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Небесная энциклопедия

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

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Мониторинг СМИ

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

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Поддерживает ввод нескольких поисковых фраз (по одной на строку). При поиске обеспечивает поддержку морфологии русского и английского языка
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Применить Всего найдено 12196. Отображено 100.
05-01-2012 дата публикации

Dense vertically cracked thermal barrier coatings

Номер: US20120003102A1
Автор: Albert Feuerstein, Ann Bolcavage, Danny Lee Appleby, Neil Hitchman, Thomas Alan Taylor
Принадлежит: Praxair Technology Inc

This invention relates to dense, vertically cracked thermal barrier coatings made from high purity yttria or ytterbia stabilized zirconia powders. The high purity yttria or ytterbia stabilized zirconia powder consisting essentially of less than about 0.01 weight percent silicon dioxide (silica), less than about 0.002 weight percent aluminum oxide (alumina), less than about 0.005 weight percent calcium oxide, less than about 0.005 weight percent ferric oxide, less than about 0 to about 0.002 weight percent magnesium oxide, less than about 0 to about 0.005 weight percent titanium dioxide, from about 1.5 to about 2 weight percent hafnium oxide (hafnia), from about 6 to about 25 weight percent yttrium oxide (yttria), less than 0.1 weight percent other impurity oxides, and the balance zirconium oxide (zirconia) and the balance zirconium oxide (zirconia). The thermal barrier coatings are intended to be used in cyclic thermal environments such as for gas turbine blades, vanes and seal surfaces exposed in the hot section of gas turbine engines.

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Номер записи: 1
05-01-2012 дата публикации

Method for depositing nanoparticles on a support

Номер: US20120003397A1
Автор: Francois Reniers, Frederic Demoisson, Jean-Jacques Pireaux
Принадлежит: Universite Libre de Bruxelles ULB

A method for depositing nanoparticles on a support includes taking a colloidal solution of nanoparticles. The method also includes nebulizing the colloidal solution of nanoparticles on a surface of the support in an atmospheric plasma.

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Номер записи: 2
16-02-2012 дата публикации

Dual nozzle cap for thermal spray coating

Номер: US20120037728A1
Автор: Byung Doo Kim
Принадлежит: Individual

Disclosed is a dual nozzle cap for thermal spray coating to which both a thermal spray coating method and a kinetic spray coating method are applied. The dual nozzle cap includes a nozzle unit including inner and outer nozzles, a gun insertion hole, into which the front end of a spray gun is inserted, and a gas connection hole, into which a gas connector to supply the gas is inserted, formed through one surface of the nozzle unit. In a space between the inner and outer nozzles, a gas collection part to uniformly distribute the high-pressure subsidiary gas injected through the connection hole, a neck part to apply pressure to the high-pressure subsidiary gas to accelerate the subsidiary gas, and a gas spray hole to spray the subsidiary gas supplied from the neck part together with a material sprayed from the spray gun are sequentially formed.

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Номер записи: 3
01-03-2012 дата публикации

Minimizing blockage of holes in turbine engine components

Номер: US20120052200A1
Автор: Benjamin Joseph Zimmerman
Принадлежит: Individual

An airfoil for use in a gas turbine engine is provided, the airfoil having a hole therein. A ceramic plug is inserted in the hole so that the plug extends above a depth of a thermal barrier coating, such as a ceramic, to be placed on the airfoil. The airfoil is then coated by non-line of sight vapor deposition and the plugs are then removed.

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Номер записи: 4
08-03-2012 дата публикации

Carbon Bodied Bicycle Rim with Ceramic Brake Portion

Номер: US20120056468A1
Автор: Carlos Tsai
Принадлежит: Individual

According to the present invention, a carbon bodied bicycle rim with ceramic brake portion comprises a carbon bodied bicycle rim and a protective film thermal sprayed on the carbon bodied bicycle. The carbon bodied bicycle rim includes two brake portion respectively formed on two sides thereof. Each brake portion has an outer surface. The protective film is thermal sprayed on the outer surface of the brake portion, by which the brake portion has a characteristic of wear-resisting and thermal dissipation. The protective film includes an aluminum layer thermal sprayed on the brake portion and a ceramic layer thermal sprayed on the aluminum layer.

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Номер записи: 5
26-04-2012 дата публикации

Process for depositing a coating on metal or non-metal items, and item obtained therefrom

Номер: US20120100382A1
Автор: Andrea Fabbri, Arturo Sabbioni
Принадлежит: Eurocoating SpA

A process for depositing coatings on metal or non-metal pieces includes phases of arranging at least a piece on which to deposit the surface coating, arranging at least a plasma torch, igniting the plasma torch and supplying the coating material to the plasma torch. An electric arc is established between the plasma torch and the piece during the coating deposit phase.

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Номер записи: 6
14-06-2012 дата публикации

Method of fabricating a component using a two-layer structural coating

Номер: US20120148769A1
Автор: Don Mark Lipkin, Ronald Scott Bunker
Принадлежит: General Electric Co

A method of fabricating a component is provided. The fabrication method includes depositing a first layer of a structural coating on an outer surface of a substrate. The substrate has at least one hollow interior space. The fabrication method further includes machining the substrate through the first layer of the structural coating, to define one or more openings in the first layer of the structural coating and to form respective one or more grooves in the outer surface of the substrate. Each groove has a respective base and extends at least partially along the surface of the substrate. The fabrication method further includes depositing a second layer of the structural coating over the first layer of the structural coating and over the groove(s), such that the groove(s) and the second layer of the structural coating together define one or more channels for cooling the component. A component is also disclosed.

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Номер записи: 7
05-07-2012 дата публикации

Process for surface treating aluminum or aluminum alloy and article made with same

Номер: US20120171511A1
Автор: Cheng-Shi Chen, Dun Mao, Hsin-Pei Chang, Huann-Wu Chiang, Wen-Rong Chen
Принадлежит: Hon Hai Precision Industry Co Ltd, Hongfujin Precision Industry Shenzhen Co Ltd

A process for treating the surface of aluminum or aluminum alloy comprises providing a substrate made of aluminum or aluminum alloy. Then a zinc-plating layer is formed on the substrate by electroless plating with a zinc electroless plating solution, and a ceramic coating comprising refractory compound is next formed on the zinc-plating layer using physical vapor deposition.

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Номер записи: 8
02-08-2012 дата публикации

Non-magnetic drill string member with non-magnetic hardfacing and method of making the same

Номер: US20120193148A1
Автор: James L. Overstreet, Jimmy W. Eason, Travis Puzz
Принадлежит: Baker Hughes Inc

A method for applying a non-magnetic, abrasive, wear-resistant hardfacing material to a surface of a drill string member includes providing a non-magnetic drill string member formed of a non-magnetic material, the drill string member having an outer surface. It also includes providing a non-magnetic hardfacing precursor material comprising a plurality of non-magnetic, sintered carbide pellets and a non-magnetic matrix material; heating a portion of the non-magnetic hardfacing precursor material to a temperature above the melting point of the matrix material to melt the matrix material. It further includes applying the molten non-magnetic matrix material and the plurality of non-magnetic, sintered carbide pellets to the exterior surface of the drill string member; and solidifying the molten non-magnetic matrix material to form a layer of a non-magnetic hardfacing material having a plurality of non-magnetic, sintered carbide pellets dispersed in the hardfacing material.

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Номер записи: 9
06-09-2012 дата публикации

Method for manufacturing insulating glazing

Номер: US20120222373A1
Автор: Francois Closset, Olivier Bouesnard
Принадлежит: AGC Glass Europe SA

The present invention relates to a method for manufacturing at least one portion of a seal ensuring gas-tightness between at least one first and one second glass panel in a glazing system, the method including the following steps: depositing a first adhesive layer on a first peripheral area of the first panel and a second adhesive layer on a second peripheral area of the second panel; welding a first metal seal element to the first adhesive layer; welding a second metal seal element or said first metal seal element to the second adhesive layer. According to the invention, the first and second adhesive layers are deposited using a high-speed oxy-fuel flame-spraying method.

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Номер записи: 10
20-09-2012 дата публикации

Thermocouple and method of forming a thermocouple on a contoured gas turbine engine component

Номер: US20120236899A1
Автор: Anand A. Kulkarni, Kevin C. Sheehan, Ramesh Subramanian
Принадлежит: Siemens Energy Inc

A method of forming a thermocouple ( 12 ), including: depositing a first material on a component ( 10 ) to form a first leg ( 14 ); depositing a second material through a mask ( 30 ) to form a pattern ( 50 ) on the component ( 10 ), the pattern ( 50 ) forming a plurality of discrete second leg junction ends ( 20 ) and a continuous patch ( 52 ) of the second material comprising indiscrete lead ends of the second legs ( 16 ), each second leg junction end ( 20 ) spanning from a respective junction ( 18 ) with the first leg ( 14 ) to the continuous patch ( 52 ); and laser-ablating the continuous patch ( 52 ) to form discrete lead ends ( 22 ) of the second legs ( 16 ), each lead end ( 22 ) electrically connected to a respective junction end ( 20 ), thereby forming discrete second legs ( 16 ).

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Номер записи: 11
22-11-2012 дата публикации

Method for Producing a Metal Layer on a Substrate and Device

Номер: US20120292773A1
Автор: Hans-Joachim Schulze, Khalil Hosseini
Принадлежит: INFINEON TECHNOLOGIES AG

A method produces a metal layer on a semiconductor substrate. A metal layer is produced on the semiconductor substrate by depositing metal particles. The metal particles include cores made of a first metal material and shells surrounding the cores. The shells are made of a second metal material that is resistant to oxidation.

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Номер записи: 12
06-12-2012 дата публикации

Sliding element having adjustable properties

Номер: US20120306158A1
Автор: Marc-Manuel Matz, Marcus Kennedy, Michael Zinnabold
Принадлежит: Individual

A sliding element, particularly a piston ring for an internal combustion engine, includes a substrate, and a wear-protection layer, obtained by thermal spraying of a powder comprising the element proportions 2-50 percent by weight iron, FE; 5-60 percent by weight tungsten, W; 5-40 percent by weight chrome, Cr; 5-25 percent by weight nickel, Ni; 1-5 percent by weight molybdenum, Mo; 1-10 carbon, C and 0.1-2 percent by weight silicon, Si; and a running-in layer, obtained by thermal spraying of a powder comprising the element proportions 60-95 percent by weight nickel; 5-40 percent by weight carbon.

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Номер записи: 13
06-12-2012 дата публикации

Method of manufacturing a thermal barrier coating structure

Номер: US20120308733A1
Автор: Konstantin Von Niessen, Malko Gindrat, Richard K. Schmid
Принадлежит: Sulzer Metco AG

To manufacture a thermal barrier coating structure on a substrate surface, a working chamber having a plasma torch is provided, a plasma jet is generated in that a plasma gas is conducted through the plasma torch and is heated therein by means of electric gas discharge, electromagnetic induction or microwaves, and the plasma jet is directed to the surface of a substrate introduced into the working chamber. To manufacture the thermal barrier coating, a voltage is additionally applied between the plasma torch and the substrate to generate an arc between the plasma torch and the substrate and the substrate surface is cleaned by means of the light arc, wherein the substrate remains in the working chamber after the arc cleaning and an oxide layer is generated on the cleaned substrate surface and a thermal barrier coating is applied by means of a plasma spray process.

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Номер записи: 14
17-01-2013 дата публикации

Thermal sprayed coating of jig for producing glass sheet, and jig for producing glass sheet

Номер: US20130014543A1
Автор: Kazuo Hamashima, Yasunari Ishikawa
Принадлежит: Asahi Glass Co Ltd

To provide a thermal sprayed coating of a jig for producing glass having favorable wear resistance and lubricity at high temperature of at least the strain point of a glass sheet. A thermal sprayed coating of a jig for producing a glass sheet, to be used for a jig for producing glass to be in contact with a glass sheet at a temperature of at least the strain point, which comprises tungsten carbide; at least one metal carbide selected from the group consisting of titanium carbide, zirconium carbide, hafnium carbide, niobium carbide, tantalum carbide, chromium carbide and molybdenum carbide; a metal containing Ni; and inevitable impurities, and a jig for producing a glass sheet comprising the thermal sprayed coating.

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Номер записи: 15
21-03-2013 дата публикации

Spray powder for cermet-coating of doctor blades

Номер: US20130071647A1
Автор: Alexander Etschmaier, Antje Berendes, Hubert Bischof, Norbert Gamsjäger, Wolfgang Peter Mayr
Принадлежит: VOITH PATENT GMBH

The invention relates to a spray powder for the production of a Cermet coating on a doctor blade surface, wherein the spray powder includes a mixture of a metal powder and a hard material powder, wherein at least 90 percent of the granules of the metal powder are smaller than 63 μm, and preferably smaller than 48 μm, and at least 90 percent of the granules of the hard material powder are smaller than 2 μm.

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Номер записи: 16
18-04-2013 дата публикации

POWDER FOR THERMAL SPRAYING AND PROCESS FOR FORMATION OF SPRAYED COATING

Номер: US20130095250A1
Автор: Sato Kazuto
Принадлежит:

A thermal spray powder, which includes granulated and sintered cermet particles that contain a metal having an indentation hardness of 500 to 5,000 N/mm, is disclosed. The granulated and sintered cermet particles have an average size of 30 μm or less. The granulated and sintered cermet particles are composed of primary particles having an average size of 6 μm or less. The granulated and sintered cermet particles have a compressive strength of from 100 to 600 MPa. It is preferable that the metal contained in the granulated and sintered cermet particles includes at least one selected from the group consisting of cobalt, nickel, iron, aluminum, copper, and silver. The thermal spray powder is usable in a low-temperature thermal spraying process such as cold spraying using nitrogen as a working gas. 1. A thermal spray powder that is usable in a low-temperature thermal spraying process , comprising granulated and sintered cermet particles that contain a metal having an indentation hardness of 500 to 5 ,000 N/mm , whereinthe granulated and sintered cermet particles have an average size of 30 μm or less;the granulated and sintered cermet particles are composed of primary particles having an average size of 6 μm or less, andthe granulated and sintered cermet particles have a compressive strength of from 100 to 600 MPa.2. The thermal spray powder according to claim 1 , wherein the metal contained in the granulated and sintered cermet particles includes at least one selected from the group consisting of cobalt claim 1 , nickel claim 1 , iron claim 1 , aluminum claim 1 , copper claim 1 , and silver.3. The thermal spray powder according to claim 1 , wherein the low-temperature thermal spraying process is cold spray that utilizes a working gas containing nitrogen as a main component.4. A method for forming a thermal spray coating claim 1 , the method comprising forming a thermal spray coating through a low-temperature thermal spraying process of the thermal spray powder according ...

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Номер записи: 17
25-04-2013 дата публикации

Deposition System, Method And Materials For Composite Coatings

Номер: US20130098267A1
Автор: Vladimir E. Belashchenko
Принадлежит: Individual

A composite powder for a deposition of a composite coating comprises a nonmetallic component and a metallic component, the metallic component having an amorphous structure or a nanocrystalline structure. The metallic component may include an amorphous metallic alloy. The metallic alloy may include constituents having the amorphous structure. The metallic component may include a combination of the metallic alloy existing in the amorphous state and constituents of the amorphous metallic alloy in the amorphous state. The composite metal-ceramic powders are used for depositing composite coatings on a selected surface. Disclosed are several methods and systems for producing such composite powders. Disclosed are also several methods and systems for depositing composite coatings. Advantageously, the deposited coatings exhibit high corrosion resistance, high wear resistance, and excellent structural properties.

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Номер записи: 18
25-04-2013 дата публикации

Method for adhering a coating to a substrate structure

Номер: US20130101806A1
Автор: Andres Garcia Crespo, Glenn Curtis Taxacher, Herbert Chidsey Roberts, Iii
Принадлежит: General Electric Co

A method for adhering a coating to a substrate structure comprises selecting a substrate structure having an outer surface oriented substantially parallel to a direction of radial stress, modifying the outer surface to provide a textured region having steps to adhere a coating thereto, and applying a coating to extend over at least a portion of the textured region, wherein the steps are oriented substantially perpendicular to the direction of radial stress to resist deformation of the coating relative to the substrate structure. A rotating component comprises a substrate structure having an outer surface oriented substantially parallel to a direction of radial stress. The outer surface defines a textured region having steps to adhere a coating thereto, and a coating extends over at least a portion of the textured region. The steps are oriented substantially perpendicular to the direction of radial stress to resist creep.

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Номер записи: 19
02-05-2013 дата публикации

Process for producing a repair coating on a coated metallic surface

Номер: US20130108782A1
Автор: Manfred Walter, Mats Eriksson
Принадлежит: Individual

A process for producing a repair coating on at least one metallic surface that is coated with at least one corrosion protecting coating A applied with at least one composition selected from the group of pretreatment compositions, of organic compositions and of silicon compound(s) containing compositions, whereby the at least one corrosion protecting coating A has been at least partially removed in the area Z, whereby a thin corrosion protecting coating B containing at least one silicon compound is applied with a solution or dispersion containing a silane, a silanol, a siloxane, or a polysiloxane on at least a part of the area Z. A further corrosion protecting coating C may be applied.

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Номер записи: 20
02-05-2013 дата публикации

METAL COMPONENT, METHOD FOR PRODUCING A METAL COMPONENT, AND FITTING, PIECE OF FURNITURE AND HOUSEHOLD APPLIANCE

Номер: US20130108886A1
Автор: Gebhardt Björn, Grigat Willi, Jährling Peter, Krause Arthus, Rehage Daniel, Schrubke Lars, Sobolewski Uwe
Принадлежит: PAUL HETTICH GMBH & CO. KG

A metal component for one or more of a fitting, a piece of furniture and a household appliance. The metal component includes a coating, at least in sections, the coating including one of a hardness-containing composite material and a ceramic-metal composite material. 1. A metal component for one or more of a fitting , a piece of furniture and a household appliance , the metal component comprising:a coating, at least in sections; andthe coating including one of a hardness-containing composite material and a ceramic-metal composite material.2. The metal component according to claim 1 , wherein the coating has a Vickers hardness of more than 300 HV10.3. The metal component according to claim 1 , wherein the melting point of the coating is higher than 300° C.4. The metal component according to claim 1 , wherein the composite material includes at least one of a hard material and one of a metal claim 1 , ceramic claim 1 , fiber and synthetic material.5. The metal component according to claim 1 , wherein the composite material has a mass fraction of over 50% of one or both of a metal and a ceramic.6. The metal component according to claim 1 , wherein the composite material includes a hard material claim 1 , selected from a group consisting of carbides claim 1 , nitrides claim 1 , borides and silicides.7. The metal component according to claim 1 , wherein the composite material includes one or more of corundum claim 1 , fluorapatite claim 1 , silicon nitride and/or molybdenum silicide.8. The metal component according to claim 1 , wherein the composite material includes a lubricant.9. A method of producing the metal component according to claim 1 , the method steps comprising:providing the metal component; andapplying the coating, at least in sections, by one of gas-phase deposition, chemical deposition, electrochemical deposition, thermal spraying, and welding.10. A household appliance comprising the metal component according to claim 1 , arranged one of in and on the ...

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Номер записи: 21
09-05-2013 дата публикации

PRE-TREATMENT APPARATUS AND METHOD FOR IMPROVING ADHESION OF THIN FILM

Номер: US20130115378A1
Автор: Ko Kyung Hyun, Lee Hyuk Jun
Принадлежит: AJOU UNIVERSITY INDUSTRY COOPERATION FOUNDATION

Provided are a pre-treatment apparatus and method for improving an adhesion of a thin film The pre-treatment apparatus includes: a gas compressor that compresses gas supplied from the outside and contained, and supplies a process gas that is compressed; a powder feeder for supplying a coating powder including a single metal or alloy supplied from the outside and contained; and a spray nozzle through which the process gas supplied from the gas compressor and the coating powder supplied from the powder feeder are cold sprayed on a surface of a base metal on which a thin film is to be deposited so as to form a porous metal coating layer on the surface of the base metal. The pre-treatment method includes: preparing a base metal including a single metal or alloy; preparing a coating powder including powder of one or more single metals or an alloy thereof; forming a porous metal coating layer on a surface of the base metal, on which a thin film is to be deposited, by cold-spraying the coating powder and a process gas to the surface of the base metal; and depositing the thin film on the coating layer, wherein the thin film includes metal. 1. A pre-treatment apparatus for improving an adhesion of a thin film , the pre-treatment apparatus comprising:a gas compressor that compresses gas supplied from the outside and contained, and supplies a process gas that is compressed;a powder feeder for supplying a coating powder comprising a single metal or alloy supplied from the outside and contained; anda spray nozzle through which the process gas supplied from the gas compressor,wherein the coating powder supplied from the powder feeder is cold sprayed on a surface of a base metal, on which a thin film is to be deposited, so as to form a porous metal coating layer on the surface of the base metal.2. The pre-treatment apparatus of claim 1 , further comprising a gas heater for heating the process gas to increase a spray speed thereof between the gas compressor and the spray nozzle.3. ...

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Номер записи: 22
13-06-2013 дата публикации

Water-reactive al-based composite material, water-reactive al-based thermally sprayed film, process for production of such al-based thermally sprayed film, and constituent member for film-forming chamber

Номер: US20130145961A1
Автор: Katsuhiko Mushiake, Tomoko Saitou, Yutaka Kadowaki
Принадлежит: Ulvac Inc

Herein provided are a water-reactive Al-based composite material which is characterized in that it is produced by incorporating, into Al, 2.0 to 3.5% by mass of In, 0.2 to 0.5% by mass of Si and 0.13 to 0.25% by mass of Ti, and which can be dissolved in water through the reaction thereof in a water-containing atmosphere; a water-reactive Al-based thermally sprayed film produced using this composite material; a method for the production of this Al-based thermally sprayed film; and a constituent member for a film-forming chamber which is provided with this Al-based thermally sprayed film on the surface thereof.

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Номер записи: 23
04-07-2013 дата публикации

Process for producing a beam element of a co-ordinate measuring machine, and measuring machine provided with said beam element

Номер: US20130167390A1
Автор: Alberto Tarizzo
Принадлежит: Hexagon Metrology SpA

A process for producing a beam element of a co-ordinate measuring machine, comprising the steps of applying a machinable metal coating by spraying on a structural substrate made of ceramic material, impregnating the coating with a resin, and executing on the coating a surface-finishing machining operation and a treatment of surface hardening.

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Номер записи: 24
18-07-2013 дата публикации

METHOD AND DEVICE FOR THERMAL SPRAYING

Номер: US20130183453A1
Автор: Gartner Frank, Heinrich Peter, Klassen Thomas, Kreye Heinrich, Krommer Werner
Принадлежит:

A thermal spraying method is provided, wherein spray particles of a powdered spray material are introduced into a hot carrier gas stream, heated by the carrier gas stream and then sprayed onto the surface of a substrate by a spray nozzle, wherein the temperature of the spray particles upon impact onto the substrate is below the melting temperature of the spray material. The spray particles are heated in the hot carrier gas stream upstream of the nozzle throat to a temperature that causes at least partial melting of the spray particles in that location. 1. A thermal spraying method , wherein spray particles of a powdered spray material are introduced into a hot carrier gas stream , heated by the carrier gas stream and then sprayed onto the surface of a substrate by means of a spray nozzle , wherein the temperature of the spray particles upon impact onto the substrate is below the melting temperature of the spray material , characterized in that the spray particles are heated in the hot carrier gas stream upstream of the nozzle throat to a temperature that causes at least partial melting of the spray particles in that location.2. The method as claimed in claim 1 , wherein the temperature to which the spray particles are heated upstream of the nozzle throat is adjusted by controlling a temperature of the carrier gas stream and/or a pressure at which the carrier gas stream is supplied to the spray nozzle.3. The method as claimed in claim 1 , wherein the temperature to which the spray particles are heated upstream of the nozzle throat is adjusted such that the temperature of at least a portion of the spray particles upon impact onto the substrate is more than 60% of the melting temperature of the appropriate spray material in Kelvin.4. The method as claimed in wherein said temperature is more than 70% of the melting temperature of the appropriate spray material in Kelvin.5. The method as claimed in wherein said temperature is more than 80% of the melting temperature of ...

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Номер записи: 25
25-07-2013 дата публикации

THERMAL SPRAY APPLICATIONS USING IRON BASED ALLOY POWDER

Номер: US20130186237A1
Автор: "LEsperance Gilles", Christopherson, JR. Denis B., Koth Jeremy
Принадлежит: FEDERAL-MOGUL CORPORATION

A thermal spray powder 20 is provided for use in a thermal spray technique, such as flame spraying, plasma spraying, cold spraying, and high velocity oxygen fuel spraying (HVOF). The thermal spray powder 20 is formed by water or gas atomization and comprises 3.0 to 7.0 wt. % carbon, 10.0 to 25.0 wt. % chromium, 1.0 to 5.0 wt. % tungsten, 3.5 to 7.0 wt. % vanadium, 1.0 to 5.0 wt. % molybdenum, not greater than 0.5 wt. % oxygen, and at least 40.0 wt. % iron, based on the total weight of the thermal spray powder 20. The thermal spray powder 20 can be applied to a metal body, such as a piston or piston ring, to form a coating. The thermal spray powder 20 can also provide a spray-formed part. 1. A powder metal material for use in a thermal spray technique , comprising: 3.0 to 7.0 wt. % carbon , 10.0 to 25.0 wt. % chromium , 1.0 to 5.0 wt. % tungsten , 3.5 to 7.0 wt. % vanadium , 1.0 to 5.0 wt. % molybdenum , not greater than 0.5 wt. % oxygen , and at least 40.0 wt. % iron , based on the total weight of the powder metal material.2. The powder metal material of including 3.5 to 4.0 wt. % carbon claim 1 , 11.0 to 15.0 wt. % chromium claim 1 , 1.5 to 3.5 wt. % tungsten claim 1 , 4.0 to 6.5 wt. % vanadium claim 1 , 1.0 to 3.0 wt. % molybdenum claim 1 , not greater than 0.3 wt. % oxygen claim 1 , and 50.0 to 81.5 wt. % iron.3. The powder metal material of consisting of 3.8 wt. % carbon claim 2 , 13.0 wt. % chromium claim 2 , 2.5 wt. % tungsten claim 2 , 6.0 wt. % vanadium claim 2 , 1.5 wt. % molybdenum claim 2 , 0.2 wt. % oxygen claim 2 , 70.0 to 80.0 wt. % iron claim 2 , and impurities in an amount not greater than 2.0 wt. %.4. The powder metal material of including at least one of cobalt claim 1 , niobium claim 1 , titanium claim 1 , manganese claim 1 , sulfur claim 1 , silicon claim 1 , phosphorous claim 1 , zirconium claim 1 , and tantalum.5. The powder metal material of including metal carbides in an amount of at least 15.0 vol. % claim 1 , based on the total volume of ...

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Номер записи: 26
08-08-2013 дата публикации

PROCESS FOR PRODUCING THERMAL BARRIER COATING, TURBINE MEMBER PROVIDED WITH THERMAL BARRIER COATING, AND GAS TURBINE

Номер: US20130202912A1
Автор: Inoue Yoshiaki, Kaneko Hideaki, Mega Masahiko, Mori Kazutaka, Nagano Ichiro, Okada Ikuo, Okajima Yoshifumi, Torigoe Taiji, Tsukagoshi Keizo, Uemura Yoshitaka
Принадлежит: MITSUBISHI HEAVY INDUSTRIES, LTD.

A process for producing a thermal barrier coating having an excellent thermal barrier effect and superior durability to thermal cycling. Also, a turbine member having a thermal barrier coating that has been formed using the production process, and a gas turbine. The process for producing a thermal barrier coating includes: forming a metal bonding layer () on a heat-resistant alloy substrate (), and forming a ceramic layer () on the metal bonding layer () by thermal spraying of thermal spray particles having a particle size distribution in which the 10% cumulative particle size is not less than 30 μm and not more than 100 μm. 1. A process for producing a thermal barrier coating , the process comprising:forming a metal bonding layer on a heat-resistant alloy substrate, andforming a ceramic layer on the metal bonding layer by thermal spraying of thermal spray particles having a particle size distribution in which a 10% cumulative particle size is not less than 30 μm and not more than 100 μm.2. The process for producing a thermal barrier coating according to claim 1 , whereinthe thermal spray particles have a maximum particle size of not more than 150 μm, and comprise not more than 3% of particles having a particle size of 30 μm, and not more than 8% of particles having a particle size of 40 μm.3. A turbine member claim 1 , comprising a thermal barrier coating formed using the process according to .4. A gas turbine claim 3 , comprising the turbine member according to .5. A turbine member claim 2 , comprising a thermal barrier coating formed using the process according to . The present invention relates to a process for producing a thermal barrier coating having excellent durability, and relates particularly to a process for producing a ceramic layer used as the top coat of a thermal barrier coating.In recent years, enhancement of the thermal efficiency of thermal power generation has been investigated as a potential energy conservation measure. In order to enhance the ...

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Номер записи: 27
15-08-2013 дата публикации

METHOD FOR DEPOSITING A BIOCIDAL COATING ON A SUBSTRATE

Номер: US20130209811A1
Автор: Dams Roel, Paulussen Sabine, Sheel David, Vangeneugden Dirk
Принадлежит:

A method produces a biocidal coating on a substrate, by a flame assisted chemical vapour deposition and a plasma assisted chemical vapour deposition step. In a first step, a biocidal material is deposited onto the substrate, possibly in combination with a first coating forming material. The second step provides a coating forming material onto the first layer, possibly in combination with a second biocidal material. The first step can be a flame assisted CVD step and the second step a plasma assisted CVD step or vice versa. 1. A method for producing a coating on a substrate , comprising the subsequent steps of:providing a substrate,subjecting the substrate to a flame-assisted chemical vapour deposition (FACVD), by exposing the substrate to a flame or the gas stream resulting therefrom and by introducing a first biocidal material into said flame or the reactive gas stream resulting therefrom, and by introducing a first coating-forming material into the flame or the gas stream resulting therefrom, said first coating forming material being introduced simultaneously with or after said first biocidal material,subjecting the substrate to a plasma-assisted chemical vapour deposition (PACVD) at atmospheric or intermediate pressure, by exposing the substrate to a plasma discharge or the reactive gas stream resulting therefrom and by introducing a second coating-forming material into said discharge or the reactive gas stream resulting therefrom, wherein the second coating forming material comprises an organosilicon precursor.2. The method according to claim 1 , wherein a second biocidal material is introduced into the plasma discharge or the reactive gas stream resulting therefrom claim 1 , said second coating forming material being introduced simultaneously with or after said second biocidal material.3. A method for producing a coating on a substrate claim 1 , comprising the subsequent steps of:providing a substrate,subjecting the substrate to a plasma-assisted chemical ...

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Номер записи: 28
05-09-2013 дата публикации

Substrate for cvd deposition of diamond and method for the preparation thereof

Номер: US20130230715A1
Автор: Andrey Bol'Shakov, Ekaterina V. Azarova, Evgeny A. Levashov, Evgeny E. Ashkinazi, Hiroshi Ishizuka, Satoru Hosomi, Victor G. Ralchenko
Принадлежит: General Physics Inst of Russian Academy of Science, National Univ of Science and Tech "Misis", Tomei Diamond Co Ltd

A substrate for depositing diamond by CVD, comprising a base body of hard material and a coating layer that holds diamond particles as seed crystal in a matrix and is deposited joined thereto on a surface of said base body, wherein: the seed diamond particles have an average particle size of 1 μm or smaller; the matrix comprises a first metal selected from a first group of Si, Ti, Zr, Hf, V, Nb, Ta, Cr, Mo and W and/or a first compound between said first metal and a non-metallic substance selected from boron, carbon and nitrogen, said matrix holding the diamond particles distributed therein; and a joint zone developed as a result of a diffusion process and extending over said base body and coating layer comprises either or both atoms of said first metal and a component metal of the hard material.

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Номер записи: 29
05-09-2013 дата публикации

COATING METHOD FOR FORMING CRACK-RESISTANT COATINGS HAVING GOOD ADHERENCE AND COMPONENT COATED IN THIS MANNER

Номер: US20130230723A1
Автор: Bamberg Joachim, Hertter Manuel, Hessert Roland
Принадлежит:

A method for coating a component, in particular a component of a gas turbine or of an aircraft engine, is disclosed. The coating is applied to the component by kinetic cold gas spraying, where prior to the deposition of the coating, the surface of the component to be coated is cleaned and compacted by shot peening with a blasting media. A component produced in this manner is also disclosed. 1. A method for coating a component , comprising the steps of:shot peening a surface of the component; andapplying a coating to the shot peened surface by kinetic cold gas spraying.2. The method according to claim 1 , further comprising the step of cleaning the surface of the component prior to the step of applying.3. The method according to claim 1 , wherein the shot peening is performed in at least two stages and wherein a blasting velocity of a blasting media of the shot peening is less during a first stage than during a second stage.4. The method according to claim 1 , wherein the shot peening is performed in multiple stages and wherein each stage has a different blasting velocity of a blasting media of the shot peening.5. The method according to claim 1 , wherein the shot peening has a continuously increasing blasting velocity of a blasting media of the shot peeing during the shot peening.6. The method according to claim 1 , further comprising the step of maintaining a blasting velocity of a blasting media of the shot peeing such that the blasting media does not substantially adhere to the surface.7. The method according to claim 1 , further comprising the step of maintaining a blasting velocity of a blasting media of the shot peening below a speed of sound at a beginning of the shot peening.8. The method according to claim 1 , further comprising the step of maintaining a blasting velocity of a blasting media of the shot peening above a speed of sound at an end of the shot peening.9. The method according to claim 2 , wherein the cleaning is performed with a blasting media.10 ...

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Номер записи: 30
12-09-2013 дата публикации

SURFACE TREATMENT

Номер: US20130236696A1
Автор: De Nys Rocky, Gulizia Stefan, Jahedi Mahnaz, King Peter, Poole Andrew James
Принадлежит: Commonwealth Scientific and Industrial Research Organisation

A method of protecting a polymer surface against fouling, which method comprises embedding in the polymer surface particles having antifouling properties, wherein the particles are embedded in the polymer surface by a spray mechanism in which the particles are accelerated and sprayed onto the polymer surface with a suitable velocity such that the particles become embedded in the polymer surface, wherein the particles are embedded in the polymer surface without an adhesive or binder and wherein the particles do not form a continuous layer on the polymer surface. 1. A method of protecting a polymer surface against fouling , which method comprises embedding in the polymer surface particles having antifouling properties , wherein the particles are embedded in the polymer surface by a spray mechanism in which the particles are accelerated and sprayed onto the polymer surface with a suitable velocity such that the particles become embedded in the polymer surface , wherein the particles are embedded in the polymer surface without an adhesive or binder and wherein the particles do not form a continuous layer on the polymer surface.2. The method according to claim 1 , wherein the particles provide antifouling properties by a chemical release mechanism.3. The method according to claim 1 , wherein the polymer is a thermoplastic or cured thermoset polymer.4. The method according to claim 1 , wherein the particles have an average particle size of up to 100 μm.5. The method according to claim 1 , wherein the particles provide anti-biofouling properties to the polymer surface.6. The method according to claim 1 , wherein the particles are anti-biofouling particles selected from the group consisting of copper claim 1 , zinc and/or compounds and alloys composed therefrom.7. The method according to claim 1 , wherein the polymer surface is a polymer layer provided over another substrate.8. The method according to claim 1 , wherein the particles are sprayed on to the polymer surface at ...

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Номер записи: 31
26-09-2013 дата публикации

Amorphous-nanocrystalline-microcrystalline coatings and methods of production thereof

Номер: US20130251910A1
Автор: Ardy Simon Kleyman, James Knapp, Tetyana P. Shmyreva
Принадлежит: Praxair ST Technology Inc

This invention relates to thermally sprayed coatings having an amorphous-nanocrystalline-microcrystalline composition structure, said thermally sprayed coating comprising from about 1 to about 95 volume percent of an amorphous phase, from about 1 to about 80 volume percent of a nanocrystalline phase, and from about 1 to about 90 volume percent of a microcrystalline phase, and wherein said amorphous phase, nanocrystalline phase and microcrystalline phase comprise about 100 volume percent of said thermally sprayed coating. This invention also relates to methods for producing the coatings, thermal spray processes for producing the coatings, and articles coated with the coatings. The thermally sprayed coatings of this invention provide enhanced wear and corrosion resistance for articles used in severe environments (e.g., landing gears, airframes, ball valves, gate valves (gates and seats), pot rolls, and work rolls for paper processing).

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Номер записи: 32
03-10-2013 дата публикации

COATING AND METHODS THEREOF

Номер: US20130260047A1
Автор: BAMOLA Rajan
Принадлежит:

The present invention discloses a nano-crystalline ceramic structure coat of resistive material and a method thereof for a substrate. The coating method includes the use of a resistive material solution diluted to a composition that is capable of atomization into atomized vapor particles, and conveyance of the atomized vapor particles onto a substrate, forming a conformal layer of substantially dehydrated compound. Further application of thermal energy consolidates the conformal layer into a coating of the nano-crystalline ceramic structure, with enhanced ceramic bonding with the substrate. 1. A method for coating a substrate , comprising:providing a solvent;dissolving desired solute within the solvent to form a solution;diluting the solution to a composition capable of atomization;cleaning the substrate;heating the substrate;atomizing the diluted solution into atomized vapor particles;directing atomized vapor particles of the diluted solution towards the heated substrate to form a conformal layer of substantially dehydrated compound thereon; andconsolidating the substantially dehydrated compound into a coating of a nano-crystalline ceramic structure, with enhanced ceramic bonding with the substrate.2. The method for coating a substrate as set forth in claim 1 , wherein:the solvent is substantially vaporized.3. The method for coating a substrate as set forth in claim 1 , wherein:the solute is a resistive material.4. The method for coating a substrate as set forth in claim 1 , wherein:the coating is transparent.5. The method for coating a substrate as set forth in claim 1 , further comprising:cleaning the coated substrate to remove loose particulates.6. A method for coating a substrate claim 1 , comprising:providing a combustible solvent;dissolving desired solute within the solvent to form a solution;diluting the solution to a composition capable of atomization;atomizing the diluted solution into atomized vapor particles;igniting the atomized vapor particles of the ...

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Номер записи: 33
17-10-2013 дата публикации

Metallic bondcoat or alloy with a high gamma/gamma' transition temperature and a component

Номер: US20130272917A1
Автор: Anand A. Kulkarni, Jonathan E. Shipper, JR., Werner Stamm
Принадлежит: SIEMENS AG

A metallic bondcoat with phases of γ and γ′ is provided. The metallic coating or alloy is nickel based. The metallic coating or alloy has γ and γ′ phases and optionally has β-phase. The new addition in nickel based coating stabilizes the phases γ and γ′ at high temperatures leading to a reduction of local stresses.

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Номер записи: 34
31-10-2013 дата публикации

Method for roughening and coating a surface

Номер: US20130284140A1
Автор: Alexander Schwenk, Clemens Maria Verpoort, Enrico Hauser, Leander Schramm
Принадлежит: FORD GLOBAL TECHNOLOGIES LLC

A method for roughening and thermally coating a surface, in particular a cylinder running surface of an internal combustion engine, the roughening being the preparation of the surface for the thermal coating of the surface with a coating. The method is characterized in that different roughening profiles are introduced into the surface during the roughening and the coating has different properties distributed over the surface. This allows the coating or spraying process during the later thermal coating to be carried out with substantially constant spraying parameters. The different properties of the coating, such as hardness, porosity, machinability, chemical composition, oxidation and adhesion, are then obtained just on the basis of the differently roughened surface.

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Номер записи: 35
07-11-2013 дата публикации

Cylinder Bore With Selective Surface Treatment And Method of Making The Same

Номер: US20130291823A1
Автор: David Alan Stephenson, David Garrett Coffman, Keith Raymond Bartle, Rodney G. Whitbeck
Принадлежит: FORD GLOBAL TECHNOLOGIES LLC

A cylinder bore with selective surface treatment includes a longitudinal axis and a cylindrical wall extending along the longitudinal axis, the cylindrical wall including first and second end portions and a middle portion positioned between the first and second end portions, the middle portion having a greater surface roughness than at least one of the first and second end portions.

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Номер записи: 36
14-11-2013 дата публикации

ZIRCONIUM ALLOY FOR IMPROVING RESISTANCE TO OXIDATION AT VERY HIGH TEMPERATURE AND FABRICATION METHOD THEREOF

Номер: US20130302639A1
Автор: CHOI Byoung-Kwon, Jung Yang-Il, Kim Hyun-Gil, Kim Il-Hyun, KOO Yang-Hyun, PARK Dong Jun, Park Jeong-yong, Song Kun-Woo
Принадлежит:

A zirconium alloy for use in nuclear fuel assemblies is provided, which provides increased resistance against oxidation and corrosion and also improved bonding with parent material, because pure metallic material such as silicon (Si) or chromium (Cr) is evenly coated on the surface of the parent material by plasma spraying. Because the plasma spray coating used to coat the pure metallic material on the zirconium alloy does not require vacuum equipment and also is not limited due to the shape of the coated product, this is particularly useful when evenly treating the surface of the component such as 4 m-long tube or spacer grip arrangement which is very complicated in shape. Furthermore, because the coated zirconium alloy confers excellent resistance to oxidation and corrosion under emergency such as accident as well as normal service condition, both the economic and safety aspects of nuclear fuel are improved. 1. A zirconium alloy coated article , comprising a zirconium alloy parent material bearing a plasma sprayed coating of a pure metallic material comprised of silicon (Si) or chromium (Cr) on a surface of a parent material.2. The article as set forth in claim 1 , wherein the zirconium alloy parent material is selected from a group consisting of Zircaloy-4 claim 1 , Zircaloy-2 claim 1 , ZIRLO claim 1 , M5 and HANA.3. The article as set forth in claim 1 , wherein the pure metallic material is coated on the parent material to a thickness ranging between 1 and 500 μm.4. The article as set forth in claim 1 , wherein the article is a component of a nuclear fuel assembly.5. The article as set forth in claim 4 , wherein the component of the nuclear fuel assembly comprises at least one of a cladding tube claim 4 , a guide tube claim 4 , an instrumentation tube and a spacer grid.6. The article as set forth in claim 1 , wherein the pure metallic material has a resistance against oxidation by being oxidized at high temperature to form silicon dioxide (SiO) or chromium oxide ...

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Номер записи: 37
05-12-2013 дата публикации

ZINC-FREE SPRAY POWDER, COPPER-CONTAINING THERMAL SPRAY LAYER, AS WELL AS METHOD OF MANUFACTURING A COPPER-CONTAINING THERMAL SPRAY LAYER

Номер: US20130319367A1
Автор: Distler Bernd, Ernst Peter
Принадлежит:

The invention relates to a zinc-free spray powder for thermally coating a substrate, in particular for thermally coating a bearing part of a bearing apparatus, which spray powder has the following composition except for unavoidable contaminants: tin=5% to 30% weight percent; aluminum=0.1% to 5% weight percent; iron=at most 1% weight percent, and copper=difference to 100% weight percent. The invention furthermore relates to a layer system applied via thermal spraying, a work piece, particularly a connecting rod, as well as a spray method for manufacturing a spray layer. 1. A zinc-free spray powder for thermally coating a substrate , in particular for thermally coating a bearing part of a bearing apparatus , which spray powder has the following composition except for unavoidable contaminants:Tin=5% to 30% weight percent;Aluminum=0.1% to 5% weight percent;Iron=at most 1% weight percent;Copper=difference to 100% weight percent.2. A spray powder in accordance with claim 1 , wherein the spray powder includes a tin content of between 15% and 25% weight percent claim 1 , preferably of 20% weight percent tin.3. A spray powder in accordance with claim 1 , wherein the spray powder includes an aluminum content of between 0.5% and 2% weight percent claim 1 , preferably of 1% weight percent aluminum.4. A spray powder in accordance with claim 1 , wherein the spray powder includes at most an iron content of 0.5% weight percent claim 1 , preferably of at most 0.2% weight percent iron.5. A spray powder in accordance with claim 1 ,wherein the size of the particles of the spray powder lies between 5 μm and 120 μm, preferably between 10 μm and 60 μm.6. A spray powder in accordance with claim 1 , wherein the spray powder is manufactured via gas atomization claim 1 , water atomization claim 1 , sintering claim 1 , flash drying claim 1 , or mechanical alloying.7. A zinc-free layer system applied via thermal spray claim 1 , having a surface layer claim 1 , in particular a bearing layer of a ...

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Номер записи: 38
05-12-2013 дата публикации

Turbine Blade for Industrial Gas Turbine and Industrial Gas Turbine

Номер: US20130323069A1
Автор: Akira Mebata, Hideyuki Arikawa, Tadashi Kasuya, Takeshi Izumi, Toshio Narita, Yoshitaka Kojima
Принадлежит: HITACHI LTD, Hokkaido University NUC

A turbine blade for industrial gas turbine is used which includes a blade substrate formed of a single-crystal heat-resistant alloy containing C: 0.06 to 0.08%, B: 0.016 to 0.035%, Hf: 0.2 to 0.3%, Cr: 6.9 to 7.3%, Mo: 0.7 to 1.0%, W: 7.0 to 9.0%, Re: 1.2 to 1.6%, Ta: 8.5 to 9.5%, Nb: 0.6 to 1.0%, Al: 4.9 to 5.2%, Co: 0.8 to 1.2%, and the remainder substantially consisting of Ni with reference to mass, and includes a diffusion barrier layer, a metal layer, a bond coat, and a top coat, these layers and coats being stacked in this order on a surface of the blade substrate, the metal layer having a thickness of 5 to 30 μm. Thus, the turbine blade can be provided which has a thermal barrier coating formed without loss of a function of the diffusion barrier layer.

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Номер записи: 39
13-02-2014 дата публикации

Metal Foil Provided with Electrically Resistive Layer, and Board for Printed Circuit Using Said Metal Foil

Номер: US20140041910A1
Автор: Toshio Kurosawa
Принадлежит: JX Nippon Mining and Metals Corp

Metal foil provided with an electrically resistive layer, characterized in that an alloy (in particular, a NiCrAlSi alloy) resistive layer containing 1 to 6 mass % of Si is formed on the metal foil controlled to have a ten-point average roughness Rz, which was measured by an optical method, of 4.0 to 6.0 μm, and the variation in the resistance value of the electrically resistive layer is within ±10%. Provided is a copper foil that allows embedding of a resistive material in a board by further forming an electrically resistive layer on the copper foil, and further allows improving the adhesiveness and suppressing the variation in resistance value within a certain range. As needed, metal foil provided in advance with a copper-zinc alloy layer formed on the surface thereof and a stabilizing layer composed of at least one component selected from zinc oxide, chromium oxide, and nickel oxide formed on the copper-zinc alloy layer is used.

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Номер записи: 40
13-02-2014 дата публикации

Process for producing a repair coating on a coated metallic surface

Номер: US20140044868A1
Автор: Manfred Walter, Mats Eriksson
Принадлежит: Chemetall GmbH

A process for producing a repair coating on at least one metallic surface that is coated with at least one corrosion protection coating A applied with at least one composition selected from the group of pretreatment compositions, of organic compositions and of silicon compound(s) containing compositions, whereby the at least one corrosion protecting coating A has been at least partially removed in the area Z, whereby a thin corrosion protecting coating B containing at least one silicon compound is applied with a solution or dispersion containing at least one silane, at least one silanol, at least one siloxane, at least one polysiloxane or any mixture of these (=“siloxane composition”) on at least a part of the area Z. Optionally, a further corrosion protecting coating C may he applied on the thin corrosion protecting coating B generated with the siloxane composition whereby the at least one further corrosion protecting coating C is generated with at least one organic composition like a primer, a wet-primer, an e-coat, a powder coat, a base-coat or a clear-coat or with at least one composition which is the same or another siloxane composition as for the thin film B.

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Номер записи: 41
13-03-2014 дата публикации

Spallation-resistant multilayer thermal spray metal coatings

Номер: US20140072821A1
Автор: Danie Jacobus Dewet, David A. Lee, Heidi Lynette de Villiers-Lovelock, James B. C. Wu
Принадлежит: Kennametal Inc

A multilayer, wear- and corrosion-resistant coating on a metal substrate comprising a first metal coating layer comprising a composite carbide material; a second metal coating layer over the first metal coating layer comprising at least about 50 wt % of a metal selected from the group consisting of Co, Ni, and Fe; and a surface metal coating layer comprising a cemented carbide material having a third-layer carbide material and a third-layer Co-based or Ni-based binder material.

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Номер записи: 42
06-01-2022 дата публикации

COATING FOR ENHANCED PERFORMANCE AND LIFETIME IN PLASTIC PROCESSING APPLICATIONS

Номер: US20220002880A1
Автор: ARNDT Mirjam, BOLVARDI Hamid, Khatibi Ali, NEFF Florian, Ramm Jürgen
Принадлежит: Oerlikon Surface Solutions AG, Pfäffikon

An improved coating used in plastic processing applications including a first layer system that includes at least one corrosion resistant material layer; a second layer system that includes at least one abrasion resistant material layers; and a transition layer provided between the first layer and the second layer. The coating is resistant to both abrasion and corrosion, while maintaining ductility and impact resistance. 1. A coating deposited on a surface of a substrate , said coating comprising:a first layer comprising at least one corrosion resistant material layer;a second layer comprising at least one abrasion resistant material layers; anda transition layer provided between the first layer and the second layer,wherein the first layer is deposited closer to the substrate than the second layer.2. The coating according to claim 1 , whereinthe first layer is part of a first layer system deposited closer to the substrate than the second layer, said first layer system comprising one or more corrosion resistant layers, wherein at least one corrosion resistant layer being an AlCrO layer.3. The coating according to claim 1 , whereinthe second layer is part of a second layer system deposited more distant from the substrate than the first layer system, said second layer system comprising one or more abrasion resistant layers, wherein at least one abrasion resistant layer being a CrON layer.4. The coating according to claim 1 , whereinthe transition layer is part of a transition layer system, said transition layer system comprising one or more transition layers, wherein at least one transition layer being a CrON layer.5. The coating according to claim 1 , wherein{'sub': 2', '3, 'the transition layer system comprises a CrOlayer.'}6. The coating according to claim 3 , whereinthe second layer system comprises at least one CrN layer.7. The coating according to claim 3 , whereinthe second layer system comprises at least one CrO layer.8. The coating according to claim 3 , ...

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Номер записи: 43
05-01-2017 дата публикации

Steel Armor Wire Coatings

Номер: US20170001415A1
Автор: Barmatov Evgeny, Hughes Trevor, Protasov Vadim, Varkey Joseph, Wanjau Paul
Принадлежит:

A wire includes a ferrous core. The ferrous core can be coated. The coatings can include nickel, molybdenum, zinc and Fe. A process of forming a wire can include placing a metal strip alongside a ferrous wire core, bending the strip around the core, and seam welding the strip to form a metal tube around the core. The process of forming a wire can include applying a metal layer to a ferrous metal rod to form a plated rod, placing a metal strip alongside the rod, bending the strip around the rod, and seam welding the strip to form a metal tube around the rod. The process of forming a wire can include coating a ferrous wire core with a layer of nickel, molybdenum or a nickel alloy that circumferentially surrounds the ferrous wire core. 1. A process of forming a wire comprising:coating a ferrous wire core with an interface layer of nickel, molybdenum or a nickel alloy,wherein the interface layer circumferentially surrounds the ferrous wire core; andcoating the interface layer with an outer layer.2. The process of claim 1 , wherein the ferrous wire core is steel.3. The process of claim 1 , wherein the interface layer has a thickness of between 2 and 60 microns.4. The process of claim 1 , wherein outer layer has a thickness of between 1 and 50 microns.5. The process of claim 1 , wherein the outer layer comprises a zinc alloy claim 1 , and wherein the zinc allow comprises:binary Zn—Ni or Zn—Co alloy; orternary Zn—Ni—Co, Zn—Ni—Mo or Zn—Co—Mo alloy.6. The process of claim 1 , further comprising an Fe layer claim 1 , wherein the Fe layer circumferentially surrounds the interface layer and is circumferentially surrounded by the outer layer.7. The process of claim 6 , wherein the Fe layer has a thickness of between 2 and 20 microns.8. The process of claim 1 , further comprising a galvanized zinc coating. The present disclosure relates to steel armor wire strength member coating compositions, structures, and processes.Armor wire strength members used in wireline cables for ...

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Номер записи: 44
05-01-2017 дата публикации

COATING MATERIAL

Номер: US20170002444A1
Автор: "OSULLIVAN MICHAEL", KATHREIN MARTIN
Принадлежит:

A coating material has Cr-rich regions having a Cr content >95% by mass which form Cr-containing particles. At least some of these particles are present in the form of aggregates or agglomerates, at least some have pores and have in the Cr-rich regions a mean nanohardness of ≦4 GPa and/or a mean surface area, measured by BET, >0.05 m/g. The coating material is particularly suitable for cold gas spraying. There is also described a process for the production of a coating, and to a coating produced by the process. 128-. (canceled)29. A coating material , comprising:Cr-rich regions having a Cr content >95% by mass, said Cr-rich regions forming Cr-containing particles; andwherein one or more of the following is true:at least some of said Cr-containing particles are present in the form of aggregates or agglomerates;at least some of said Cr-containing particles have pores formed therein;{'sub': 'HIT 0.005/5/1/5', 'said Cr-rich regions have a mean nanohardness of ≦4 GPa; or'}said Cr-containing particles have a mean surface area >0.05 m2/g, measured by way of Brunauer-Emmett-Teller.30. The coating material according to claim 29 , configured in powder form or granulate form.31. The coating material according to claim 29 , wherein at least some of said Cr-containing particles have a mean porosity claim 29 , determined by quantitative image analysis claim 29 , of >10% by volume.32. The coating material according to claim 29 , which comprises a material with a lower yield strength than Cr applied to a surface of said Cr-containing particles claim 29 , at least in regions thereof.33. The coating material according to claim 29 , wherein said Cr-containing particles have a mean particle size or granule size d50 claim 29 , measured by laser diffractometry claim 29 , of 5 μm Подробнее

Номер записи: 45
07-01-2016 дата публикации

Polymer Electrospinning Apparatus

Номер: US20160002824A1
Автор: Roach Paul, Yang Ying
Принадлежит: University of Keele

The present invention relates to an apparatus for producing electrospun polymer fibres with a modified surface, processes for producing a polymer fibre with a modified surface, non-woven polymer fibre mats or meshes comprising an electrospun polymer fibre, including multi-layered electrospun polymer fibre meshes, and a kit including a directional plasma device. 1. A plasma-electrospinning apparatus comprising a polymer electrospinning device for producing a polymer fibre and a directional plasma device , the directional plasma device being a plasma torch or a plasma plume-generating device , whereby the directional plasma device is arranged so that , during operation , a polymer composition from the polymer electrospinning device passes through a plasma jet or plasma plume from the directional plasma device.2. The plasma-electrospinning apparatus according to claim 1 , wherein the directional plasma device is arranged so the plasma jet or plume extends at an angle more than 0° with respect to the overall direction of the jet of polymer composition along the polymer path from the polymer solution outlet to the polymer fibre collector.3. The plasma-electrospinning apparatus according to claim 1 , wherein the plasma electrode tip is arranged coaxially to the direction of the polymer path from the polymer composition outlet to the polymer fibre collector.4. The plasma-electrospinning apparatus according to claim 3 , wherein the plasma electrode is tubular and forms the gas carrier conduit claim 3 , and the electrospinning capillary tube is located within the gas carrier conduit/plasma electrode.5. A plasma-electrospinning apparatus according to where the polymer electrospinning device comprises at least two different plasma zones claim 1 , whereby the plasma zones are arranged so that claim 1 , during operation claim 1 , the polymer composition from the electrospinning device passes through at least two distinct plasmas.6. The plasma-electrospinning apparatus according ...

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Номер записи: 46
07-01-2016 дата публикации

VISUAL INDICATOR OF COATING THICKNESS

Номер: US20160003092A1
Автор: Chamberlain Adam Lee, Lazur Andrew Joseph, Lee Kang N.
Принадлежит:

In some examples, a coating may include at least one feature that facilitates visual determination of a thickness of the coating. For example, the coating may include a plurality of microspheres disposed at a predetermined depth of the coating. The plurality of microspheres may define a distinct visual characteristic. By inspecting the coating and viewing at least one of the microspheres, the thickness of the coating may be estimated. In some examples, the plurality of microspheres may be embedded in a matrix material, and the distinct visual characteristic of the microspheres may be different than the visual characteristic of the matrix material. In other examples, the at least one feature may include at least one distinct layer in the coating system that includes a distinct visual characteristic, such as a color of the distinct layer. 1. An article comprising:a substrate; anda coating on the substrate, wherein the coating comprises at least one abradable layer, wherein the at least one abradable layer comprises a matrix material and a plurality of microspheres located within the at least one abradable layer at a predetermined depth from an outer surface of the coating, wherein the plurality of microspheres define a visual characteristic distinct from the matrix material, and wherein the plurality of microspheres comprise at least one rare earth oxide, at least one rare earth silicate, or at least one rare earth oxide and at least one rare earth silicate.2. The article of claim 1 , wherein the coating further comprises an environmental barrier coating layer claim 1 , wherein the environmental barrier coating layer comprises at least one rare earth silicate claim 1 , and wherein the environmental barrier coating layer is between the substrate and the at least one abradable layer.3. The article of claim 1 , wherein the coating further comprises a bond layer between the substrate and the at least one abradable layer claim 1 , wherein the bond layer comprises silicon.4 ...

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Номер записи: 47
04-01-2018 дата публикации

Composite wires for coating substrates and methods of use

Номер: US20180002801A1
Автор: Bruce Lindsay CARLTON, Leo Vinod Marcus ANTONY
Принадлежит: General Electric Technology GmbH

A composite wire utilized in connection with forming a resistant coating on a substrate includes a metallic outer sheath and an inner core, the inner core having a total fill weight above 15% total composite wire weight and including less than less 35% by weight of boron carbide in the inner core, and method of making the same.

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Номер записи: 48
07-01-2021 дата публикации

METHOD AND ARRANGEMENT FOR MACHINING A WORKPIECE

Номер: US20210002753A1
Автор: PEHNELT Sebastian, Ullrich Wolfgang
Принадлежит: STURM MASCHINEN-& ANLAGENBAU GMBH

The invention relates to a method and an arrangement for machining a workpiece with a surface, into which a groove structure with grooves and interposed ribs is introduced, wherein undesirable burrs can develop on the groove structure. According to the invention, for testing and determining the formation of burrs a measuring means is provided which emits a light to the surface of the groove structure and receives light reflected from the surface, wherein a degree of the burr formation is determined depending on the reflected light. 1. Method for machining a workpiece with a surface , in particular in a bore , into which a groove structure with grooves and interposed ribs is introduced , wherein undesirable burrs can develop on the groove structure ,characterized in thatfor testing and determining a formation of burrs a measuring means is provided which emits a light to the surface of the groove structure and receives light reflected from the surface, wherein a degree of the burr formation is determined depending on the reflected light.2. Method according to claim 1 ,characterized in thatby means of the measuring means the determination of the burr formation is carried out simultaneously or immediately after the introduction of the groove structure.3. Method according to claim 1 ,characterized in thatthe light is chromatic.4. Method according to claim 1 ,characterized in thatthe measuring means has at least one confocal point sensor which emits and receives the light.5. Method according to claim 1 ,characterized in thata reduction of a ratio between reflected light and emitted light is considered as a degree of an increase in the burr formation.6. Method according to claim 1 ,characterized in thatthe groove structure is introduced with a material removing tool, in particular a cutting head or a rotary chisel.7. Method according to claim 6 ,characterized in thaton reaching a predetermined value for the reflected light the material removing tool is readjusted and/or ...

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Номер записи: 49
07-01-2021 дата публикации

COMPONENT FOR USE IN PLASMA PROCESSING APPARATUS, PLASMA PROCESSING APPARATUS, AND METHOD FOR MANUFACTURING THE COMPONENT

Номер: US20210002754A1
Автор: MITSUHASHI Koji, Nishimura Satoshi
Принадлежит: TOKYO ELECTRON LIMITED

A component for use in a plasma processing apparatus, which is to be exposed to a plasma, includes a base material, an alumite layer and a thermally sprayed film. The base material has a plurality of through holes and a rough surface at which one end of each of the through holes is opended. The alumite layer is formed on a surface of the base material having the rough surface by an anodic oxidation process. The thermally sprayed film is formed on the rough surface with the alumite layer therebetween. 1. A component for use in a plasma processing apparatus , which is to be exposed to a plasma , the component comprising:(i) a base material having a plurality of through holes and a first rough surface at which one end of each of the through holes is opened, the first rough surface of the base material formed only on a surface of the base material disposed outside of the through holes,(ii) an alumite layer having a second rough surface formed on the first rough surface of the base material by an anodic oxidation process, and(iii) a thermally sprayed film formed on the second rough surface of the alumite layer,wherein the plurality of through holes include substantially vertical sidewalls and tapered ends,wherein the alumite layer is formed on the substantially vertical sidewalls and the tapered ends,wherein the thermally sprayed film is formed on the alumite layer but is not provided on the substantially vertical sidewalls of the through holes, andwherein at a location of the first rough surface, the alumite layer is formed on the first rough surface and the thermally sprayed film is formed on the alumite layer while, on the substantially vertical sidewalls of the through holes, only the alumite layer is formed.2. The component of claim 1 , wherein the first rough surface of the base material has an arithmetic average roughness ranging from 1.5 μm to 5 μm.3. The component of claim 1 , wherein the component is configured to inject a gas into a processing chamber of the ...

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Номер записи: 50
13-01-2022 дата публикации

COATED CUTTING TOOL

Номер: US20220009002A1
Автор: FUKUSHIMA Naoyuki
Принадлежит: TUNGALOY CORPORATION

An object of the invention is to provide a coated cutting tool whose tool life can be extended by having excellent wear resistance and fracture resistance. The coated cutting tool includes: a substrate; and a coating layer formed on a surface of the substrate, in which the coating layer includes a lower layer, an intermediate layer, and an upper layer in this order from a substrate side to a surface side of the coating layer, the lower layer includes one or more Ti compound layers formed of a specific Ti compound, the intermediate layer contains TiCNO, TiCO, or TiAlCNO, the upper layer contains α-type AlO, an average thickness of the lower layer is 2.0 μm or more and 8.0 μm or less, an average thickness of the intermediate layer is 0.5 μm or more and 2.0 μm or less and is 10% or more and 20% or less of a thickness of the entire coating layer, an average thickness of the upper layer is 0.8 μm or more and 6.0 μm or less, and in the intermediate layer, a ratio of a length of CSL grain boundaries to a total length 100% of a total grain boundary is 20% or more and 60% or less. 1. A coated cutting tool , comprising:a substrate; anda coating layer formed on a surface of the substrate, whereinthe coating layer includes a lower layer, an intermediate layer, and an upper layer in this order from a substrate side to a surface side of the coating layer,the lower layer includes one or more Ti compound layers formed of a Ti compound containing Ti and at least one element selected from the group consisting of C, N, and B,the intermediate layer contains TiCNO, TiCO, or TiAlCNO,{'sub': 2', '3, 'the upper layer contains cit-type AlO,'}an average thickness of the lower layer is 2.0 μm or more and 8.0 μm or less,an average thickness of the intermediate layer is 0.5 μm or more and 2.0 μm or less and is 10% or more and 20% or less of a thickness of the entire coating layer,an average thickness of the upper layer is 0.8 μm or more and 6.0 μm or less, and.in the intermediate layer, a ratio ...

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Номер записи: 51
07-01-2021 дата публикации

APPARATUS FOR FEEDING AND DOSING POWDER, APPARATUS FOR PRODUCING A LAYER STRUCTURE ON A SURFACE AREA OF A DEVICE, PLANAR HEATING ELEMENT AND METHOD FOR PRODUCING A PLANAR HEATING ELEMENT

Номер: US20210007184A1
Автор: FLADE Enrico, RIEMENSPERGER Reinhold
Принадлежит:

An apparatus for feeding and dosing powder includes a powder storage container, an oscillating feeder with feeder with adjustable feeding rate for dispensing the powder to a powder outlet, a conduit arrangement for feeding the powder dispensed from the oscillating feeder in a feeding gas as a powder-gas mixture and for supplying the powder-gas mixture to a powder processor, wherein a decoupler is provided in the conduit arrangement to extract a defined proportion of the powder from the powder-gas mixture, a powder quantity measuring arrangement for detecting the decoupled powder quantity and for providing a powder quantity information signal, wherein the extracted powder quantity has a predetermined ratio to the fed powder quantity of the oscillating feeder, and controller configured to adjust the adjustable feeding rate of the oscillating feeder to a predetermined set value based on the powder quantity information signal provided. 1. Apparatus for feeding and dosing powder , comprising:a powder storage container for storing and providing powder,an oscillating feeder comprising a feeding unit with an adjustable feeding rate for dispensing the powder to a powder outlet with the adjustable feeding rate,a conduit arrangement for feeding the powder dispensed by the oscillating feeder in a feeding gas as a powder-gas mixture and for supplying the powder-gas mixture to a powder processor, wherein a decoupler is provided in the conduit arrangement for extracting a defined proportion of the powder from the powder-gas mixture,a powder quantity measuring arrangement for detecting the decoupled powder quantity per unit time and for providing a powder quantity information signal, wherein the decoupled powder quantity per unit time comprises a predetermined ratio to the fed powder quantity of the oscillating feeder within a tolerance range, anda controller configured to adjust the adjustable feeding rate of the oscillating feeder to a predetermined set value based on the powder ...

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Номер записи: 52
03-01-2019 дата публикации

INTEGRATED WIRING SYSTEM FOR COMPOSITE STRUCTURES

Номер: US20190008065A1
Автор: Dalal Hardik, Duce Jeffrey Lynn, Merriweather Breana K., Robbins Brent A., Rosillo Yelina
Принадлежит:

A composite part comprising an electronic device and method for making the same. A primer is deposited on a surface of the composite part. An electronic device comprising a group of conductive elements is deposited on the primer. Power may be supplied to a device connected to the composite part through current flowing through the group of conductive elements. 1. An apparatus comprising:a composite part;a primer deposited on a surface of the composite part; andan electronic device comprising a group of conductive elements deposited on the primer, wherein power is supplied to a device connected to the composite part through current flowing through the group of conductive elements.2. The apparatus of claim 1 , wherein the primer comprises:a layer of metallic material sprayed on the surface of the composite part using a thermal plasma spray; anda layer of ceramic material sprayed on the layer of metallic material using the thermal plasma spray.3. The apparatus of claim 1 , wherein conductive material is sprayed on the primer using a thermal plasma spray to form the group of conductive elements.4. The apparatus of claim 3 , wherein the conductive material is selected from at least one of copper claim 3 , copper alloy claim 3 , carbon claim 3 , graphene claim 3 , titanium claim 3 , nickel claim 3 , or silver.5. The apparatus of claim 1 , wherein the composite part is an aircraft part.6. The apparatus of claim 5 , wherein the composite part is selected from one of a skin panel claim 5 , an interior panel claim 5 , a stringer claim 5 , a frame claim 5 , a spar claim 5 , a wing claim 5 , a winglet claim 5 , a fuselage claim 5 , an empennage claim 5 , and a control surface.7. The apparatus of claim 1 , wherein the group of conductive elements comprises at least one of an electrical trace claim 1 , an interconnect claim 1 , a wire claim 1 , a transistor claim 1 , an integrated circuit claim 1 , or a conductive connector.8. The apparatus of claim 1 , wherein the device ...

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Номер записи: 53
14-01-2021 дата публикации

CUTTING TOOL

Номер: US20210008633A1
Автор: Imamura Shinya, OKUNO Susumu, Ono Satoshi, Paseuth Anongsack
Принадлежит: Sumitomo Electric Hardmetal Corp.

A cutting tool includes: a substrate including a rake face; and a coating film that coats the rake face, wherein the coating film includes an α-AlOlayer disposed on the substrate, the α-AlOlayer includes crystal grains of α-AlO, an area ratio of crystal grains oriented in (001) among the crystal grains is 50% to 90% in the α-AlOlayer at the rake face, and a film residual stress Adetermined based on a crystal plane interval of a (001) plane of the α-AlOlayer at the rake face is more than 0 MPa and less than or equal to 2000 MPa, and a film residual stress Bdetermined based on a crystal plane interval of a (110) plane of the α-AlOlayer at the rake face is more than or equal to −1000 MPa and less than 0 MPa. 1. A cutting tool comprising: a substrate including a rake face; and a coating film that coats the rake face , wherein{'sub': 2', '3, 'the coating film includes an α-AlOlayer disposed on the substrate,'}{'sub': 2', '3', '2', '3, 'the α-AlOlayer includes crystal grains of α-AlO,'}{'sub': 2', '3, 'an area ratio of crystal grains oriented in (001) among the crystal grains is more than or equal to 50% and less than or equal to 90% in the α-AlOlayer at the rake face, and'}{'sup': '2', 'claim-text': [{'sub': A', '2', '3, 'a film residual stress Adetermined based on a crystal plane interval of a (001) plane of the α-AlOlayer at the rake face is more than 0 MPa and less than or equal to 2000 MPa, and'}, {'sub': A', '2', '3, 'a film residual stress Bdetermined based on a crystal plane interval of a (110) plane of the α-AlOlayer at the rake face is more than or equal to −1000 MPa and less than 0 MPa.'}], 'in a residual stress measurement performed in accordance with a 2θ-sinψ method using X rays,'}2. The cutting tool according to claim 1 , wherein{'sub': 2', '3, 'the α-AlOlayer has a thickness of more than or equal to 1 μm and less than or equal to 20 μm,'}{'b': 1', '1', '2', '1', '2, 'sub': 10', '2', '3', '10', '2', '3', '40', '2', '3', '2', '3, 'claim-text': [{'sub': 2', ' ...

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Номер записи: 54
14-01-2021 дата публикации

Method for Machining a Crankcase and Machining Device

Номер: US20210008646A1
Автор: Frank Danneberg, Patrick Woisetschlaeger, Wolfram Wagener
Принадлежит: Bayerische Motoren Werke AG

A method for machining a crankcase includes providing a machining device. The machining device comprises a mechanical machining unit and a cooling/rinsing system, which is configured to cool and/or rinse the mechanical machining unit or a surface which is to be machined. The method also includes creating a structure in a cylinder wall of a crankcase using the mechanical machining unit. The method also includes using a fluid stream of the cooling/rinsing system to reshape at least certain regions of the structure.

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Номер записи: 55
27-01-2022 дата публикации

GALVANIZED STEEL SHEET HAVING EXCELLENT HARDNESS AND GALLING RESISTANCE, AND MANUFACTURING METHOD THEREFOR

Номер: US20220025503A1
Автор: Jung Woo-Sung, Jung Yong-Hwa, Kim Tae-Yeob, KO Kyoung-Pil, Nam Kyung-Hoon
Принадлежит:

Provided is a galvanized steel sheet plated by vacuum deposition and, more specifically, to a galvanized steel sheet having excellent hardness and galling resistance, and a method for manufacturing same. The zinc coated steel sheet includes: a base steel sheet; and a zinc coated layer formed on the base steel sheet. The zinc coated layer is formed of a columnar structure, and a content of Mn included in the zinc coated layer is 0.1 to 0.4 wt %. 1. A zinc coated steel sheet having excellent hardness and galling resistance , comprising:a base steel sheet; anda zinc coated layer formed on the base steel sheet,wherein the zinc coated layer is formed of a columnar structure, and a content of Mn included in the zinc coated layer is 0.1 to 0.4 wt %.2. The zinc coated steel sheet having excellent hardness and galling resistance of claim 1 , wherein the zinc coated layer satisfies the following relational formula 1 claim 1 ,{'br': None, '[content of Mg present in a zinc grain boundary (wt. %)]/[content of Mg in a coated layer (wt. %)−0.1]≥0.95\u2003\u2003[Relational expression 1]'}3. The zinc coated steel sheet having excellent hardness and galling resistance of claim 1 , wherein the zinc coated layer has an average size of zinc grains of the zinc coated layer of 80 to 200 nm.4. A method of manufacturing a zinc coated steel sheet having excellent hardness and galling resistance comprising:preparing a base steel sheet;forming a zinc coated layer through spraying vapor generated by electromagnetic levitation induction heating of a coating raw material onto the base steel sheet,wherein the coating raw material is a Zn—Mg alloy or a mixture of Zn and Mg having a content of Mg of 0.1 to 0.4 wt %.5. The method of a zinc coated steel sheet having excellent hardness and galling resistance of claim 4 , wherein the forming a zinc coated layer is performed at a vacuum degree of 1×10mbar or less.6. The method of a zinc coated steel sheet excellent having excellent hardness and galling ...

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Номер записи: 56
14-01-2016 дата публикации

Sliding member and method of manufacturing the sliding member

Номер: US20160010198A1
Автор: Naoki Sato, Ryoichi Kurata, Satoshi Masuda, Takashi AKAGAWA
Принадлежит: Senju Metal Industry Co Ltd

To provide a sliding member which has joined strength that is suitable for the circumstance, to which heavy load is applied, and which is excellent in abrasion resistance property. The sliding member 1 contains a supporting layer 2 composed of ferrous metallic material, and a sliding layer 3 composed of copper metallic material, which is formed on a surface 2 a of the supporting layer 2. The surface 2 a of the supporting layer 2 and the sliding layer 3 are configured to be not a plane and a sliding surface 3 a formed on a surface of the sliding layer 3 is configured to be not a plane. The sliding layer is formed on the roughed surface 2 a of the supporting layer 2 by thermal spaying.

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Номер записи: 57
14-01-2016 дата публикации

PROCESSES AND SYSTEMS FOR DEPOSITING COATING SYSTEMS, AND COMPONENTS COATED THEREWITH

Номер: US20160010199A1
Автор: Miner Robert Glynn, Nerz John Edmund, Rodgers Matthew Alan
Принадлежит: GENERAL ELECTRIC COMPANY

Processes and systems for forming a coating system on a component. The process of forming the coating system on the component includes placing an apparatus in a location that promotes coating particles in flight to be redirected towards a surface on the component. The surface is obstructed by portions of the component limiting line-of-sight from a source of the coating particles to the surface. The coating particles are then deposited onto the surface of the component. The coating particles initially travel in a direction of initial particle travel and are redirected by the apparatus towards the surface on the component at a direction of final particle travel relative to the surface. The line-of-site from the source of the coating particles is at an angle of less than 30 degrees relative to the surface of the component and the direction of final particle travel is at an angle of 30 degrees or more relative to the surface of the component. 1. A process of forming a coating system on a component , the process comprising:placing an apparatus in a location that promotes coating particles in flight to be redirected towards a surface on the component, wherein the surface is obstructed by portions of the component limiting line-of-sight from a source of the coating particles to the surface; and thendepositing the coating particles onto the surface of the component, wherein the coating particles initially travel in a direction of initial particle travel and are redirected by the apparatus towards the surface on the component at a direction of final particle travel relative to the surface, wherein the direction of initial particle travel forms an angle relative the surface on the component that is different than the angle formed by the direction of final particle travel relative to the surface.2. The process of claim 1 , wherein the line-of-site from the source of the coating particles is at an angle of less than 30 degrees relative to the surface of the component and the ...

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Номер записи: 58
14-01-2016 дата публикации

Component for use in plasma processing apparatus, plasma processing apparatus, and method for manufacturing the component

Номер: US20160010200A1
Автор: Koji Mitsuhashi, Satoshi Nishimura
Принадлежит: Tokyo Electron Ltd

A component for use in a plasma processing apparatus, which is to be exposed to a plasma, includes a base material, an alumite layer and a thermally sprayed film. The base material has a plurality of through holes and a rough surface at which one end of each of the through holes is opended. The alumite layer is formed on a surface of the base material having the rough surface by an anodic oxidation process. The thermally sprayed film is formed on the rough surface with the alumite layer therebetween.

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Номер записи: 59
09-01-2020 дата публикации

PROCESSING APPARATUS FOR PROCESSING A WORKPIECE SURFACE WITH FLUID FLOW SHIELDING

Номер: US20200009608A1
Автор: BOHNHEIO Christian
Принадлежит: OERLIKON METCO AG, WOHLEN

Processing apparatus for processing a workpiece surface in form of an internal coating of cylinder bores which are arranged in a row. The apparatus includes a shield unit which is provided to separate from one another—at least during operation—a part region of the workpiece surface provided for the processing and an adjacently arranged part region of the workpiece surface, whereby the shield unit has at least one blocking nozzle which is provided to generate a fluid flow for separating the at least two part regions, wherein the blocking nozzle is positioned such that the fluid flow flows along the workpiece surface and the blocking nozzle is directed to the part region between two cylinder bores. 1. A processing apparatus for processing a workpiece surface in form of an internal coating of cylinder bores which are arranged in a row , the apparatus including a shield unit which is provided to separate from one another—at least during operation—a part region of the workpiece surface provided for the processing and an adjacently arranged part region of the workpiece surface , whereby the shield unit has at least one blocking nozzle which is provided to generate a fluid flow for separating the at least two part regions wherein the blocking nozzle is positioned such that the fluid flow flows along the workpiece surface and the blocking nozzle is directed to the part region between two cylinder bores.2. A processing apparatus in accordance with claim 1 , wherein the at least one blocking nozzle is configured as a compressed air nozzle.3. A processing apparatus in accordance with claim 1 , wherein the blocking nozzle is provided to generate a flat jet.4. A processing apparatus in accordance with claim 1 , further comprising a torch for processing the workpiece surface.5. A processing apparatus in accordance with claim 4 , wherein the fluid flow which can be generated by way of the at least one blocking nozzle is provided for deflecting a torch jet of the torch.6. A ...

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Номер записи: 60
14-01-2016 дата публикации

HYBRID MANUFACTURING FOR ROTORS

Номер: US20160010469A1
Автор: Guo Changsheng
Принадлежит:

A method for manufacturing a rotor includes manufacturing a hub using a conventional manufacturing process and manufacturing an airfoil on the hub using a layer-by-layer additive manufacturing process. A rotor includes a hub that has been manufactured with a conventional manufacturing process and an airfoil that has been manufactured on the hub with a layer-by-layer additive manufacturing process. 1. A method for manufacturing a rotor , the method comprising:manufacturing a hub using a conventional manufacturing process; andmanufacturing an airfoil on the hub using a layer-by-layer additive manufacturing process.2. The method of claim 1 , wherein the conventional manufacturing process is a process selected from the group consisting of machining claim 1 , forging claim 1 , milling claim 1 , or combinations thereof.3. The method of claim 1 , wherein the layer-by-layer additive manufacturing process is a process selected from the group consisting of cold spray claim 1 , thermal spray claim 1 , plasma spray claim 1 , selective laser sintering claim 1 , direct metal laser sintering claim 1 , electron beam melting claim 1 , selective laser melting claim 1 , and combinations thereof.4. The method of claim 1 , wherein manufacturing the hub includes manufacturing the hub out of a first material claim 1 , and wherein manufacturing the airfoil includes manufacturing the airfoil out of a second material.5. The method of claim 1 , wherein manufacturing the airfoil includes manufacturing a first portion of the airfoil out of a first airfoil material and manufacturing a second portion of the airfoil out of a second airfoil material.6. The method of claim 1 , and further comprising:manufacturing a plurality of airfoils on the hub using a layer-by-layer additive manufacturing process.7. The method of claim 6 , wherein the plurality of airfoils are manufactured simultaneously.8. The method of claim 6 , wherein the plurality of airfoils are manufactured one at a time.9. The method of ...

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Номер записи: 61
14-01-2016 дата публикации

WEAR PROTECTION ARRANGEMENT FOR A TURBOMACHINE, PROCESS AND COMPRESSOR

Номер: US20160010488A1
Автор: ALBERS Lothar, BOCK Stephan, Schneiderbanger Stefan
Принадлежит:

The present invention relates to a wear protection arrangement for a turbomachine, comprising at least one adjustable guide vane, a casing in which the guide vane is arranged in an adjustable manner, an inner ring, made from a metallic material, in or on which the guide vane is arranged in an adjustable manner, a first gap between an inner guide vane tab and the inner ring and a second gap between an outer guide vane tab and the casing, at least one wear protection coating, wherein the wear protection coating(s) is/are connected to the inner ring and/or to the inner guide vane tab and the wear protection coating(s) forms or form the first gap, at least in certain regions, and/or the wear protection coating(s) is/are connected to the casing and/or to the outer guide vane tab and the wear protection coating(s) forms/form the second gap, at least in certain regions. The invention further relates to a method for applying an abradable wear protection coating and for applying an abrasive wear protection coating and to a compressor for a turbomachine having a wear protection arrangement. 114.-. (canceled)15. A wear protection arrangement for a turbomachine , wherein the arrangement comprisesat least one adjustable guide vane,a casing in which the at least one guide vane is arranged in an adjustable manner,an inner ring made from a metallic material, in or on which ring the at least one guide vane is arranged in an adjustable manner,a first gap between an inner guide vane tab and the inner ring and a second gap between an outer guide vane tab and the casing,one or more wear protection coatings connected to the inner ring and/or to the inner guide vane tab and forming the first gap, at least in certain regions,and/or one or more wear protection coatings connected to the casing and/or to the outer guide vane tab and forming the second gap, at least in certain regions.16. The wear protection arrangement of claim 15 , wherein the one or more wear protection coatings are ...

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Номер записи: 62
10-01-2019 дата публикации

COLD SPRAY NOZZLES

Номер: US20190010612A1
Автор: Chiappetta Louis, Haas Martin, Klecka Michael A., Nardi Aaron T.
Принадлежит:

A nozzle assembly for a cold spray deposition system includes a nozzle body with an axial bore. The axial bore defines a converging segment, a diverging segment downstream of the converging segment, and a throat fluidly connected between the converging and diverging segments of the axial bore. A particulate conduit is fixed within the axial bore and extends along the axial bore diverging segment for issuing solid particulate into the diverging segment of the axial bore. 1. A nozzle assembly for a cold spray system , comprising: a converging segment;', 'a diverging segment downstream of the converging segment;', 'a throat fluidly connected between the converging and diverging segments; and, 'a nozzle body with an axial bore, the axial bore defininga particulate conduit fixed within the axial bore and extending along the axial bore into the diverging segment for issuing solid particles into the diverging segment of the axial bore.2. An assembly as recited in claim 1 , wherein the particulate conduit includes an outlet disposed in the diverging segment.3. An assembly as recited in claim 2 , wherein the particulate conduit defines a substantially uniform flow area within both the diverging and converging segments of the axial bore.4. An assembly as recited in claim 1 , wherein the nozzle body includes a steel material.5. An assembly as recited in claim 1 , further including a motive gas coupling connected to the particulate conduit.6. An assembly as recited in claim 5 , wherein the motive gas coupling is a first motive gas coupling claim 5 , and further including a second motive gas coupling connected to the converging segment of the axial bore.7. An assembly as recited in claim 1 , further including an insert seated within the axial bore and fixing the particulate conduit within the axial bore.8. An assembly as recited in claim 7 , wherein the insert is seated within the converging segment of the axial bore.9. An assembly as recited in claim 7 , wherein the insert ...

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Номер записи: 63
10-01-2019 дата публикации

Method for manufacture of high temperature cylindrical component for a gas turbine engine

Номер: US20190010811A1
Автор: Luke Freeman, Oliver Jones
Принадлежит: Rolls Royce PLC

A method for the manufacture of a cylindrical component suited to use in a high temperature environment and incorporating an erosion resistant coating (4) on its outer cylindrical surface (6) is described. The method comprises, in sequential steps; providing a work piece (1) having a cylindrical body including a pair of axially spaced radially extending ribs (3a, 3b) defining an annular trough (2) therebetween. Shot peening the work piece (1). Applying an erosion resistant coating (4) in the annular trough (2) to a depth which sits radially inwardly of the radially outermost ends of the ribs (3a, 3b). Turning the radially outermost ends of the ribs (3a, 3b) whereby to match the depth of the coating (4) and provide an outer cylindrical surface with a consistent diameter across both ribs (3a, 3b) and the coating (4).

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Номер записи: 64
09-01-2020 дата публикации

METHOD OF COATING AN ARTICLE, PASTE AND PLUG FOR PREVENTING HOLE BLOCKAGE DURING COATING

Номер: US20200010944A1
Автор: Cao Lei, EMINOGLU Cem Murat, Hardwicke Canan Uslu, PAN Zhida, Peng Wenqing, Zhang Liming, ZHAO Jianzhi
Принадлежит: GENERAL ELECTRIC COMPANY

A method includes masking at least one hole of an article with a paste, wherein the hole opens onto a surface of the article, applying a coating to the surface of the article, and removing the paste including contacting the paste with water, leaving at least one open hole in the surface of the coated article. The paste includes about 40-80 wt % of a filler material, about 0.5-20 wt % of an inorganic binder, about 0.5-15 wt % of a polyhydroxy compound and about 5-25 wt % of water. The filler material includes a first material which includes alkali metal doped alumina, zirconium oxide, titanium oxide, silicon dioxide, or a combination thereof and a second material which includes a silicate. A weight ratio between the first and second materials is in a range of about 1-10. 1. A method comprising:masking at least one hole of an article with a paste, wherein the hole opens onto a surface of the article;applying at least one coating to the surface of the article; andremoving the paste comprising contacting the paste with water, leaving at least one open hole in the surface of the coated article, from about 40 weight percent to about 80 weight percent of a high temperature resistant filler material comprising a first material and a second material, wherein the first material comprises alkali metal doped alumina, zirconium oxide, titanium oxide, silicon dioxide, or a combination thereof, the second material comprises a silicate, and a weight ratio between the first material and the second material is in a range from about 1 to about 10;', 'from about 0.5 weight percent to about 20 weight percent of an inorganic binder;', 'from about 0.5 weight percent to about 15 weight percent of a polyhydroxy compound; and', 'from about 5 weight percent to about 25 weight percent of water., 'wherein the paste comprises2. The method of claim 1 , wherein the high temperature resistant filler material has an average particle size in a range from about 0.1 micron to about 100 microns.3. The ...

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Номер записи: 65
09-01-2020 дата публикации

STRUCTURE OR STRUCTURAL MEMBER FOR HIGH TEMPERATURE APPLICATIONS AND METHOD AND APPARATUS FOR PRODUCING THEREOF

Номер: US20200010945A1
Автор: Laure Stefan, Steinwandel Jürgen, Uhlmann Franziska, Wilhelmi Christian
Принадлежит:

A structure for high temperature applications includes a base structure which includes a ceramic composite material, and a coating of a metal-semimetal compound, a metal boride, a metal carbide and/or a metal nitride. Furthermore, a production method and a coating device produces structures which resist high temperature applications with higher process temperatures and difficult chemical conditions. 1. A structure for high temperature application comprising:a base structure which includes a ceramic composite material; anda coating of a coating material which contains at least a metal-semimetal compound, a metal boride, a metal carbide and a metal nitride.2. The structure according to claim 1 , wherein at least one of the followingthe base structure has fibers and a matrix; andthe coating has a thickness of 0.1 μm to 200 μm.3. The structure according to claim 2 , wherein at least one of the following{'sub': 2', '2', '2', '2', '2, 'the fibers are formed from one or several fiber materials, which are selected from a group of fiber materials which comprises C, ceramic materials, SiC, HfC, ZrC, TaC, TiC, ZrB, HfB, TiB, TaBand NbBand nitride materials; and'}{'sub': 2', '2', '2', '2', '2, 'the matrix is formed from one or several matrix materials which are selected from a group of matrix materials comprising C, ceramic matrix materials, SiC, SiSiC, HfC, ZrC, TaC, TiC, ZrB, HfB, TiB, TaBand NbBand nitride materials.'}4. The structure according to claim 1 , wherein at least one of the followingthe coating is formed from a metal boride;the coating is formed from a metal carbide; and{'sub': 2', '2', '2', '2', '2, 'the coating is selected from one or several coating materials of a group of coating materials which comprises SiC, HfC, ZrC, TaC, TiC, ZrB, HfB, TiB, TaBand NbBand nitride materials.'}5. The structure according to claim 1 , wherein{'sub': '2', 'the coating is formed from ZrBand SiC.'}6. The structure according to claim 1 , whereinthe base structure comprises carbon ...

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Номер записи: 66
09-01-2020 дата публикации

Method for Processing a Cylinder

Номер: US20200011418A1
Автор: Patrick Woisetschlaeger, Wolfram Wagener
Принадлежит: Bayerische Motoren Werke AG

A method for processing an inner wall of a cylinder of an internal combustion engine includes providing a cylinder and processing an inner wall of the cylinder. The cylinder extends along a cylinder axis. The inner wall of the cylinder is processed in such a manner that at least one first structural region and one second structural region are formed along the cylinder axis. A geometry of the first structural region differs in design from a geometry of the second structural region.

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Номер записи: 67
19-01-2017 дата публикации

COATING COMPOSITIONS, APPLICATIONS THEREOF, AND METHODS OF FORMING

Номер: US20170014865A1
Автор: Cheney Justin Lee, Kusinski Grzegorz Jan
Принадлежит:

A method to protect and modify surface properties of articles is disclosed. In one embodiment of the method, an intermediate layer is first deposited onto a substrate of the article. The intermediate layer has a thickness of at least 2 mils containing a plurality of pores with a total pore volume of 5 to 50% within a depth of at least 2 mils. A lubricant material is deposited onto the intermediate layer, wherein the lubricant material infiltrates at least a portion of the pores and forms a surface layer. The surface layer can be tailored with the selection of the appropriate material for the intermediate layer and the lubricant material, for the surface layer to have the desired surface tension depending on the application. 127-. (canceled)28. A method for producing a wear resistant coating on an inner surface of an oil tubular good , the method comprising:depositing a metallic layer on the oil tubular good via a thermal spray process to produce a porous coating;depositing a fluoropolymer in the form of a slurry on the porous coating; andheating the fluoropolymer to infiltrate into pores in the porous coating of the metallic layer to form the wear resistant coating;wherein the wear resistant coating comprises subsections of hydrophilic and hydrophobic regions.29. The method of claim 28 , wherein the wear resistant coating comprises alternating layers of metallic particles with a surface tension of 75 dynes/cm or higher and fluoropolymer regions with a surface tension of 20 dynes/cm or lower.30. The method of claim 28 , wherein the metallic layer is deposited by a twin wire arc spray process.31. The method of claim 28 , wherein a high atomization pressure of 80-100 psi is used to deposit a first portion of the metallic layer claim 28 , and a low atomization pressure of 20-50 psi is used to deposit a second portion of the metallic layer.32. The method of claim 31 , wherein the first metallic layer is 1-5 mils in thickness claim 31 , and the second metallic layer is 15 ...

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Номер записи: 68
15-01-2015 дата публикации

ROTARY PISTON ENGINE AND METHOD FOR PRODUCING A ROTARY PISTON ENGINE

Номер: US20150017044A1
Автор: Huber Gerd, SIGMUND Ernst, Steinwandel Jürgen
Принадлежит:

A rotary piston engine comprises a stationary housing and a piston movably accommodated in the housing. The housing and the piston form at least one chamber with a chamber surface. At least one partial portion of the chamber surface has a thermal barrier coat for reducing a thermal conductivity of the partial portion of the chamber surface. At least one partial portion of the chamber surface has a metallic spray coat. A method for producing such a rotary piston engine can also be achieved. 1. A rotary piston engine , comprisinga stationary housing; anda piston movably accommodated in the housing, the housing and the piston forming at least one chamber with a chamber surface, at least one partial portion of the chamber surface having a thermal barrier coat configured to reduce a thermal conductivity of the partial portion of the chamber surface, and at least one partial portion of the chamber surface having a metallic spray coat.2. The rotary piston engine according to claim 1 , whereinthe thermal barrier coat has an oxide ceramic coat including zirconium oxide.3. The rotary piston engine according to claim 2 , whereinthe zirconium oxide is at least partially stabilized by yttrium.4. The rotary piston engine according to claim 1 , whereinthe thermal barrier coat has a lanthanum aluminate coat or a hexaaluminate coat.5. The rotary piston engine according to claim 2 , wherein at least one of the followingthe oxide ceramic coat is applied to the at least one partial portion of the chamber surface by high-speed flame spraying, laser powder coating or arc spraying; andthe lanthanum aluminate coat or the hexaaluminate coat is applied to the at least one partial portion of the chamber surface by an atmospheric high-temperature coating method including plasma spraying, high-speed flame spraying, laser powder coating or arc spraying.6. The rotary piston engine according to claim 1 , whereinthe metallic spray coat has at least one of a corrosion coat and a tribological coat.7. ...

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Номер записи: 69
15-01-2015 дата публикации

COMPONENT WITH A METALLURGICALLY BONDED COATING

Номер: US20150017430A1
Автор: Matthaeus Goetz
Принадлежит: Thermico GmbH & Co. KG

The invention relates to a component () having a coating () that is metallurgically bonded on as well as thermally sprayed on and re-melted. In order to prevent wear phenomena from continuing to occur when force impacts occur in the component () and further surface stress occurs, the invention provides that the coating () is provided with a thermal spray layer (). 113. Component () having a coating () that is metallurgically bonded as well as thermally sprayed on and re-melted ,wherein{'b': 3', '4, 'the coating () is provided with at least one thermal spray layer ().'}2. Component according to claim 1 ,wherein{'b': '4', 'the layer () is re-melted.'}3. Component according to claim 2 ,wherein{'b': '4', 'the thickness of the layer () amounts to between 5 and 500 μm.'}4. Component according to claim 2 ,wherein{'b': '4', 'the thickness of the layer () amounts to between 5 and 150 μm.'}5. Component according to claim 3 ,wherein{'b': '4', 'the thickness of the layer () amounts to between 5 and 30 μm.'}6. Component according to claim 1 ,wherein{'b': '4', 'the layer () is a plasma layer composed of oxide ceramic material.'}7. Component according to claim 1 ,wherein{'b': '4', 'the layer () is composed of metal-bonded carbides, particularly an HVOF layer composed of WC—CrC—Ni.'}8. Component according to claim 1 ,wherein{'b': '3', 'the coating () is composed of a hot-gas-oxidation-resistant material.'}9. Component according to claim 1 ,wherein{'b': '3', 'the coating () is corrosion-resistant.'}10. Component according to claim 1 ,wherein{'b': 3', '2', '1, 'the coating () is situated on the surface () and/or the inner surface of the component ().'}11321. Method for the production of a metallurgically bonded coating () claim 1 , which is thermally sprayed onto a surface () of a component () and re-melted by means of a laser claim 1 ,wherein{'b': 4', '3, 'at least one further layer () is thermally sprayed onto the coating ().'}12. Method according to claim 11 ,wherein{'b': '4', ' ...

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Номер записи: 70
19-01-2017 дата публикации

CORROSION-RESISTANT SPRAYED COATING, METHOD FOR FORMING SAME AND SPRAYING DEVICE FOR FORMING SAME

Номер: US20170015838A1
Автор: HOTTA Toshifumi, KUMAI Takashi, Kurahashi Ryurou, Morimoto Toshiharu, NISHIURA Yusuke, Omori Yasuhiro, OTSUBO Fumiaki, SHIN Yoshio
Принадлежит:

[Problem] To provide a corrosion-resistant coating that exhibits greater corrosion protection in saltwater environments and the like than was conventional, a method for forming the same, and a device for forming the same. 1. A corrosion-resistant alloy sprayed coating ,which is a corrosion-resistant sprayed coating covering a substrate surface,comprising aluminum, wherein, without laser irradiation or extrusion processing in addition to thermal spraying, and with the surface thereof unsealed, the porosity is 1% or less, and a microstructure is formed with a grain size of 10 μm or less.2. The corrosion-resistant alloy sprayed coating according to claim 1 , comprising aluminum and comprising 0.3 to 15 mass % magnesium.3. The corrosion-resistant alloy sprayed coating according to claim 1 , comprising magnesium claim 1 , silicon claim 1 , manganese claim 1 , titanium claim 1 , copper and aluminum.4. The corrosion-resistant alloy sprayed coating according to claim 1 , wherein the content of oxygen is 0.2 mass % or less.5. A corrosion-resistant alloy sprayed coating claim 1 ,which is a corrosion-resistant sprayed coating covering a substrate surface,comprising aluminum, wherein the porosity is 1% or less, with the surface thereof unsealed, and a microstructure is formed with a grain size of 10 μm or less, andsome of the microstructure includes a nanostructure with a submicron grain size.6. The corrosion-resistant alloy sprayed coating according to claim 1 , wherein the coating surface is sealed by covering with a silicone or epoxy resin.7. A method for forming a corrosion-resistant sprayed coating claim 1 , wherein a corrosion-resistant alloy sprayed coating comprising aluminum that has a porosity of 1% or less claim 1 , with the surface thereof unsealed claim 1 , and that forms a microstructure with a grain size of 10 μm or less claim 1 , is formed on a substrate surface claim 1 , using a thermal spray gun having a function wherein a flame including melted material ...

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Номер записи: 71
19-01-2017 дата публикации

Method for Color Register Spraying of Hub

Номер: US20170016106A1
Автор: Li Changhai, Wang Yongning, ZHANG LE, Zhang Shengchao, Zhu Zhihua
Принадлежит: CITIC Dicastal CO., LTD

The present invention provides a method for color register spraying of a hub, which includes machining and turning for glossy finish after spraying a black paint on the surface of a hub, and then spraying a color transparent paint onto the hub. The method provided by the invention achieves a spraying-based color register effect through spraying of the color transparent paint, which greatly improves the production efficiency and is available for batch production. 1. A method for color register spraying of a hub , comprising:machining and turning, for a glossy finish, after spraying a black paint on a surface of a hub, and then spraying a color transparent paint onto the hub.2. The method according to claim 1 , further comprising the following steps:preprocessing, baking, spraying of priming powder, curing, spraying of a black paint, curing, machining and turning for glossy finish, preprocessing, baking, spraying of transparent powder, curing, spraying of a color transparent paint, and curing.3. The method according to claim 2 , wherein the method is performed by adopting one or more of the following working conditions:(1) in the step of spraying of the priming powder, an electrostatic spray gun is used for spraying, with a voltage controlled to be 60 KV to 80 KV and a powder output controlled to be 10 g/s to 15 g/s, thereby guaranteeing excellent inter-coating adhesion;(2) in the step of curing of the priming powder, the surface temperature of a workpiece is controlled to be 180° C. for 8 to 12 min, thereby allowing the powder to maintain certain flexibility and better inter-coating adhesion;(3) in the step of spraying of the black paint, an air spray gun is used for spraying, with an air output controlled to be 50 cc/min to 100 cc/min and a sector atomization pressure being 2 bar to 3 bar, thereby guaranteeing the black paint to be sprayed onto the surface of the hub evenly and fully;(4) in the step of curing of the black paint, the temperature of the workpiece is ...

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Номер записи: 72
21-01-2016 дата публикации

Blades and Manufacture Methods

Номер: US20160017725A1
Автор: Bogue William, JR. Joseph J., Parkos, TABOR Timothy J.
Принадлежит: UNITED TECHNOLOGIES CORPORATION

A blade () has an airfoil () having a leading edge (), a trailing edge (), a pressure side (), and a suction side () and extending from an inboard end () to a tip (). An attachment root () is at the inboard end. The blade comprises an aluminum alloy substrate () and a coating at the tip (). The coating () comprises an anodic layer () atop the substrate and an aluminum oxide layer () atop the anodic layer. 1100. A blade () comprising:{'b': 106', '114', '116', '118', '120', '110', '112, 'an airfoil () having a leading edge (), a trailing edge (), a pressure side (), and a suction side () and extending from an inboard end () to a tip (); and'}{'b': '108', 'an attachment root (),'}wherein:{'b': 102', '130', '112, 'the blade comprises an aluminum or aluminum alloy substrate () and a coating () at the tip (); and'}{'b': 130', '160', '162, 'the coating () comprises an anodic layer () atop the substrate and an aluminum oxide layer () atop the anodic layer.'}2. The blade of wherein:the substrate is an outer layer and the blade further has an inner layer.3. The blade of wherein:the substrate comprises 7XXX or 2XXX-series;{'sub': '1', 'the anodic layer has a characteristic thickness (T) of at least 10 micrometers; and'}{'sub': '2', 'the aluminum oxide layer has a characteristic thickness (T) of at least 50 micrometers and has lower density and greater porosity than the anodic layer.'}4. The blade of wherein:{'sub': '1', 'the anodic layer has a characteristic thickness (T) of 25-75 micrometers; and'}{'sub': '2', 'the aluminum oxide layer has a characteristic thickness (T) of 75-400 micrometers.'}5. The blade of wherein:{'b': '104', 'the airfoil has an erosion coating () away from the tip.'}6. The blade of wherein:{'b': 162', '160, 'the coating consists of the aluminum oxide layer () and the anodic layer ().'}7. The blade of wherein:{'b': 162', '160, 'the aluminum oxide layer () is directly atop the anodic layer (); and'}{'b': 160', '102, 'the anodic layer () is directly atop ...

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Номер записи: 73
18-01-2018 дата публикации

Material joining

Номер: US20180016671A1
Автор: Neal Magdefrau, Paul Sheedy, Sonia Tulyani
Принадлежит: Hamilton Sundstrand Corp

A method of joining includes bringing a bulk metallic glass (BMG) material to a temperature lower than the crystallization temperature of the BMG material and depositing the BMG material onto a first substrate with interlock surface features such that the BMG material interlocks with the interlock surface features of the substrate. The method includes joining a second substrate to the BMG material, wherein the second substrate includes interlock surface features such that the BMG material interlocks with the interlock surface features of both the first and second substrates, joining the first and second substrates together to produce a fully amorphous joint between the first and second substrates.

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Номер записи: 74
16-01-2020 дата публикации

PRETREATMENT OF WELD FLANGES TO MITIGATE LIQUID METAL EMBRITTLEMENT CRACKING IN RESISTANCE WELDING OF GALVANIZED STEELS

Номер: US20200016679A1
Автор: Karagoulis Michael J., MELLAS Spyros P., Teng Zhenke, Wang Pei-Chung
Принадлежит:

A method to mitigate liquid metal embrittlement cracking in resistance welding of galvanized steels includes modifying at least one face of a steel member to create a first workpiece by: applying a zinc containing material in a first layer to the at least one face of the steel member; and spraying a second layer of a copper containing material onto the first layer of the zinc containing material. The at least one face of the first workpiece is abutted to a second workpiece of a steel material. A resistance welding operation is performed to join the first workpiece to the second workpiece. A temperature of the resistance welding operation locally melts the zinc containing material and the copper containing material to create a brass alloy of the zinc containing material and the copper containing material. 1. A method for pretreatment to mitigate liquid metal embrittlement cracking for welding of coated steels , including galvanized , galvannealed , and ZAM (zinc , aluminum , magnesium alloy) steels , comprising:layering a zinc containing material and a copper containing material on at least one face of a steel member to create a first workpiece;abutting the at least one face of the first workpiece to a second workpiece of a steel material; andperforming a welding operation to join the first workpiece to the second workpiece wherein a temperature of the welding operation creates an alloy of the zinc containing material and the copper containing material.2. The method of claim 1 , wherein during the layering step the zinc containing material is directly applied onto the steel member and the copper containing material is subsequently applied onto the zinc containing material.3. The method of claim 1 , wherein during the layering step the copper containing material is directly applied onto the steel member and the zinc containing material is subsequently applied onto the copper containing material.4. The method of claim 1 , further including applying the copper ...

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Номер записи: 75
17-01-2019 дата публикации

PRETREATMENT ASSEMBLY AND METHOD FOR TREATING WORK PIECES

Номер: US20190017160A1
Автор: DiDonato Russell, Dominico James W., Jablonski Wenick (Rex) E., VerHoven Leonard A.
Принадлежит: STOLLE MACHINERY COMPANY, LLC

A pretreatment assembly includes a product support assembly and a pretreatment device. The product support assembly includes a primary support assembly, a primary drive assembly, a number of secondary support assemblies, and a secondary drive assembly. The primary drive assembly is operatively coupled to the primary support assembly. The primary drive assembly imparts a generally constant motion to the primary support assembly. Each secondary support assembly is structured to support a number of work pieces. Each secondary support assembly is movably coupled to the primary support assembly. The secondary drive assembly is operatively coupled to each secondary support assembly. The secondary drive assembly selectively imparts a motion to each secondary support assembly. The pretreatment device is disposed adjacent the product support assembly. 1. A product support assembly for a pretreatment assembly , said coating pretreatment assembly structured to process a number of work pieces , said pretreatment assembly including a number of ion generating stations , said product support assembly comprising:a primary support assembly;a primary drive assembly;said primary drive assembly operatively coupled to said primary support assembly;wherein said primary drive assembly imparts a constant motion to said primary support assembly;a number of secondary support assemblies;each secondary support assembly structured to support a number of work pieces;each secondary support assembly movably coupled to said primary support assembly;a secondary drive assembly;said secondary drive assembly operatively coupled to each secondary support assembly; andwherein said secondary drive assembly selectively imparts a motion to each secondary support assembly.2. The product support assembly of wherein:said primary support assembly is a turret assembly;said turret assembly including a body structured to support each secondary support assembly at a first radius;said turret assembly body having an ...

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Номер записи: 76
21-01-2021 дата публикации

FILM-FORMING MATERIAL

Номер: US20210017036A1
Автор: FUKAGAWA Naoki, MATSUKURA Kento, SATO Ryuichi, SHIGEYOSHI Yuji
Принадлежит: NIPPON YTTRIUM CO., LTD.

A film-forming material of the present invention contains an oxyfluoride of yttrium represented by YOF(X and Y are numbers satisfying 0 Подробнее

Номер записи: 77
16-01-2020 дата публикации

Ni-BASED THERMAL SPRAYING ALLOY POWDER AND METHOD FOR MANUFACTURING ALLOY COATING

Номер: US20200017949A1
Автор: Emami Mohammad, HAYASHI Shigenari, Ishikawa Eiji, KOGIN Takashi, NOGUCHI Manabu, TAKASAKI Nobuhiro, TANAKA Eichi
Принадлежит:

There are provided a Ni-based thermal spraying alloy powder having excellent corrosion resistance and erosion-corrosion resistance even in an environment in which corrosion acts or corrosion and erosion act simultaneously, and a method for manufacturing an alloy coating. A Ni-based thermal spraying alloy powder comprising Cr: 15 wt % or more and 25 wt % or less, Mo: 0 wt % or more and 5 wt % or less, Si: 0.5 wt % or more and less than 2 wt %, Fe: 5 wt % or less, C: 0.3 wt % or more and 0.7 wt % or less, and B: 4 wt % or more and 7 wt % or less, with the balance being Ni and incidental impurities. 1. A Ni-based thermal spraying alloy powder comprising Cr: 15 wt % or more and 25 wt % or less , Mo: 0 wt % or more and 5 wt % or less , Si: 0.5 wt % or more and less than 2.0 wt % , Fe: 5 wt % or less , C: 0.3 wt % or more and 0.7 wt % or less , and B: 4 wt % or more and 7 wt % or less , with the balance being Ni and incidental impurities.2. The Ni-based thermal spraying alloy powder according to claim 1 , wherein a content of Si and B satisfies −0.25 B (wt %)+1.75≤Si (wt %)≤−0.25 B (wt %)+2.75.3. The Ni-based thermal spraying alloy powder according to claim 1 , comprising Mo: 0 wt % or more and 1 wt % or less.4. The Ni-based thermal spraying alloy powder according to claim 1 , comprising Mo: 1 wt % or more and 5 wt % or less.5. A method for manufacturing an alloy coating comprising thermally spraying the Ni-based thermal spraying alloy powder according to to onto a substrate to form an alloy coating claim 1 , and remelting the alloy coating to reduce porosity in the alloy coating and improve adhesiveness between the alloy coating and the substrate.6. The method for manufacturing the alloy coating according to claim 5 , wherein the remelting is performed by high frequency induction heating. The present invention relates to a Ni-based thermal spraying alloy powder and a method for manufacturing alloy coating, and particularly to a Ni-based thermal spraying alloy powder that ...

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Номер записи: 78
22-01-2015 дата публикации

PROCESS AND DEVICE FOR SUBSTRATE WITH INCREASED SLIP RESISTANCE

Номер: US20150024235A1
Автор: Friedman Jeff, Gauntt Joe
Принадлежит:

Disclosed is a process and apparatus for preparing a substrate having a high coefficient of friction on a surface, and the high friction substrate. A pre-process of sanding can be used, followed by thermal wire coating of the sanded surface. The surface can have a static and dynamic coefficient of friction greater than or equal to than 0.85. 1. A system for increasing the coefficient of friction of a substrate comprising:at least one pair of spray tips configured to melt a metallic material;at least one sander configured to generally irregularly sand a surface of a substrate; anda spray gun configured to spray the metallic material onto a sanded surface of the substrate;wherein the spray device is configured to deposit the metallic material onto the surface of the substrate so that the surface has a static coefficient of friction of greater than or equal to about 0.85.2. The system of claim 1 , wherein the sander and spray gun are configured to move in the X-Y-Z axes.3. The device of claim 2 , wherein the substrate can be non-flat.4. The system of claim 1 , wherein the surface has a static coefficient of friction of greater than or equal to about 0.90.5. The system of claim 1 , wherein the surface has a static coefficient of friction of greater than or equal to about 0.95.6. The system of claim 1 , wherein the surface has a static coefficient of friction of greater than or equal to about 1.0.7. A method of treating a surface for increasing friction comprising:providing a substrate with at least one surface;generally irregularly sanding the at least one surface of the substrate; anddepositing a material on the surface of the substrate through spray coating;wherein the surface of the substrate has a coefficient of friction after depositing the material of greater than or equal to about 0.85.8. The method of claim 7 , wherein the surface of the substrate has a static coefficient of friction of greater than or equal to about 0.90.9. The method of claim 7 , wherein the ...

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Номер записи: 79
28-01-2016 дата публикации

Cold Gas Dynamic Spray Apparatus, System and Method

Номер: US20160024633A1
Автор: Jiaren Jiang, Lijue Xue, Shaodong Wang
Принадлежит: NATIONAL RESEARCH COUNCIL OF CANADA

A system for cold gas dynamic spraying of particulate material has a de Laval nozzle and two or more radial particle inlets located between the throat and the outlet of the nozzle, the two or more particle inlets arranged symmetrically around a linear flow path of the nozzle. Blocking of the inlets is reduced by controlling pressure of particle carrier gas to provide a stable particulate material injection pressure before and during introduction of working gas into the nozzle, and/or by clearing the particle inlets of residual particles after a spraying process. Such a system and associated method combines benefits of both downstream and upstream cold gas spray systems. Further, a nozzle for spraying particulate material having a cross-sectional shape that is narrower in a middle section compared to edge sections provides coatings with superior cross-sectional profiles.

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Номер записи: 80
28-01-2016 дата публикации

METHOD FOR PRODUCING A BRAKE DISK AND A BRAKE DISK

Номер: US20160025167A1
Автор: BRODA Maik, Grabiec Tomasz Pawel, Verpoort Clemens Maria
Принадлежит:

The disclosure relates to a brake disk and a method for producing a brake disk. The method may include roughening at least some area(s) of a surface of the main body, forming a metal coating on at least some area(s) of the roughened region of the surface of the main body, applying an enamel slip to at least some area(s) of the surface of the main body, drying the applied enamel slip, and heating the main body to form the enamel coating and to join the metal coating metallurgically to the main body. The brake disk may include a main body having an enamel coating arranged at least in some area(s). A metal coating may additionally be formed on the surface of the main body, at least in some area(s), wherein the metal coating is joined metallurgically to the main body. 1. A method for producing a brake disk , comprising:roughening at least some area or areas of a surface of a main body of the brake disk;forming a metal coating on at least some area or areas of the roughened area or areas of the surface of the main body;applying an enamel slip to at least some area or areas of the surface of the main body;drying the applied enamel slip; andheating the main body provided with the metal coating and the dried enamel slip to form an enamel coating and to join the metal coating metallurgically to the main body.2. The method of claim 1 , wherein the metal coating is formed by a thermal spraying method.3. The method of claim 1 , wherein the metal coating is formed in a layer thickness of from 150 μm to 350 μm.4. The method of claim 1 , wherein an anchoring thread is introduced into the surface and/or the surface is pretreated by corundum blasting in order to roughen the main body.5. The method of claim 1 , wherein the drying of the applied enamel slip is carried out in a furnace at 90° C.6. The method of claim 1 , wherein the heating of the main body provided with the metal coating and the dried enamel slip is carried out in a temperature range of from 800° C. to 900° C. using a ...

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Номер записи: 81
10-02-2022 дата публикации

CERAMIC MATERIAL, LAYER AND LAYER SYSTEM

Номер: US20220041510A1
Автор: Flores Renteria Arturo, Stamm Werner
Принадлежит: Siemens Energy Global GmbH & Co. KG

A ceramic material which contains yttrium oxide as stabilizers and at least one of the materials erbium oxide or ytterbium oxide provides a phase having sintering stability for a ceramic material for ceramic layers and a ceramic layer system which maintain the mechanical and thermal properties for a long time even when used at high temperatures. 1. A ceramic material based on{'sub': 2', '2', '3, 'zirconium oxide (ZrO) with yttrium oxide (YO) and'} [{'sub': 2', '3, 'erbium oxide (ErO) and'}, {'sub': 2', '3, 'ytterbium oxide (YbO) and'}, {'sub': 2', '2, 'optionally with at least one further oxide, in particular with at least two further oxides, selected from the group consisting of: hafnium oxide (HfO), cerium oxide (CeO), calcium oxide (CaO) and/or magnesium oxide (MgO) present in a proportion of in particular at least 0.1 mol %, in particular at least 0.5 mol % and in particular at most 5 mol %, in particular in that the ceramic material consists thereof.'}], 'at least one further oxide selected from the group consisting of2. The ceramic material as claimed in claim 1 ,{'sub': 2', '3', '2', '3', '2', '3', '2', '2, 'in which yttrium oxide (YO), erbium oxide (ErO) and ytterbium oxide (YbO) are used as oxides, optionally with at least one further oxide, in particular with at least two further oxides, selected from the group consisting of: hafnium oxide (HfO), cerium oxide (CeO), calcium oxide (CaO) and/or magnesium oxide (MgO), in particular only these.'}3. The ceramic material as claimed in claim 1 ,{'sub': 2', '3', '2', '3', '2', '2, 'in which yttrium oxide (YO) and erbium oxide (ErO) are used as oxides, optionally with at least one further oxide, in particular with at least two further oxides, selected from the group consisting of: hafnium oxide (HfO), cerium oxide (CeO), calcium oxide (CaO) and/or magnesium oxide (MgO), in particular only these.'}4. The ceramic material as claimed in claim 1 ,{'sub': 2', '3', '2', '3', '2', '2, 'in which yttrium oxide (YO) and ...

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Номер записи: 82
25-01-2018 дата публикации

Method for Producing Plug

Номер: US20180023179A1
Автор: HIDAKA Yasuyoshi, HIGASHIDA Yasuto, Inoue Yuji, Shimoda Kazuhiro, Shimooka Shusuke, YAMANE Kouji
Принадлежит:

A method for producing a plug includes: a step of preparing a plug base metal having a concave portion along a circumferential direction in an outer peripheral surface; and an arc spraying step of spraying a spraying wire rod material onto the outer peripheral surface of the plug base metal by arc spraying to form films containing Fe and Fe oxides on the outer peripheral surface of the plug base metal. The arc spraying step includes: a separating step of separating the outer peripheral surface of the plug base metal into a plurality of regions along an axial direction; and a step of performing arc spraying separately in each of the regions. In the separating step, a boundary between the regions is set at the concave portion. In this way, peeling of films at a connecting portion is prevented, and the lifetime of the plug can be increased. 1. A method for producing a plug that is used in a piercing-rolling mill when producing a seamless steel pipe , the method comprising:a step of preparing a plug base metal having a concave portion along a circumferential direction in an outer peripheral surface, andan arc spraying step of spraying a spraying wire rod material onto the outer peripheral surface of the plug base metal by arc spraying to form films containing Fe and Fe oxides on the outer peripheral surface of the plug base metal;wherein:the arc spraying step includes:a separating step of separating the outer peripheral surface of the plug base metal into a plurality of regions along an axial direction, anda step of performing arc spraying separately in each of the regions; andin the separating step, a boundary between the regions is set at the concave portion.2. The method for producing a plug according to claim 1 , wherein:in the plug base metal, the outer peripheral surface is formed by connecting a plurality of divided faces successively in the axial direction, and has the concave portion at a joint between the divided faces; and{'b': 1', '2, 'claim-text': {'br': ...

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Номер записи: 83
23-01-2020 дата публикации

CMAS RESISTANT THERMAL BARRIER COATINGS

Номер: US20200024718A1
Автор: Rosenzweig Larry Steven, Ruud James Anthony, Sivaramakrishnan Shankar
Принадлежит:

The present application provides Calcia-Magnesia-Alumina-Silica (CMAS) (or molten silicate) resistant thermal barrier coatings (IBC). The coatings include elongate growth domains of non-equiaxed, randomly arranged overlapping grains or splats. The elongate growth domains include overlapping individual, randomly distributed splats of tough and soft phases. In some embodiments, the elongate growth domains are formed via air plasma spray. In some embodiments, the tough phases are at least partially stabilized zirconia and/or hafnia compositions, and the soft phases are CMAS (or molten silicate) reactive or resistant compositions. Within each elongate growth domain, the mixture of the tough and soft phases act together to limit penetration of CMAS and also provide sufficient domain toughness to minimize cracking forces produced during crystallization of infiltrated CMAS. The soft phases may react with the CMAS and increase its melting point, increase its viscosity, and reduce the destabilization of the tough phases. 119.-. (canceled)20. A method of forming a thermal barrier coating on a substrate , the method comprising:obtaining a substrate;obtaining a feedstock consisting of about micron or sub-micron ceramic particles of tough and soft phases suspended in a liquid agent, wherein the tough phases are at least one of partially stabilized zirconia compositions and partially stabilized hafnia compositions, and the soft phases are at least one of CMAS reactive compositions and CMAS resistant compositions; andutilizing an air plasma spray apparatus to heat and deposit the tough and soft phases of the feedstock on the substrate in randomly distributed overlapping splats that form a plurality of elongate material growth domains of at least about 75% density defined between domain boundaries.21. The method of claim 20 , wherein at least about 75% of the splats of the domains include a width to length aspect ratio of greater than or equal to about 3:1 and a substantially ...

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Номер записи: 84
23-01-2020 дата публикации

Turbine abrasive blade tips with improved resistance to oxidation

Номер: US20200024975A1
Автор: Christopher W. STROCK, Kevin Seymour
Принадлежит: United Technologies Corp

An abrasive coating for a substrate of a component in a gas path exposed to a maximum temperature of 1750 degree Fahrenheit, comprising a plurality of grit particles adapted to be placed on a top surface of the substrate; a matrix material bonded to the top surface; the matrix material partially surrounds the grit particles, wherein the grit particles extend above the matrix material relative to the top surface; a film of oxidant resistant coating applied over the plurality of grit particles and the matrix material and a thermal barrier coating material applied over said film of oxidant resistant coating.

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Номер записи: 85
23-01-2020 дата публикации

SEAL COATING

Номер: US20200025014A1
Автор: Farris John R., McCaffrey Michael G.
Принадлежит:

A method of forming a coating includes disposing a substrate having a plurality of protrusions on a seal and layering a topcoat over the protrusions. The method of forming a coating also includes creating a wear pattern and converting the topcoat. A turbine section includes a casing, a plurality of blades within the casing, and a substrate deposited on the casing having a plurality of protrusions. The turbine also includes an unconverted topcoat disposed over the plurality of protrusions, the topcoat having segmented portions defining a plurality of faults extending from the protrusions through the topcoat. A method of forming a coating includes creating a channel in the coating during an initial rub event and converting the coating during a high-temperature event. Converting the coating includes preserving the channel created during the initial rub event. 1. A method of forming a coating comprising:disposing a substrate having a plurality of protrusions on a seal;depositing a topcoat over the protrusions;creating a wear pattern in the topcoat; andconverting the topcoat.2. The method of claim 1 , wherein the seal is a blade outer air seal.3. The method of claim 1 , wherein the topcoat comprises a thermally insulating ceramic material having a porosity between 5 and 70 volume percent.4. The method of claim 1 , wherein the topcoat comprises segmented portions defining a plurality of faults extending from the plurality of protrusions through the topcoat.5. The method of claim 1 , wherein depositing the topcoat over the plurality of protrusions forms a surface having a plurality of dimples.6. The method of claim 5 , wherein creating a wear pattern comprises rubbing a blade tip against the topcoat during an initial rub event.7. The method of claim 6 , wherein rubbing the blade tip against the topcoat during the initial rub phase forms a channel depth that is less than a depth of the plurality of dimples.8. The method of claim 7 , wherein the wear pattern allows for ...

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Номер записи: 86
23-01-2020 дата публикации

Method of Manufacturing Conductive Film Holes

Номер: US20200025085A1
Автор: Slavens Thomas N., Zacchera Kevin L.
Принадлежит: UNITED TECHNOLOGIES CORPORATION

A method for applying a coating to a substrate having a plurality of holes. The method comprises: applying a braze material to a substrate having a plurality of holes; heating the substrate to melt the braze material to form a melt; cooling the substrate to solidify the melt to form plugs in the respective holes; applying a coating to the substrate; and further heating the substrate to melt the plugs. 1. A method for applying a coating to a substrate having a plurality of holes , the method comprising:applying a braze material to a substrate having a plurality of holes;heating the substrate to melt the braze material to form a melt;cooling the substrate to solidify the melt to form plugs in the respective holes; 'during the applying of the coating, the coating preferentially deposits away from the plugs so that the deposition leaves a gap or thinning in the coating over the exposed plug surface; and', 'applying a coating to the substrate, whereinfurther heating the substrate to melt the plugs.2. The method of the applying the coating comprises:applying a metallic bondcoat; andapplying a ceramic coating atop the bondcoat.3. The method of wherein the applying the braze paste comprises:applying the braze material to portions of a surface of the substrate aside the hole but not plugging the holes.4. The method of wherein:the braze material is an Au—Cu braze material.5. (canceled)6. The method of wherein:the braze material is applied via a braze paste.7. The method of wherein:the braze paste comprises a water-based gel binder.8. The method of wherein:the braze paste comprises particles of an alloy having a by weight composition of Au, Cu, and no more than 5% all other elements total, if any.9. The method of wherein:a ratio of Au to Cu in said alloy is between 67/33 and 56/44.10. The method of wherein:said particles of said alloy form at least 95% of alloy in the braze paste.11. The method of wherein:said water-based gel binder forms 8% to 25% by weight of the braze paste ...

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Номер записи: 87
28-01-2021 дата публикации

Method of Coating High Atomic Number Metals Onto Oxygen or Hydroxyl Rich Surfaces

Номер: US20210025047A1
Автор: Alexa Joel A., III Donald L., Sankaran Sankara N., Thomsen
Принадлежит:

Methods for making layered materials and layered materials including high atomic number metals and metal alloys adhered to surfaces are provided. Such surfaces may be oxygen or hydroxyl rich surfaces. Certain methods include depositing a tie down layer of a first metal or metal alloy particles onto a first surface of base material and depositing a high atomic number metal or metal alloy layer onto the first surface after depositing the tie down layer, wherein particles comprising the high atomic number metal or metal alloy layer have a higher atomic number than the first metal or metal alloy particles. 1. A method for making a layered material , comprising:depositing a tie down layer comprising particles of at least one of a first metal or a first metal alloy onto a first surface of base material; anddepositing a high atomic number metal layer onto the first surface after depositing the tie down layer comprising particles of at least one of a high atomic number metal or metal alloy, having a higher atomic number than the particles of at least one first metal or first metal alloy.2. The method of claim 1 , wherein at least one of the depositing of the tie down layer and the depositing of the high atomic number metal layer comprises a thermal spraying process.3. The method of claim 2 , wherein the thermal spraying process comprises a radio frequency (RF) plasma spraying process.4. The method of claim 1 , wherein the first surface of the base material is an oxygen or hydroxyl rich surface.5. The method of claim 4 , wherein the particles of the tie down layer comprise a metal or an alloy selected from the group consisting: titanium claim 4 , palladium claim 4 , tin claim 4 , aluminum claim 4 , aluminum alloy claim 4 , antimony claim 4 , antimony alloy claim 4 , and combinations thereof.6. The method of claim 4 , wherein the particles of the high atomic number metal layer comprise at least one of tantalum or tantalum alloy.7. The method of claim 5 , wherein the particles ...

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Номер записи: 88
04-02-2016 дата публикации

Bonding of Titanium Coating to Cast CoCr

Номер: US20160030632A1
Автор: Ault James, Barrett James K., Schleicher John
Принадлежит:

Described is a medical implant having a CoCr cast body and a commercially pure (CP) Ti coating. The CP Ti coating is diffusion bonded to the CoCr body and is 5-3000 μm thick. Also described is a process for producing the medical implant that includes preparing the cast CoCr body for coating, applying a coating using a cold spray process, and diffusion bonding the coating to the body using hot isostatic pressing. 1. A process for coating a CoCr alloy medical implant comprising:applying a coating of commercially pure Ti to the surface of the medical implant using a cold spray process; anddiffusion bonding the coating and the CoCr alloy medical implant using hot isostatic pressing.2. The process according to claim 1 , wherein the cold spray process comprises applying to the surface of the medical implant a particle stream comprising particles of commercially pure Ti and a pressurized gas.3. The process according to claim 2 , wherein the pressurized gas is supplied at a pressure of 1.0-10.0 MPa.4. The process of claim 2 , wherein the pressurized gas is an inert gas.5. The process of claim 2 , wherein the pressured gas is compressed air.6. The process of claim 2 , wherein the particle stream is at a temperature of 0-1300° F.7. The process according to claim 2 , wherein the particles of commercially pure Ti in the particle stream have a diameter of 1-100 μm.8. The process of claim 2 , wherein the particles of commercially pure Ti in the particle stream travel at a velocity of 300-1500 m/s.9. The process of claim 1 , wherein the hot isostatic pressing is performed at a temperature of 900-1850° F.10. The process of claim 1 , wherein the hot isostatic pressing is performed at a pressure of 10 claim 1 ,000-25 claim 1 ,000 psi.11. The process of claim 1 , wherein the hot isostatic pressing is performed at a temperature of 900-1850° F. claim 1 , a pressure of 10 claim 1 ,000-25 claim 1 ,000 psi claim 1 , and for a time period of 1-5 hours.12. The process of claim 2 , wherein ...

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Номер записи: 89
29-01-2015 дата публикации

METHOD FOR FORMING AN IMPROVED THERMAL BARRIER COATING (TBC), THERMAL-BARRIER-COATED ARTICLE AND METHOD FOR THE REPAIR THEREOF

Номер: US20150030877A1
Автор: Casillo Raffaele, Della Femina Maurizio, ROSSI Marco, Silvestro Carlo
Принадлежит: GE AVIO S.r.I.

The invention refers to a process for the formation of a thermal barrier coating on a substrate, comprising the steps of: 1102101. A method for forming a thermal barrier coating () on a substrate () , comprising the steps of:{'b': 103', '101, 'a) applying a bond coat () on said substrate ();'}{'b': 103', '103, 'b) subjecting said bond coat () to a low activity aluminizing process, thus obtaining a temporary intermediate diffusion layer on said bond coat ();'}characterized in that it comprises the steps ofc) applying on said temporary intermediate diffusion layer obtained from said phase b) aluminium powder in suspension with a solvent or aqueous base, said aluminium powder having a size distribution from 15 to 150 μm;{'sup': −', '−, 'b': 105', '103, 'd) carrying out a vacuum heat treatment on the substrate, bond coat and temporary intermediate diffusion layer as a whole, at a pressure from 103 to 105 bar, at a temperature from 800° C. to 1050° C. and with an active phase in the range of 60 min-4 h, thus obtaining an enriched intermediate diffusion layer () on said bond coat (); and'}{'b': 104', '105, 'e) applying a definitive barrier layer () on said enriched intermediate diffusion layer ().'}2. A method according to claim 1 , wherein said aluminium powder has a size distribution from 30 to 100 μm.3. A method according to claim 1 , wherein said step c) of applying said aluminium powder is repeated 1-4 times.4. A method according to claim 1 , wherein said step d) of heat treatment is carried out at a temperature from 850° C. to 1000° C.5. A method according to claim 1 , wherein said step d) of heat treatment has an active phase with a duration in the range of 90-180 min.6. A method according to claim 1 , wherein said step d) of heat treatment is repeatedly carried out 1-6 times.7100101102102. An article () comprising a substrate () and a thermal barrier coating () applied on said substrate claim 1 , characterized in that said thermal barrier coating () is formed by ...

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Номер записи: 90
04-02-2016 дата публикации

Method and apparatus for forming a structure on a substrate

Номер: US20160031043A1
Автор: Dariusz Korzec, Stefan Nettesheim
Принадлежит: Maschinenfabrik Reinhausen GmbH

The invention relates to a method for forming at least one structure on a substrate. By means of a low-temperature plasma jet, powder, of which the structure shall be constructed, is applied to a surface of the substrate. By means of at least one laser beam, heat is input into the substrate and/or the powder within a laser incidence region on the substrate. The heat input delays solidification of the powder particles, which are partly or fully melted in the plasma jet, on the substrate and thereby enables the formation of good adhesion between the applied powder, and thus the structure constructed thereof, and the substrate. The invention further relates to an apparatus for performing the method.

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Номер записи: 91
04-02-2016 дата публикации

Coatings for metallic substrates

Номер: US20160031186A1
Автор: Andrew Joseph Detor, Andrew William EMGE, David Paul Mourer, James Anthony Ruud, Kenneth Rees Bain, Leonardo Ajdelsztajn, Michael James Weimer
Принадлежит: General Electric Co

Coatings for substrates, such as superalloy substrates, are provided. The coating can include: 15 wt % to 45 wt % cobalt; 20 wt % to 40 wt % chromium; 2 wt % to 15 wt % aluminum; 0.1 wt % to 1 wt % yttrium; and nickel. The coatings may include nickel, cobalt, chromium and aluminum, and other optional additives to improve oxidation and corrosion resistance of the substrate without significant debit to its mechanical properties.

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Номер записи: 92
02-02-2017 дата публикации

YTTRIUM-BASE SPRAYED COATING AND MAKING METHOD

Номер: US20170029628A1
Автор: Hamaya Noriaki, Takai Yasushi
Принадлежит: SHIN-ETSU CHEMICAL CO., LTD.

An yttrium-base sprayed coating is obtained by thermally spraying yttrium oxide, yttrium fluoride or yttrium oxyfluoride onto a substrate to form a coating of 10-500 μm thick, and chemically cleaning the coating with a cleaning liquid of organic acid, inorganic acid or a mixture thereof until the population of particles with a size of up to 300 nm becomes no more than 5 particles/mmof the coating surface. The yttrium-base sprayed coating exhibits high corrosion resistance even in a halogen gas plasma atmosphere and prevents yttrium-base particles from spalling off during etching treatment. 1. An yttrium-base sprayed coating comprising at least one compound selected from the group consisting of yttrium oxide , yttrium fluoride , and yttrium oxyfluoride and having a thickness of 10 to 500 μm , wherein particles with a size of up to 300 nm are present on a coating surface in a population of no more than 5 particles per square millimeters.2. The yttrium-base sprayed coating of having a thickness of 80 to 400 μm.3. The yttrium-base sprayed coating of which is sprayed onto a surface of a substrate of metallic aluminum claim 1 , aluminum oxide or metallic silicon.4. A method for preparing a yttrium-base sprayed coating claim 1 , comprising the steps of:thermally spraying a particulate spray material comprising at least one compound selected from the group consisting of yttrium oxide, yttrium fluoride, and yttrium oxyfluoride to form a yttrium-base sprayed coating having a thickness of 10 to 500 μm andchemically cleaning a surface of the coating with a cleaning liquid which is an organic acid aqueous solution, inorganic acid aqueous solution or organic acid/inorganic acid aqueous solution until a population of particles with a size of up to 300 nm is no more than 5 particles per square millimeters of the coating surface.5. The method of wherein the cleaning liquid is an aqueous solution of an acid selected from the group consisting of a monofunctional carboxylic acid claim ...

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Номер записи: 93
02-02-2017 дата публикации

Turbine blade with hot-corrosion-resistant coating

Номер: US20170030203A1
Автор: Andrzej Paczoski, Remy Synnott, Yulia Panchenko
Принадлежит: Pratt and Whitney Canada Corp

A turbine blade of a gas turbine engine is described which includes an airfoil extending away from the hub platform to a blade tip. The airfoil defines a leading edge, a trailing edge, and a span-wise length extending between the platform and the blade tip. A hot-corrosion-resistant coating is located on the leading edge of the airfoil within a radially inner portion thereof, the radially inner portion extending away from the hub platform a desired distance along said span-wise length.

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Номер записи: 94
04-02-2016 дата публикации

PROCESS FOR FABRICATING AN AIRCRAFT PART COMPRISING A SUBSTRATE AND A SUBSTRATE COATING LAYER

Номер: US20160032440A1
Автор: GAYDU Regis, MONERIE-MOULIN Francis
Принадлежит: MESSIER-BUGATTI-DOWTY

A method of fabricating a part () comprising a metal substrate (Sub) at least partially covered in a coating layer (Rev). The method comprises: preparing (A) a surface of the substrate (Sub) to obtain a prepared surface of roughness Ra lying in the range 0.6 μm to 1.6 μm, and; forming (C) the coating layer (Rev) on the prepared surface of the substrate, this coating layer (Rev) being formed by spraying, using an HVOF type spraying method to spray a powder mixture containing grains (G) of metal carbide, the grains (G) having dimensions that are strictly less than 1 μm and the thickness (Epmin) of the coating layer (Rev) as formed in this way being less than 50 μm; then finishing at least one surface of said coating layer (Rev) by polishing (D) in such a manner as to ensure that its roughness Ra is less than 1.6 μm. 11. A method of fabricating a part () comprising a metal substrate (Sub) at least partially covered in a coating layer (Rev) , the method comprising:preparing (A) a surface of the substrate (Sub) for covering in order to obtain a prepared surface of roughness Ra lying in the range 0.6 μm to 1.6 μm, and preferably in the range 0.8 μm to 1.6 μm;forming (C) the coating layer (Rev) on the prepared surface of the substrate, this coating layer (Rev) being formed by spraying, using an HVOF type spraying method to spray a powder mixture containing grains (G) of metal carbide, the grains (G) having dimensions that are strictly less than 1 μm and the thickness (Ep min) of the coating layer (Rev) as formed in this way being less than 50 μm; thenfinishing at least one surface of said coating layer (Rev) by polishing (D) in such a manner as to ensure that its roughness Ra is less than 1.6 μm.2. A method according to claim 1 , wherein the preparation (A) of the substrate surface (Sub) for covering is performed by sand blasting.3. A method according to claim 1 , wherein the coating layer that is formed has thickness lying in the range 30 μm to 50 μm and the size of the ...

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Номер записи: 95
04-02-2016 дата публикации

COATING PROCESS AND COATED ARTICLE

Номер: US20160032736A1
Автор: Harris, Healy Michael James, JR. John Wesley
Принадлежит: GENERAL ELECTRIC COMPANY

A coating process and coated article are provided. The coating process includes providing a turbine component, applying a coating repellant to a predetermined region of the turbine component, and depositing a coating material on the turbine component. The coating repellant directs the coating material away from the predetermined region of the turbine component, to at least partially form a channel. A coating process for a hot gas path turbine component and coated article are also disclosed. 1. A coating process , comprising:providing a turbine component;applying a coating repellant to a predetermined region of the turbine component; anddepositing a coating material on the turbine component;wherein the coating repellant directs the coating material away from the predetermined region of the turbine component, to at least partially form a channel.2. The coating process of claim 1 , wherein the coating repellant is an elastomer claim 1 , a silicon-based compound claim 1 , or a combination thereof.3. The coating process of claim 1 , wherein the coating material is a bond coat claim 1 , a thermal barrier coating claim 1 , or a combination thereof.4. The coating process of claim 1 , wherein the predetermined region of the turbine component comprises a pre-formed channel.5. The coating process of claim 1 , further comprising a removing of the coating repellant from the predetermined region of the turbine component.6. The coating process of claim 5 , further comprising the removing of the coating repellant with a leaching agent.7. The coating process of claim 5 , further comprising the removing of the coating repellant with a releasing agent.8. The coating process of claim 5 , further comprising the removing of the coating repellant with heat.9. The coating process of claim 5 , wherein the removing of the coating repellant exposes a substrate surface.10. The coating process of claim 1 , further comprising machining cooling holes in the exposed substrate surface within the ...

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Номер записи: 96
04-02-2016 дата публикации

Cost Effective Manufacturing Method for GSAC Incorporating a Stamped Preform

Номер: US20160032774A1
Автор: Christopher W. STROCK, Paul M. Lutjen
Принадлежит: United Technologies Corp

A process for manufacturing a preformed sheet having geometric surface features for a geometrically segmented abradable ceramic thermal barrier coating on a turbine engine component, the process comprising the steps of providing a preformed sheet material. The process includes forming a partially of geometric surface features in the sheet material. The process includes joining the sheet material to a substrate of the turbine engine component. The process includes disposing a thermally insulating topcoat over the geometric surface features and forming segmented portions that are separated by faults extending through the thermally insulating topcoat from the geometric surface features.

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Номер записи: 97
01-02-2018 дата публикации

THERMAL BARRIER COATING, TURBINE MEMBER, GAS TURBINE, AND MANUFACTURING METHOD FOR THERMAL BARRIER COATING

Номер: US20180030584A1
Автор: INOUE Yoshiyuki, KUDO Daisuke, Kuwabara Masamitsu, OKAYA Naotoshi, OSAWA Kei, Torigoe Taiji, Uemura Yoshitaka
Принадлежит:

A thermal barrier coating () includes a heat-resistant alloy substrate which is used in a turbine member and a ceramic layer () which is formed on the heat-resistant alloy substrate and in which vertical cracks (C) extending in a thickness direction are dispersed in a surface direction and a plurality of pores (P) are included on the inside. Thermal spray particles composed of YbSZ having a particle-size distribution in which a 50% particle diameter in a cumulative particle-size distribution is 40 μm to 100 μm are thermally sprayed at a thermal spray distance of 80 mm or less, the vertical cracks (C) are dispersed at a pitch of 0.5 cracks/mm to 40 cracks/mm in the surface direction, and the ceramic layer () of which a porosity attributable to the vertical cracks (C) and the pores (P) combined is 4% to 15% is formed. 15-. (canceled)6. A manufacturing method for a thermal barrier coating , comprising a ceramic layer forming process of forming a ceramic layer on a heat-resistant alloy substrate used in a turbine member by thermally spraying thermal spray particles composed of YbSZ having a particle-size distribution in which a 50% particle diameter in a cumulative particle-size distribution is 40 μm to 100 μm at a thermal spray distance of 80 mm or less , wherein in the ceramic layer , vertical cracks extending in a thickness direction are dispersed in a surface direction , wherein the vertical cracks are dispersed at a pitch of 0.5 cracks/mm to 40 cracks/mm in the surface direction , wherein a plurality of pores are included inside the ceramic layer , and wherein a porosity of the ceramic layer attributable to the vertical cracks and the pores combined is 4% to 15%.7. A manufacturing method for a thermal barrier coating , comprising a ceramic layer forming process of forming a ceramic layer on a heat-resistant alloy substrate used in a turbine member by thermally spraying thermal spray particles composed of YbSZ having a particle-size distribution in which a 50% ...

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Номер записи: 98
01-02-2018 дата публикации

WEAR RESISTANT COATING

Номер: US20180030585A1
Автор: COLLIER Sean, REYNOLDS Steve
Принадлежит:

A method of forming a wear resistant and galling resistant coating for abrasive environments and a feed material for the method are disclosed. The feed material is for forming a wear resistant and galling resistant coating on a substrate by a welding process that heats the feed and the substrate. The feed material comprises 35 to 50 wt % titanium nitride particles and a balance of commercially pure titanium or titanium alloy particles and incidental impurities. The method involves delivering the feed material to a surface of a substrate and exposing the feed material and the substrate to sufficient energy to cause at least the commercially pure titanium or titanium alloy particles in the feed to melt and at least some of the titanium nitride particles in the feed to melt, thereby forming a melt pool. On solidification of the melt pool, at least some of the titanium nitride particles are embedded in a matrix formed from melt pool, thereby forming a wear resistant and galling resistant coating on the substrate. A wear resistant and galling resistant coating formed of the feed material is also disclosed. 2. The method defined in claim 1 , wherein the substrate is a component of an autoclave.3. The method defined in claim 2 , wherein the autoclave component is an agitator.4. The method defined in claim 1 , wherein the corrosive and abrasive environment comprises autoclave processing conditions that extract valuable minerals from a mined ore.5. The method defined in claim 4 , wherein the corrosive and abrasive environment comprises autoclave processing conditions involving an elevated pressure in the range of 30 to 52 atm claim 4 , temperatures in the range of 120° C. to 270° C. and acid addition to a slurry of ground ore and water of 200 to 500 kg/t of ore.6. A method as defined in claim 1 , wherein the method involves depositing one or more layers of the wear resistant coating on the substrate to build up the thickness of the wear resistant coating.7. A method as ...

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Номер записи: 99
01-02-2018 дата публикации

Outer Airseal Abradable Rub Strip Manufacture Methods and Apparatus

Номер: US20180030586A1
Автор: Strock Christopher W.
Принадлежит: UNITED TECHNOLOGIES CORPORATION

A method for applying an abradable coating, comprises: generating a plasma; introducing a matrix-forming first particulate to the plasma at a first location; introducing a second particulate of an organic particulate and/or salt particulate to the plasma at a second location downstream from the first location to mix with the matrix-forming first particulate, the second particulate having a characteristic size in the range 6.0 micrometers to 45.0 micrometers; and directing the first particulate and the second particulate to a target to form a coating on the target. 1. A method for applying an abradable coating , the method comprising:generating a plasma;introducing a matrix-forming first particulate to the plasma at a first location; andintroducing a second particulate of an organic particulate and/or salt particulate to the plasma at a second location downstream from the first location to mix with the matrix-forming first particulate, the second particulate having a characteristic size in the range 6.0 micrometers to 45.0 micrometers; anddirecting the first particulate and the second particulate to a target to form a coating on the target.2. The method of further comprising:removing the second particulate from the coating so as to leave porosity.3. The method of wherein:the second particulate characteristic size is a D50 size.4. The method of wherein:the D50 size is 15 micrometers to 35 micrometers.5. The method of wherein:the second particulate has a D90 size of at most 45 micrometers.6. The method of wherein the first particulate has metallic particles of D50 particle size of 11-90 micrometers.7. The method of wherein the metallic particles comprise Cu—Ni alloy or an MCrAlY.8. The method of wherein the first particulate is an agglomerate of said metallic particles and particles of an inorganic non-metallic filler.9. The method of wherein:the second particulate is introduced at a volume flow rate of 40% to 80% of a total particulate flow rate.10. The method of ...

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