier.7. The method as claimed in claim 1 , in which claim 1 , before the diffusion claim 1 , the hardening material is applied to the side of the first metal foil that is facing the carrier.8. The method as claimed in claim ...

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02-01-2020 дата публикации

Processes and tooling associated with diffusion bonding the periphery of a cavity-back airfoil

Номер: US20200001411A1
Принадлежит: United Technologies Corp

A fixture assembly includes a first fixture portion, a second fixture portion that interfaces with the first fixture portion, and a sub-fixture movably mounted to the first fixture portion. A multiple of actuators selectively move the sub-fixture toward the second fixture portion. A method of manufacturing a fan blade includes deploying the sub-fixture from the first fixture portion to effectuate a peripheral diffusion bond to join the blade body and the cover of the fan blade.

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04-01-2018 дата публикации

SEMICONDUCTOR DEVICE

Номер: US20180005981A1
Принадлежит: ROHM CO., LTD.

A semiconductor device according to the present invention includes a semiconductor chip, an electrode pad made of a metal material containing aluminum and formed on a top surface of the semiconductor chip, an electrode lead disposed at a periphery of the semiconductor chip, a bonding wire having a linearly-extending main body portion and having a pad bond portion and a lead bond portion formed at respective ends of the main body portion and respectively bonded to the electrode pad and the electrode lead, and a resin package sealing the semiconductor chip, the electrode lead, and the bonding wire, the bonding wire is made of copper, and the entire electrode pad and the entire pad bond portion are integrally covered by a water-impermeable film. 1. A semiconductor device comprising:an interlayer insulating film formed on a semiconductor substrate;an uppermost layer wiring made of copper and formed on the interlayer insulating film;a passivation film formed on the uppermost layer wiring and selectively exposing a top surface of the uppermost layer wiring as an electrode pad; anda bonding wire made of copper and bonded directly to the electrode pad.2. The semiconductor device according to claim 1 , wherein the bonding wire is stitch bonded directly to the electrode pad.3. The semiconductor device according to claim 1 , wherein the bonding wire is bonded to the electrode pad by a stud bump.4. The semiconductor device according to claim 1 , wherein a thickness of the electrode pad is no less than 10 μm.5. The semiconductor device according to claim 1 , wherein a thickness of the electrode pad is 10 μm to 15 μm.6. The semiconductor device according to claim 1 , further comprising a lower layer wiring covered with the interlayer insulating film claim 1 , whereinthe uppermost layer wiring includes a protrusion extending inside the interlayer insulating film,the lower layer wiring is electrically connected to the electrode pad via a pathway including the protrusion.7. The ...

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02-01-2020 дата публикации

Integrate Rinse Module in Hybrid Bonding Platform

Номер: US20200006052A1
Принадлежит:

A method includes performing a plasma activation on a surface of a first package component, removing oxide regions from surfaces of metal pads of the first package component, and performing a pre-bonding to bond the first package component to a second package component. 1. A method comprising: performing a plasma treatment on the package component in the surface treatment station;', 'removing oxides on surface metal pads of the package component in the integrated cleaning station; and', 'cleaning the package component using de-ionized water in the integrated cleaning station., 'using an apparatus to form a package component, the apparatus comprising a surface treatment station and an integrated cleaning station, and the method comprising2. The method of further comprising:dispensing a first chemical on the package component;collecting the first chemical using a first container in a chamber in the integrated cleaning station;dispensing a second chemical on the package component; andcollecting the second chemical using a second container in the first container.3. The method of claim 2 , wherein the collecting the first chemical comprises spinning the first chemical into the first container claim 2 , and the first chemical passes top edges of the second container and drops into the first container.4. The method of claim 2 , wherein the second container is fully inside the first container claim 2 , and the second container has top edges lower than top edges of the first container.5. The method of further comprising:cleaning the package component using de-ionized water; andcollecting the de-ionized water using a third container in the chamber.6. The method of further comprising:draining the collected first chemical out of the first container through a first outlet connecting from outside of the chamber to the first container; anddraining the collected second chemical out of the second container through a second outlet connecting from outside of the chamber to the second ...

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12-01-2017 дата публикации

ENHANCED FRICTION-STIR-WELDING JOINT STRENGTH BETWEEN STEEL AND ALUMINUM WITH SURFACE COATING AND PREFORMED LOCAL TEXTURE

Номер: US20170008121A1
Автор: Li Huaxin
Принадлежит:

A method and device for enhancing friction-stir-welding joint strength between aluminum and steel that has a surface coating by forming a local texture of points of raised elevation on the steel by stamping the steel, and then mechanically intermixing the steel and the aluminum with friction-stir-welding to form the joint. 1. A method for enhancing friction-stir-welding joint strength between a steel plate and an aluminum plate comprising:providing an aluminum plate and a steel plate;coating a surface of the steel plate with a layer of zinc, aluminum, and silicon;stamping at least a portion of the surface of the steel plate comprising the surface coating to produce the preformed local texture formed of points of raised elevation in the at least the portion of the steel plate; and placing the steel plate in contact with the aluminum plate;', 'generating heat between a friction-stir-weld tool and the steel plate and the aluminum plate to form a softening of each of the metal plates near the friction-stir-weld tool;', 'applying, via the friction-stir-weld tool, mechanical pressure to the softened metals; and', 'mechanically intermixing the steel plate and the aluminum plate to form the joint between them, the surface coating and the preformed local texture of the steel plate residing therewithin., 'friction-stir-welding to form the joint, wherein the friction-stir-welding comprises2. The method of claim 1 , the stamping further comprising producing the points of raised elevation to a height of about one-hundred to about two-hundred microns.3. The method of claim 2 , the stamping further comprising producing the points of raised elevation such that each of the raised points comprises a dome shape.4. The method of claim 3 , the stamping further comprising producing the points of raised elevation in a series of rows.5. The method of claim 1 , further comprising providing the surface coating over the entire surface of the steel plate claim 1 , and forming the joint by ...

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15-01-2015 дата публикации

METHOD FOR BONDING A TANTALUM STRUCTURE TO A COBALT-ALLOY SUBSTRATE

Номер: US20150014397A1
Принадлежит:

Methods for bonding a porous tantalum structure to a substrate are provided. The method includes placing a compressible or porous interlayer between a porous tantalum structure and a cobalt or cobalt-chromium substrate to form an assembly. The interlayer comprising a metal or metal alloy that has solid state solubility with both the substrate and the porous tantalum structure. Heat and pressure are applied to the assembly to achieve solid state diffusion between the substrate and the interlayer and the between the porous tantalum structure and the interlayer. 1. (canceled)2. A method of bonding , comprising:providing a substrate comprising cobalt or cobalt-chromium;providing a subassembly that includes a porous tantalum structure with a compressible interlayer formed on a surface portion of the porous tantalum structure, said compressible interlayer having a porosity of between 5% and 40% and consisting essentially of interconnected metal or metal alloy particles that exhibit solid solubility with tantalum and with cobalt or cobalt-chromium, said interconnected metal or metal alloy particles defining collapsible pores therebetween;bending the subassembly from a first configuration to a second configuration;forming an assembly which includes placing an exposed surface of the compressible interlayer in contact with the substrate after said bending; andapplying heat and pressure to the assembly for a time sufficient to achieve solid-state diffusion between the substrate and the compressible interlayer and between the compressible interlayer and the porous tantalum structure.3. The method of claim 2 , wherein the compressible interlayer has a substantially uniform thickness before said bending.4. The method of claim 2 , wherein said applying heat and pressure to the assembly includes compressing a portion of the compressible interlayer from a first thickness to a second claim 2 , reduced thickness.5. The method of claim 2 , wherein said applying heat and pressure to the ...

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19-01-2017 дата публикации

METHOD FOR PRODUCING METAL LAMINATE MATERIAL

Номер: US20170014941A1
Принадлежит: TOYO KOHAN CO., LTD.

An object of the present invention is to provide a production method for efficiently producing a metal laminate having high bonding strength. A method for producing a metal laminate material comprising the steps of: sputter etching faces to be bonded of a stainless steel and an aluminum such that an oxide layer remains on each face; temporarily bonding the faces to be bonded of the stainless steel and the aluminum by roll pressure bonding; and thermally treating the temporarily bonded laminate material at a temperature lower than the recrystallization temperature of the stainless steel to thermally diffuse at least a metal element comprised in the stainless steel into the aluminum. 1. A method for producing a metal laminate material comprising the steps of:sputter etching faces to be bonded of a stainless steel and an aluminum such that an oxide layer remains on each face;temporarily bonding the faces to be bonded of the stainless steel and the aluminum by roll pressure bonding, andthermally treating the temporarily bonded laminate material at a temperature lower than the recrystallization temperature of the stainless steel to thermally diffuse at least a metal element comprised in the stainless steel into the aluminum.2. The method for producing a metal laminate material according to claim 1 , wherein claim 1 , in the thermally diffusing step claim 1 , 8 atm % or more of at least Fe element comprised in the stainless steel is diffused at a point 5 nm in the aluminum direction from the bonding interface.3. The method for producing a metal laminate material according to claim 1 , wherein the thermally diffusing step comprises thermally treating the temporarily bonded laminate material at a temperature lower than the recrystallization temperature of the stainless steel to thermally diffuse the metal element comprised in the stainless steel and the aluminum to each other.4. The method for producing a metal laminate material according to claim 1 , wherein the thermal ...

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15-01-2015 дата публикации

PROCESSING OF METAL OR ALLOY OBJECTS

Номер: US20150017475A1
Принадлежит:

Disclosed are methods of processing an object, the object being made of a metal or an alloy, the object having a plurality of open cavities, the method comprising: performing a sealing process on the object to seal the openings of the open cavities, thereby forming a plurality of closed cavities; and reducing the sizes of the closed cavities by performing a consolidation process on the object having the closed cavities. Sealing process may comprise shot peening or coating the object. A consolidation process may comprise a hot isostatic pressing process. The sizes of the closed cavities may be reduced until the closed cavities are no longer present in the object. 119-. (canceled)20. A method of processing an object , the object being made of a metal or an alloy , the method comprising:coating the surface of the object with a solid layer of material thereby providing a coated object, wherein the material is a metal or alloy that is different to the metal or alloy from which the object is made, the layer of material and the object forming a eutectic composition at or proximate to the interface between the layer of material and the object; andheating the coated object to a temperature above a melting point of the eutectic composition so as to cause the eutectic composition to melt, thereby forming a liquid layer between the solid layer of material and the solid object.21. A method according to claim 20 , wherein heating of the coated object is performed at least until diffusion or dissolving of the object and/or the layer of material into the liquid layer causes a melting point of the composition of the layer of material and the object to increase above the temperature to which the coated object is heated claim 20 , thereby causing solidification of the liquid layer.22. A method according to claim 20 , wherein heating of the coated object is performed at least until the entire solid layer of material has been dissolved into the liquid layer.23. A method according to ...

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14-01-2021 дата публикации

Method and Apparatus for Flexible Circuit Cable Attachment

Номер: US20210014977A1
Принадлежит: Jabil Inc

A method and apparatus for multiple flexible circuit cable attachment is described herein. Gold bumps are bonded on interconnection pads of a substrate to create a columnar structure and solder or conductive epoxy is dispensed on the flexible cable circuit. The substrate and flexible cable circuit are aligned and pressed together using force or placement of a weight on either the substrate or flexible cable circuit. Appropriate heat is applied to reflow the solder or cure the epoxy. The solder wets to the substrate pads, assisted by the gold bumps, and have reduced bridging risk due to the columnar structure. A nonconductive underfill epoxy is applied to increase mechanical strength.

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17-01-2019 дата публикации

JOINING OF DISSIMILAR MATERIALS USING IMPACT WELDING

Номер: US20190015925A1
Автор: Daehn Glenn, Vivek Anupam
Принадлежит:

A system and method for joining dissimilar metals. In one embodiment, a method comprises providing a first metal plate, a second metal plate, and an intermediate body that is positioned between the first metal plate and the second metal plate. The first metal plate is then driven into the intermediate body, which causes at least a portion of the intermediate body to collide with the second metal plate. As a result, the material of the intermediate body joins the first metal plate to the second plate. In another embodiment, a method for joining dissimilar metals comprises providing a first metal that is not amenable to welding, a second metal that is joinable to the first metal, and an intermediate body that is not joinable to at least the first metal. The intermediate body may have at least one hole such that the first metal and the second metal are positioned over and on opposite sides of the hole(s). At least a portion of the second metal may then be driven into the hole(s) to be joined to first metal. 1. A method for joining dissimilar metals , said method comprising:providing a flyer plate comprised of a first metal, a target plate comprised of a second metal, and an intermediate body that is positioned between said flyer plate and said target plate, said intermediate body comprised of a material that is amenable to be joined to said first metal and said second metal; anddriving at least a portion of said flyer plate into said intermediate body, which causes at least a portion of said intermediate body to collide with said target plate;whereby said material of said intermediate body joins said flyer plate to said target plate.2. The method of claim 1 , further comprising the step of providing a vaporizing foil actuator that drives said portion of said flyer plate into said intermediate body.3. The method of claim 1 , wherein said intermediate body has an H-shaped profile.4. The method of claim 1 , wherein said intermediate body has a modified X-shaped profile ...

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16-01-2020 дата публикации

METHOD AND APPARATUS TO FORM A WORKPIECE EMPLOYING VIBRATION WELDING

Номер: US20200016685A1
Принадлежит: GM GLOBAL TECHNOLOGY OPERATIONS LLC

A workpiece is described, and includes a substrate, a cable, and a cover piece. A portion of the cable is joined to the substrate employing a vibration welding tool, and the cover piece is interposed between the portion of the cable and the vibration welding tool during the joining. 1. A method for joining a shape-memory alloy (SMA) cable to a substrate employing a vibration welding system , the method comprising:positioning a portion of the SMA cable onto a surface of the substrate;interposing an aluminum cover piece overtop of the portion of the SMA cable;placing the substrate, the portion of the SMA cable and the cover piece onto an anvil of the vibration welding system such that the cover piece is interposed between the SMA cable and a sonotrode of the vibration welding system; andapplying, via the sonotrode of the vibration welding system, vibration energy onto the cover piece, the portion of the SMA cable and the substrate;wherein applying the vibration energy mechanically joins the substrate, the SMA cable and the cover piece.2. The method of claim 1 , further comprising:forming a channel on the surface of the substrate; andpositioning the portion of the SMA cable in the channel formed on the surface of the substrate.3. A method for mechanically joining a cable to a substrate employing a vibration welding system claim 1 , wherein the vibration welding system includes an anvil and a sonotrode claim 1 , the method comprising:positioning a portion of the cable onto a surface of the substrate;interposing a cover piece overtop of the portion of the cable;placing the substrate, the portion of the cable and the cover piece onto the anvil of the vibration welding system such that the cover piece is interposed between the cable and the sonotrode of the vibration welding system; andapplying, via the sonotrode of the vibration welding system, vibration energy onto the cover piece, the portion of the cable and the substrate;wherein applying the vibration energy ...

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17-04-2014 дата публикации

Method and apparatus related to joining dissimilar metal

Номер: US20140102164A1
Принадлежит: General Electric Co

A method of forming a dual alloy member for joining two dissimilar materials includes selecting a first material and a second material that is different from the first material, metallurgically combining the first and second materials, forming the first and second materials into a preform using a hot work metal working process, shaping the preform into using another metal working process, and machining the perform to obtain a predetermined shape.

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19-01-2017 дата публикации

Method of manufacturing secondary battery

Номер: US20170018752A1
Принадлежит: Samsung SDI Co Ltd

A method of manufacturing a secondary battery includes: ultrasonic-welding a first electrode plate of an electrode assembly and a first electrode tab to each other by using a first horn including a first protruding tip; ultrasonic-welding a second electrode plate of the electrode assembly and a second electrode tab to each other by using a second horn including a second protruding tip, the second protruding tip having a positioning direction different from a positioning direction of the first protruding tip; and preparing the electrode assembly by arranging a separator between the first and second electrode plates.

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18-01-2018 дата публикации

METAL-METAL DIRECT BONDING METHOD

Номер: US20180019124A1
Принадлежит:

A method for assembling a first substrate and a second substrate by metal-metal direct bonding, includes providing a first layer of a metal at the surface of the first substrate and a second layer of the metal at the surface of the second substrate, the first and second metal layers having a tensile stress (σ) between 30% and 100% of the tensile yield strength (σ) of the metal; assembling the first and second substrates at a bonding interface by directly contacting the first and second tensile stressed metal layers; and subjecting the assembly of the first and second substrates to a stabilization annealing at a temperature lower than or equal to a temperature threshold beyond which the first and second tensile stressed metal layers are plastically compressively deformed. 1. A method for assembling a first substrate and a second substrate by a metal-metal direct bonding , comprising:providing a first layer of a metal at a surface of the first substrate and a second layer of said metal at a surface of the second substrate, the first and second metal layers having a tensile stress comprised between 30% and 100% of the tensile yield strength of said metal;assembling the first and second substrates at a bonding interface by directly contacting the first and second metal layers;subjecting the assembly of the first and second substrates to a stabilization annealing at a temperature lower than or equal to a temperature threshold beyond which the first and second tensile stressed metal layers are plastically compressively deformed.2. The method according to claim 1 , comprising calculating said temperature threshold from the tensile stress of the first and second metal layers and the thermo-elastic coefficient of said metal.3. The method according to claim 1 , wherein the providing comprises depositing the first metal layer onto a face of the first substrate and the second metal layer onto a face of the second substrate.4. The method according to claim 3 , wherein the ...

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18-01-2018 дата публикации

Wedge bonding component

Номер: US20180019224A1
Автор: Hidekazu Shigeyoshi
Принадлежит: Kyocera Corp

There is provided with a surface for contacting a wire. At least a part of the surface comprises a surface of a ceramic sintered body containing aluminum oxide as a main ingredient and titanium carbide as an accessory ingredient.

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26-01-2017 дата публикации

BALL BAT INCLUDING MULTIPLE ALLOYS

Номер: US20170021249A1
Принадлежит:

A ball bat includes a barrel section welded, adhered, or mechanically affixed to a handle section at a joint positioned in a taper region of the bat. The joint may alternatively be positioned in other regions, such as in the barrel region or the handle region. The barrel section may include a different metal alloy than the handle section. For example, the barrel section may include 6061 aluminum alloy and the handle section may include 7050 aluminum alloy. In some embodiments, the welded joint may be formed from a spin-welding process. The bat provides a strong handle in combination with a barrel that meets BBCOR or other performance requirements. 1. A ball bat comprising:a barrel section comprising a first metal alloy; anda handle section joined to the barrel section at a joint, the handle section comprising a second metal alloy that is stronger than the first metal alloy.2. The ball bat of wherein the barrel section has a first diameter and the handle section has a second diameter smaller than the first diameter.3. The ball bat of wherein the joint comprises an overlapping interface in which at least a portion of the handle section is positioned within the barrel section.4. The ball bat of wherein the joint comprises an overlapping interface in which at least a portion of the barrel section is positioned within the handle section.5. The ball bat of wherein the barrel section generally abuts the handle section at the joint.6. The ball bat of wherein the first metal alloy comprises 6061 aluminum alloy and the second metal alloy comprises 7050 aluminum alloy.7. The ball bat of wherein the barrel section is welded to the handle section at the joint.8. A ball bat comprising:a first bat section comprising a first metal alloy;a second bat section attached to the first bat section at a joint, the second bat section comprising a second metal alloy that is stronger than the first metal alloy;wherein the first bat section forms at least a part of a barrel region and the ...

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26-01-2017 дата публикации

METHOD OF JOINING HEAT-TREATABLE ALUMINUM ALLOY MEMBERS BY FRICTION STIR WELDING

Номер: US20170021447A1
Принадлежит: SUMITOMO LIGHT METAL INDUSTRIES, LTD.

A method of joining heat-treatable aluminum alloy members by friction stir welding, including the steps of: a T4-treatment-performing step of performing a T4 treatment on heat-treatable aluminum alloy members so as to impart T4 temper to the heat-treatable aluminum alloy members; a joining step of joining the heat-treatable aluminum alloy members with T4 temper by friction stir welding to provide a joined product; and a reversion-treatment-performing step of performing a reversion treatment, the reversion-treatment-performing step being carried out prior to or after the joining step. 1. A method of joining heat-treatable aluminum alloy members by friction stir welding , comprising the steps of:a T4-treatment-performing step of performing a T4 treatment on heat-treatable aluminum alloy members so as to impart T4 temper to the heat-treatable aluminum alloy members;a joining step of joining the heat-treatable aluminum alloy members with T4 temper by friction stir welding, wherein each heat-treatable aluminum alloy member has a length and a width, and wherein heat-treatable aluminum alloy members are butted together along the lengths thereof and friction stir welded along the abutted lengths to provide a joined product; anda reversion-treatment-performing step of applying heat from a reversion treatment directly across an entire width of the heat-treatable aluminum alloy members, the reversion-treatment-performing step being carried out after the joining step,wherein the joined product has a stir zone along said welded length of the joined product, with a heat-affected zone located outwardly of the stir zone and base material portions of the joined product being areas other than the stir zone and the heat-affected zone in a widthwise direction of the joined product, andwherein upon completing both the joining step and the reversion-treatment-performing step, a hardness of the stir zone is the highest, with a hardness of the heat-affected zone being the second highest, ...

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25-01-2018 дата публикации

Ultrasonic welding device and method for ultrasonic welding

Номер: US20180021884A1
Принадлежит:

Ultrasonic welding device having a sonotrode () and an anvil (), in which a flat part and at least one joining part are arranged between the sonotrode () and the anvil () during ultrasonic welding, and wherein a fastening element is held in a positively locking manner between the flat part and the joining part, and a damping element () that presses on the fastening element () is provided, which is pressed on the fastening element in such a way that a relative movement between the fastening element and the flat part and/or the joining part is restricted during ultrasonic welding 123-. (canceled)24. A method of ultrasound welding comprising:captively arranging a fastening element on a flat part;arranging a damping element on the fastening element so that the fastening element is pressed against the flat part by means of the damping element; andapplying ultrasonic oscillations to the flat part to form a weld, wherein a relative movement between the fastening element and the flat part during the ultrasonic welding is restricted.25. The method according to claim 24 , wherein the relative movement between the fastening element and the flat part is restricted via a force applied by a holding arm perpendicularly to the damping element.26. The method according to claim 25 , wherein the force applied by the holding arm through the damping element against the fastening element is a contact pressure between 3 bar and 6 bar.27. The method according to claim 25 , wherein the holding arm pushes the damping element against the fastening element such that the flat part is elastically deformed.28. The method according to claim 24 , wherein the fastening element is arranged on the flat part in a free-running manner.29. The method according to claim 24 , further comprising arranging at least one joining part on the flat part claim 24 , wherein the joining part encompasses the fastening element.30. The method according to claim 24 , wherein the fastening element is a rotating fastening ...

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28-01-2016 дата публикации

Maxmet Composites for Turbine Engine Component Tips

Номер: US20160024955A1
Принадлежит:

A turbine engine system includes a turbine engine component having an airfoil portion and a tip, which turbine engine component having a MAXMET composite bonded to the tip. The MAXMET composite has MAX phases in a metal matrix. 1. A turbine engine system comprising:a turbine engine component having an airfoil portion and a tip;said turbine engine component having a MAXMET composite bonded to said tip.2. The turbine engine system according to claim 1 , wherein said MAXMET composite is a composite having MAX phases and a metal matrix.3. The turbine engine system according to claim 2 , wherein said metal matrix is at least one of a low claim 2 , medium claim 2 , and high melting point metal or metal alloy.4. The turbine engine system according to claim 2 , wherein said MAX phases are defined by the formula MAXwhere M is an early transition metal element claim 2 , A is an A-group element claim 2 , X is C or N claim 2 , and n=1 to 3.5. The turbine engine system according to claim 1 , further comprising an abradable coating which is engaged by the tip of said turbine engine component with said MAXMET composite.6. The turbine engine system according to claim 1 , wherein said turbine engine component is a vane.7. The turbine engine system according to claim 1 , wherein said turbine engine component is a blade.8. A turbine engine component comprising:an airfoil portion having a tip; anda MAXMET composite bonded to said tip.9. The turbine engine component according to claim 8 , wherein said MAXMET composite is a composite having MAX phases and a metal matrix.10. The turbine engine component according to claim 9 , wherein said metal matrix is at least one of a low claim 9 , medium claim 9 , and high melting point metal or metal alloy.11. The turbine engine component according to claim 9 , wherein said MAX phases are defined by the formula MAXwhere M is an early transition metal element claim 9 , A is an A group element claim 9 , X is carbon or nitrogen claim 9 , and n=1 to 3. ...

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26-01-2017 дата публикации

HYBRID BONDED TURBINE ROTORS AND METHODS FOR MANUFACTURING THE SAME

Номер: US20170022827A1
Принадлежит: HONEYWELL INTERNATIONAL INC.

Hybrid bonded turbine rotors and methods for manufacturing the same are provided. A method for manufacturing a hybrid bonded turbine rotor comprises the steps of providing turbine disk having a rim portion comprising a live rim of circumferentially continuous material and a plurality of live rim notches in an outer periphery of the turbine disk alternating with a plurality of raised blade attachment surfaces defining the outer periphery; providing a plurality of turbine blades, each of which comprising an airfoil portion and a shank portion, the shank portion having a base surface; metallurgically bonding a compliant alloy material layer to either or both of the raised blade attachments surfaces of the turbine disk and the base surfaces of the blade shanks; and linear friction welding the plurality of blades to the turbine disk so as to form a bond plane between the raised blade attachments surfaces of the turbine disk and the base surfaces of the blade shanks, the compliant alloy material layer being disposed at the bond plane. 1. A method for manufacturing a hybrid bonded turbine rotor comprising the steps of:providing turbine disk having a rim portion comprising a live rim of circumferentially continuous material and a plurality of live rim notches in an outer periphery of the turbine disk alternating with a plurality of raised blade attachment surfaces defining the outer periphery;providing at least one turbine blade, the at least one turbine blade comprising an airfoil portion and a shank portion, the shank portion having a base surface;metallurgically bonding a compliant alloy material layer to either or both of one or more of the raised blade attachment surfaces of the turbine disk and the base surface of the blade shank, wherein the compliant alloy is bonded only to the one or more of the raised blade attachment surfaces and not any other portion of the turbine disk, only to the base surface of the blade shank and not any other portion of the at least one ...

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24-01-2019 дата публикации

FRICTION WELDING METHOD

Номер: US20190022789A1
Принадлежит:

A friction welding method includes: applying axial force to first and second metallic components so as to force the components against each other at an interface therebetween, while oscillating the two components relative to each other in a cyclic motion, so as to generate friction and heat at the interface; rapidly stopping the cyclic motion; and applying a spike in the axial force to complete a weld between the first and second components. 1. A friction welding method , comprising:applying axial force to first and second metallic components so as to force the components against each other at an interface therebetween, while oscillating the two components relative to each other in a cyclic motion, so as to generate friction and heat at the interface;stopping the cyclic motion; andonce the cyclic motion is stopped, applying a spike in the axial force to raise the axial force from a baseline axial force to a peak axial force and complete a weld between the first and second components.2. The method according to claim 1 , wherein the cyclic motion is stopped in less than 0.2 seconds.3. The method according to claim 1 , wherein the cyclic motion is stopped in less than 0.025 seconds.4. The method according to claim 1 , wherein the cyclic motion is stopped in less than 0.0125 seconds.5. The method according to claim 1 , wherein application of the spike in the axial force begins simultaneously with the cyclic motion being stopped.6. The method according to wherein the spike in the axial force from the baseline axial force to the peak axial force occurs in less than about 0.2 seconds.7. The method according to wherein the spike in the axial force from the baseline axial force to the peak axial force occurs in less than about 0.2 seconds.8. The method according to claim 1 , wherein the spike in the axial force is applied in an open loop without feedback control.915. The method according to claim 1 , wherein the spike in the axial force has a peak magnitude of at least about ...

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23-01-2020 дата публикации

METHOD OF DIFFUSION BONDING

Номер: US20200023460A1
Принадлежит: ROLLS-ROYCE PLC

A method of diffusion bonding two components together comprises providing a first component having a first bonding surface, and a second component having a second bonding surface. Each of the first bonding surface and the second bonding surface is etched. A cold working process is applied to each of the first bonding surface and the second bonding surface. Each of the first bonding surface and the second bonding surface is then etched. The first component is positioned adjacent to the second component with the first bonding surface abutting against the second bonding surface, to define a joint surface between the first component and the second component. A peripheral edge of the joint surface is sealed. The first bonding surface is diffusion bonded to the second bonding surface. 1. A method of diffusion bonding two components together , the method comprising the steps of:(a) providing a first component having a first bonding surface, and a second component having a second bonding surface;(b) applying a cold working process to at least one of the first bonding surface and the second bonding surface;(c) etching each of the first bonding surface and the second bonding surface;(d) position the first component adjacent to the second component with the first bonding surface abutting against the second bonding surface, to define a joint surface between the first component and the second component;(e) sealing a peripheral edge of the joint surface; and(f) diffusion bonding the first bonding surface to the second bonding surface.2. The method as claimed in claim 1 , wherein step (b) comprises the prior step of:(b)′ etching each of the first bonding surface and the second bonding surface.3. The method as claimed in claim 1 , wherein step (b) comprises the step of:(b1) applying a cold working process to each of the first bonding surface and the second bonding surface, to produce a cold worked layer having a depth from the surface of less than 1 mm.4. The method as claimed in ...

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28-01-2021 дата публикации

ROLL-BONDED BODY AND METHOD FOR PRODUCING ROLL-BONDED BODY

Номер: US20210023648A1
Принадлежит: TOYO KOHAN CO., LTD

It is an object of the present invention to provide a roll-bonded laminate controlled in warping and a method for producing the same. The method produces the roll-bonded laminate having a two-layer structure of a first metal layer and a second metal layer, by roll-bonding a first metal plate and a second metal plate, wherein the surface hardness Hv of the first metal plate is lower than the surface hardness Hv of the second metal plate; and the method comprises roll-bonding so as to satisfy the following expression (1): 2. The method for producing a roll-bonded laminate according to claim 1 , wherein the total thickness of the roll-bonded laminate is 0.1 mm to 0.5 mm.3. The method for producing a roll-bonded laminate according to claim 1 , wherein the first metal layer comprises copper claim 1 , aluminum or an alloy thereof; and the second metal layer comprises a stainless steel claim 1 , titanium claim 1 , a titanium alloy or a nickel alloy.4. The method for producing a roll-bonded laminate according to claim 1 , wherein the first metal layer comprises copper; and the second metal layer comprises a stainless steel.5. The method for producing a roll-bonded laminate according to claim 1 , wherein a difference in hardness between the surface hardness Hv of the second metal plate and the surface hardness Hv of the first metal plate is 35 to 305.6. A roll-bonded laminate having a two-layer structure of a first metal layer and a second metal layer claim 1 ,wherein a surface hardness Hv of the first metal layer is lower than a surface hardness Hv of the second metal layer; anda warping radius as measured by the following warping test is 43.8 mm or more:the warping test: a sample cut out from the roll-bonded laminate is placed on a horizontal plane so that the first metal layer is positioned on the upper side; a height of a point of the sample whose height from the horizontal plane is maximum is taken as a warping amount; and from the warping amount and a length of the ...

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28-01-2021 дата публикации

FRICTION WELDING APPARATUS AND METHOD OF OPERATING THE SAME

Номер: US20210023649A1
Принадлежит: KAWASAKI JUKOGYO KABUSHIKI KAISHA

A friction welding apparatus is provided, which includes a tool, a rotary driver, a linear driver, and a control device. The control device controls the linear driver and the rotary driver so that the tool is rotated while a tip-end part thereof is pressed against a to-be-joined part of a to-be-joined object to increase a temperature of the to-be-joined part at or above an A1 transformation point, the tip-end part of the tool reaches a given first position so that a softened second member sticks into a softened first member, and the tool is drawn out from the to-be-joined part while the tool is rotated. 1. A friction welding apparatus configured to join a to-be-joined object having a first member and a second member by softening with frictional heat , comprising:a tool formed cylindrically, and rotatable about an axis thereof and reciprocatable in a direction along the axis;a rotary driver configured to rotate the tool about the axis;a linear driver configured to reciprocate the tool along the axis; anda control device,wherein the first member is disposed opposing to the tool and is made of a different type of material from the second member, and the second member is made of steel, andwherein the control device controls the linear driver and the rotary driver so that:(A) the tool is rotated about the axis while a tip-end part of the tool is pressed against a to-be-joined part of the to-be-joined object to increase a temperature of the to-be-joined part at or above an A1 transformation point;(B) while the temperature of the to-be-joined part is maintained at or above the A1 transformation point, the tip-end part of the tool reaches a given first position set beforehand so that the softened second member sticks into the softened first member; and(C) the tool is drawn out from the to-be-joined part, while the temperature of the to-be-joined part is maintained at or above the A1 transformation point and the tool is rotated.2. The friction welding apparatus of claim 1 , ...

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24-04-2014 дата публикации

System and method for cleaning bond wire

Номер: US20140110461A1
Принадлежит: Individual

A system for cleaning bond wire for use by a wire bonding machine includes a bond wire supply station, a bond wire cleaning bath station, a bond wire neutralizing station, a bond wire drying station, and a wire bonding machine. In operation, the bonding machine is supplied with bond wire stored at the supply station, which is firstly de-oxidized with a cleaning solution in the cleaning bath station. Next, the cleaning solution on the bond wire is neutralized with a neutralizing liquid in the neutralizing station. The bond wire is then dried in the drying station. The speed of the bond wire passing through the cleaning bath station, neutralizing station and drying station is controlled by the wire bonding machine.

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24-01-2019 дата публикации

TECHNIQUES FOR JOINING ONE OR MORE STRUCTURES OF AN ELECTRONIC DEVICE

Номер: US20190025874A1
Принадлежит:

Techniques for bonding structural features together in an enclosure of an electronic device are disclosed. A structural feature may be ultrasonically soldered to the enclosure to provide structural support and form a magnetic circuit within the device. Also, ultrasonic welding can bond various features to an interior region of the enclosure without leaving a mark or trace to an exterior region of the enclosure in a location corresponding to the various features. Further, one or more features can be actuated against the enclosure to bond the one or more features by friction welding. In addition, a rotational friction welding machine can rotate a feature having a relatively small diameter at relatively high speeds against the enclosure to drive the feature into the enclosure and frictionally weld the feature with the enclosure. Also, the friction welding does not leave any an appearance of cosmetic deformation on the exterior region. 1. A method for forming an electronic device having an enclosure comprising a first part and a second part rotatably coupled with the first part , the second part comprising a magnet , the method comprising:engaging an attachment feature with a bonding tool configured to bond the attachment feature with the first part; andactuating the attachment feature via the bonding tool that causes a solder material disposed between the attachment feature and the first part to melt and bond the attachment feature with the first part.2. The method of claim 1 , wherein in a closed configuration between the first part and the second part claim 1 , the attachment feature magnetically couples with the magnet to define a magnetic circuit claim 1 , and the first part is separated from the second part by a gap that is based upon the magnetic circuit.3. The method of claim 1 , further comprising co-planarizing the attachment feature and the enclosure.4. The method of claim 1 , wherein the solder material is disposed in a channel of the enclosure and wherein ...

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02-02-2017 дата публикации

TUBE PROFILE MACHINING PROCESS

Номер: US20170028503A1
Принадлежит:

In a first embodiment, at a time of magnetic pulse welding, a stepped tube profile machining process axially bores a walled tube from an end inward to a transition depth to form a section with a reduced wall thickness and then axially bores the walled tube from the transition depth to a fall off depth, thereby forming a section with a maximized welding wall section. In a second embodiment, also at a time of magnetic pulse welding, a surface angle tube profile machining process axially bores at a surface angle a walled tube from an end to a bore length to form an angular welding wall thickness inward to a maximized wall section. For both embodiments, the bored surfaces are virgin with no pits, oil, residue, or oxidation thereon, thus making the machined walled tubes available for immediate magnetic pulse welding. 1. A tapered tube profile machining process , comprising:axially boring a walled tube inward at a tapered surface angle from an end thereof to a bore length, wherein the axially boring removes pits, oil, debris, and oxidation from the end of the walled tube to the bore length, so as to form a bored surface within the walled tube having an angular welding wall thickness inward to a maximized welding wall section;wherein the axially boring step requires no additional processing time of using acid for cleaning the bored walled tube surface of oil, of ridding the acid from the bored walled tube surface, of drying the bored walled tube surface, or further of removing pits, oil, debris, or oxidation from the bored walled tube, since the axially boring step occurs immediately just before a time of attachment of the walled tube to a workpiece, by magnetic pulse welding the tapered bored surface of the walled tube to the workpiece.2. The tapered tube profile machining process of claim 1 , wherein the workpiece is an end fitting inserted into the bored end of the axially tapered bored walled tube until the end fitting is in contact with the maximized welding wall ...

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04-02-2016 дата публикации

METHOD OF MAKING AN ASSEMBLY HAVING A CAST IRON SUBASSEMBLY

Номер: US20160031005A1
Автор: Melekian Joseph
Принадлежит:

A method of making an assembly having a cast iron subassembly. The method may include providing a steel insert having a first joining surface and bonding the steel insert to a cast iron part to form a cast iron subassembly such that the first joining surface may be an exterior surface of the cast iron subassembly. 1. A method of making an assembly having a cast iron subassembly , comprising:providing a steel insert having a first joining surface;bonding the steel insert to a cast iron part to form a cast iron subassembly such that the first joining surface is an exterior surface of the cast iron subassembly;providing a steel component having a second joining surface;abutting the second joining surface with the first joining surface; andjoining the cast iron subassembly to the steel component proximate the first and second joining surfaces.2. The method of wherein cast iron subassembly is joined to the steel component by welding.3. The method of wherein the cast iron part is cast around the steel insert.4. The method of wherein the steel insert is configured as a ring.5. The method of wherein the cast iron part is made of ductile cast iron.6. The method of wherein the steel component is a cast steel bracket.7. The method of wherein the steel insert protrudes from the cast iron part.8. A method of making an assembly having a cast iron subassembly claim 1 , comprising:providing a first steel insert having a first faying surface;casting a first cast iron part about the first steel insert to make a first cast iron subassembly;providing a second steel insert having a second faying surface;casting a second cast iron part about the second steel insert to make a second cast iron subassembly;aligning the first faying surface with the second faying surface; andwelding the first cast iron subassembly to the second cast iron subassembly along the first faying surface and the second faying surfaces such that the weld does not extend to and does not carburize the first cast iron ...

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10-02-2022 дата публикации

Pre-Plating of Solder Layer on Solderable Elements for Diffusion Soldering

Номер: US20220046792A1
Принадлежит: INFINEON TECHNOLOGIES AG

A pre-soldered circuit carrier includes a carrier having a metal die attach surface, a plated solder region on the metal die attach surface, wherein a maximum thickness of the plated solder region is at most 50 μm, the plated solder region has a lower melting point than the first bond pad, and the plated solder region forms one or more intermetallic phases with the die attach surface at a soldering temperature that is above the melting point of the plated solder region.

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01-02-2018 дата публикации

ROTARY FRICTION WELDING

Номер: US20180029157A1
Принадлежит: ROLLS-ROYCE PLC

The present disclosure provides a rotary friction welding process including: providing an outer axisymmetric workpiece having a front first annular weld surface at a radially inward extent and a rear first annular weld surface at a radially inward extent; providing a front inner axisymmetric workpiece, the front inner workpiece having a front second annular weld surface at a radially outward extent of the front inner workpiece; providing a rear inner axisymmetric workpiece, the rear inner workpiece having a rear second annular weld surface at a radially outward extent of the rear inner workpiece; and rotary welding the workpieces together. 1. A rotary friction welding process including:providing an outer axisymmetric workpiece for machining into a rim portion of a rotor disc of a multi-stage rotor assembly of a gas turbine engine, the outer workpiece having a front first annular weld surface at a radially inward extent of the outer workpiece and a rear first annular weld surface at a radially inward extent of the outer workpiece;providing a front inner axisymmetric workpiece for machining into a front diaphragm of the rotor disc, the front inner workpiece having a front second annular weld surface at a radially outward extent of the front inner workpiece;providing a rear inner axisymmetric workpiece for machining into a rear diaphragm of the rotor disc, the rear inner workpiece having a rear second annular weld surface at a radially outward extent of the rear inner workpiece;aligning the outer workpiece and the front inner workpiece on a common axis (X-X) with the front first and second weld surfaces facing each other, rotating one of the outer and front inner workpieces about the axis relative to the other aligned workpiece, engaging the aligned workpieces at the front first and second weld surfaces such that the rotation raises the temperature at the front weld surfaces to create a front weld interface, and ceasing the rotation and allowing the front weld ...

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17-02-2022 дата публикации

METHOD OF PREPARING AN ALUMINUM METAL PIECE FOR WELDING

Номер: US20220048141A1
Принадлежит:

A method of preparing aluminum metal pieces for welding, along with welded sheet metal assemblies formed from the prepared aluminum metal pieces. In one embodiment, a scanning beam of a laser is directed at an edge portion of the sheet metal piece such that a portion of the scanning beam is configured to impact an oxide layer at the edge portion. The laser is pulsed in a series of ablating pulses at the edge portion, with the ablating pulses creating an ablation plume that includes ablated material from the oxide layer of the primary surface and the peripheral surface of the edge portion. The ablation plume is analyzed, and ablation and analyzing continues until a threshold of at least one constituent in the ablation plume or the analysis plume is met or exceeded. One or more operating parameters of the laser are adjusted based on the analysis of the ablation plume or analysis plume. In some embodiments, two aluminum metal pieces are simultaneously prepared. 1. A method of preparing an aluminum metal piece for welding , the aluminum metal piece having an oxide layer , the method comprising the steps of:directing a beam of a laser at an edge portion of the aluminum metal piece such that a portion of the beam is configured to impact the oxide layer at the edge portion, wherein the edge portion includes at least a part of a primary surface of the aluminum metal piece, at least a part of a secondary surface of the aluminum metal piece, and at least a part of a peripheral surface of the aluminum metal piece, the peripheral surface being situated between the primary surface and the secondary surface;pulsing the laser in a series of cleaning pulses at the edge portion, wherein the cleaning pulses create a cleaning plume that includes ablated material from the oxide layer located at the primary surface and ablated material from the oxide layer located at the peripheral surface;analyzing the cleaning plume for the series of cleaning pulses or analyzing an analysis plume ...

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30-01-2020 дата публикации

ROLL-BONDED LAMINATE AND METHOD FOR PRODUCING THE SAME

Номер: US20200031096A1
Принадлежит: TOYO KOHAN CO., LTD.

This invention provides a metal laminate that maintains functionality such as radiation performance and is excellent in dimensional accuracy after press work. Such metal laminate is a roll-bonded laminate composed of 2 or more metal layers, which exhibits a ratio σ/T of the standard deviation σ of thickness Tof the outermost layer to thickness T of the roll-bonded laminate of 0% of 4.0%, the thickness T of 2 mm or less, and the deviation of the thickness T of 4.0% or less. 1. A roll-bonded laminate , comprising:two or more metal layers,wherein a ratio σ/T of a standard deviation σ of an outermost layer thicknesses to a thickness T of the roll-bonded laminate is 0% to 4.0%, andwherein the thickness T is 2 mm or less, and a standard deviation of the thickness T is 4.0% or less.2. The roll-bonded laminate according to claim 1 , wherein the standard deviation σ of the outermost layer thicknesses is less than 4.0 μm.3. The roll-bonded laminate according to claim 1 , wherein the two or more metal layers each independently comprise a metal selected from a group consisting of Al claim 1 , Cu claim 1 , Mg claim 1 , Fe claim 1 , and Ti claim 1 , or an alloy thereof.4. A method for producing the roll-bonded laminate according to claim 1 , comprising:{'sub': 0', '0, 'bonding the two or more metal layers to each other so as to adjust a change in Vickers hardness of a hardest metal layer among the two or more metal layers before and after bonding within 80, wherein a ratio ΔT/Tof a reduction ΔT to a total thickness Tof the two or more metal layers before bonding is less than 1.0.'}5. The method for producing the roll-bonded laminate according to claim 4 , wherein bonding the two or more metal layers to each other is performed by subjecting the metal layer surfaces to be bonded to each other to sputter etching and roll-bonding the metal layer surfaces subjected to the sputter etching.6. A molded product comprising the roll-bonded laminate according to .7. The roll-bonded laminate ...

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05-02-2015 дата публикации

NANO-GRAINED MULTILAYER COPPER ALLOY SHEET HAVING HIGH STRENGTH AND HIGH ELECTRICAL CONDUCTIVITY, AND METHOD FOR MANUFACTURING SAME

Номер: US20150037609A1

In a high strength and high electrical conductive nano crystalline grain multi-layer copper alloy sheet, a plurality of high strength and high electrical conductive nano crystalline grain multi-layer sheets manufactured by roll-bonding an oxygen free copper (OFC) alloy sheet and a deoxidized low-phosphorous copper (DLP) alloy sheet are plastically bonded by roll-bonding method so that an OFC alloy layer and a DLP alloy layer are alternated to each other to have electrical conductivity of 85 IACS (%) or more and tensile strength of 500 MPa or more. 1. A high strength and high electrical conductive nano crystalline grain multi-layer copper alloy sheet , comprising:an oxygen free copper (OFC) alloy and a deoxidized low-phosphorous copper (DLP) alloy that are repeatedly roll-bonded to have electrical conductivity of 85 IACS (%) or more and tensile strength of 500 MPa or more.2. The high strength and high electrical conductive nano crystalline grain multi-layer copper alloy sheet of claim 1 , whereinan OFC alloy layer and a DLP alloy layer alternately overlap with each other.3. The high strength and high electrical conductive nano crystalline grain multi-layer copper alloy sheet of claim 2 , whereinthe multi-layer copper alloy sheet includes two or more OFC alloy layers and DLP alloy layers.4. A manufacturing method of a high strength and high electrical conductive nano crystalline grain multi-layer copper alloy sheet claim 2 , the method comprising:a material preparing step of preparing a sheet formed by an oxygen free copper (OFC) alloy and a deoxidized low-phosphorous copper (DLP) alloy;a surface-treatment step of surface-treating the sheet; anda sheet forming step of forming a high strength and high electrical conductive nano crystalline grain multi-layer copper alloy sheet having electrical conductivity of 85 IACS (%) or more and tensile strength of 400 MPa or more by repeatedly roll-bonding the sheet.5. The manufacturing method of a high strength and high ...

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17-02-2022 дата публикации

FOIL FOR SECONDARY BATTERY NEGATIVE ELECTRODE COLLECTOR

Номер: US20220052348A1
Принадлежит: HITACHI METALS, LTD.

This foil for a secondary battery negative electrode collector (negative electrode-collecting foil ) includes a first Cu layer () made of Cu or a Cu-based alloy, a stainless steel layer (), and a second Cu layer () made of Cu or a Cu-based alloy, which are disposed in this order, a total thickness is 200 μm or less, and 0.01% proof stress is 500 MPa or more. 1. A foil for a secondary battery negative electrode collector comprising , in the following order:{'b': '51', 'a first Cu layer () made of Cu or a Cu-based alloy;'}{'b': '52', 'a stainless steel layer () made of stainless steel containing Ni of more than 0.6% by mass and 3.0% by mass or less, in which a ferrite phase and a martensite phase are present; and'}{'b': '53', 'a second Cu layer () made of Cu or a Cu-based alloy,'}wherein a total thickness is 200 μm or less and a 0.01% proof stress is 500 MPa or more.2. The foil for a secondary battery negative electrode collector according to claim 1 , wherein a tensile strength is 800 MPa or more.3. The foil for a secondary battery negative electrode collector according to claim 1 , wherein an electrical resistivity is 7.5 μΩ·cm or less.4. The foil for a secondary battery negative electrode collector according to claim 1 , wherein the stainless steel layer contains Cr of 10.5% by mass or more and 20% by mass or less and C of 0.3% by mass or less.5. The foil for a secondary battery negative electrode collector according to claim 1 , wherein the stainless steel layer contains Cr of 15% by mass or more and 18% by mass or less and C of 0.01% by mass or more and 0.2% by mass or less.6. The foil for a secondary battery negative electrode collector according to claim 1 , wherein the stainless steel layer contains Ni of 1.5% by mass or more and 2.5% by mass or less.7. The foil for a secondary battery negative electrode collector according to claim 1 , wherein the 0.01% proof stress is 550 MPa or more.8. The foil for a secondary battery negative electrode collector according ...

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11-02-2016 дата публикации

Electrode Cartridge for Pulse Welding

Номер: US20160039041A1
Принадлежит: FORD GLOBAL TECHNOLOGIES LLC

A cartridge assembly for a tool includes a cartridge body or casing that contains a conductor. A conductor is connected to a pulse generator or source of stored charge that is discharged to vaporize the conductor and create an electro-hydraulic or electro-magnetic shockwave that is used to impact or pulse weld two parts together.

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11-02-2016 дата публикации

Method for Friction Welding Subsea Flowline Connectors

Номер: US20160039042A1
Принадлежит:

Methods of rotary friction welding a (e.g., concentrically) threaded connector to a subsea-type riser or flowline pipe segment and/or of rotary friction welding cladded pipe segments. Subsea-type riser or flowline pipe segment with a (e.g., concentrically) threaded connector fused to the pipe segment at an autogeneous friction welded seam, and/or subsea-type riser or flowline cladded pipe segments fused together at a friction welded seam. 1. A method comprising:rotary friction welding a threaded first connector to an undersea-type riser or flowline pipe segment.2. The method of claim 1 , where the rotary friction welding comprises:rotating the first connector in contact with the pipe segment until a portion of the first connector reaches a plastic state and a portion of the pipe segment reaches a plastic state; andpressing the first connector and the pipe segment together until the first connector and pipe segment have fused together.3. The method of claim 2 , where the connector and the pipe segment are pressed together at a pressure of between 14 claim 2 ,000 pounds per square inch (psi) and 60 claim 2 ,000 psi.4. The method of claim 3 , where portions of the connector and the pipe segment reach temperatures of between 900° C. and 1100° C. during the rotary friction welding.5. The method of claim 2 , where at least a portion of the pressing is simultaneous with at least a portion of the rotating.6. The method of claim 1 , where the first connector is concentrically threaded.7. The method of claim 1 , where the first connector is configured to be joined with a second connector by forcing the first and second connectors together without rotation along a common longitudinal axis.8. The method of claim 1 , where the first connector includes an annular pipe mating surface claim 1 , and the pipe includes an annular connector mating surface configured to mate with the pipe mating surface of the first connector.9. The method of claim 1 , where the pipe has an outer ...

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09-02-2017 дата публикации

STRUCTURAL COMPONENT AND METHOD OF MANUFACTURE

Номер: US20170036256A1
Принадлежит:

A structural component is provided comprising a base member comprising at least two sidewalls and a space therebetween, the base member having a predetermined curvilinear configuration formed using hot stretch forming. The structural component comprises at least one reinforcing member linear friction welded to the at least two sidewalls so that the reinforcing member is positioned at least partially within the space between the at least two sidewalls. 1. A method for manufacturing a structural component , the method comprising:forming a base member such that the base member comprises at least two sidewalls and a space therebetween;hot stretch forming the base member so that the base member has a predetermined curvilinear configuration;linear friction welding at least one reinforcing member to the at least two sidewalls so that the reinforcing member is positioned at least partially within the space between the at least two sidewalls; andwherein the structural component has substantially no residual stress following the hot stretch forming and linear friction welding.2. A method according to wherein at least one of the base member and reinforcing member is formed of titanium or a titanium alloy.3. A method according to wherein at least one of the base member and reinforcing member is formed of aluminum or an aluminum alloy.4. A method according to wherein the base member and reinforcing member are formed of the same material.5. A method according to wherein the base member and reinforcing member are formed of different materials.6. A method for manufacturing a structural component claim 1 , the method comprising:positioning a profile comprising at least two sidewalls and a space therebetween in a heat-insulating enclosure in which a die is disposed such that the profile is in forming proximity to the die;resistance heating the profile to a working temperature by passing electrical current through the profile;moving the profile and the die relative to each other while ...

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09-02-2017 дата публикации

Linear Friction Welding System With Phase Change Assembly

Номер: US20170036298A1
Автор: Johnson Stephen A.
Принадлежит:

A linear friction welding system in one embodiment includes a ram configured to vibrate along a welding axis, a cam follower operably connected to the ram, an eccentric including an eccentric outer periphery operably engaged with the cam follower, and an inner periphery, a first power shaft slidingly engaged with the eccentric, a second power shaft eccentrically engaged with the inner periphery, a timing component operably connected to the first power shaft and the second power shaft, a motor configured to drive the timing component, and a phase change mechanism engaged with the timing component and movable between a first position defining a first phase relationship between the first power shaft and the second power shaft, and a second position defining a second phase relationship between the first power shaft and the second power shaft. 1. A linear friction welding system , comprising:a ram configured to vibrate along a welding axis;a cam follower operably connected to the ram;an eccentric including an eccentric outer periphery operably engaged with the cam follower, and an inner periphery;a first power shaft slidingly engaged with the eccentric;a second power shaft eccentrically engaged with the inner periphery;a timing component operably connected to the first power shaft and the second power shaft;a motor configured to drive the timing component; anda phase change mechanism engaged with the timing component and movable between a first position defining a first phase relationship between the first power shaft and the second power shaft, and a second position defining a second phase relationship between the first power shaft and the second power shaft.2. The welding system of claim 1 , wherein:the timing component includes a timing component load segment between the first power shaft and the second power shaft;the phase change mechanism defines a first timing component load segment length when the phase change mechanism is in the first position;the phase change ...

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08-02-2018 дата публикации

METHOD AND APPARATUS FOR FRICTION WELDING

Номер: US20180036834A1
Принадлежит:

A method and apparatus for friction welding of workpieces (), which are softened and welded in a friction phase (R) with frictional contact and under frictional pressure (p) in a relative rotational movement about a process axis () through the effect of frictional heat. The frictional pressure (p) applied during axial advancement of one of the workpieces () is preferably ramped and increased during the friction phase (R). 1. A method for the friction welding of workpieces , the method comprising:plasticizing and welding together the workpieces by frictional heat during a friction phase in frictional contact and with a frictional pressure during a relative motion about a process axis;{'sup': 2', '2, 'changing and increasing the frictional pressure during the duration of the friction phase in a range of about 4 N/mm, initially, to 100 N/mm.'}2. (canceled)3. A method in accordance with claim 1 , wherein the frictional pressure is changed and increased during the friction phase steadily according to a linear ramp.4. A method in accordance with claim 1 , wherein the frictional pressure is changed and increased continuously during most of the friction phase or during the entire friction phase.5. A method in accordance with claim 1 , wherein the frictional pressure is increased from an initial value of 5 N/mmto 80 N/mmduring the friction phase.6. A method in accordance with claim 1 , wherein the frictional pressure is applied along the process axis.7. A method in accordance with claim 1 , wherein workpieces are pressed axially against one another during an upset phase following the friction phase.8. A method in accordance with claim 1 , wherein workpieces with a frictionally active diameter of 200 mm or larger claim 1 , preferably 500 mm to 650 mm claim 1 , are friction-welded.9. (canceled)10. A method in accordance with claim 1 , wherein the workpieces are rotated relative to one another during the friction phase at a speed of about 500 rpm.11. A method in accordance with ...

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12-02-2015 дата публикации

METHOD OF FRICTION-STIR WELDING OF STEEL SHEET

Номер: US20150041521A1
Принадлежит:

When friction-stir welding steel sheets, for the rotating tool, rotation speed RS is 100-1000 rpm, rotational torque RT 50-500 Nm, and travel speed TS 10-1000 mm/min, and HIPT (kJ/mm) is 0.3-1.5. The steel sheets used have a composition including 0.01-0.2 mass % of C, 0.5-2.0 mass % of Mn, 0.6 mass % or less of Si, 0.030 mass % or less of P, 0.015 mass % or less of S, and 0.0060 mass % or less of 0, with a content of Ti [% Ti] and a content of N [% N] being restricted in relation to the HIPT, Ceq being 0.5 mass % or less, and the balance being Fe and incidental impurities. As a result, local change in the frictional heat and plastic flow generated by friction can be prevented, yielding a weld portion with uniform and good toughness. 2. The method according to claim 1 , wherein the composition of the steel sheets additionally include at least one selected from the group consisting of Al: 0.005 mass % to 0.10 mass % and V: 0.003 mass % to 0.10 mass %.3. The method according to claim 1 , wherein the composition of the steel sheets further comprises at least one selected from the group consisting of Cu: 0.05 mass % to 1.0 mass % claim 1 , Ni: 0.05 mass % to 1.0 mass % claim 1 , Cr: 0.05 mass % to 0.50 mass % claim 1 , Mo: 0.02 mass % to 0.50 mass % claim 1 , and Nb: 0.003 mass % to 0.050 mass %.4. The method according to claim 2 , wherein the composition of the steel sheets further comprises at least one selected from the group consisting of Cu: 0.05 mass % to 1.0 mass % claim 2 , Ni: 0.05 mass % to 1.0 mass % claim 2 , Cr: 0.05 mass % to 0.50 mass % claim 2 , Mo: 0.02 mass % to 0.50 mass % claim 2 , and Nb: 0.003 mass % to 0.050 mass %. This disclosure relates to a method of friction-stir welding of steel sheets by causing plastic flow to occur while softening the steel sheets.Friction-stir welding is a technique for welding metal materials by first softening the metal materials through the production of frictional heat in the metal materials and then causing plastic ...

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24-02-2022 дата публикации

Structure body, structure body manufacturing method, and electronic apparatus

Номер: US20220055343A1
Принадлежит: Sony Group Corp, Tohoku University NUC

A structure body according to an embodiment of the present disclosure includes: a first base having one surface, and having a density lower than a density that is determined by a crystal structure and a composition of a constituent material; a second base disposed to face the one surface of the first base; and a buffer layer provided between the first base and the second base, and containing at least a metal element.

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07-02-2019 дата публикации

JOINING METHOD

Номер: US20190039168A1
Принадлежит:

A joining method for joining a first metal member with a second metal member with use of a rotary tool having a stirring pin is provided. The joining method includes steps of: butting the first metal member with the second metal member to form a butted portion; arranging an auxiliary member to be in surface-contact with the first metal member or the second metal member; and frictional stirring the butted portion in which the rotating stirring pin is inserted from a front surface of the auxiliary member and the rotary tool is relatively moved in the butted portion to join the first metal member, the second metal member and the auxiliary member, in the state that only the stirring pin is brought in contact with the first metal member, the second metal member and the auxiliary member. 1. A joining method for joining a first metal member with a second metal member with use of a rotary tool having a stirring pin , comprising steps of:butting the first metal member with the second metal member to form a butted portion;arranging an auxiliary member to be in surface-contact with the first metal member or the second metal member; andfrictional stirring the butted portion in which the rotating stirring pin is inserted from a front surface of the auxiliary member and the rotary tool is relatively moved in the butted portion to join the first metal member, the second metal member and the auxiliary member, in the state that only the stirring pin is brought in contact with the first metal member, the second metal member and the auxiliary member.2. The joining method according to claim 1 , further comprising a step of:removing the auxiliary member having a burr from the first metal member or the second metal member.3. The joining method according to claim 2 , wherein claim 2 , in the frictional stirring step claim 2 , a joining condition is set such that the burr to be generated in frictional stir joining is generated on the auxiliary member.4. A joining method for joining a first ...

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12-02-2015 дата публикации

TAILORED BLANK FOR HOT STAMPING, HOT STAMPED MEMBER, AND METHODS FOR MANUFACTURING SAME

Номер: US20150043962A1
Принадлежит:

A tailored blank for hot stamping includes a welded portion formed by butt-welding a first aluminum-plated steel sheet and a second aluminum-plated steel sheet, an Average Al concentration of a weld metal in the welded portion is in a range of 0.3 mass % to 1.5 mass %, an Acpoint of the weld metal is 1250° C. or lower, and furthermore, an aluminum layer formed during the butt-welding is present on a surface of the welded portion. 1. A tailored blank for hot stamping comprising:a welded portion formed by butt-welding a first aluminum-plated steel sheet and a second aluminum-plated steel sheet,{'sub': '3', 'wherein an average Al concentration of a weld metal in the welded portion is 0.3 mass % to 1.5 mass %, in the following formula (1), an Acpoint of the weld metal defined in unit ° C. is 1250° C. or lower, and'} [{'br': None, '[Expression 1]'}, {'br': None, 'sub': '3', 'sup': '0.5−15.2', 'Ac=910−230×C×Ni+44.7×Si+104×V+31.5×Mo+13.1×W−30×Mn−11×Cr−20×Cu+700×P+400×Al+120×As+400×Ti\u2003\u2003Formula (1)'}], 'furthermore, an aluminum layer formed during the butt-welding is present on a surface of the welded portion,'}where, C, Ni, Si, V, Mo, W, Mn, Cr, Cu, P, Al, As, and Ti in the formula represent amounts of individual elements in the weld metal in mass %, and elements not contained are considered to have an amount of zero in computation.4. The tailored blank for hot stamping according to claim 1 ,wherein, when a thickness of a thinnest portion of the weld metal is represented by t in unit mm, a sheet thickness of the first aluminum-plated steel sheet is represented by t1 in unit mm, and a sheet thickness of the second aluminum-plated steel sheet is represented by t2 in unit mm,in a case in which the t1 is equal to the t2, the t is 80% or more of the t1; andin a case in which the t1 is different from the t2, the t is 80% or more of smaller of the t1 and the t2.5. The tailored blank for hot stamping according to claim 1 ,wherein, in a case in which the t1 that is the ...

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07-02-2019 дата публикации

KINETICALLY LIMITED NANO-SCALE DIFFUSION BOND STRUCTURES AND METHODS

Номер: US20190039347A1
Принадлежит:

Bulk materials having a kinetically limited nano-scale diffusion bond is provided. The bulk materials having a kinetically limited nano-scale diffusion bond includes transparent material, absorbent opaque material and a diffusion bond. The transparent material has properties that allow an electromagnetic beam of a select wavelength to pass there through without more than minimal energy absorption. The absorbent opaque material has properties that significantly absorb energy from the electromagnetic beam. The diffusion bond is formed by the electromagnetic beam bonding the transparent material to the absorbent opaque material. Moreover, the diffusion bond has a thickness that is less than 1000 nm. 1. Bulk materials having a kinetically limited nano-scale diffusion bond comprising:transparent material having properties that allow an electromagnetic beam of a select wavelength to pass there through without more than minimal energy absorption;absorbent opaque material having properties that significantly absorb energy from the electromagnetic beam; anda diffusion bond formed by the electromagnetic beam bonding the transparent material to the absorbent opaque material, the diffusion bond having a thickness less than 1000 nm, the diffusion bond including an interfacial bond joint region that is less than 200 nm and an amorphous diffusion zone that is less than 60 nm thick and within the interfacial bond joint region; andan undisturbed transparent material and undisturbed absorbent opaque material outside the interfacial bond joint, the undisturbed transparent material and undisturbed absorbent opaque material not being affected by the formation of the diffusion bond.2. The bulk materials having a kinetically limited nano-scale diffusion bond of claim 1 , further comprising:the diffusion bond including an interfacial bond joint region that is less than 1000 nm; andundisturbed transparent material and undisturbed absorbent opaque material outside the interfacial bond joint, ...

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08-02-2018 дата публикации

BONDED BODY, SUBSTRATE FOR POWER MODULE WITH HEAT SINK, HEAT SINK, METHOD FOR PRODUCING BONDED BODY, METHOD FOR PRODUCING SUBSTRATE FOR POWER MODULE WITH HEAT SINK, AND METHOD FOR PRODUCING HEAT SINK

Номер: US20180040535A1
Принадлежит:

A bonded body is provided in which an aluminum alloy member formed from an aluminum alloy, and a metal member formed from copper, nickel, or silver are bonded to each other. The aluminum alloy member is constituted by an aluminum alloy in which a concentration of Si is in a range of 1 mass % to 25 mass %. The aluminum alloy member and the metal member are subjected to solid-phase diffusion bonding. A compound layer, which is formed through diffusion of Al of the aluminum alloy member and a metal element of the metal member, is provided at a bonding interface between the aluminum alloy member and the metal member. A Mg-concentrated layer, in which a concentration of Mg is to 3 mass % or greater, is formed at the inside of the compound layer, and the thickness of the Mg-concentrated layer is in a range of 1 μm to 30 μm. 13-. (canceled)4. A method of manufacturing a bonded body in which an aluminum alloy member formed from an aluminum alloy , and a metal member formed from copper , nickel , or silver are bonded to each other ,wherein the aluminum alloy member is constituted by an aluminum alloy in which a concentration of Si is in a range of 1 mass % to 25 mass %,in the aluminum alloy member before bonding, a concentration of Mg at least in a region which ranges from a bonding surface with the metal member to 50 μm in a depth direction is in a range of 0.3 mass % to 15 mass %, andthe aluminum alloy member and the metal member are subjected to solid-phase diffusion bonding.5. The method of manufacturing a bonded body according to claim 4 ,wherein the aluminum alloy member and the metal member are laminated, and are electrically heated while being pressurized in a laminating direction to subject the aluminum alloy member and the metal member to the solid-phase diffusion bonding.6. A method of manufacturing a power module substrate with heat sink which includes an insulating layer claim 4 , a circuit layer that is formed on one surface of the insulating layer claim 4 , a ...

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18-02-2016 дата публикации

JOINED BODY AND METHOD FOR PRODUCING THE SAME

Номер: US20160046531A1
Принадлежит:

A joined body includes a porous ceramic made of porous ceramic, a metal member made of a metal, and a joint formed of an oxide ceramic that penetrates into pores of the porous ceramic and joins the porous ceramic to the metal member . The penetration depth of the oxide ceramic into the pores of the porous ceramic is preferably 10 μm or more, and more preferably 15 to 50 μm. The joined body may be produced through a joining step of forming a joint by placing a metal raw material between a porous ceramic and a metal member and firing the metal raw material in the air at a temperature in the range of 400° C. to 900° C., where an oxide ceramic produced by oxidation of the metal raw material penetrates into the pores of the porous ceramic in the joint. 1. A joined body , comprising:a porous ceramic;a metal member; anda joint of an oxide ceramic that penetrates into pores of the porous ceramic and joins the porous ceramic to the metal member.2. The joined body according to claim 1 , wherein a penetration depth of the oxide ceramic into the pores of the porous ceramic is 10 μm or more.3. The joined body according to claim 1 , wherein a penetration depth of the oxide ceramic in the pores of the porous ceramic is in the range of 15 to 50 μm.4. The joined body according to claim 1 , wherein the average pore size of the porous ceramic is A (μm) claim 1 , the average particle size of a raw material powder of the oxide ceramic is B (μm) claim 1 , and B/A is in the range of 0.1 to 5.0.5. The joined body according to claim 1 , wherein the thickness of a reaction layer at an interface between the porous ceramic and the oxide ceramic is 0.1 μm or less.6. The joined body according to claim 1 , wherein the porosity of the oxide ceramic penetrating into the porous ceramic is in the range of 0% to 50% by volume.7. The joined body according to claim 1 , wherein the joint includes a penetrating portion in which the oxide ceramic penetrates into the pores and a non-penetrating portion ...

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16-02-2017 дата публикации

METHOD OF MANUFACTURING COMPOSITE MATERIAL

Номер: US20170043428A1
Автор: LEE Kwangjin, SONG Ram
Принадлежит:

The present invention provides a method of manufacturing composite material, comprising the steps of: coating a thermally conductive composition on a surface portion of a metal material in at least one configuration from among a paste, film, and tape; and friction stirring the metal material, coated with the thermally conductive composition, at least once, and reacting at least a part of the surface portion of the metal material with the thermally conductive composition to form a composite material. 1. A method of manufacturing a composite material , the method comprising:coating a thermally conductive composition on a surface portion of a metallic material, the thermally conductive composition being in at least one form of a paste, a film, and a tape; andperforming a friction stir processing on the metallic material coated with the thermally conductive composition at least once such that at least part of the surface portion of the metallic material reacts with the thermally conductive composition to form a composite material.2. The method of claim 1 , wherein a thermally conductive material used as the thermally conductive composition comprises at least one of graphite claim 1 , carbon nanotubes (CNT) claim 1 , and graphene.3. The method of claim 2 , wherein the thermally conductive composition comprises the thermally conductive material in an amount of 0.1 wt % to 30.0 wt %.4. The method of claim 1 , wherein the thermally conductive composition comprises at least one of an organic compound claim 1 , a silicon-based compound claim 1 , and a lightweight polymer.5. The method of claim 1 , wherein the thermally conductive composition further comprises hydrocarbons.6. The method of claim 1 , wherein claim 1 , the performing a friction stir processing further comprises:after a rotating tool is installed on the surface portion of the metallic material coated with the thermally conductive composition, heating the surface portion of the metallic material coated with the ...

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15-02-2018 дата публикации

JOINING METHOD AND METHOD FOR MANUFACTURING COMPOSITE ROLLED MATERIAL

Номер: US20180043465A1
Автор: Hori Hisashi
Принадлежит:

A joining method is capable of suitably joining metal members of different kinds. The joining method includes a step of preparing a first metal member having a first upper surface, a first lower surface and a first inclined surface connecting the first upper surface and the first lower surface, and a second metal member having a second upper surface, a second lower surface and a second inclined surface connecting the second upper surface and the second lower surface. The second metal member has a higher melting temperature than the first metal member. A butting interface is formed by butting the first inclined surface and the second inclined surface. The first and second metal members are joined by moving a rotary tool along the butting interface while the rotary tool is inserted from the first upper surface and a stirring pin is in contact with the first metal member. 1. A joining method of joining a pair of metal members made of different materials by using a rotary tool provided with a stirring pin having a diameter becoming smaller toward an extremity of the stirring pin , comprising: a first metal member having a first upper surface, a first lower surface, and a first inclined surface connecting the first upper surface and the first lower surface, and', 'a second metal member having a second upper surface, a second lower surface, and a second inclined surface connecting the second upper surface and the second lower surface, the second metal member having a higher melting temperature than the first metal member;, 'a preparatory step of preparing'}a butting step of forming a butting interface by butting the first inclined surface and the second inclined surface against each other in such a manner that a first upper intersecting line formed by the first upper surface and the first inclined surface is positioned further in a direction of the second metal member than a first lower intersecting line formed by the first lower surface and the first inclined surface, ...

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15-02-2018 дата публикации

SYSTEM FOR AND METHOD OF LINKING BY FRICTION WELDING A FIRST PIECE OF STEEL TO A SECOND PIECE OF STEEL WITH USE OF NI-BASED ALLOYS ADAPTER

Номер: US20180043467A1
Автор: Huysmans Staf
Принадлежит: Laborelec CVBA

A system () is provided, comprising a two-sided adapter (), made of a Ni-based alloy, that is connected at each of the two sides with a different type of metal, e.g. steel (), and wherein the connection () of the different types of metal, e.g. steel () with the adapter (), wherein it is achieved at least in part by use of friction welding. A method for linking different types of metal, e.g. steel () by using a two-sided adapter () as an intermediate, wherein at least one of the adapter-metal (e.g. steel) connections () is made by means of friction welding, is also provided. 1. A system comprising: a two-sided tubular adapter made of a Ni-based alloy , connected to either a first piece of metal and/or to a second piece of metal , wherein the first and second piece differ in at least one chemical or physical parameter; wherein the connection of at least the first or the second piece with the adapter is is made by friction welding.2. The system of claim 1 , wherein the first piece of metal and/or the second piece of metal are made of steel.3. The system of claim 1 , wherein the two-sided tubular adapter is a ring shape or donut shaped.4. The system of claim 1 , wherein the first piece of material is made of martensitic steel and/or the second piece of material is made of austenitic steel.5. The system of claim 1 , wherein the Ni-based alloy is additive manufactured.6. The system of claim 1 , wherein the Ni-based alloy is made of EPRI P87 alloy claim 1 , A617 alloy claim 1 , or A82 alloy.7. The system of claim 1 , wherein the first piece of material is made of austenitic steel claim 1 , and/or the second piece of material is made of another Ni-based alloy claim 1 , differing from the Ni-based alloy out of which the two-sided tubular adapter is made.8. The system of claim 1 , wherein the two-sided tubular adapter is provided with edge-shaped end surfaces.9. A method for linking a first piece of metal to a second piece of metal claim 1 , wherein the first and second piece ...

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18-02-2016 дата публикации

METHOD OF FORMING AN INFLATED AEROFOIL

Номер: US20160047249A1
Автор: QUIGLEY David Adrian
Принадлежит:

There is proposed a method of forming an inflated aerofoil (), the method comprising the steps of: forming a layered, planar pre-form (); providing at least one stress-relieving opening () through the pre-form; hot creep forming and inflating the pre-form () to form an intermediate aerofoil; and subsequently removing material from the intermediate aerofoil, including at least a region containing the or each stress-relieving opening (), to form a finished aerofoil. 1. A method of forming an inflated aerofoil , the method comprising the steps of: forming a layered , planar pre-form; providing at least one stress-relieving opening through the pre-form; hot creep forming and inflating the pre-form to form an intermediate aerofoil; and subsequently removing material from the intermediate aerofoil , including at least a region containing the or each stress-relieving opening , to form a finished aerofoil.2. A method according to claim 1 , further including the step of providing at least one datum region on the pre-form claim 1 , for use in locating the pre-form during said hot creep forming and inflating steps claim 1 , wherein said step of forming said at least one stress-relieving opening involves forming the or each opening in or adjacent a said datum region claim 1 , and said step of removing material from the intermediate aerofoil involves removing the or each datum region.3. A method according to claim 1 , further including a step of defining on the pre-form a nominal profile of the aerofoil to be formed.4. A method according to claim 3 , wherein said step of defining a nominal profile involves machining the nominal profile on at least one outwardly directed face of the pre-form.5. A method according to claim 2 , further including a step of defining on the pre-form a nominal profile of the aerofoil to be formed claim 2 , wherein the or at least one said stress-relieving opening is provided through the pre-form at a position located between a said datum region and a ...

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07-02-2019 дата публикации

Wire bonding method

Номер: US20190043645A1
Автор: Yasunori Nabeta
Принадлежит: Yazaki Corp

A wire bonding method includes: arranging a plurality of wires by inserting the wires with partially-exposed conductors into each groove of a wire arrangement tool provided with a plurality of grooves; and sandwiching the conductors of the plurality of wires arranged by the wire arrangement tool in a predetermined direction and bonding the conductors to each other. Further, in this wire bonding method, the sandwiching causes one arbitrary conductor among the conductors to receive a biasing force in a direction intersecting a direction of a force applied by the sandwiching, from another conductor in contact with the one arbitrary conductor among the conductors.

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06-02-2020 дата публикации

APPARATUS FOR STACKING SUBSTRATES AND METHOD FOR THE SAME

Номер: US20200043860A1
Принадлежит: NIKON CORPORATION

A substrate stacking apparatus that stacks first and second substrates on each other, by forming a contact region where the first substrate held by a first holding section and the second substrate held by a second holding section contact each other, at one portion of the first and second substrates, and expanding the contact region from the one portion by releasing holding of the first substrate by the first holding section, wherein an amount of deformation occurring in a plurality of directions at least in the first substrate differs when the contact region expands, and the substrate stacking apparatus includes a restricting section that restricts misalignment between the first and second substrates caused by a difference in the amount of deformation. In the substrate stacking apparatus above, the restricting section may restrict the misalignment such that an amount of the misalignment is less than or equal to a prescribed value. 124-. (canceled)25. A substrate processing method for processing at least one of a first substrate and a second substrate to be stacked on each other , comprising:forming a structure on each of the first substrate and the second substrate, the structure of the at least one of the first substrate and the second substrate being formed at a position such that misalignment is restricted between the structure of the first substrate and the structure of the second substrate once the first substrate and the second substrate have been stacked on each other to form a substrate stack.26. The substrate processing method according to claim 25 , whereinthe structure of the at least one of the first substrate and the second substrate is formed at the position according to an amount of deformation of the first substrate.27. The substrate processing method according to claim 26 , whereinthe amount of deformation includes an amount of deformation generated in the first substrate during a process of stacking the first substrate and the second substrate on ...

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14-02-2019 дата публикации

Ultrasonic bonding jig, ultrasonic bonding method, and bonding structure

Номер: US20190047079A1
Принадлежит: Nippon Mektron KK

An ultrasonic bonding jig includes: a plurality of protrusions; and a planar portion among protrusions formed among base ends of the protrusions. The protrusions have side surfaces of tapered surfaces, the side surfaces being positioned in a vibration direction. At the tapered surfaces, an inclination of a tangent at distal ends of the protrusions, with respect to the vibration direction, is larger than an inclination of a tangent at the base ends of the protrusions, with respect to the vibration direction.

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14-02-2019 дата публикации

CLAD MATERIAL AND METHOD FOR MANUFACTURING CLAD MATERIAL

Номер: US20190047254A1
Автор: Yamamoto Shinji
Принадлежит: HITACHI METALS, LTD.

A clad material includes a first layer made of stainless steel and a second layer made of Cu or a Cu alloy and roll-bonded to the first layer. In the clad material, a grain size of the second layer measured by a comparison method of JIS H 0501 is 0.150 mm or less. 1. A clad material comprising:a first layer made of stainless steel; anda second layer made of Cu or a Cu alloy and roll-bonded to the first layer, whereina grain size of the second layer measured by a comparison method of JIS H 0501 is 0.150 mm or less.2. The clad material according to claim 1 , wherein the grain size of the second layer is 0.130 mm or less.3. The clad material according to claim 1 , further comprising a third layer made of stainless steel and roll-bonded to a side of the second layer opposite to the first layer.4. The clad material according to claim 1 , wherein the stainless steel is austenitic stainless steel.512-. (canceled) The priority application number JP2017-154123, Clad Material and Method for Manufacturing Clad Material, Aug. 9, 2017, Shinji Yamamoto, upon which this patent application is based, is hereby incorporated by reference.The present invention relates to a clad material and a method for manufacturing the clad material, and more particularly, it relates to a clad material in which Cu or a Cu alloy and stainless steel are roll-bonded to each other and a method for manufacturing the clad material.A clad material in which stainless steel and Cu or a Cu alloy are roll-bonded to each other is known in general, as disclosed in Japanese Patent Laid-Open No. 2005-134073, for example.Japanese Patent Laid-Open No. 2005-134073 discloses a stainless steel-copper clad formed by rolling or pressure-bonding (cladding) a skin material made of copper to both the front and back surfaces of a core material made of stainless steel.Japanese Patent Laid-Open No. 2005-134073 does not describe in detail a specific rolling or pressure-bonding method for the stainless steel-copper clad. However, ...

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14-02-2019 дата публикации

METHOD FOR MANUFACTURING CLAD MATERIAL

Номер: US20190047256A1
Автор: Yamamoto Shinji
Принадлежит: HITACHI METALS, LTD.

A clad material includes a first layer made of stainless steel and a second layer made of Cu or a Cu alloy and roll-bonded to the first layer. In the clad material, a grain size of the second layer measured by a comparison method of JIS H 0501 is 0.150 mm or less. 1. A method for manufacturing a clad material , comprising:softening annealing for softening a first metal plate made of stainless steel and softening a second metal plate made of Cu or a Cu alloy;clad rolling for rolling and bonding the first metal plate and the second metal plate, which have undergone the softening annealing, to each other in a state where the first metal plate and the second metal plate are stacked on each other so as to produce a pressure-bonded material; anddiffusion annealing for performing a diffusion treatment on the pressure-bonded material, whereinthe clad material including a first layer made of stainless steel and a second layer made of Cu or a Cu alloy and roll-bonded to the first layer, in which a grain size of the second layer measured by a comparison method of JIS H 0501 is 0.150 mm or less, is produced by reducing a thickness of the second metal plate in the pressure-bonded material before the diffusion annealing to 20% or more of a thickness of the second metal plate after the softening annealing.2. The method for manufacturing a clad material according to claim 1 , whereinthe thickness of the second metal plate in the pressure-bonded material before the diffusion annealing is reduced to 25% or more and 50% or less of the thickness of the second metal plate after the softening annealing.3. The method for manufacturing a clad material according to claim 1 , whereinthe diffusion annealing is performed under a temperature condition of 850° C. or more and 1000° C. or less.4. The method for manufacturing a clad material according to claim 3 , whereinthe diffusion annealing is performed under a temperature condition of 900° C. or more and 1000° C. or less.5. The method for ...

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03-03-2022 дата публикации

Liquid cooling head and manufacturing method thereof

Номер: US20220065561A1
Принадлежит: Auras Technology Co Ltd

A liquid cooling head manufacturing method includes the following steps. First, a liquid channel main body is provided. Then, a heat dissipation bottom plate and a heat sink are disposed in different recessed indentations in the liquid channel main body. The heat dissipation bottom plate and the heat sink are welded in the liquid channel main body and a cover plate is sealed on the liquid channel main body.

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25-02-2016 дата публикации

METHOD FOR CONNECTING A TUBULAR CABLE LUG TO A STRAND PRODUCED FROM ALUMINIUM

Номер: US20160052081A1
Автор: REGENBERG Claus
Принадлежит: Telsonic Holding AG

A method for connecting a tubular cable lug produced from a non-ferrous metal to a strand produced from aluminium, includes steps of providing a tubular cable lug having a tubular portion and a connecting portion, providing an ultrasonic welding device having a sonotrode that has a pressure surface and having an anvil that has a mating pressure surface, securing the connecting portion to the anvil by clamping such that the tubular portion faces the mating pressure surface of the anvil, inserting one end of the strand into the tubular portion of the tubular cable lug, bringing the pressure surface into contact with the tubular portion, pressing the pressure surface against the tubular portion such that the tubular portion is forced against the mating pressure surface, and generating an ultrasound vibration oriented approximately perpendicular to a tube axis of the tubular portion by means of the sonotrode. 1. A method for connecting a tubular cable lug produced from a non-ferrous metal to a strand produced from aluminium , said method comprising the following steps:providing a tubular cable lug having a tubular portion and a connecting portion extending therefrom,providing an ultrasonic welding device having a sonotrode that has a pressure surface curved in a comb-like manner and having an anvil that has a mating pressure surface curved in a comb-like manner,securing the connecting portion to the anvil by clamping in such a way that the tubular portion faces the mating pressure surface of the anvil,inserting one end of the strand into the tubular portion of the tubular cable lug,bringing the pressure surface into contact with the tubular portion,pressing the pressure surface against the tubular portion such that the tubular portion is forced against the mating pressure surface, andgenerating an ultrasound vibration oriented approximately perpendicular to a tube axis of the tubular portion by means of the sonotrode, in such a way that the tubular portion is deformed ...

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13-02-2020 дата публикации

Friction stir welding machines and methods

Номер: US20200047279A1
Автор: Heath Edward Misak
Принадлежит: Spirit AeroSystems Inc

A friction stir welding machine and method that injects filler materials into a weld joint and determines the amount of materials to add by monitoring and compensating for insufficient internal weld pressures in the joint. Two workpieces are placed adjacent one another in an abutting relationship with a joint formed between them. A pin tool is inserted in the joint, rotated, and moved along the joint as the pin is rotating so as to mix and heat materials in the joint. Internal weld pressures in the joint adjacent the pin tool are monitored, and filler materials are injection into the joint when an internal weld pressure below a threshold weld pressure is detected.

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23-02-2017 дата публикации

Bonding method and bonded structure

Номер: US20170050262A1
Принадлежит: Ultex Corp

A bonding target member 1 having a solid bonding material 3 with aluminum as a main component is interposed between a metal member 2 and a ceramic member 4 and an elastic member 12 are pressurized by a pressurizing section 13 and a bonding tool section 15 of a resonator 14 in a vertical direction. The bonding tool section 15 of the resonator 14 resonates with sound vibration or ultrasound vibration transmitted from an oscillator 16. An interfacial portion between the metal member 2 and the bonding material 3 with aluminum as a main component and an interfacial portion between the bonding material 3 with aluminum as a main component and the ceramic member 4 each receive pressurization and vibration energy to be bonded together. The metal member 2 and the ceramic member 4 can be bonded together at ordinary temperature in the atmosphere with the bonding material 3 with aluminum as a main component. When the ceramic member 4 has a thickness resistant to pressurization and vibration energy at the time of bonding to resist crack, the elastic member 12 may be disposed on a metal member 2 side, or may not be used.

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23-02-2017 дата публикации

IMPROVED STRUCTURAL ELEMENTS OBTAINED BY LINEAR FRICTION WELDING

Номер: US20170050264A1
Принадлежит: Constellium Issoire

The invention concerns a method for forming by welding along a flat surface an article. The method according to the invention is particularly useful to improve strength and elongation of welded joints obtained by linear friction welding. Structural articles of aircrafts obtained with the method of the invention are advantageous, in particular aircraft structural members. 1. A method for forming by welding along a flat surface an article comprising at least a first metallic member in the form of an aluminium alloy wrought product having elongated grains in a longitudinal direction (L10) , with an anisotropy index in a longitudinal oriented surface of at least 4 according to ASTM E112 and/or an anisotropy index in a planar oriented surface of at least 1.5 according to ASTM E112 the first metallic member is positioned in contact with the second metallic member so that said longitudinal direction (L10) of the elongated grains is positioned substantially within the weld plane,', 'the article is formed by linear friction welding., 'and at least a second metallic member, wherein'}2. A method according to wherein the transverse direction (T10) of the grains of said first metallic member is substantially perpendicular to the weld plane.3. A method according to wherein the oscillating direction is substantially parallel to the planar direction of the grains (P10) of said first metallic member.4. A method according to wherein said first metallic member is a forge member and wherein said second metallic member is an oscillating member.5. A method according to wherein said first metallic member is in a temper that is not artificially aged claim 1 , optionally T3 or T4 claim 1 , before welding and wherein a post weld heat treatment is carried out.6. A method according to wherein said second metallic member is in the form of an aluminium alloy wrought product claim 5 , in a temper that is not artificially aged claim 5 , having elongated grains in a longitudinal direction (L11) ...

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22-02-2018 дата публикации

COMPONENTS AND SYSTEMS FOR FRICTION STIR WELDING AND RELATED PROCESSES

Номер: US20180050419A1
Принадлежит: Novelis Inc.

Described herein are tools and systems for friction stir welding, including cooling and clamping systems. Also disclosed are process parameters for friction stir welding aluminum metals, in some cases thick gauge aluminum metals, to other metals. The tool and process parameters can be used in transportation, electronics, industrial and motor vehicle applications, just to name a few. 1. A friction stir welding tool comprising:a shoulder comprising a diameter; anda pin extending from the shoulder, the pin comprising a length extending from a tip of the pin to a base of the pin, wherein the diameter of the shoulder is greater than three times the length of the pin.2. The friction stir welding tool of claim 1 , wherein the diameter of the shoulder is greater than approximately 3.5 times the length of the pin claim 1 , and wherein the shoulder of the tool comprises a concave surface.3. The friction stir welding tool of claim 1 , wherein the pin comprises a plurality of generally planar surfaces that are separated from one another by threads.4. The friction stir welding tool of claim 3 , wherein the plurality of generally planar surfaces comprises five generally planar surfaces.5. The friction stir welding tool of claim 1 , wherein the pin is tapered along its length.6. The friction stir welding tool of claim 1 , wherein the tip of the pin is domed such that the tip comprises a convex surface.7. The friction stir welding tool of claim 1 , wherein the friction stir welding tool is formed of M42 high-speed tool steel.8. A system for friction stir welding comprising:a friction stir welding tool, wherein the friction stir welding tool comprises a shoulder comprising a diameter and a pin extending from the shoulder, the pin comprising a length extending from a tip of the pin to a base of the pin, wherein the diameter of the shoulder is greater than three times the length of the pin;a first metal plate having a first thickness;a second metal plate having a second thickness ...

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22-02-2018 дата публикации

APPARATUSES AND METHODS FOR FABRICATING METAL MATRIX COMPOSITE STRUCTURES

Номер: US20180050420A1
Автор: Verma Ravi
Принадлежит: The Boeing Company

A method for forming a metal matrix composite (MMC) structure includes forming an assembly including at least two blocks of a primary phase material sharing an interface at which a secondary phase material is disposed. The assembly has a length, a width, and a thickness. The method also includes clamping the assembly to at least one of urge the at least two blocks toward each other or maintain the at least two blocks at a predetermined position. Also, the method includes passing a rotating friction-stir pin along the interface from the front edge to the rear edge. The friction-stir pin has a mixing length extending at least the width of the assembly, and passing the friction-stir pin along the length of the assembly disperses the secondary phase material into the primary phase material and welds the at least two blocks together. 1. A method for forming a metal matrix composite (MMC) structure , the method comprising:forming an assembly including at least two blocks of a primary phase material sharing an interface at which a secondary phase material is disposed, the assembly having a length extending from a front edge to a rear edge, a width extending perpendicular to the length, and a thickness;clamping the assembly to at least one of urge the at least two blocks toward each other or maintain the at least two blocks at a predetermined position;passing a rotating friction-stir pin along the interface from the front edge to the rear edge, wherein the friction-stir pin has a mixing length extending at least the width of the assembly, wherein the passing the friction-stir pin disperses the secondary phase material into the primary phase material and welds the at least two blocks together.2. The method of claim 1 , further comprising supporting the friction-stir pin at opposite ends as the stir friction pin is passed along the interface.3. The method of claim 2 , further comprising driving the friction-stir pin at the opposite ends as the stir friction pin is passed ...

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26-02-2015 дата публикации

Method for Producing a Nickel Aluminide Coating on a Metal Substrate, and Part having One Such Coating

Номер: US20150056467A1
Принадлежит:

The invention relates to a method for producing a nickel aluminide coating on a metal substrate. Said method includes the following steps: a) coating the substrate with a nickel deposit; b) applying an aluminum sheet onto the nickel deposit from step a) so as to form an assembly made up of the substrate coated with the nickel deposit and the aluminum sheet; and c) subjecting said assembly to heat treatment at a temperature that is lower than the melting point of aluminum, and at a low pressure so as to induce a reaction between the aluminum and the nickel and thus form a β-NiAl nickel aluminide layer mounted on a nickel layer. The invention is particularly of use for protecting the materials used in turbines of aircraft engines. 1. Method for obtaining a nickel aluminide coating on a metal substrate , characterized in that it comprises the following steps:a) coating the substrate with a deposition of nickel;b) applying an aluminium foil to the deposition of nickel of step a) in order to form an assembly constituted by the substrate coated with the deposition of nickel and the aluminium foil; andc) subjecting the assembly to heat treatment at a temperature below the melting temperature of aluminium and under reduced pressure in order to cause a reaction between the aluminium and the nickel and thus form a layer of nickel aluminide β-NiAl on top of a layer of nickel.2. Method according to claim 1 , characterized in that step a) comprises a deposition of pure nickel or of a nickel alloy.3. Method according to claim 2 , characterized in that the nickel alloy comprises at least one element chosen from W claim 2 , Ce claim 2 , Cr claim 2 , Pt claim 2 , Pd claim 2 , Hf claim 2 , Y and Zr.4. Method according to either or claim 2 , characterized in that step a) comprises a deposition of nickel followed by a deposition of a nickel alloy claim 2 , in particular of a nickel-palladium alloy.5. Method according to either or claim 2 , characterized in that step a) is preceded by a ...

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25-02-2016 дата публикации

Cold Plate, Device Comprising a Cold Plate and Method for Fabricating a Cold Plate

Номер: US20160056088A1
Принадлежит:

A cold plate includes a single piece member and a channel. A top side of the channel is open. A bottom side of the channel opposite the top side has an inlet and an outlet. 1. A device , comprising:a semiconductor module; anda cold plate comprised of a single piece member.2. The device of claim 1 , wherein the cold plate comprises a channel.3. The device of claim 2 , wherein a main face of the semiconductor module forms a top part of an inner surface of the channel.4. The device of claim 1 , wherein the semiconductor module is a power semiconductor module.5. The device of claim 1 , wherein the cold plate is coupled to the semiconductor module via one or more of a sintering bond claim 1 , a solder bond claim 1 , a welded joint claim 1 , and an active metal brazing bond.6. The device of claim 1 , wherein the cold plate comprises one or more of aluminum claim 1 , an aluminum alloy claim 1 , copper claim 1 , and a copper alloy.7. The device of claim 3 , wherein the semiconductor module comprises a base plate claim 3 , and wherein the main face of the semiconductor module forming the top part of the inner surface of the channel is a main face of the base plate.8. The device of claim 3 , wherein the semiconductor module comprises a substrate comprising a stack of more than one material layers claim 3 , and wherein the main face of the semiconductor module forming the top part of the inner surface of the channel comprises an outer layer of the stack.9. The device of claim 1 , wherein the single piece member comprises one or more of a stamped metal plate claim 1 , a rolled metal plate claim 1 , and a pressed metal plate.10. The device of claim 2 , wherein the channel comprises structures configured to cause turbulences in a cooling fluid flowing through the channel.11. The device of claim 10 , wherein a main face of the semiconductor module forms a top part of an inner surface of the channel claim 10 , and wherein the structures are arranged in a bottom part of the inner ...

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25-02-2016 дата публикации

Leadframe and method of manufacturing the same

Номер: US20160056092A1
Принадлежит: INFINEON TECHNOLOGIES AUSTRIA AG

A hybrid leadframe is provided comprising a thin leadframe layer comprising a diepad and a structured region; and a metal layer being thicker than the thin leadframe layer and arranged on the diepad.

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14-02-2019 дата публикации

METHOD FOR MANUFACTURING COMPOSITE WAFER PROVIDED WITH OXIDE SINGLE CRYSTAL THIN FILM

Номер: US20190051525A1
Автор: Akiyama Shoji
Принадлежит: SHIN-ETSU CHEMICAL CO., LTD.

A composite wafer includes an oxide single crystal thin film of lithium tantalate or lithium niobate transferred onto the entire face of a support wafer and is free from cracking or peeling on a bonding interface between the support wafer and the oxide single crystal thin film. A method for manufacturing a composite wafer at least includes a step of forming an ion-implanted layer in an oxide single crystal wafer, a step of subjecting at least one of the ion-implanted surface of the oxide single crystal wafer and a surface of a support wafer to a surface activation treatment, a step of bonding the ion-implanted surface of the oxide single crystal wafer to the surface of the support wafer to form a laminate, a step of subjecting the laminate to a first heat treatment at a temperature not less than 90° C. and not causing cracking, a step of applying a mechanical impact to the ion-implanted layer, and a step of subjecting the support wafer having the transferred oxide single crystal thin film to a second heat treatment at 250° C. to 600° C. to yield a composite wafer. 1. A method for manufacturing a composite wafer including an oxide single crystal thin film on a support wafer , the method at least comprising the steps of:implanting atomic hydrogen ions or molecular hydrogen ions through a surface of an oxide single crystal wafer that is a lithium tantalate wafer or a lithium niobate wafer to form an ion-implanted layer in the oxide single crystal wafer;subjecting at least one of the ion-implanted surface of the oxide single crystal wafer and a surface of a support wafer to be bonded to the oxide single crystal wafer, to a surface activation treatment;after the surface activation treatment, bonding the ion-implanted surface of the oxide single crystal wafer to the surface of the support wafer to yield a laminate;subjecting the laminate to a first heat treatment at a temperature not less than 90° C. and not causing cracking;applying a mechanical impact to the ion- ...

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10-03-2022 дата публикации

LINEAR MOTION SHAFT FOR STEERING DEVICE, STEERING DEVICE, AND METHOD OF MANUFACTURING THESE

Номер: US20220072602A1
Автор: Unno Kentaro
Принадлежит:

A method for manufacturing a linear motion shaft includes: manufacturing a first shaft portion, and connecting the first shaft portion and a second shaft portion by friction welding. A first input section is formed in a material for the first shaft portion to obtain the first shaft portion and then a gripped section for centering is formed on the outer peripheral surface of an axially end portion of the first shaft portion on the side connected to the second shaft portion based on the first input section. The friction welding is performed by abutting the axially end portions of the first shaft portion and the second shaft portion in a state where the gripped section is gripped by a first gripping tool for centering, the first shaft portion is rotated with the first gripping tool, and the second shaft portion remains without rotating. 1. (canceled)2. (canceled)3. A method for manufacturing a linear motion shaft for a steering device ,the linear motion shaft comprising: a first shaft portion having a first input section on an outer peripheral surface thereof to which a driving force for making linear motion in an axial direction is input, a second shaft portion, and a joint between the first shaft portion and the second shaft portion,the manufacturing method comprising:a process of manufacturing the first shaft portion, anda process of connecting the first shaft portion and the second shaft portion by friction welding,the process of manufacturing the first shaft portion including a process of forming the first input section in a material for the first shaft portion and a process of forming a gripped section for centering on an outer peripheral surface of an end portion in the axial direction of the first shaft portion on a side connected to the second shaft portion based on the first input section after forming the first input section, andthe friction welding is performed by abutting an end portion in the axial direction of the first shaft portion and an end portion ...

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05-03-2015 дата публикации

PLATE HEAT EXCHANGER

Номер: US20150060030A1
Принадлежит:

Disclosed is a method for producing a permanently joined plate heat exchanger comprising a plurality of metal heat exchanger plates having a solidus temperature above 1100° C., provided beside each other and forming a plate package with first plate interspaces for a first medium and second plate interspaces for a second medium, wherein the first and second plate interspaces are provided in an alternating order in the plate package, wherein each heat exchanger plate comprises a heat transfer area and an edge area comprising bent edges which extend around the heat transfer area, wherein a first surface of the plates forms a convex shape and a second surface of the plates forms a concave shape, wherein the heat transfer area comprises a corrugation of elevations and depressions, wherein said corrugation of the plates and the bent edges are provided by pressing the plates. Also disclosed is a plate heat exchanger produced by the method. 2. The method according to claim 1 , wherein the boron originates from any of elemental boron and boron of a boron compound selected from any of the following compounds: boron carbide claim 1 , silicon boride claim 1 , nickel boride and iron boride.3. The method according to claim 1 , wherein the silicon originates from any of elemental silicon and silicon of a silicon compound selected from any of the following compounds: silicon carbide claim 1 , silicon boride and ferrosilicon.4. The method according to claim 1 , wherein the melting depressant component comprises at least 40 wt % boron and silicon.5. The method according to claim 1 , wherein the melting depressant component comprises at least 85 wt % boron and silicon.6. The method according to claim 1 , wherein boron constitutes at least 10 wt % of the boron and silicon content of the melting depressant compound.7. The method according to claim 1 , wherein boron constitutes at least 55 wt % of the boron and silicon content of the melting depressant compound.8. The method according to ...

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21-02-2019 дата публикации

HANDLE FOR EXOTHERMIC MOLD WITH SPRING CONNECTORS

Номер: US20190054557A1
Принадлежит:

Disclosed is a handle clamp for an exothermic mold. The clamp includes a pair of legs, each having a plurality of rods that are shaped to fit into engagement holes on sections of the mold. The rods of each leg engage with one section of the mold. Engagement brackets are rotatably disposed on one or more or the rods. The brackets each have a thumb bolt that can be extended toward a mold section connected with the clamp. When engaged with the mold section, the thumb bolt stabilizes the mold section on the handle. A detent mechanism is provided between the bracket and the leg of the handle. The detent mechanism releaseably holds the bracket in one of a selected plurality of rotational positions with respect to the rod. By selecting different rotational positions for the brackets, the handle can be configured to engage with different configurations of mold. The thumb bolts that are biased toward the mold section by a spring. The bolts include a key that can be aligned or misaligned with a key slot on the bracket. By aligning the key with the key with the key slot, the bolt can be moved toward or away from the mold section under the biasing force of the spring. By misaligning the key and key slot, the bolt can be locked into engagement with the mold section or else held in a disengaged position. 1. A handle clamp for an exothermic mold comprising:a pair of grips;a pair of legs connected with respective ones of the grips, the legs arranged to move toward and away from one another in response to motion of the grips;a plurality of engagement rods disposed on each of the legs, wherein the engagement rods on each leg are adapted to engage with respective sections of an exothermic mold;one or more brackets, each bracket rotatably disposed on one of the rods; anda detent mechanism to releasably hold the bracket in a selected angular position with respect to the rod.2. The handle clamp of claim 1 , wherein the detent mechanism comprises a convex feature and a plurality of ...

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02-03-2017 дата публикации

METHOD OF JOINING MULTIPLE COMPONENTS AND AN ASSEMBLY THEREOF

Номер: US20170057005A1
Принадлежит: GM GLOBAL TECHNOLOGY OPERATIONS LLC

A method of joining multiple components is disclosed. The method includes arranging a first component having a first surface, an opposing second surface, and a feature, in contact with a second component having a first surface, an opposing second surface, and defining an aperture. When so arranged, the first surface of the first component is adjacent to the second surface of the second component. The method also includes positioning a fastener on the first surface of the second component and in contact with the feature of the first component, such that at least a portion of the fastener overlaps the aperture on the first surface of the second component. The method additionally includes abutting and fusing the fastener to the feature of the first component to thereby affix the first component to the second component. 1. A method of joining multiple components , the method comprising:arranging a first component having a first surface, an opposing second surface, and a feature in contact with a second component, wherein the second component has a first surface, an opposing second surface, and defines an aperture, such that the first surface of the first component is adjacent to the second surface of the second component;positioning a fastener on the first surface of the second component and in contact with the feature of the first component, such that at least a portion of the fastener overlaps the aperture on the first surface of the second component; andabutting and fusing the fastener to the feature of the first component and thereby affixing the first component to the second component via the fastener.2. The method of claim 1 , wherein the first component is constructed from plastic and the second component is constructed from metal.3. The method of claim 2 , wherein the plastic is a carbon fiber reinforced thermoplastic (CFRTP) and the metal is steel.4. The method of claim 2 , wherein the fastener is a one-sided rivet constructed from plastic.5. The method of ...

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01-03-2018 дата публикации

ROTARY FRICTION WELDED BLANK FOR PECVD HEATED SHOWERHEAD

Номер: US20180057940A1
Автор: Kern Kurt, Madsen Eric
Принадлежит:

A deposition apparatus for processing substrates includes a vacuum chamber including a processing zone in which a substrate may be processed. A showerhead assembly includes a stem, face plate and back plate wherein the stem is rotary friction welded to the back plate. A substrate pedestal assembly is configured to support a substrate on an upper surface thereof when a substrate is processed in the deposition apparatus. 1. A blank for a plasma enhanced chemical vapor deposition (PECVD) heated showerhead comprising a stem , back plate and face plate , the blank comprising a stem precursor blank and a back plate precursor blank joined by rotary friction welding.2. The blank of claim 1 , wherein the stem precursor blank comprises a round bar of aluminum material having a length of at least about 6 inches and diameter of at least about 3 inches and the back plate precursor blank comprises a circular plate of aluminum material having a thickness of at least about 1 inch and diameter of at least about 13 inches claim 1 , the axial end of the stem precursor blank rotary friction welded to the center of one side of the back plate precursor blank.3. The blank of claim 1 , wherein the back plate precursor blank includes a raised hub on one side thereof claim 1 , the raised hub rotary friction welded to the axial end of the stem precursor blank.4. The blank of claim 1 , wherein the back plate precursor blank comprises a rolled plate of an aluminum alloy and the stem precursor blank comprises an extruded bar of an aluminum alloy.5. The blank of claim 4 , wherein the aluminum alloy is 6061.6. A showerhead assembly comprising a face plate and the blank of claim 1 , wherein the blank has been machined to remove weld flash around the weld interface claim 1 , the stem precursor blank has been machined to desired dimensions of a stem claim 1 , the back plate precursor blank has been machined to desired dimensions of a back plate claim 1 , the face plate has been attached to the back ...

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28-02-2019 дата публикации

DEVICES, SYSTEMS, AND METHODS FOR INCREASED WEAR RESISTANCE DURING LOW TEMPERATURE FRICTION STIR PROCESSING

Номер: US20190061046A1
Принадлежит:

A method of friction stir processing (FSP) includes contacting a first workpiece with a FSP tool, where the first workpiece is a low-melting temperature metal or alloy and the FSP tool is a single-body FSP tool having a diamond working surface. The method also includes rotating the FSP tool in contact with the first workpiece at an interface and generating thermal energy at the interface to heat the first workpiece. The method further includes conducting thermal energy away from the interface with the FSP tool, and friction stirring the first workpiece at a temperature of the FSP tool below 800° C. 1. A method of friction stir processing (FSP) , the method comprising:contacting a first workpiece with a FSP tool, the first workpiece being a low-melting temperature metal or alloy and the FSP tool being a single-body FSP tool having a diamond working surface;rotating the FSP tool in contact with the first workpiece at an interface;generating thermal energy at the interface to heat the first workpiece;conducting thermal energy away from the interface with the FSP tool; andfriction stirring the first workpiece at a temperature of the FSP tool below 800 degrees Celsius.2. The method of claim 1 , the first workpiece being a single-phase low melting temperature alloy.3. The method of claim 1 , wherein the first workpiece is aluminum or aluminum alloy.4. The method of claim 1 , further comprising positioning a second workpiece in contact with the first workpiece and friction stir welding the first workpiece to the second workpiece at a temperature below 800 degrees Celsius of the FSP tool.5. The method of claim 4 , the first workpiece and second workpiece being a single-phase low melting temperature alloy.6. The method of claim 4 , the first workpiece and second workpiece being aluminum or aluminum alloy.7. The method of claim 1 , rotating the FSP tool including rotating the FSP tool at a rotational speed greater than 10 revolutions per minute.8. The method of claim 1 , the ...

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12-03-2015 дата публикации

DEVICE AND METHOD FOR BONDING SUBSTRATES

Номер: US20150069115A1
Автор: Rebhan Bernhard
Принадлежит: EV Group E. Thallner GmbH

A device for bonding of one bond side of a first substrate to one bond side of a second substrate, the device having one module group with a common working space which can be closed especially gastight to the environment, at least one bond module is connected in a sealed manner to the working space, and a movement apparatus for moving the first and second substrate in the working space, 18-. (canceled)9. A device for bonding of a bond side of a first substrate to a bond side of a second substrate , said device comprising:a module group with a common working space, which working space can be closed, gastight relative to the surrounding environment,at least one reduction module which is connected in a sealed manner to the working space for reducing the bond sides,at least one bond module connected in a sealed manner to the working space, a reduction space in the reduction module and/or a bond space in the bond module can be separated from the working space in a sealed manner,', 'the working space with the reduction space separated and/or bond space separated can be exposed to a reducing atmosphere, and', 'the movement apparatus is arranged in a central module., 'a movement apparatus for moving the first and second substrate in the working space, wherein'}10. The device as claimed in claim 9 , wherein the reduction space can be exposed separately from the working space to a reducing atmosphere by plasma reduction and/or gas reduction.11. The device as claimed in one of or claim 9 , wherein the reduction space and/or the bond space can be heated separately from the working space by separate heating means to a reduction temperature (reduction space) or bond temperature (bond space).12. The device as claimed in one of or claim 9 , wherein the reduction space can be exposed to a temperature profile and/or pressure profile claim 9 , coupled with repeated flushing of the reduction space with a reduction medium.13. A method for bonding of one bond side of a first substrate to ...

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08-03-2018 дата публикации

METHOD OF MAKING AN EDGE-TO-EDGE METAL COMPOSITE

Номер: US20180065206A1
Принадлежит:

A clad metal composite produced according to a method for edge-to-edge cladding of two or more different metals (such as aluminum and copper). The metals are joined next to each other to form an edge-to-edge or side-by-side clad bimetal. In one embodiment, nine metal strips are used to create the desired clad metal composite. The design includes strips of metal that have industry standard cut edges (such as, slit-cut edges). The clad metal composite may include multiple layers of metals positioned edge-to-edge. 1. A method for creating a clad metal composite strip comprising the steps of:a) providing a first layer of metal strips including a first side strip of a first metal, a second side strip of the first metal and a center strip of a second metal, the first side strip abutting one edge of the center strip and the second side strip abutting the opposite edge of the first center strip, wherein the first center strip has a first width and the first and second side strips having a second width;b) aligning a second layer of metal strips with the first layer of metal strips, the second layer of metal strips having a width commensurate with the width of the first layer of metal strips and including a second center strip of the second metal and a third and fourth side strips of the first metal, the third side strip abutting one edge of the second center strip and the fourth side strip abutting the opposite edge of the second center strip, wherein the second center strip has a third width and the third and fourth side strips have a fourth width;c) aligning a third layer of metal strips with the second layer of metal strips, the third layer of metal strips having a width commensurate with the width of the first and second layers of metal strips and including a third center strip of the second metal and a fifth and sixth side strips of the first metal, the fifth side strip abutting one edge of the third center strip and the sixth side strip abutting the opposite edge of ...

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09-03-2017 дата публикации

PRESSURE APPLYING UNIT

Номер: US20170066075A1
Автор: Matsubayashi Ryo
Принадлежит:

Provided is a pressure applying unit used in baking a metal particle paste of an assembled body formed by arranging an electronic part on a substrate with the metal particle paste interposed therebetween by heating the assembled body while applying pressure to the assembled body using a pair of heating parts. The pressure applying unit includes: a pair of transferring members which transfers pressure and heat to the assembled body by sandwiching the assembled body therebetween; guide members which movably connect the pair of transferring members to each other; and a distance adjusting mechanism being configured to make the second transferring member separated from the assembled body during a pressure non-applying time and brings both the first transferring member and the second transferring member into contact with the assembled body during a pressure applying time. 1. A pressure applying unit used in baking a metal particle paste of an assembled body formed by arranging an electronic part on a substrate with the metal particle paste interposed therebetween by heating the assembled body while applying pressure to the assembled body using a pair of heating parts , whereinassuming a time during which pressure is not applied to the pressure applying unit as a pressure non-applying time and a time during which predetermined pressure is applied to the pressure applying unit as a pressure applying time,the pressure applying unit comprises:a pair of transferring members which is constituted of a plate-like first transferring member being in contact with the substrate at least during the pressure applying time and a plate-like second transferring member being in contact with the electronic part at least during the pressure applying time and transfers pressure and heat to the assembled body by sandwiching the assembled body therebetween in sintering the metal particle paste;a guide member which connects the pair of transferring members to each other, and allows the movement ...

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09-03-2017 дата публикации

Mechanical dimpling for vapor expression in welding

Номер: US20170066076A1
Принадлежит: GM GLOBAL TECHNOLOGY OPERATIONS LLC

A method for welding together two workpieces. The method includes stamping, using a stamping system, a first workpiece comprising a material that creates vapor when melted, such as zinc. The first workpiece is stamped at a first preselected region to form a plurality of depressions in the first preselected region. The method further includes positioning the first preselected region adjacent a second preselected region of a second workpiece. After stamping and positioning as such, the method includes applying energy to at least one of the first preselected region and the second preselected region to melt material of the first and second workpieces to form a joint connecting together the first and second workpieces. Based on the configuration and arrangement created, any vapor formed by molten material vents from the joint being formed, between the depressions formed, and away from the first and second workpieces.

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09-03-2017 дата публикации

PROCESS FOR FRICTION STIR WELDING INCLUDING A MOBILE COUNTER-BEARING

Номер: US20170066077A1
Принадлежит:

System for friction stir welding of two parts which includes a welding unit which includes at least one welding head fitted with a rotating pin and a counter-bearing unit which has a support surface to support the parts against a pressure exerted by the welding head, and wherein each welding head can be moved relative to the support surface in a first direction parallel to an axis of rotation of the rotating pin and in a second direction orthogonal to the axis of rotation, and wherein the support surface can be moved in the second direction and is formed of two coaxial clamp rollers which are set apart from each other. 2. The process according to claim 1 , wherein movement of the support surface is achieved by the clamp rollers moving along the contact interface by implementing rolling of the main circumferential tracks on the first part causing a rotation of each of the clamp rollers around its axis of revolution.3. The process according to claim 2 , wherein:the clamp rollers each have a circumferential shoulder pressed onto an edge of the first part;the clamp rollers each have a secondary circumferential track connected to the main circumferential track of the clamp roller by the circumferential shoulder of the clamp roller;the secondary circumferential track of each clamp roller is pressed against the second part and rolls on the latter as the clamp roller moves along the contact interface.4. The process according to claim 1 , wherein the clamp rollers are made to move towards each other so that the two respective side-walls of the clamp rollers sandwich a portion of the first part.5. The process according to claim 1 , wherein:the welding system includes a non-destructive inspection device carried by the welding unit and/or a non-destructive inspection device carried by the counter-bearing unit;each non-destructive inspection device is moved in a manner which is synchronised with and delayed in relation to each welding head of the welding device, so as to carry ...

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12-03-2015 дата публикации

FUSION WELDABLE FILLER ALLOYS

Номер: US20150072170A1
Принадлежит:

Al—Mg and Al—Mg—Zn weld filler alloy compositions for use with fusion weldable 7xxx, 6xxx, 5xxx and 2xxx series aluminum alloy base metals are disclosed. The weld filler alloys may be used for joining a first aluminum base metal segment to a second aluminum base metal segment, where the base metal segments is at least one of 7xxx, 6xxx, 5xxx and 2xxx series aluminum alloy. The weld filler alloys, in wire or rod form, may also be used to repair a defective weld. 1. A weld filler alloy comprising:from about 5.6 wt. % Mg to about 8.0 wt. % Mg;from about 0.01 wt. % to about 0.5 wt. % of a grain refiner; andup to about 94.4 wt. % Al.2. The weld filler alloy of having from about 5.6 wt. % Mg to about 6.2 wt. % Mg.3. The weld filler alloy of having about 5.9 wt. % Mg.4. The weld filler alloy of claim 1 , further comprising:from about 0.05 wt. % Zn to about 3.5 wt. % Zn.5. The weld filler alloy of having about 1.7 wt. % Zn to about 2.3 wt. % Zn.6. The weld filler alloy of having about 2.0 wt. % Zn.7. The weld filler alloy of claim 1 , wherein the grain refiner is at least one of Zr claim 1 , Ti and B.8. The weld filler alloy of claim 1 , wherein the weld filler alloy is substantially free of Mn.9. A product comprising:a first aluminum alloy segment;a second aluminum alloy segment; anda weldment joining the first aluminum alloy segment to the second aluminum alloy segment, wherein the weldment comprises a weld filler alloy having from about 5.6 wt. % Mg to about 8.0 wt. % Mg, from about 0.01 wt. % to about 0.5 wt. % of a grain refiner, and up to about 94.4 wt. % Al.10. The product of claim 9 , wherein the weld filler alloy includes from about 0.05 wt. % Zn to about 3.5 wt. % Zn.11. The product of claim 9 , wherein each of the first aluminum alloy segment and the second aluminum alloy segment comprises at least one of a 6xxx series aluminum alloy.12. The product of claim 9 , wherein each of the first aluminum alloy segment and the second aluminum alloy segment comprises at ...

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